U.S. patent number 3,780,710 [Application Number 05/191,259] was granted by the patent office on 1973-12-25 for rotary internal-combustion engine.
Invention is credited to Zdislaw Ryszard Przybylski.
United States Patent |
3,780,710 |
Przybylski |
December 25, 1973 |
ROTARY INTERNAL-COMBUSTION ENGINE
Abstract
A rotary internal combustion piston engine providing for
relative operative positioning of the movable portions, such as
rotary cogs and pistons to allow for multiple and varied
utilization of the engine working volume. The pistons are divided
into operative segments comprising suction-exhaust pistons and
power-compression pistons having reduced clearance power loses and
minimal or maximum pressure differentials as required by the
relative pistons to allow for maximum efficiency.
Inventors: |
Przybylski; Zdislaw Ryszard
(Munich, DT) |
Family
ID: |
19952606 |
Appl.
No.: |
05/191,259 |
Filed: |
October 21, 1971 |
Foreign Application Priority Data
|
|
|
|
|
Oct 22, 1970 [PO] |
|
|
P-144010 |
|
Current U.S.
Class: |
123/246; 418/188;
418/196 |
Current CPC
Class: |
F01C
1/20 (20130101); F02B 53/04 (20130101); F01C
19/00 (20130101); F01C 19/02 (20130101); F01C
1/36 (20130101); F02B 2075/027 (20130101); Y02T
10/17 (20130101); Y02T 10/12 (20130101) |
Current International
Class: |
F01C
1/36 (20060101); F01C 1/00 (20060101); F02B
53/00 (20060101); F02B 53/04 (20060101); F01C
19/02 (20060101); F01C 1/20 (20060101); F01C
19/00 (20060101); F02B 75/02 (20060101); F01c
001/14 (); F02b 053/04 () |
Field of
Search: |
;123/8.27,8.31,8.47
;418/188,196 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Croyle; Carlton R.
Assistant Examiner: Koczo, Jr.; Michael
Claims
What I claim is:
1. A rotary internal combustion engine comprising:
a housing having a central cylindrical seat seated in a principal
axis of symmetry of said housing and at least one peripheral
cylindrical seat located in parallel to said central seat, the
spacing of said seats being determined so that their generating
surfaces penetrate one another within the housing;
a piston rotor coaxially rotatably mounted in said central seat of
the housing, two frontal cover plates fixed to end faces of said
rotor and being provided on the circumference thereof with at least
one pair of pistons, one of the pistons of said pair forming a
suction-exhaust piston sucking in air with a rear face thereof and
simultaneously exhausting expanded combustion gases with a front
face thereof, the other of the pistons of said pair forming a
power-compression piston exposed at a rear face thereof to the
action of the expanding gases while a front face of said piston
compresses the sucked-in air;
at least one chambered rotor rotatably mounted in said peripheral
seats of the housing and being adapted for co-operation with said
piston rotor, each said chambered rotor having on its circumference
at least one combustion chamber adapted to receive said pistons of
the piston rotor and dimensioned to provide a close dimensional
tolerance during operative co-operation of said elements, so as to
form forwardly and rearwardly of said pistons, and within said
combustion chambers, working chambers of the engine;
a gear transmission synchronizing the rotary motion of said rotors
and comprising a gear wheel of said piston rotor and gear wheels of
said chambered rotors operatively, engaged therewith;
at least one inlet passage disposed in said piston rotor and
extending from an air inlet through said rear faces of the
suction-exhaust pistons, with said passages the air is sucked into
all said working chambers being formed behind said rear faces of
the suction-exhaust pistons;
at least one outlet passage disposed in at least one of said cover
plates of the piston rotor and partially in said front faces of the
suction-exhaust pistons, said passages providing for exhaustion of
the combustion gases from all of said working chambers being formed
before said front faces of the suction-exhaust pistons;
at least one annular collector located in said housing to which
said outlet passages are connected, and at least one exhaust
passage extending from said collector, whereby the combustion gases
flow into said annular collector and then flow out of said
collector toward the exterior of the engine;
at least one fuel injector mounted in said housing, said injector
during of the compression cycles supplying fuel into said working
chambers being formed before the front faces of the
power-compression pistons; and
at least one ignition plug mounted in each said power-compression
piston, said plugs ignite the air-fuel mixture at the right moment
during of the immersion of each power-compression piston in said
combustion chambers of the chambered rotors.
