U.S. patent application number 15/370811 was filed with the patent office on 2018-12-13 for engine device.
This patent application is currently assigned to YANMAR CO., LTD.. The applicant listed for this patent is YANMAR CO., LTD.. Invention is credited to Koichi HIROSE, Taishi MURAKAMI, Tatsuro OHSARA.
Application Number | 20180355807 15/370811 |
Document ID | / |
Family ID | 54766683 |
Filed Date | 2018-12-13 |
United States Patent
Application |
20180355807 |
Kind Code |
A9 |
HIROSE; Koichi ; et
al. |
December 13, 2018 |
ENGINE DEVICE
Abstract
An engine device includes a main throttle valve disposed at a
portion where an outlet of a supercharger and an inlet of an
intercooler are coupled to each other, an exhaust bypass flow path
configured to couple an outlet of an exhaust manifold to an exhaust
outlet of the supercharger, an exhaust bypass valve disposed in the
exhaust bypass flow path, an air supply bypass flow path configured
to bypass a compressor of the supercharger, and an air supply
bypass valve disposed in the air supply bypass flow path. Within a
low load range of a load on the engine device, when the load is
lower than a predetermined load, feedback control is performed on
the main throttle valve, and when the load is higher than the
predetermined load, map control based on a data table is performed
on the main throttle valve.
Inventors: |
HIROSE; Koichi; (Osaka,
JP) ; OHSARA; Tatsuro; (Osaka, JP) ; MURAKAMI;
Taishi; (Osaka, JP) |
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Applicant: |
Name |
City |
State |
Country |
Type |
YANMAR CO., LTD. |
Osaka |
|
JP |
|
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Assignee: |
YANMAR CO., LTD.
|
Prior
Publication: |
|
Document Identifier |
Publication Date |
|
US 20170082041 A1 |
March 23, 2017 |
|
|
Family ID: |
54766683 |
Appl. No.: |
15/370811 |
Filed: |
December 6, 2016 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
|
|
PCT/JP2015/065455 |
May 28, 2015 |
|
|
|
15370811 |
|
|
|
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Current U.S.
Class: |
1/1 |
Current CPC
Class: |
F02D 11/105 20130101;
F02B 43/02 20130101; F02D 2200/1002 20130101; Y02T 10/30 20130101;
F02D 19/06 20130101; F02D 19/0642 20130101; F02D 2041/0022
20130101; F02D 41/2422 20130101; F02M 35/10157 20130101; Y02T 10/42
20130101; F02D 41/0002 20130101; F02D 45/00 20130101; F01N 13/10
20130101; F02B 37/16 20130101; Y02T 10/146 20130101; F02D 2041/1409
20130101; F02D 41/0007 20130101; F02D 41/1488 20130101; F02D 23/00
20130101; F02D 2200/101 20130101; F02D 21/08 20130101; F02D 41/3094
20130101; F02D 2011/102 20130101; F02D 2041/141 20130101; Y02T
10/36 20130101; F02D 41/0025 20130101; F02D 41/0027 20130101; F02D
2041/142 20130101; Y02T 10/12 20130101; F02B 29/0406 20130101; F02M
35/104 20130101; Y02T 10/144 20130101; F02B 37/18 20130101; F02D
9/02 20130101; F02D 41/1401 20130101; Y02T 10/40 20130101; F02D
19/10 20130101 |
International
Class: |
F02D 41/00 20060101
F02D041/00; F02B 37/18 20060101 F02B037/18; F02M 35/10 20060101
F02M035/10; F02M 35/104 20060101 F02M035/104; F01N 13/10 20060101
F01N013/10; F02B 43/02 20060101 F02B043/02; F02B 29/04 20060101
F02B029/04; F02D 9/02 20060101 F02D009/02 |
Foreign Application Data
Date |
Code |
Application Number |
Jun 6, 2014 |
JP |
2014-118036 |
Jun 6, 2014 |
JP |
2014-118037 |
Claims
1. An engine device comprising: at least one cylinder; an intake
manifold configured to supply air into the at least one cylinder;
an exhaust manifold configured to discharge exhaust gas from the at
least one cylinder; at least one main fuel injection valve
configured to inject liquid fuel into the at least one cylinder to
cause combustion of the liquid fuel; at least one gas injector
configured to mix gas fuel with the air supplied by the intake
manifold; a supercharger comprising a compressor and configured to
compress air through a use of the exhaust gas from the exhaust
manifold; an intercooler configured to cool compressed air
resulting from the compression by the supercharger and supply
resultant cooled air to the intake manifold; a main throttle valve
disposed at a portion where an outlet of the supercharger and an
inlet of the intercooler are coupled to each other; an exhaust
bypass flow path configured to couple an outlet of the exhaust
manifold to an exhaust outlet of the supercharger; an exhaust
bypass valve disposed in the exhaust bypass flow path; an air
supply bypass flow path configured to bypass the compressor of the
supercharger; and an air supply bypass valve disposed in the air
supply bypass flow path, wherein within a low load range of a load
on the engine device, when the load is lower than a predetermined
load, feedback control is performed on the main throttle valve, and
when the load is higher than the predetermined load, map control
based on a data table is performed on the main throttle valve.
2. The engine device according to claim 1, wherein within the low
load range, when the load is higher than the predetermined load,
feedback control is performed on the exhaust bypass valve and map
control is performed on the air supply bypass valve.
3. The engine device according to claim 1, wherein within the low
load range, when the load is lower than the predetermined load, the
exhaust bypass valve is caused to fully open and the air supply
bypass valve is caused to be fully closed.
4. The engine device according to claim 1, wherein within a medium
and high load range of the load, an opening degree of the main
throttle valve is kept to a fully-open opening degree, and each of
the exhaust bypass valve and the air supply bypass valve is
controlled to allow pressure inside the intake manifold to be
adjusted to a target value appropriate to the load.
5. The engine device according to claim 4, wherein within the
medium and high load range, feedback control is performed on the
exhaust bypass valve, and map control is performed on the air
supply bypass valve.
Description
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] The present application is a continuation application of
International Application No. PCT/JP2015/065455, filed May 28,
2015, which claims priority to Japanese Patent Application No.
2014-118036, filed Jun. 6, 2014, Japanese Patent Application No.
2014-118037, filed Jun. 6, 2014. The contents of these applications
are incorporated herein by reference in their entirety.
BACKGROUND OF THE INVENTION
[0002] The present invention relates to an engine device.
[0003] Heretofore, in ships, such as a tanker and a transport ship,
and land-based power generation facilities, diesel engines have
been used as their driving sources. Exhaust gas discharged from
such a diesel engine, unfortunately, contains a large number of
exhaust emissions, such as oxides of nitrogen, oxides of sulfur,
and particulate matter, that are likely to become harmful
substances that impede environmental preservation. For this reason,
recently, a gas engine, one of engines each serving as a substitute
for the diesel engine and being capable of reducing the amount of
generated harmful substances, has been widely used.
[0004] Moreover, as an engine configured to combine the
characteristics of the diesel engine and the characteristics of the
gas engine, a dual fuel engine configured to combine a premixed
combustion method that allows combustion of gaseous fuel (fuel
gas), such as natural gas, having been mixed with air and supplied
to a combustion chamber, and a diffusion combustion method that
allows combustion of liquid fuel, such as heavy oil, having been
injected into a combustion chamber, has been proposed (see Japanese
Examined Patent Publication No. 2002-004899 and Japanese Examined
Patent Publication No. 2008-202545).
SUMMARY OF THE INVENTION
[0005] In such a dual fuel engine, for a diesel mode and a gas
mode, there is a difference in a required air-fuel ratio, and
further, an air flow amount required in the gas mode is small
compared with the diesel mode relative to the same load. For this
reason, a supercharger is required to meet a specification in the
diesel mode, whereas, when operated in the gas mode, the
supercharger is required to be capable of providing air amount
appropriate to an air-fuel ratio in the gas mode. Further, in
conventional dual fuel engines, when operated in the gas mode,
there is room for improvement to realize sufficient responsiveness
in air flow amount control, and high trackability and
appropriateness relative to a load variation in air-fuel ratio
control.
[0006] Thus, it is a technical object of the present invention to
provide a multi-fuel employment type engine device in which
improvements based on considerations in view of such current
situations as described above have been incorporated.
[0007] According to a first aspect of the present invention, an
engine device includes at least one cylinder; an intake manifold
configured to supply air into the at least one cylinder; an exhaust
manifold configured to discharge exhaust gas from the at least one
cylinder; at least one main fuel injection valve configured to
inject liquid fuel into the at least one cylinder to cause
combustion of the liquid fuel; at least one gas injector configured
to mix gas fuel with the air supplied by the intake manifold; a
supercharger including a compressor and configured to compress air
through a use of the exhaust gas from the exhaust manifold; an
intercooler configured to cool compressed air resulting from the
compression by the supercharger and supply resultant cooled air to
the intake manifold; a main throttle valve disposed at a portion
where an outlet of the supercharger and an inlet of the intercooler
are coupled to each other; an exhaust bypass flow path configured
to couple an outlet of the exhaust manifold to an exhaust outlet of
the supercharger; an exhaust bypass valve disposed in the exhaust
bypass flow path; an air supply bypass flow path configured to
bypass the compressor of the supercharger; and an air supply bypass
valve disposed in the air supply bypass flow path. Further, within
a low load range of a load on the engine device, when the load is
lower than a predetermined load, feedback control is performed on
the main throttle valve, and when the load is higher than the
predetermined load, map control based on a data table is performed
on the main throttle valve.
[0008] According to a second aspect of the present invention, in
the engine device according to the first aspect of the present
invention, within the low load range, when the load is higher than
the predetermined load, feedback control may be performed on the
exhaust bypass valve and map control may be performed on the air
supply bypass valve.