2. A rotary internal combustion engine according to claim 1, a
central inlet for the air being located in the principal axis of
symmetry of said housing and of said piston rotor, said inlet being
connected with said inlet passages.
3. A rotary internal combustion engine according to claim 1, said
suction-exhaust pistons and said power-compression pistons being
approximately of the same outer shapes, the front and rear face of
each said piston in its principal cross-section forming an
epicycloid, and the lateral, circumferential surface of each said
piston having a profile conforming to the central seat of said
piston rotor.
4. A rotary internal combustion engine according to claim 1, the
shape of each said combustion chamber of each chambered rotor in
its principal cross-section being a combination of an arc of a
circle and two sections of a straight line, each said chamber
having two edges of which the distance is conformed to the
thickness of said pistons so as to obtain the required close
dimensional tolerance during operative co-operation of said
elements.
5. A rotary internal combustion engine according to claim 1, the
number of said combustion chambers of each of said chambered rotor
being an odd number.
6. A rotary internal combustion engine according to claim 1, the
number of said chambered rotors being equal to the sum of all said
pistons of the piston rotor.
7. A rotary internal combustion engine according to claim 1, the
number of said chamber rotors being lower by one than the sum of
all said pistons of the piston rotor.
8. A rotary internal combustion engine according to claim 1, the
number of said chambered rotors being higher by one than the sume
of all said pistons of the piston rotor.
9. A rotary internal combustion engine according to claim 1, in
said housing having passages extending from each said peripheral
seat of the chambered rotor to said central seat of the piston
rotor in the proximity of penetrating edges of said seats, so as to
provide for the equalization of the pressures between the working
chamber of the engine.
10. A rotary internal combustion engine according to claim 1, said
housing having closeable passages connecting said peripheral seats
of the chambered rotors to atmosphere, said passages being located
in portions of the housing at the remotest distance from the
principal axis of symmetry of the housing, said passages providing
for escape of the remainder of combustion gases and scavenging
air.
11. A rotary internal combustion engine according to claim 1, said
ignition plugs being positioned within said power-compression
pistons and extending parallel to the principal axis of the piston
rotor.
12. A rotary internal combustion engine according to claim 1, said
fuel injectors being mounted on the circumference of said housing
proximate before each said chambered rotor in relation to the
direction of rotation of said piston rotor.
13. A rotary internal combustion engine according to claim 1,
comprising, in the front part of said housing in its principal axis
of symmetry, an ignition control device having a commutator
connected by a jack shaft to said piston rotor, said commutator
having a casing with carbon brushes adapted to be set in
predetermined angular positions.
14. A rotary internal combustion engine according to claim 1, each
said gear wheel of the chambered rotor being mounted on a neck of
said rotor so as to enable it to be set in a predetermined angular
position, said gear wheel being pressed by a nut against a frontal
surface of a stationary flanged sleeve, said sleeve being mounted
by a key on said neck, and said gear wheel being angularly
restrained in relation to said sleeve.
15. A rotary internal combustion engine according to claim 1,
comprising a driving shaft rotatably mounted in the principal axis
of symmetry of said housing and being kinematically coupled with
said piston rotor by means of an internal gear and said gear wheels
of the chambered rotors, said internal gear being swingably
connected to said driving shaft and engaging simultaneously all
said gear wheels of the piston rotors, so as to eliminate
clearances in said gear transmission synchronizing the rotors, the
rotational speed of said driving shaft of the engine being
considerably lower than the rotational speed of said piston
rotor.