[0009] According to a third aspect of the present invention, in the
engine device according to the first aspect of the present
invention, within the low load range, when the load is lower than
the predetermined load, the exhaust bypass valve may be caused to
fully open and the air supply bypass valve may be caused to be
fully closed.
[0010] According to a fourth aspect of the present invention, in
the engine device according to the first aspect of the present
invention, within a medium and high load range of the load, the
opening degree of the main throttle valve may be kept to a
fully-open opening degree, and each of the exhaust bypass valve and
the air supply bypass valve may be controlled to allow pressure
inside the intake manifold to be adjusted to a target value
appropriate to the load.
[0011] According to a fifth aspect of the present invention, in the
engine device according to the fourth aspect of the present
invention, within the medium and high load range, the feedback
control may be performed on the exhaust bypass valve, and the map
control may be performed on the air supply bypass valve.
[0012] According to the embodiment of the present invention, an
engine device includes at least one cylinder; an intake manifold
configured to supply air into the at least one cylinder; an exhaust
manifold configured to discharge exhaust gas from the at least one
cylinder; at least one main fuel injection valve configured to
inject liquid fuel into the at least one cylinder to cause
combustion of the liquid fuel; at least one gas injector configured
to mix gas fuel with the air supplied by the intake manifold; a
supercharger including a compressor and configured to compress air
through a use of the exhaust gas from the exhaust manifold; an
intercooler configured to cool compressed air resulting from the
compression by the supercharger and supply resultant cooled air to
the intake manifold; a main throttle valve disposed at a portion
where an outlet of the supercharger and an inlet of the intercooler
are coupled to each other; an exhaust bypass flow path configured
to couple an outlet of the exhaust manifold to an exhaust outlet of
the supercharger; an exhaust bypass valve disposed in the exhaust
bypass flow path; an air supply bypass flow path configured to
bypass the compressor of the supercharger; and an air supply bypass
valve disposed in the air supply bypass flow path. Further, within
a low load range of a load on the engine device, when the load is
lower than a predetermined load, feedback control is performed on
the main throttle valve, and when the load is higher than the
predetermined load, map control based on a data table is performed
on the main throttle valve. Thus, in a state in which the
supercharger is optimized in accordance with a combustion mode
specification for liquid fuel, in a combustion mode using gas fuel,
control of each of the opening degree of the exhaust bypass valve
and the opening degree of the air supply bypass valve in accordance
with the variation of the engine load also realizes an air-fuel
ratio optimized to the engine load. During a load variation,
therefore, the deficiency of the amount of air needed for the
combustion is eliminated or minimized, and as a result, the engine
device also operates in a suitable condition in the gas mode in a
state in which the supercharger optimized for use in the diesel
mode is used.
[0013] Further, within the low load range, when the engine load is
higher than the predetermined load, feedback control on the exhaust
bypass valve and map control on the air supply bypass valve are
concurrently performed, and thus, the responsiveness of flow amount
control by the exhaust bypass valve is complemented by the air
supply bypass valve, and a control range of the air supply bypass
valve is complemented by the exhaust bypass valve. Moreover, within
the low load range, in the case where the engine load is lower than
the predetermined load, even when air pressure inside the intake
manifold becomes negative during a low load operation, concurrent
control of causing the exhaust bypass valve to fully open and of
causing the air supply bypass valve to be fully closed realizes
securing an air amount needed for the combustion.
[0014] Further, according to the embodiment of the present
invention, within a medium and high load range, each of the exhaust
bypass valve and the air supply bypass valve is controlled so as to
allow pressure inside the intake manifold to be adjusted to a
target value appropriate to the load. Thus, in a state in which the
supercharger is optimized in accordance with a combustion mode
specification for liquid fuel, in a combustion mode using gas fuel,
the air-fuel ratio is controlled so as to be responsive to the
variation of the engine load. In this regard, during a load
variation, the deficiency of the amount of air needed for the
combustion is eliminated or minimized, and as a result, the engine
device also operates in a more suitable condition in the gas mode
in a state in which the supercharger is optimized for use in the
diesel mode is used.
[0015] Further, within the medium and high load range, feedback
control on the air supply bypass valve and map control on the
exhaust bypass valve that are concurrently performed realize
supplying the engine device with air adapted to an air-fuel ratio
needed for the combustion of the gas fuel. Control of the opening
degree of the exhaust bypass valve in accordance with the variation
of an engine load realizes supplying the engine with air adapted to
an air-fuel ratio needed for the combustion of the gas fuel.
Further, a combination with responsive control operation by the air
supply bypass valve increases trackability relative to a load
variation in the gas mode. Moreover, control of air pressure by
both of the air supply bypass valve and the exhaust bypass valve
realizes expansion of a control range of the control of air
pressure.
BRIEF DESCRIPTION OF THE DRAWINGS
[0016] FIG. 1 is a side view of the whole of a ship according to an
embodiment of the present invention;
[0017] FIG. 2 is a cross-sectional side view of a machine room;
[0018] FIG. 3 is a plan view of the machine room;
[0019] FIG. 4 is a schematic diagram illustrating a configuration
of fuel supply paths in an engine device according to an embodiment
of the present invention;
[0020] FIG. 5 is a schematic diagram illustrating a configuration
of air supply and exhaust paths in the engine device;
[0021] FIG. 6 is a block diagram illustrating a control system of
the engine device;
[0022] FIG. 7 is a diagram illustrating a relation between a
pressure ratio and an air flow amount in a supercharger of the
engine device;
[0023] FIG. 8 is a right side view of an engine device according to
an embodiment of the present invention;
[0024] FIG. 9 is a left side view of the engine device;
[0025] FIG. 10 is a plan view of the engine device;
[0026] FIG. 11 is a rear view of the engine device;
[0027] FIG. 12 is a front view of the engine device;
[0028] FIG. 13 is a perspective view of the engine device
illustrating a configuration of an exhaust manifold installation
side (right side) of the engine device;
[0029] FIG. 14 is a perspective view of the engine device
illustrating a configuration of a fuel injection pump installation
side (left side) of the engine device;
[0030] FIG. 15 is a perspective view of the engine device when
viewed from an upper side of a supercharger installation side
(upper front side) of the engine device;
[0031] FIG. 16 is a flowchart illustrating control operation on a
main throttle valve of an engine device according to an embodiment
of the invention;
[0032] FIG. 17 is a flowchart illustrating control operation on an
air supply bypass valve of the engine device;
[0033] FIG. 18 is a flowchart illustrating control operation on an
air supply throttle valve of the engine device; and
[0034] FIG. 19 is a diagram illustrating control of an air-fuel
ratio relative to a load during a gas mode operation of the engine
device.
DESCRIPTION OF THE EMBODIMENTS
[0035] Hereinafter, an embodiment resulting from embodying the
present invention will be described on the basis of figures when
this embodiment is applied to a pair of propulsion and
power-generation mechanisms mounted in a ship of a twin-engine and
twin-shaft type.
[0036] First, the outline of a ship will be described. As shown in
FIGS. 1 to 3, a ship 1 according to this embodiment includes a hull
2, a cabin 3 (a bridge deck), a funnel 4 (a smoke stack), a pair of
propellers 5, and a rudder 6. The cabin 3 is disposed at the aft
side of the hull 2. The funnel 4 is disposed behind the cabin 3.
The pair of propellers 5 and the rudder 6 are disposed in a lower
portion of the rear side of the hull 2. In this case, a pair of
skegs 8 are formed integrally with an aft portion of a bottom 7.
Propulsion shafts 9 are each rotatably supported by a corresponding
one of the skegs 8. The propulsion shafts 9 each drivingly rotate a
corresponding one of the propellers 5. The slegs 8 are formed in a
shape that is left-right symmetric about a hull center line CL (see
FIG. 3). This hull center line CL divides a left-right direction
side of the hull 2. That is, in a first embodiment, a twin skeg is
employed as an aft-side shape of the hull 2.
[0037] A hold 10 is disposed in a fore portion and a center portion
inside the hull 2, and, in an aft portion inside the hull 2, a
machine room 11 is disposed. In the machine room 11, a pair of
propulsion and power-generation mechanisms 12 are separately
disposed at left and right portions sandwiching the hull center
line CL. The propulsion and power-generation mechanisms 12 each
serve as both of a driving source for a corresponding one of the
propellers 5 and an electric-power supply source for the ship 1.
Each of the propellers 5 is drivingly rotated by rotation power
transmitted from a corresponding one of the propulsion and
power-generation mechanisms 12 to a corresponding one of the
propulsion shafts 9. The inside of the machine room 11 is
partitioned in an upper-lower direction by an upper deck 13, a
second deck 14, a third deck 15, and an inner bottom plate 16. The
propulsion and power-generation mechanisms 12 according to the
first embodiment are disposed on the inner bottom plate 16 located
at the lowest stage of the machine room 11. Although not
illustrated, the hold 10 is partitioned into a plurality of
sections.
[0038] As shown in FIGS. 2 and 3, each of the propulsion and
power-generation mechanisms 12 is a mechanism resulting from
combining a medium-speed engine device 21 (a dual-fuel engine in
this embodiment), a reduction gear 2, and a shaft drive power
generator 23. The medium-speed engine device 21 is a driving source
of a corresponding one of the propellers 5. The reduction gear 22
transmits power of a corresponding one the engine devices 21 to a
corresponding one of the propulsion shafts 9. The shaft drive power
generator 23 is driven by the power of a corresponding one of the
engine devices 21 to generate electric power. Here, the
"medium-speed" engine means an engine that drives at a rotation
speed of approximately 500 to 1000 revolutions per one minute.
Incidentally, a "low-speed" engine drives at a rotation speed of
500 rotations or less per one minute, and a "high-speed" engine
drives at a rotation speed of 1000 rotations or more per one
minute. The engine device 21 in this embodiment is configured to
drive at a constant rotation speed falling within a medium speed
range (a range approximately from 700 to 750 revolutions per one
minute).
[0039] The engine device 21 includes a cylinder block 25 including
an engine output shaft 24 (a crankshaft), and cylinder heads 26
mounted on the cylinder block 25. A base table 27 is installed on
the inner bottom plate 16 at the lowest stage of the machine room
11 so as to be directly or via a vibration isolator (omitted from
illustration). The cylinder block 25 of the engine device 21 is
mounted on the base table 27. The engine output shaft 24 is
extended in a direction along a front-rear length direction of the
hull 2. That is, the engine device 21 is disposed inside the engine
room 11 in a state in which the engine output shaft 24 is directed
along the front-rear length direction of the hull 2
[0040] The reduction gear 22 and the shaft drive power regenerator
23 are disposed at the aft side of the engine device 21. The rear
end of the engine output shaft 24 protrudes from the rear face side
of the engine device 21. The reduction gear 22 is coupled to the
rear end side of the engine output shaft in a power transmissible
manner. The shaft drive power generator 23 is disposed at the
opposite side of the reduction gear 22 from the engine device 21.
The engine device 21, the reduction gear 22, and the shaft drive
power generator 23 are disposed so as to be arranged in this order
from the front side of the inside of the engine room 11. In this
case, the reduction gear 22 and the shaft drive power generator 23
are disposed inside or adjacent to the skeg 8, which is located at
the aft side. With this configuration, therefore, the engine device
21 is disposed at a position as close to the aft side as possible
without being subjected to any restriction pertaining to a buttock
line of the ship 1, and this disposition of the engine device 21
contributes to downsizing of the engine room 11.
[0041] The propulsion shaft 9 is disposed at the downstream side of
the reduction gear 22 in a power transmission direction. The
contour of the reduction gear 22 protrudes downward from the engine
device 21 and the shaft drive power generator 23. The front end
side of the propulsion shaft 9 is coupled to the rear face side of
the protruding portion in a power transmissible manner. The engine
output shaft 24 (shaft core) and the propulsion shaft 9 are located
in a state of causing their shafts to overlap each other in a plan
view. The propulsion shaft 9 extends in the front-rear length
direction of the hull 2 in a state of causing the position of the
core of the propulsion shaft 9 to be shifted vertically relative to
the engine output shaft 24 (shaft core). In this case, the
propulsion shaft 9 is disposed at a position lower than the
positions of the shaft drive power generator 23 and the engine
output shaft 24 (shaft core) and close to the inner bottom plate
16. That is, the shaft drive power generator 23 and the propulsion
shaft 9 are respectively separated to an upper portion and a lower
portion, and do not interfere with each other. This configuration,
therefore, downsizes each of the propulsion and power-generation
mechanisms 12.
[0042] The constant-speed power output of the engine device 21 is
transmitted from the rear end side of the engine output shaft 24 to
the reduction gear 22, and then is branched and transmitted to each
of the shaft drive power generator 23 and the propulsion shaft 9 by
the reducer gear 22. One portion of the constant-speed power output
of the engine 21 is subjected to reduction of its speed by the
reduction gear 22 to a rotation speed of, for example, 100 to 120
revolutions per one minute, and then is transmitted to the
propulsion shaft 9. The propeller 5 is drivingly rotated by the
speed-reduced power from the reduction gear 22. Here, a variable
pitch propeller capable of adjusting a ship speed through the
change of a pitch angle of its propeller blades is employed as the
propeller 5. Further, another portion of the constant-speed power
output of the engine device 21 is subjected to increase of its
speed by the reduction gear 22 to a rotation speed of, for example,
1200 to 1800 revolutions per one minute, and then is transmitted to
a PTO shaft rotatably supported by the reduction gear 22. The rear
end side of this PTO shaft of the reduction gear 22 is coupled to
the shaft drive power generator 23 in a power transmissible manner
to allow the power generation of the shaft drive power generator 23
to be driven based on the rotational power from the reduction gear
22. Electric power resulting from the power generation driven by
the shaft drive power generator 23 is supplied to an electric
system inside the hull 2.
[0043] The engine device 21 is coupled to an intake path (omitted
from illustration) and an exhaust path 28. The intake path is used
for taking air into the inside, and the exhaust path 28 is used for
discharging exhaust gas to the outside. The air having been taken
into the inside through the intake path is sent into each of
cylinders 36 (i.e., into each of cylinders during an intake
stroke). Further, since there exist two engine devices 21, two
exhaust paths 28 exist. Each of the exhaust paths 28 is coupled to
a corresponding one of extension paths 29. The extension paths 29
are configured to extend to the funnel 4 so as to directly
communicate with the outside. The exhaust gas from each of the
engine devices 21 is discharged to the outside of the ship 1 via a
corresponding one of the exhaust gas paths 28 and a corresponding
one of the extension paths 29.
[0044] As clear from the above description, the pair of propulsion
and power-generation mechanisms 12, each constituted by combining
the engine device 21, the reduction gear 22, which transmits the
power of the engine device 21 to the propulsion shaft 9, which
drivingly rotates the propeller 5, which is a propeller for ship
propulsion, and the shaft drive power generator 23, which is
allowed to generate electric power by the power of the engine
device 21, are provided, and further, the pair of propulsion and
power-generation mechanisms 12 are separated to and disposed at
left and right portions sandwiching the hull center line CL in the
machine room 11 inside the hull 2, and thus, an engine installation
space in the engine room 11 is configured to be small compared with
a conventionally structured machine room in which a plurality of
engines (a main-engine and a sub-engine) are disposed. Further,
this configuration shortens the front-rear length of the machine
room 11 so as to compactly configure the machine room 11, and
eventually, this compactly configured machine room 11 facilitates
securing a space of the hold (i.e., a space other than the machine
room 11) in the hull 2. The existence of the two propellers 5
increases the propulsion efficiency of the ship 1.
[0045] Moreover, since two engine devices 21 each being a main
engine are provided, for example, even when one of the two engine
devices 21 fails and is brought into a drive disabled state, the
other one of the engine devices 21 enables the ship 1 to navigate,
and secures redundancy to be provided in the vessel prime mover
device, and eventually secures redundancy to be provided in the
ship 1. Moreover, as described above, since each of the engine
devices 21 drivingly rotates the propeller 5 and drives the shaft
drive power generator 23, any one of the shaft drive power
generators 23 is allowed to serve as a spare for the other one of
them during a normal navigation. Thus, when any one of the engine
devices 21 or any one of the shaft drive power generators 23 fails
and this failure brings the supply of electric power to a halt, the
supply of electric power is recovered merely by activating the
other one of the shaft drive power generators 23 and establishing
its frequency and voltage. Further, when, during a navigation using
only one of the engine devices 21, the only one engine device 21
has been brought to a halt, the supply of electric power is
recovered merely by activating the other one of the engine devices
21, which is in a halt state, and further by activating a shaft
drive power generator 23 corresponding to the other one of the
engine devices 21 and establishing its frequency and voltage.
[0046] Next, an outline of the configuration of a dual fuel engine
21 will be described with reference to FIGS. 4 to 7. This dual fuel
engine 21 is used as a main engine in the ship 1. The dual fuel
engine 21 (hereinafter referred to as just an "engine device 21")
optionally selects and drives one of a premixed combustion method
that allows combustion of gas fuel, such as natural gas, having
been mixed with air gas and supplied to a combustion chamber, and a
diffusion combustion method that allows combustion of liquid fuel,
such as heavy oil, having been injected into a combustion chamber.
FIG. 4 is a diagram illustrating fuel systems for supplying fuel to
the engine device 21. FIG. 5 is a diagram illustrating an intake
system and an exhaust system of the engine device 21. FIG. 6 is a
control block diagram of the engine device 21.
[0047] As shown in FIG. 4, the engine device 21 is supplied with
fuel from two systems of fuel supply paths 30 and 31, a gas fuel
tank 32 being coupled to the fuel supply path 30, which is one of
the two systems, a liquid fuel tank 33 being coupled to the fuel
supply path 31, which is the other one of the two systems. That is,
the engine device 21 is configured to allow fuel gas to be supplied
to the engine device 21 through the fuel supply path 30, and allow
fuel oil to be supplied to the engine device 21 through the fuel
supply path 31. The fuel supply path 30 includes the gas fuel tank
32, a vaporization device 34, and a gas valve unit 35. The gas fuel
tank 32 stores gas fuel in a liquefied state in itself. The
vaporization device 34 vaporizes the liquefied fuel (fuel gas) of
the gas fuel tank 32. The gas valve unit 35 adjusts an amount of
fuel gas supplied from the vaporization device 34 to the engine
device 21. That is, the fuel supply path 30 is configured to allow
the vaporization device 34 and the gas valve unit 35 to be arranged
in this order from the gas fuel tank 32 toward the engine device
21.
[0048] As shown in FIG. 5, the engine device 21 is configured to
allow the plurality of cylinders 36 (six cylinders in this
embodiment) to be arranged in series in the cylinder block 25. Each
of the cylinders 36 communicates with an intake manifold (intake
flow path) 67 (see FIG. 20) via a corresponding one of intake ports
37. The intake manifold 67 and the intake ports 37 are disposed
inside the cylinder block 25. Each of the cylinders 36 communicates
with an exhaust manifold (exhaust flow path) 44 via a corresponding
one of exhaust ports 38. The exhaust manifold 44 and the exhaust
ports 38 are disposed above the cylinder heads 26. A gas injector
98 is disposed at the intake port 37 of each of the cylinders 36.