16. A rotary internal combustion engine according to claim 1, said
piston rotor being cantilever-mounted in rolling bearings and
closed within said central seat on the side of said central inlet
by a ring-shaped insert, said chambered rotors being supported on
both sides through necks in removable sliding bearings set in
predetermined axial positions, said piston rotor and said chambered
rotors being closed on both sides at required axial clearances.
17. A rotary internal combustion engine according to claim 1, said
housing being of unitary structure and adapted to be cooled with a
cooling medium, each said peripheral seat of the chambered rotors
having a constant diameter extending through said housing.
18. A rotary internal combustion engine according to claim 1, said
two frontal cover plates of the piston rotors having in their outer
faces circumferential grooves forming a labyrinth seal, and the
cylindrical surfaces of all of said rotors having labyrinth seal
grooves extending parallel to the axes of said rotors, the frontal
surfaces of said chambered rotors having flat cavities forming
multidirectional labyrinth seals.
19. A rotary internal combustion engine according to claim 1, each
said chambered rotor having a compression ratio control device
comprising: slidable inserts of lenticular cross-section of which
the number is equal to the number of said combustion chambers, an
element integrating said inserts, a sleeve fixed on a neck of said
chambered rotor, oblong cavities in said neck forming an extension
of said combustion chambers, a bearing for shifting said inserts by
means of said element in the axial direction of said combustion
chambers, said inserts being tightly fitted within said oblong
cavities in said neck and the inner surface of said sleeve fixed on
the neck.
20. A rotary internal combustion engine according to claim 1, said
pistons of the piston rotor having radial sliding seals composed of
at least one flat insert and at least one groove formed along the
top of said pistons for receiving said inserts, the length of said
inserts being greater than the width of the piston rotor, whereby
the two ends of each of said inserts slide during the turn of the
piston rotor along the inner circumferential surface of said
central seat in the housing.
21. A rotary internal combustion engine according to claim 1, each
of said two frontal cover plates of the piston rotor being provided
with at least one circumferential groove having therein elastic
slidable rings movable during the turn of the piston rotor along
the inner frontal surfaces of the housing.
22. A rotary internal combustion engine according to claim 1, said
piston rotor being provided with flat inserts seated in grooves
formed along the generating lines of the cylindrical surface of
said rotor, said inserts being pressed by centrifugal force into
the cylindrical surfaces of said chambered rotors, the length of
said inserts being greater than the width of the piston rotor, and
the ends of said inserts being mounted in blind openings made in
the inner faces of said two frontal cover plates of the piston
rotor.
23. A rotary internal combustion engine according to claim 1, each
of said chambered rotors being provided interiorly of its
combustion chambers with yawing inserts which, under the influence
of pressure of gases within said chambers, are pressed against the
front and rear faces of said power-compression pistons of the
piston rotor.
24. A rotary internal combustion engine according to claim 1, each
said chambered rotor including elastic frontal seals extending into
circumferential and radial grooves made in frontal surfaces of said
rotors, said seals being mounted on necks of the chambered
rotors.
25. A rotary internal combustion engine according to claim 1, said
chambered rotors having inside passages adapted to facilitate
cooling of said rotors by a cooling medium.
26. A rotary internal combustion engine according to claim 1, fuel
burning occurring in only selected of said chambered rotors, so as
to enable the engine to operate as a self-driving rotary internal
combustion compressor.
Description
This invention relates to a rotary internal combustion piston
engine with two or more rotors providing for multiple utilization
of the working volume, the engine being adapted to be the prime
mover, and particularly in cases where very small dimensions and a
low weight are required.
In technical and patent literature there may be found descriptions
of numerous rotary engines which in different aspects are similar
to those hereinafter described. Concerned are engines each provided
with a rotor having radial pistons generally coupled by means of a
gear transmission with rotary sealing elements, the so-called
rotary gates or combustion rotors, in which there are provide
suitable chambers adapted to receive the pistons of the rotor. In
all of these engines the rotor and the rotary gates have the shape
of a circular cylinder. The rotor pistons are mounted on the outer
side of the cylindrical surface of the rotor, while the chambers of
the rotary gates are provided within the cylindrical surface of the
gates. Both the rotor and the gates disposed thereabout are mounted
in a conveniently shaped body and they are dimensioned to cooperate
with one another and with the said body as tightly as possible.
The performance characteristics of these engines and the ranges of
their applications are closely connected with the tasks fulfilled
by the essential constructional elements of the given engine and
they result from its essential constructional features. In
particular, these characteristics depend upon the arrangement and
shape of the inlet and outlet passages for the working medium, the
shape of the rotor pistons and of the chambers in the rotary gates,
on the number of the pistons and chambers and on the number of the
rotary gates. Other constructional details such as the seals for
the working volumes, the manner of supplying the fuel, the kind of
ignition, the cooling system etc. are also of varying degrees of
importance.
In the majority of known combustion engines of this kind all rotor
pistons are all-purpose double-acting pistons. Each of the pistons
sucks in with its rear side the working medium and simultaneously
it compresses through its frontal side the medium sucked-in by the
previously acting piston. In the successive working space between
the rotary gates the rear side of the same piston is exposed to the
action of the expanding gases, while the frontal side of that
piston pushes out the combustion gases. This versatility of all
pistons is indeed an advantage, but it also concurrently creates a
number of disadvantages. For example: the pressure difference
between the frontal and the back sides of each piston is at a
maximum in all instances and results in considerable clearance
losses. The individual working cycles of the engine always repeat
in the same working spaces between the rotary gates, so as to cause
very unequal heating of the body of the engine and of the rotary
gates. This leads to considerable thermal deformations and to a
reduction in the sealing of the working spaces, leading
consequently to a lowering of the efficiency and shortening of the
life of the engine. Every other gate is provided with a combustion
chamber. Due to this fact, the sealing gates are insufficiently
heated, whereas the gates and the combustion chambers become very
hot. Still worse, there is no possibility of economically cooling
these gates. The permissible heat loading limit of the gates
considerably limits the specific power and specific weight of the
engine. Besides, the mechanical loading of the rotary gates, of
their bearings and gear wheels coupling them with the rotor shaft,
is not uniform. These are all reasons in view of which the life of
such an engine is relatively short.
The inlet and outlet passages for the working medium are, as a
rule, arranged in the case of the engine and they are disposed
either on its circumference or on its front surfaces. Consequently
they are more or less overlapped by the rotor pistons or rotary
gates, while frequently they are completely closed. This gives rise
to various losses in the inlet and outlet passages and lowers the
efficiency of the engine. Even in cases where these passages are
only partially arranged in the rotor, they are improperly shaped.
In connection therewith the hydraulic losses in these passages are
accordingly comparatively high.
As far as concerns the shape of the rotor pistons and that of the
chambers of the rotary gates, which are to some extent dependent
upon the former, there are employed a lot of different combinations
of rectilinear, circular, cycloidal, epicycloidal and hypocycloidal
profiles. The shapes of these elements determines not only the
facility of making them, but also influences, in different aspects,
the magnitude of the entire working space of the engine, the
character of the suction and pressing process, the repetition of
the processes occuring in the individual working spaces, the
quality of mutual sealing etc. In this respect, each known rotary
engine reveals advantageous features while being simultaneously
being subject to certain disadvantages.
The optimum number of rotor pistons, that of the rotary gates and
of the chambers in the gates, is very different to determine in
known rotary engines. There are a great many possible combinations,
which is not only of formal but of practical significance. On the
basis of the number of the elements depends their dimensions. To
some extent these numbers determine the distribution and shapes of
the inlet and outlet passages. They indirectly decide the main
characteristics of the engine, among others, its specific power,
rotational speed, repeatability of working cycles, uniformity of
the torque, and the value of shearing forces. The selection of the
best combination of the numbers of the elements, from the point of
view of obtaining particularly favourable properties of the engine,
in connection, of course, with the above-mentioned constructional
features, is rather difficult. Therefore, it is not without good
reason, that each of the known rotary engines of this type shows
apart from advantages also a series of essential disadvantages.