Thus, air from the intake manifold 67 is supplied to each of the
cylinders 36 via a corresponding one of the intake ports 37,
whereas exhaust gas from each of the cylinders 36 is discharged to
the exhaust manifold 44 via a corresponding one of the exhaust
ports 38. Further, when the engine device 21 operates in a gas
mode, for each of the cylinders 36, fuel gas is supplied to a
corresponding intake port 37 through a corresponding gas injector
98 to allow the fuel gas to be mixed with air from the intake
manifold 67 and then be supplied to the each cylinder 36.
[0049] An exhaust inlet of a turbine 49a of a supercharger 49 is
coupled to an exhaust outlet side of the exhaust manifold 44, and
an air discharge outlet (fresh air outlet) of an intercooler 51 is
coupled to an air inlet side (fresh air inlet side) of the intake
manifold 67. An air discharge outlet (fresh air outlet) of a
compressor 49b of the supercharger 49 is coupled to an air intake
inlet (fresh air inlet) of the intercooler 51. A main throttle
valve V1 is disposed between the compressor 49b and the intercooler
51, and the opening degree of the main throttle valve V1 is
adjusted to adjust the flow amount of air supplied to the intake
manifold 67.
[0050] An air supply bypass flow path 17 couples an air inlet side
of the intercooler 51 to an air intake inlet (fresh air inlet) side
of the compressor 49b. The air supply bypass flow path 17
recirculates part of air discharged from the outlet of the
compressor 49b to the inlet of the compressor 49b. That is, the air
supply bypass flow path 17 is released to outside air at the
upstream side of the air intake inlet of the compressor 49b, while
the air supply bypass flow path 17 is coupled to a coupling portion
where the intercooler 51 and the main throttle valve V1 are coupled
to each other. An air supply bypass valve V2 is disposed in the air
supply bypass flow path 17, and the opening degree of the air
supply bypass valve V2 is adjusted to adjust the flow amount of air
flown from the downstream side of the main throttle valve V1 into
the intercooler 51.
[0051] An exhaust bypass flow path 18 couples an exhaust outlet
side of the turbine 49a to the exhaust outlet side of the exhaust
manifold 44. That is, the exhaust bypass flow path 18 is released
to outside air at the downstream side of the exhaust outlet of the
turbine 49a, while the exhaust bypass flow path 18 is coupled to a
coupling portion where the exhaust outlet of the turbine 49a and
the exhaust inlet of the turbine 49a are coupled to each other. An
exhaust-gas valve V3 is disposed in the exhaust bypass flow path
18, and the opening degree of the exhaust bypass valve V3 is
adjusted to adjust the flow amount of exhaust gas flown into the
turbine 49a so as to allow an air compression amount of the
compressor 49b to be adjusted.
[0052] The engine device 21 includes the supercharger 49 and the
intercooler 51. The supercharger 49 allows the exhaust gas from the
exhaust manifold 44 to compresses air. The intercooler 51 cools
compressed air having been compressed by the supercharger 49, and
then supplies resultant cooled air to the intake manifold 67. The
engine device 21 includes the main throttle valve V1 at the
coupling portion where the outlet of the supercharger 49 and the
inlet of the intercooler 51 are coupled to each other. The engine
device 21 includes the exhaust bypass flow path 18, which couples
the outlet of the exhaust manifold 44 to the exhaust outlet of the
supercharger 49, and includes the exhaust bypass valve V3 in the
exhaust bypass flow path 18. In a state in which the supercharger
49 is optimized in accordance with a diesel mode specification, in
a gas mode, control of the opening degree of the exhaust bypass
valve V3 in accordance with the variation of an engine load also
realizes an air-fuel ratio optimized to the engine load. With this
configuration, therefore, during a load variation, the excess or
deficiency of an amount of air needed for combustion is eliminated
or minimized, and as a result, the engine device 21 operates
optimally in the gas mode even in a state in which the supercharger
is optimized for use in the diesel mode is used.
[0053] The engine device 21 includes the air supply bypass flow
path 17, which bypasses the supercharger 49, and includes the air
supply bypass valve V2 in the air supply bypass flow path 17.
Control of the opening degree of the air supply bypass valve V2 in
accordance with the variation of an engine load realizes supplying
the engine air adapted to an air-fuel ratio needed for the
combustion of the fuel gas. Further, a combination with responsive
control operation by the air supply bypass valve V2 increases a
response speed relative to a load variation in the gas mode.
[0054] The engine device 21 allows the air supply bypass flow path
17 to be coupled to a portion located between the inlet of the
intercooler 51 and the main throttle valve V1 to allow compressed
air discharged from the compressor 49b to be fed back to the inlet
of the inlet of the compressor 49b. With this configuration, the
responsiveness of the flow amount control by the exhaust bypass
valve V3 is complemented by the air supply bypass valve V2, and a
control range of the air supply bypass valve V2 is complemented by
the exhaust bypass valve V3. Accordingly, this configuration
improves trackability of air-fuel ratio control in the gas mode
during a load variation or upon change of an operation mode in a
use for ships.
[0055] As shown in FIG. 6, the engine device 21 includes an engine
control device 73, and this engine control device 73 controls
individual portions of the engine device 21. The engine device 21
includes, for each of the cylinders 36, a pilot fuel injection
valve 82, a fuel injection pump 89, and a gas injector 98. The
engine control device 73 respectively supplies with the pilot fuel
injection valve 82, the fuel injection pump 89, and the gas
injector 98 with control signals to control a pilot fuel injection
by the pilot fuel injection valve 82, fuel oil supply by the fuel
injection pump 89, and gas fuel supply by the gas injector 98.
[0056] The engine control device 73 supplies the main throttle
valve V1, the air supply bypass valve V2, and the exhaust bypass
valve V3 with control signals to adjust their respective opening
degrees so as to adjust air pressure (intake manifold pressure)
inside the intake manifold 67. A pressure sensor 39 measures air
pressure inside the intake manifold 67, and upon receipt of a
measurement signal from the pressure sensor 39, the engine control
device 73 detects intake manifold pressure. The engine control
device 73 receives a measurement signal from a load measurement
tool 19, such as a watt transducer or a torque sensor, and
calculates a load on the engine device 21. The engine device 73
receives a measurement signal from an engine rotation sensor 20,
such as a pulse sensor, for measuring a rotation number of the
crankshaft 24, and detects an engine rotation number of the engine
device 21.
[0057] When the engine device 21 operates in the diesel mode, the
engine control device 73 controls, for each of the cylinders 36,
the opening/closing of a control valve in the fuel injection pump
89 to cause combustion in the each cylinder 36 at predetermined
timing points. That is, the engine control device 73 allows the
control valve in the fuel injection pump 89 to open in
synchronization with the injection timing points for the each
cylinder 36 to cause fuel oil to be injected into the each cylinder
36 through a corresponding main fuel injection valve 79 so as to
cause ignition in the each cylinder 36. Further, in the diesel
mode, the engine control device 73 keeps the supply of each of the
pilot fuel and the fuel gas in a halt state.
[0058] In the diesel mode, the engine control device 73 performs
feedback control on the timing points of the injections through the
main fuel injection valve 79 in the each cylinder 36 on the basis
of an engine load (an engine output) having been measured by the
load measurement tool 19 and an engine rotation number having been
measured by the engine rotation sensor 20. With this configuration,
the engine 21 outputs an engine load needed by the propulsion and
power-generation mechanism 12 and, concurrently, rotates at an
engine rotation number adapted to a propulsion speed of the ship.
Further, the engine control device 73 controls the opening degree
of the main throttle valve V1 on the basis of the intake manifold
pressure having been measured by the pressure sensor 39 to allow
the supercharger 49 to supply the intake manifold 67 with
compressed air that becomes an air flow amount adapted to a needed
engine output.
[0059] When the engine device 21 operates in the gas mode, for each
of the cylinders 36, the engine control device 73 adjusts the
opening degree in the gas injector 98 to set the gas flow amount of
fuel supplied into the each cylinder 36. Further, the engine
control device 73 controls the opening/closing of the pilot fuel
injection valve 82 to cause combustion in the each cylinder 36 at
predetermined timing points. That is, the gas injector 98 supplies
the intake port 37 with fuel gas having a flow amount adapted to
the valve aperture to allow the fuel gas to be mixed with air from
the intake manifold 67 and then be supplied to the each cylinder
36. Further, the engine control device 73 allows the control valve
in the pilot fuel injection valve 82 to open in synchronization
with injection timing points for the each cylinder 36 to allow the
injection of the pilot fuel to generate an ignition source so as to
cause ignition in the each cylinder 36, to which the premixed gas
has been supplied. Further, in the gas mode, the engine control
device 73 keeps the supply of the fuel oil in a halt state.
[0060] In the gas mode, the engine control device 73 performs
feedback control of the flow amount of fuel gas supplied by the gas
injector 98 and timing points of the injections through the pilot
injection valve 82 in the each cylinder 36 on the basis of an
engine load having been measured by the load measurement tool 19
and an engine rotation number having been measured by the engine
rotation sensor 20. Further, the engine control device 73 adjusts
the opening degree of each of the main throttle valve V1, the air
supply bypass valve V2, and the exhaust bypass valve V3 on the
basis of the intake manifold pressure having been measured by the
pressure sensor 39. With this configuration, the intake manifold
pressure is adjusted to pressure adapted to an engine output, and
further, an air-fuel ratio for the fuel gas supplied from the gas
injectors 98 is adjusted to a value adapted to the engine
output.
[0061] The supercharger 49 has a capacity associated with the
engine device 21 with its operation in the diesel mode. Thus, when
the engine device 21 operates in the gas mode, the capacity of the
supercharger 49 is needed to be associated with the engine device
21 with its operation in the gas mode on a pseudo basis. In FIG. 7,
a relationship between a pressure ratio (a ratio of a discharge
pressure value relative to an intake pressure value in relation to
the compressor 49b) and an air flow amount (a discharge flow amount
in relation to the compressor 49b or a flow amount of air supplied
to the intake manifold 67). As shown in FIG. 7, in the case where
the engine load is the same, a compression ratio and an air flow
amount at an operation point P2 in the gas mode are respectively
lower than a compression ratio and an air flow amount at an
operation point P1 in the diesel mode.
[0062] When the diesel engine 21 has switched its operation from
the diesel mode to the gas mode, in the case where only the exhaust
bypass valve V3 is controlled to make a change between the
operation points, the exhaust bypass valve V3 is caused to open to
decrease the rotation number of the turbine 49a so as to reduce the
compression ratio and the air flow amount of the compressor 49b. In
this case, as shown in FIG. 7, the vector quantity of the operation
point P1 in the diesel mode and the vector quantity of the
operation point P2 in the gas mode are large, and thus, it takes a
long time to complete the change to the gas mode.
[0063] Meanwhile, in the case where both of the air supply bypass
valve V2 and the exhaust bypass valve V3 are controlled to make a
change between the operation points, the air supply bypass valve V2
is caused to open to bypass the compressed air discharged from the
compressor 49b to the inlet port of the compressor 49b via the air
supply bypass flow path 17, and simultaneously, the exhaust bypass
valve V3 is caused to open to decrease the rotation number of the
turbine 49a. That is, the feedback of the compressed air from the
discharge outlet to the intake inlet of the compressor 49b through
the air supply bypass flow path 17 decreases the compression ratio
of the compressor 49b, as shown in FIG. 7. With this configuration,
therefore, an amount of the decrease of the compression ratio of
the compressor 49b by the control of the exhaust bypass valve V3 is
reduced, and this reduction of the amount of the decrease of the
compression ratio shortens a switching time taken to perform the
switching to the operation point in the gas mode.
[0064] Next, the detailed configuration of the dual-fuel engine 21
(the engine device 21), having such an outline configuration as
described above, will be described with reference to FIGS. 8 to 20.
In the following description, position relations among front, rear,
left, and right directions in the configuration of the engine
device 21 are specified on the assumption that its side coupled to
the reduction gear 22 is its rear side.
[0065] As shown in FIGS. 8 to 15, the engine device 21 includes the
engine output shaft 24 in the cylinder block 25, which is installed
on the base table 17 (see FIG. 2), and a plurality of cylinder
heads 26 mounted on the cylinder block 25. Further, a plurality of
head covers 40 are arranged in one row in a front-rear direction so
as to be each mounted on a corresponding one of the cylinder heads
26. The engine device 21 is configured such that, on the right side
face of a row of the cylinder heads 26, a gas manifold (gas fuel
pipe) 41 is disposed so as to extend in parallel to the row of the
head covers 40, whereas, on the left side face of the cylinder
block 25, fuel oil pipes (liquid fuel pipes) 42 are disposed so as
to extend in parallel to the row of the head covers 40, and side
covers 43 are disposed so as to cover the fuel oil pipes 42.
Further, the exhaust manifold (exhaust flow path) 44, which will be
described later, is disposed so as to extend in parallel to the row
of the head covers 40 at the upper side of a gas manifold 41, and
the periphery of the exhaust manifold 44 is covered by heat shield
covers 45.
[0066] A supra-cylinder head cooling water pipe 46 is disposed
between the row of the head covers 40 and the heat shield covers 45
so as to extend in parallel to the row of the head covers 40. The
cooling water pipe 46 is coupled to cooling water paths inside the
cylinder heads 26. A common rail (pilot fuel pipe) 47 is disposed
above the cooling water pipe 46 so as to extend in parallel to the
row of the head covers 40, just like the cooling water pipe 46. In
this case, the cooling water pipe 46 is coupled to and supported by
the cylinder heads 26, and the common rail 47 is coupled to and
supported by the cooling water pipe 46. Further, the heat shield
covers 45 are coupled to and supported by the cooling water pipe 46
and the cylinder block 25.
[0067] The front end (exhaust outlet side) of the exhaust manifold
44 is coupled to the supercharger 49 via an exhaust relay pipe 48.
Accordingly, the exhaust gas discharged through the exhaust
manifold 44 is flown into the turbine 49a of the supercharger 49
via the exhaust relay pipe 48 to rotate the turbine 49a, and this
rotation of the turbine 49a rotates the compressor 49b including
the same shaft as that of the turbine 49a. The supercharger 49 is
disposed at the upper side of the front end of the engine device
21, and respectively includes the turbine 49a and the compressor
49b at the right side and the left side of the supercharger 49
itself. Further, an exhaust outlet pipe 50 is disposed at the right
side of the supercharger 49 and is coupled to the exhaust outlet of
the turbine 49a so as to allow the exhaust gas from the turbine 49a
to be discharged into the exhaust path 28 (see FIG. 2) through the
exhaust outlet pipe 50 itself.
[0068] The intercooler 51, which cools the compressed air from the
compressor 49b of the supercharger 49, is disposed blow the
supercharger 49. That is, the intercooler 51 is disposed at the
front end side of the cylinder block 25, and the supercharger 49 is
mounted above the intercooler 51. The air discharge outlet of the
compressor 49b is disposed at a left-right direction center layer
position of the supercharger 49 so as to communicate backward
(i.e., toward the cylinder block 25 side). Meanwhile, an upwardly
communicating air intake inlet is disposed on the upper face of the
intercooler 51, and through this air intake inlet, the compressed
air discharged from the compressor 49b is flown into the
intercooler 51. Further, the air discharge outlet of the compressor
49b and the air intake inlet of the intercooler 51 communicate with
each other through an intake relay pipe 52 with its ends coupled to
them. This intake relay pipe 52 includes the main throttle valve V1
described above (see FIG. 5).
[0069] On the front end face (the front side face) of the engine
device 21, a cooling water pump 53, a pilot fuel pump 54, a
lubricant oil pump (priming pump) 55, and a fuel oil pump 56 are
disposed at the outer circumference side of the engine output shaft
24. In this case, the cooling water pump 53 and the fuel oil pump
56 are respectively disposed at an upper portion and a lower
portion that are near the left side face, and the pilot fuel pump
54 and the lubricant oil pump 55 are respectively disposed at an
upper portion and a lower portion that are near the right side
face. Further, a rotation transmission mechanism (omitted from
illustration) for transmitting the rotation power of the engine
output shaft 24 is disposed in the front end portion of the engine
device 21. With this configuration, the rotation power from the
engine output shaft 24 is transmitted via the above rotation
transmission mechanism, and this transmitted rotation power rotates
the cooling water pump 53, the pilot fuel pump 54, the lubricant
oil pump 55, and the fuel oil pump 56, which are disposed at the
outer circumference of the engine output shaft 24. Moreover, in the
inside of the cylinder block 25, a camshaft (omitted from
illustration) whose shaft is directed in the front-rear direction
is rotatably supported at a portion above the cooling water pump
53, and the rotation power of the engine output shaft 24 is also
transmitted to the camshaft via the above rotation transmission
mechanism to rotate the camshaft.
[0070] An oil pan 57 is disposed below the cylinder block 25, and
lubrication oil flowing through the cylinder block 25 is
accumulated in this oil pump 57. The lubricate pump 55 is
configured to allow its lower side suction inlet to be coupled to
the oil pan 57 via a lubricant oil pipe to suck the lubrication oil
accumulated in the oil pan 57. Further, the lubricant oil pump 55
is configured to allow its upper discharge outlet to be coupled to
a lubricant oil inlet of a lubricant oil cooler 58 via a lubricant
oil pipe to supply the lubrication oil having been sucked from the
oil pan 57 to the lubricant oil cooler 58. The lubricant oil cooler
58 respectively includes a lubricant oil inlet and a lubricant oil
outlet at the front side and the rear side of the lubricant oil
cooler 58 itself, and allows the lubricant oil outlet to be coupled
to a lubricant oil filter 59 via a lubricant oil pipe. The
lubricant oil filter 59 respectively includes a lubricant oil inlet
and a lubricant oil outlet at the front side and the rear side of
the lubricant oil filter 59 itself, and allows the lubricant oil
outlet to be coupled to the cylinder block 25. Accordingly,
lubricant oil flown from the lubricant oil filter 55 is cooled by
the lubricant oil cooler 58, and then is purified by the lubricant
oil filter 59.
[0071] The lubricant oil cooler 58 and the lubricant oil filter 59
are fixed to the right side face of the cylinder block 25. Further,
the lubricant oil cooler 58 and the lubricant oil filter 59 are
disposed in series in the front-rear direction on the right side
face of the cylinder block 25 so as to allow the lubricant oil
cooler 58 to be anteriorly located (i.e., located at the lubricant
oil pump 55 side). Further, a cylinder block right-side cooling
water pipe 60 extends in the front-rear direction, and is disposed
at a position between the gas manifold 41 and the lubricant oil
cooler 58 so as to be distanced from the right side face of the
cylinder block 25. This cooling water pipe 60 is disposed so as to
extend along the gas manifold 41 from the front side of the
cylinder block 25 up to a position between the lubricant oil cooler
58 and the lubricant oil filter 59.