The object of the invention is to eliminate the essential faults
and inconveniences of rotary devices of this type, used as internal
combustion engines. To achieve this object, the invention sets the
task consisting, among others, in differentiating the equal role of
the rotor pistons, elaborating an effective method of supplying the
working medium, providing the most advantages shapes of rotor
pistons and chambers in the rotary gates and in choosing the most
convenient number of all these elements.
The invention encompasses a predetermined group of devices,
especially rotary internal-combustion engines designed in
compliance with a preset technical task. The tasks of the
individual pistons have been differentiated therein, by providing
the rotor -- hereinafter called piston rotor -- with two types of
pistons, namely: suction-exhaust pistons and power-compression
pistons. The outlets of the suction passages have been placed on
the rear side in relation to the direction of the movement of the
suction-exhaust pistons, while the outlets of the exhaust passages
have been disposed in one or both front cover plates of the piston
rotor, in proximity before each suction-exhaust piston.
The suction passages of the piston rotor unite in a common central
inlet in the front central part of the engine, while the exhaust
passages are connected with one, or if necessary, with two
ring-shaped combustion gases collectors, one of which may be placed
also in the front, but outer part of the engine, while the other
maybe located in its central part. All the pistons have a nearly
identical outer shape, which is a combination of e.g., an
epicycloidal and circular line.
The number of the rotary gates, hereinafter called chamber rotors,
is equal e.g., to the sum of all the pistons, or may be higher or
lower by one than the sum of the pistons. The number of combustion
chambers with which the chamber rotors are equipped, is
advantageously an odd number. In the cross section of the chamber
rotors, the combustion chambers have a profile which is a
combination of e.g., an arc of a circle and two sections of a
straight line. In the crank-case there may be located suitable
passages for equalizing the pressure differences between the
working spaces of the engine and its combustion chambers. There are
also provided passages for leading off residuals of combustion
gases from the combustion chambers, or for taking away the
scavenging air.
In the cylindrical surfaces of the chamber rotors and of the piston
rotor there are provided e.g., suitable labyrinth seal grooves. Of
equal importance are also the remaining constructional elements
which must be conveniently accommodated to the entirely new
construction of the engine, such as: location of the sparking plugs
and fuel injectors, positioning the rotors in bearings and other
design of the rotational elements, rotational speed transmission
gear of the piston rotor and of the driving shaft, method of
eventually controlling the compression ratio, solution of blocking
the toothed wheels used in synchronizing all of the rotors,
removing of clearances between said toothed wheels, location of the
ignition control device, etc.
The invention provides for exceptionally favourable performance
characteristics of the novel engine. These advantages result from
the optimal selection of all of the essential constructional
features of the novel engine and also of such features that
generally are considered to be of secondary importance in the
art.
The functional division of the pistons into suction-exhaust pistons
and power-compression pistons gives rise to some important
advantageous consequences. The first of them is the elimination, to
a great extent, of the problem of the clearance losses. The
pressure difference between the frontal and rear surfaces of the
suction-exhaust pistons is always minimal, generally never higher
than several tenths of an atmosphere. In case of power-compression
pistons the pressure difference may indeed be high, but for a very
short time only. At that time in front of the piston there takes
place the beginning of the working cycle, and behind the piston the
beginning of the compression process. Already at any little
movement of this piston, the pressure difference quickly drops to
zero, then, changes its sign and increases to a value which appears
when behind the piston there is finished the expansion of
combustion gases, and in front of the piston the compression of
air, which also only takes a very short time. In consequence of
such a distribution of pressures during the movement of the
power-compression piston, any leakages are immediately throttled
and have the tendency to revert. Longer lasting pressure
differences have been limited to locations where the seal does not
involve greater difficulties, i.e., to the contact of the
cylindrical part of the piston rotor with the cylindrical part of
the chamber rotors.