[0072] Further, the cooling water pipe 60, which is disposed so as
to extend along the gas manifold 41, is coupled to an intercooler
discharge side cooling water pipe 61, through which cooling water
discharged from the intercooler 51 is flown, and the cooling water
discharged from the intercooler 51 is supplied to the lubricant oil
cooler 58. Further, the intercooler 51 is configured to allow the
discharge side cooling water pipe 61 and a water supply side
cooling water pipe 62 to be respectively disposed at an upper
portion and a lower portion on the right side face of the
intercooler 51 itself, and allows the discharge side cooling water
pipe 61 and the water supply side cooling water pipe 62 to be
inserted into the intercooler 51 itself to cool the compressed air
from the compressor 49b of the supercharger 49.
[0073] The supercharger 49 rotatably supports the compressor 49b
and the turbine 49a. The compressor 49b and the turbine 49a include
the same shaft, and are respectively separated to and disposed at a
left portion and a right portion of the supercharger 49. Further,
the exhaust gas discharged through the exhaust manifold 44 is
introduced into the turbine 49a via the exhaust relay pipe 48 to
rotate the turbine 49a, and this rotation of the turbine 49a
rotates the compressor 49b. Further, the supercharger 49 includes
an intake filter 63 and a fresh-air path pipe 64 at a fresh-air
intake side, that is, at the left side of the compressor 49b. The
intake filter 63 purifies introduced outside air. The fresh-air
path pipe 64 couples the intake filter 63 to the compressor 49b.
With this configuration, the rotation of the compressor 49b in
synchronization with the rotation of the turbine 49a introduces
outside air (fresh air) having been sucked by the intake filter 63
into the compressor 49b itself via the supercharger 49. Further,
the compressor 49b compresses the sucked air having been introduced
from its left side, and then discharges resultant compressed air
into the intake relay pipe 52, which is disposed at the rear side
of the compressor 49b.
[0074] The intake relay pipe 52 includes an upper front-side
opening coupled to a discharge outlet on the rear face of the
compressor 49b via a bellows pipe 65, whereas the intake relay pipe
52 includes a lower-side opening coupled to an intake inlet on the
upper face of the intercooler 51. Further, the intercooler 51 is
coupled to one end of an air supply bypass pipe 66 (the air supply
bypass flow path 17) at a branch port provided in a ventilation
path disposed on the front face of the intercooler 51 so as to
allow part of the compresses air having been cooled by the
intercooler 51 to be discharged into the air supply bypass pipe 66.
The other end of the air supply bypass pipe 66 is coupled to a
branch port provided on the front face of the fresh-air path pipe
64 to allow part of the compressed air having been cooled by the
intercooler 51 to be flown back to the fresh-air path pipe 64 via
the air supply bypass pipe 66 and to join outside air from the
intake filter 63. Further, the air supply bypass pipe 66 includes
the air supply bypass valve V2 in its halfway portion.
[0075] The intercooler 51 is configured to, when, from its left
rear side, the compressed air from the compressor 49b is flown in
through the intake relay pipe 52, cool the compressed air from the
compressor 49b on the basis of a heat exchange with cooling water
supplied from a water supply pipe 62. In the inside of the
intercooler 51, the compressed air having been cooled in its left
chamber is flown into the ventilation path, disposed on its front
face, to be introduced into its right chamber, and then is
discharged into the intake manifold 67 through a discharge outlet
disposed at the rear side of the right chamber. The intake manifold
67 is disposed on the right side face of the cylinder block 25, and
is disposed so as to extend in parallel to the row of the head
covers 40 below the gas manifold 41. The flow amount of compressed
air flown back from the intercooler 51 to the compressor 49b is
determined in accordance with the opening degree of the air supply
bypass valve V2, and this determination of the flow amount of the
flown-back compressed air results in a setting of a flow amount of
the compressed air supplied to the intake manifold 67.
[0076] Further, the supercharger 49 includes a rear-side intake
inlet coupled to the exhaust relay pipe 48 and a right-side
discharge outlet coupled to the exhaust outlet pipe 50. With this
configuration, the supercharger 49 allows the exhaust gas from the
exhaust manifold 44 to be introduced into the gas turbine 49a via
the exhaust relay pipe 48 to allow the introduced exhaust gas to
rotate the turbine 40a and, simultaneously, allow this rotation of
the turbine 40a to rotate the compressor 49b. Further, the
supercharger 49 allows the exhaust gas to be discharged to the
exhaust path 28 (see FIG. 2) through the exhaust outlet port 50.
The exhaust relay pipe 48 includes its rear-side opening coupled to
the discharge outlet of the exhaust manifold 44 via a bellows pipe
68, whereas the exhaust relay pipe 48 includes its front-side
opening coupled to the rear-side intake inlet of the turbine
49a.
[0077] Further, at a halfway position of the exhaust relay pipe 48,
a branch port is disposed on its right side face, and this branch
port of the exhaust relay pipe 48 is coupled to one end of an
exhaust bypass pipe 69 (the exhaust bypass flow path 18). The
exhaust bypass pipe 69 allows its another end to be coupled to a
junction port disposed at the rear side of the exhaust outlet pipe
50 to allow part of the exhaust gas discharged from the exhaust
manifold 44 to be bypassed to the exhaust outlet pipe 50 not
through the supercharger 49. Further, the exhaust bypass pipe 69
includes the exhaust bypass valve V3 in its halfway portion. An
flow amount of the exhaust gas bypassed from the exhaust manifold
44 to the exhaust outlet pipe 50 is set in accordance with the
opening degree of the exhaust bypass valve V3, and this setting of
the flow amount of the bypassed exhaust gas results in an
adjustment of the flow amount of the exhaust gas supplied to the
turbine 49a. Further, the exhaust bypass pipe 69 includes a bellows
pipe 70 at a position between the exhaust bypass valve V3 and a
coupling portion coupled to the exhaust relay pipe 48.
[0078] A machine-side operation control device 71 is secured to the
left side face of the intercooler 51 via a support stay (support
member) 72. This machine-side control device 71 controls
stating/stopping, and any other action of the engine device 21, and
includes switches for receiving starting/stopping operation by a
worker, and a display for displaying the states of individual
portions of the engine device 21. An engine starting device 75 is
secured to a rear end side portion on the left side face of the
cylinder block 25, and this engine starting device 75 performs
operation to start up the engine device 21.
[0079] Further, the engine control device 73, which controls the
operations of individual portions of the engine device 21, are
secured to the rear end face of the cylinder block 25 via a support
stay (support member) 74. A flywheel 76 is disposed at the rear end
side of the cylinder block 25, and the engine control device 73 is
disposed above the flywheel 76. This flywheel 76 rotates in
conjunction with the reduction gear 22. The engine control device
73 is electrically coupled to sensors (pressure sensors and
temperature sensors) disposed at individual portions of the engine
device 21 to collect temperature data, pressure data, and any other
measurement data having been measured at the individual portions of
the engine device 21. Further, the engine control device 73 sends
signals to electro-magnetic valves, and any other component
disposed at individual portions of the engine device 21 to control
various operations (a fuel oil injection, a pilot fuel injection, a
gas injection, a cooling water temperature adjustment, and any
other operation).
[0080] The cylinder block 25 includes a step portion at the upper
side of the left side face of the cylinder block 25 itself, and the
fuel injection pumps 89, the number of which is the same as that of
the head covers 40 and that of the cylinder heads 26, are disposed
on the upper face of the step portion 25a of the cylinder block 25.
The fuel injection pumps 89 are arranged in one row along the left
side face of the cylinder block 25. Further, the left side face of
each of the fuel injection pumps 89 is coupled to the fuel oil
pipes (liquid fuel pipes) 42, and the upper end of each of the fuel
injection pumps 89 is coupled to the left side face of a
corresponding one of the cylinder heads 26 that is located at the
front right side of the each fuel injection pump 89 via a
corresponding one of fuel discharge pipes 90. The fuel oil pipes 42
are constituted of two upper and lower pipes, one being an oil
supply pipe for supplying fuel oil to the fuel injection pumps 89,
the other one being an oil return pipe for returning fuel oil from
the fuel injection pumps 89. Further, each of the fuel discharge
pipes 90 is coupled to a corresponding one of the main fuel
injection valves 79 via a fuel flow path inside a corresponding one
of the cylinders 26 to supply the fuel oil from a corresponding one
of the fuel injection pumps 89 to the corresponding one of the main
fuel injection valves 79.
[0081] The fuel injection pumps 89 are arranged at the left side of
and in parallel to the row of the head covers 40 on the step
portion of the cylinder block 25 such that each of the fuel
injection pumps 89 is located at the rear left side of a
corresponding one of the cylinder heads 26 that is coupled to the
each fuel injection pump 89 via a corresponding one of the fuel
discharge pipes 90. Further, the fuel injection pumps 89 are
arranged in one row at positions sandwiched by the cylinder heads
26 and the fuel oil pipes 42. As shown in FIGS. 9 to 11, the fuel
injection pumps 89 are covered together with the fuel oil pipes 42
by the side covers 43, which are disposed on the step portion 25a
of the cylinder block 25. Each of the fuel injection pumps 89
allows rotation of a pump cam in the camshaft (omitted from
illustration) inside the cylinder block 25 to cause a push-up
operation of a plunger. Further, each of the fuel injection pumps
89 allows the push-up operation of the plunger to raise pressure of
the fuel oil supplied from one of the fuel oil pipes 42 to a high
pressure level, and then allows resultant high-pressure fuel oil to
be supplied to a corresponding one of the main fuel injection
valves 79 via a corresponding one of the fuel discharge pipes
90.
[0082] As shown in FIGS. 9 and 12 to 15, the front edge of the
common rail 47 is coupled to the discharge side of the pilot fuel
pump 54 via a pilot fuel relay pipe 96 to allow pilot fuel
discharged from the pilot fuel pump 54 to be supplied to the common
rail 47. The pilot fuel relay pipe 96 has a shape configured to, in
order to allow a discharge outlet of the pilot fuel pump 54 to be
coupled to the front end of the common rail 47, extend from the
discharge outlet of the pilot fuel pump 54 toward the upper side of
the left side face of the cylinder block 25, and then bend to
extend, on the front end face of the row of the cylinder heads 26,
from the left side face of the row of the cylinder heads 26 toward
the front end of the common rail 47.
[0083] As shown in FIGS. 8, 13, and 15, the gas manifold 41 is
coupled to a gas inlet pipe 97 at the front side of the right side
face of the cylinder block 25 so as to be supplied with fuel gas in
a pressed state. The gas inlet pipe 97 is one of gas supply paths
coupled to the gas valve unit 35 (see FIG. 4). That is, the front
end of the gas manifold 41 is coupled to the gas inlet pipe 97 to
allow fuel gas from the gas valve unit 35 to be supplied to the gas
manifold 41. The gas manifold 41 is disposed so as to extend along
the row of the head covers 40 at a height-direction position where
the gas manifold 41 is interposed between the exhaust manifold 44
and the intake manifold 67
[0084] The gas manifold 41 includes a gas main pipe 41a and a
plurality of gas branch pipes 41b. The front end of the gas main
pipe 41a extends in the front-rear direction and is coupled to the
gas inlet pipe 97. The plurality of branch pipes 41b are branched
from the upper face of the gas main pipe 41a toward the cylinder
head 26. The gas main pipe 41a includes coupling flanges on its
upper face at equal distance intervals, and each of the coupling
flanges is fastened to an inlet side flange of a corresponding one
of the gas branch pipes 41b. For each of the gas branch pipes 41b,
its end portion opposite a coupling portion coupled to the gas main
pipe 41a is coupled to the right side face of a sleeve into which
the gas injector 98 is inserted from the top side.
[0085] The gas main pipe 41a and the gas branch pipes 41b
constitute the gas manifold 41, and the gas main pipe 41a and the
gas branch pipes 41b are each formed of a double-wall pipe.
Further, the gas inlet pipes 97 and the sleeves are also each
formed of a double-wall pipe. That is, each of gas pipes laid at
the downstream side of the gas valve unit 35 has a double-wall pipe
structure in which an outer pipe encloses a highly pressed inner
pipe, and this inner pipe (inner space) allows fuel gas to be flown
toward each of the gas injectors 98 via the gas manifold 41.
Further, each of the gas pipes laid at the downstream side of the
gas valve unit 35 allows leaked fuel gas to be collected and sent
to the gas valve unit 35 through a space between the outer pipe and
the inner pipe (i.e., an outer space).
[0086] As shown in FIGS. 13 and 15, the exhaust manifold 44 allows
exhaust main pipes 44a and bellows pipes 44b to be alternately
arranged in one row and allows every pair of the exhaust main pipe
and the bellows pipe to be coupled to each other. Further, the
exhaust manifold 44 allows exhaust branch pipes 44c (each being one
portion of the exhaust port 38) to be each branched from a lower
side portion of a corresponding one of the exhaust main pipes 44a
and coupled to the right side face of a corresponding one of the
cylinder heads 26. The exhaust main pipes 44a and the exhaust
branch pipes 44c are provided so as to allow the number of the
exhaust main pipes 44a and the number of the exhaust branch pipes
44c to be the same as the number of the cylinder heads 26, and each
of the exhaust branch pipes 44c is coupled to the front side of the
right side face of a corresponding one of the cylinders 26. That
is, in a front side portion of each of the cylinder heads 26, a
corresponding one of exhaust valves 81 is disposed, and the exhaust
inlet side of a corresponding one of the exhaust branch pipes 44c
is coupled to the right side face of the each cylinder head 26.
Further, the exhaust manifold 44 allows the exhaust inlet side
flange of each of the exhaust branch pipes 44c to be fastened to
the right side face of a corresponding one of the cylinder heads 26
so as to be supported by the cylinder heads 26.
[0087] As shown in FIGS. 8 and 13, the intake manifold 67 is
disposed at the upper right side of the cylinder block 25 so as to
extend in the front-rear direction at a position where a
height-direction position of the intake manifold 67 is located
below the gas manifold 41. Further, as shown in FIG. 13, for each
of the cylinder heads 26, a rear portion of its right side face
protrudes toward the gas manifold 41, and this protruding portion
on the right side face results in an intake branch portion
including in its inside an air flow path allowing the protruding
portion to communicate with a portion lying directly on the intake
manifold 67. That is, for each of the cylinder heads 26, its rear
side portion where an intake valve 80 is disposed is coupled to the
intake manifold 67 via the intake branch portion.
[0088] Next, air flow amount control in the case where the dual
fuel engine 21 (the engine device 21) having the foregoing
configuration operates in the gas mode will be described with
reference to FIGS. 5, 6, and 16 to 19.
[0089] As shown in FIG. 16, in the case where an engine load falls
within a low load range lower than a predetermined load L2, and is
lower than a predetermined load L1 (L1<L2) (Yes at STEP 1), the
engine control device 73 performs feedback control (PID control) on
the opening degree of the main throttle valve V1. At this time, the
engine control device 73 sets an intake manifold pressure target
value (a target pressure value) adapted to the engine load.
Further, upon receipt of a measurement signal from the pressure
sensor 39, the engine control device 73 confirms an intake manifold
pressure measurement value (a measured pressure value), and
calculates a difference with the target pressure value.
Subsequently, the engine control device 73 performs the PID control
on a valve aperture of the main throttle valve V1 on the basis of
the deference value between the target pressure value and the
measured pressure value to cause an air pressure value of the
intake manifold 67 to approximate the target pressure value.
[0090] In the case where the engine load falls within the low load
range, and is higher than or equal to the predetermined load L1 (No
at STEP 1 and Yes at STEP 3), the engine control device 73 performs
the map control on the opening degree of the main throttle valve V1
(STEP 4). At this time, the engine control device 73 refers to a
data table DT1 to set a valve aperture of the main throttle valve
V1 into a valve aperture associated with the engine load. Here, the
data table DT1 stores in itself valve apertures of the main
throttle valve V1 that are each associated with a corresponding one
of engine loads. Further, in the case where the engine load falls
within the middle/high load range, which covers loads each being
higher than or equal to the load L2, (No at STEP 3), the engine
control device 73 performs control so as to cause the main throttle
valve V1 to fully open.
[0091] As shown in FIG. 17, in the case where the engine load is
lower than the predetermined load L1 (Yes at STEP 101), the engine
control device 73 performs control so as to cause the exhaust
bypass valve V3 to fully open (STEP 102). In the case where the
engine load is higher than or equal to the predetermined load L1
(No at STEP 101), the engine control device 73 performs the
feedback control (PID control) on the opening degree of the exhaust
bypass valve V3 (STEP 103). At this time, the engine control device
73 performs the PID control of a valve aperture of the exhaust
bypass valve V3 on the basis of the difference value between a
target pressure value adapted to the engine load and a measured
pressure value from the pressure sensor 39 to cause an air pressure
value of the intake manifold 67 to approximate the target pressure
value.
[0092] As shown in FIG. 18, in the case where the engine load is
lower than the predetermined load L1 (Yes at STEP 201), the engine
control device 73 performs control so as to cause the air supply
bypass valve V2 to fully open (STEP 202). In the case where the
engine load is higher than or equal to the predetermined load L1
(No at STEP 201), the engine control device 73 performs the map
control on the opening degree of the air supply bypass valve V2
(STEP 203). At this time, the engine control device 73 refers to a
data table DT2 to set a valve aperture of the air supply bypass
valve V2 into a valve aperture associated with the engine load.
Here, the data table DT2 stores in itself valve apertures of the
air supply bypass valve V2 that are each associated with a
corresponding one of engine loads.
[0093] As shown in FIG. 19, within the low load range, which covers
loads each being lower than the load L2, in the case where the
engine load is lower than the predetermined load L1 (L1<L2), the
engine control device 73 performs the feedback control (PID
control) based on an intake manifold pressure value having been
measured by the pressure sensor 39 to set the opening degree of the
main throttle valve V1. Further, in the case where the engine load
is higher than the predetermined load L1, the engine control device
73 performs the map control based on the data table DT1 to set an
aperture of the main throttle valve V1. Meanwhile, within the
middle/high load range, which covers loads each being higher than
or equal to the load L2, the main throttle V1 is caused to open
with a predetermined aperture (fully open in this embodiment), and
the air supply bypass valve V2 and the exhaust bypass valve V3 are
each controlled to allow the intake manifold pressure to be
adjusted to a target value adapted to the engine load.
[0094] In a state in which the supercharger 49 is optimized in
accordance with a diesel mode specification, during an operation in
the gas mode, even when the engine load falls within the
middle/high load range within which operation points are largely
different from those in the diesel mode, responsive control is
realized in the pressure control on the intake manifold 67. Thus,
during a load variation, the excess or deficiency of the amount of
air needed for combustion is eliminated or minimized, and as a
result, even when the engine device 21 operates using the
supercharger 49, which is optimized in accordance with a diesel
mode specification, the engine device 21 optimally operates in the
gas mode.
[0095] Further, within the middle/high load range, an aperture of
the exhaust bypass valve V3 is set through the feedback control
(PID control) based on an intake manifold pressure value having
been measured by the pressure sensor 39, and simultaneously, the
opening degree of the air supply bypass valve V2 is set through the
map control based on the data table DT1. Control of the aperture of
the exhaust bypass valve V3 in accordance with the variation of an
engine load realizes supplying the engine device 21 with air
adapted to an air-fuel ratio needed for the combustion of gas fuel.
Further, a combination with responsive control operation by the air
supply bypass valve V2 increases a response speed needed to respond
to a load variation in the gas mode.
[0096] Within the low load range, in the case where the engine load
is higher than the predetermined load L1, an aperture of the
exhaust bypass valve V3 is set through the feedback control (PID
control) based on an intake manifold pressure value having been
measured by the pressure sensor 39, and simultaneously, the opening
degree of the air supply bypass valve V2 is set through the map
control based on the data table DT2. Meanwhile, in the case where
the engine load is lower than the predetermined load L1, the air
supply bypass valve V2 is caused to be fully closed, and the
exhaust bypass valve V3 is caused to fully open.
[0097] That is, when the exhaust manifold pressure becomes negative
pressure, which is pressure lower than atmospheric pressure, the
exhaust bypass valve V3 is caused to fully open to bring the drive
of the turbine 49a to a halt. Thus, this configuration eliminates
or minimizes surging in the supercharger 49 and any other undesired
operation. Further, the control of causing the air supply bypass
valve V2 to be fully closed realizes responsive control in the
intake manifold pressure control by the main throttle valve V1
during a low load operation.
[0098] The engine device 21 includes, for each of the cylinders 36,
the intake valve 80, the exhaust valve 81, the main fuel injection
valve 79, and the gas injector 98. The intake valve 80 allows air
to be taken into a main combustion chamber inside the each cylinder
36. The exhaust valve 81 allows exhaust gas to be discharged from
the main combustion chamber. The main fuel injection valve 79
injects liquid fuel into the main combustion chamber to cause
combustion of the liquid fuel. The gas injector 98 allows the air
taken into the main combustion chamber to be mixed with gas fuel.
Further, the engine device 21 is configured to allow a gas fuel
pipe 41 and the liquid fuel pipes 42 to be separated to and
disposed at both sides of the row of the head covers 40, which are
arranged in one row. The gas fuel pipe 41 supplies gas fuel to each
of the gas injectors 98. One of the liquid fuel pipes 42 supplies
liquid fuel to each of the main fuel injection valves 79. Further,
the engine device 21 is configured to allow the intake manifold 67,
which supplies air to be taken into each of the main combustion
chambers to a corresponding one of the intake valves 80, to be
disposed so as to extend in parallel to the row of the head covers
40 inside the cylinder block 25. Further, the engine device 21 is
configured to allow the gas fuel pipe 41 and the intake manifold 67
to be disposed side-by-side at one side of the row of the head
covers 40.
[0099] The engine device 21 is configured to allow the gas fuel
pipe 41 and the liquid fuel pipes 42 to be separated to and
disposed at both sides of the row of the head covers 40 so as to be
laid in peripheral regions of the row of the cylinder heads 26 on a
space-saving basis. Thus, this configuration realizes a compact
pipe layout structure. Further, the gas fuel pipe 41 and the intake
manifold 67 are disposed at one side of the row of the head covers
40. Thus, this configuration realizes shortening of the piping
distance between the gas fuel pipe 41 and each of the gas injectors
98, and thus, reduces a pressure loss in gas fuel flowing in the
gas fuel pipe 41.
[0100] The engine device 21 is configured to allow the exhaust
manifold 44, which discharges exhaust gas from the main combustion
chambers, to be disposed so as to extend in parallel to the row of
the head covers 40, and respectively allow the exhaust manifold 44
and the exhaust manifold 67 to be separated to and disposed at a
position above the gas fuel combustion pipe 41 and a position below
the gas fuel combustion pipe 41 at one side of the row of the head
covers 40. Thus, the engine device 21 allows the gas fuel
combustion pipe 41 and the exhaust manifold 44 to be laid as one
set at one side of the row of the cylinder heads 26, and thus, this
configuration enables the fuel injection pumps 89, each being
configured to supply highly pressed liquid fuel to a corresponding
one of the main fuel injection valves 79, to be disposed as one set
together with the liquid fuel pipes 42 at the other side of the row
of the cylinder heads 26.
[0101] The engine device 21 is configured to allow each of the main
combustion chambers to include a corresponding one of the pilot
fuel injection valves 82, and allows the pilot fuel pipe 47, which
supplies pilot fuel to each of the pilot fuel injection valves 82,
to be disposed so as to extend in parallel to the row of the head
covers 40. Further, the engine device 21 is configured to allow the
cooling water pipe 46 to be disposed at a position between the row
of the head covers 40 and the exhaust manifold 44 and above the
cylinder block 25 so as to extend in parallel to the row of the
head covers 40, and allow the pilot fuel pipe 47 to be supported
above the cooling water pipe 46. This support of the pilot fuel
pipe 47 on the cooling water pipe 46 reduces heating up of the
pilot fuel pipe 47 due to high temperature of the exhaust gas.
Accordingly, this configuration of disposing the pilot fuel pipe 47
at the exhaust manifold 44 side realizes a compact disposition of
the individual pipes.
[0102] The engine device 21 is configured to allow the gas fuel
pipe 41 to have the double-wall pipe structure constituted of the
inner pipe, which supplies gas fuel toward each of the gas
injectors 98, and the outer pipe, into which gas fuel is flown from
each of the gas injectors 98. This employment of such a double-wall
pipe structure as the structure of the gas fuel pipe 41 realizes
returning of leaked gas fuel to the fuel source side including the
gas valve unit 35 and any other component, and this configuration
keeps the pressure of the gas fuel pipe 41 constant.
[0103] The engine device 21 is configured to allow the supercharger
44, which allows air to be compressed by the exhaust gas from the
exhaust manifold 44, to be disposed above one end of the engine
device 21 itself, and allow the intercooler 51, which cools
compressed air resulting from the compression by the supercharger
49 and supplies resultant compressed air to the intake manifold 67,
to be disposed below the supercharger 49. The supercharger 49 and
the intercooler 51 are disposed so as to overlap with each other at
the one side of the engine device 21, and thus, this configuration
realizes a compact structure in the engine device 21. Further, the
supercharger 49 and the intercooler 51 are disposed at an upper
position and a lower position so as to allow their positions to
correspond to the upper position of the exhaust manifold 44 and the
lower position of the intake manifold 67, and thus, this
configuration realizes the shortest piping length in relation to
the exhaust manifold 44 and the intake manifold 67 without any
obstacle.
[0104] The engine device 21 is configured to allow the lubricant
oil cooler 58 and the lubricant oil filter 59 to be arranged in
series on one side face of the cylinder block 25, that is, on a gas
fuel pipe 44 side face of the cylinder block 25. Further, the
engine device 21 allows a lubricant oil cooling use cooling water
pipe (first cooling water pipe) 60 to be disposed at a position
between the gas fuel pipe 41 and the lubricant oil cooler 58 so as
to extend along the lubricant oil cooler 58 in a state of being
distanced from the one side face of the cylinder block 25. The
lubricant oil cooling use cooling water pipe (first cooling water
pipe) 60 allows cooling water supplied to the lubricant oil cooler
58 to be flown through the lubricant oil cooling use cooling water
pipe (first cooling water pipe) 60 itself. Moreover, the engine
device 21 allows a cylinder head cooling use cooling water pipe
(second cooling water pipe) 46 to be disposed at a position above
the cylinder block 25 and between the head covers 40 so as to
extend in parallel to the row of the head covers 40. The cylinder
head cooling use cooling water pipe (second cooling water pipe) 46
is coupled to the cylinder head 26.
[0105] The engine device 21 is configured to allow the lubricant
oil cooler 58 and the lubricant oil filter 59 to be disposed on one
side face of the engine device 21, that is, on a gas fuel pipe 44
side face of the engine device 21, and further allow the lubricant
oil cooling use cooling water pipe (first cooling water pipe) 60,
which supplies cooling water to the lubricant oil cooler 58, to be
disposed on the one side of the engine device 21. This
configuration realizes a compact disposition of the lubricant oil
circulation system of the engine device 21, and facilitates a
maintenance work for the lubricant oil circulation system.
Moreover, the cylinder head cooling use cooling water pipe (second
cooling water pipe) 46 is also disposed on the same face side as
that of the lubricant oil cooling use cooling water pipe (first
cooling water pipe) 60 at the upper side of the engine device 21,
and thus, this configuration realizes a compact layout of the
cooling water pipes disposed on the outer side the engine device 21
and thus, realizes shortening of the lengths of the cooling water
pipes.
[0106] The engine device 21 is configured to allow the lubricant
oil pump 55 to be disposed at a position that is located on one end
face constituting the cylinder block 25 and being vertical to the
engine output shaft 24, and that is located at the outer
circumference side of the engine output shaft 24 and is located at
the side of one side face (right side face) which constitutes the
cylinder block 25 and on which the lubricant cooler 58 is disposed,
and to further allow the lubricant oil pump 55 to supply the
lubricant oil cooler 58 with lubricant oil sucked by the lubricant
oil pump 55 itself. This configuration, therefore, allows the
lubricant oil pump 55 to be disposed adjacent to the lubricant oil
cooler 58, and thus realizes shortening of the length of a pipe for
coupling the lubricant oil pump 55 to the lubricant oil cooler
58.
[0107] Additionally, the configurations of the individual portions
are not limited to those illustrated in the above embodiment, and
may be subjected to various modifications within a scope not
departing from the gist of the present invention. Further, the
engine device according to the above embodiment is applicable to
components other than the above-described propulsion and
power-generation mechanism, that is, the engine device according to
the above embodiment is able to constitute, for example, a power
generation device for supplying electric power to an electric
system inside a ship, or a driving source in a land-based power
generation facility.
[0108] The embodiments of the present invention relate to a
multi-fuel employment type engine device capable of dealing with
both of gas fuel, such as natural gas, and liquid fuel, such as
heavy oil.
* * * * *