The second consequence of the functional division of the pistons is
the creation of perfect natural engine cooling conditions, decrease
of the head load of the chamber rotors of the engine and
equalization of the temperature distribution in its crankcase. The
natural cooling of the engine and the equalization of the
temperature distribution in its carnkcase each result from the fact
that in each working space between the chamber rotors there take
place successively all the following working cycles: exhaust,
suction, compression, work.
The decrease of the heat loading on the chamber rotors is obtained
due to the fact that the fuel combustion process takes place in the
chambers of all chamber rotors, and not as in other rotary engines
of this type -- in each other chamber rotor. Thereby the heat
loading of said rotors is reduced to one-half without any change of
the specific power of the engine -- or alternatively, this provides
the possibility of obtaining double the specific power without any
need for increasing the heat loading of the chamber rotors.
The third consequence of the functional division of the pistons is
the improved internal heat regeneration resulting from the partial
utilization of heat of the combustion gases. This is attained due
to the fact that the portion of the power-compression piston
exposed at its rear side to the continuous action of the high
temperature of the combustion gases, is intensively heating with
its frontal side the air which is being compressed in the adjacent
working space. In case of two or more piston pairs there is,
furthermore, provided a full symmetry of the forces by the pressure
of the working medium, which act upon the crankcase and the rotor,
whereas no radial forces act upon the bearing of the rotor. All
these facts advantageously influence the efficiency of the engine,
its specific power, and consequently also its dimensions weight,
and also its life expectancy.
The above described method of designing the inlet and outlet
passages provides additional favourable consequences. Above all
there are now obtained features which were unobtainable in other
combustion engines, viz. : a continuous air suction process and a
continuous process of exhausting the combustion gases. The inlet
passages as well as the outlet passages remain always open. The
flow is of continuous character and is only slightly throttled when
the suction-exhaust piston is traveling through the chambers in the
individual chamber rotors. Thus, in the engine there have been
eliminated to a great extent the losses entailed by opening and
closing of the suction and exhaust valves, by the acceleration of
the working medium at the inflow and outflow apertures, as well as
any losses connected with the flow through contractions at a
critical speed or a speed which is not much lower.
Furthermore, the inlet passages have been disposed in the piston
rotor in a manner allowing the rotor to be effectively cooled from
the inside thereof, and simultaneously to obtain the initial
compression of the air before it reaches the working spaces, viz.:a
slight supercharging of the engine. The central inlet is located in
conformance with the direction of the main axis of the engine and
then, when it is in the piston rotor, it separates into
approximately radial directions, whereby the flow is the same as in
a centrifugal compressor. The supercharging is the greater, the
higher the rotations of the engine. Such a method of designing the
inlet and outlet passages improves above all the efficiency of the
engine and increases its specific power.
The shape, as above described, of the pistons has been designed
according to the principle of improved co-operation with the
chamber rotors, facility of production, possibility of arranging
labyrinth seal grooves, and creation of sufficient space for
location of the inlet passages and sparking plugs.
As far as combustion chambers are concerned, both the shape and the
number of said chambers in each chamber rotor must be mentioned.
The adopted shape of the combustion chambers, in effect, a
combination e.g., of the semicircle and two sections of the
straight line as measured through their cross-section, assures not
only a proper co-operation with the pistons of the rotor but makes
it also possible to obtain the highest precision in the positioning
of the edges of the chambers and a very simple solution in the
construction of the mechanism of the compression ratio control
system. An odd number of the combustion chambers, particularly 3 in
number, is of extreme importance in the proper performance of the
engine. That number makes it possible to reduce and to equalize the
temperature loading of the chamber rotors, it creates conditions
for especially good scavenging of the combustion chambers, and it
also assures provisions of the most convenient proportions of the
chamber rotors in relation to the piston rotor.
The piston rotor is provided with an even number of pistons, the
suction-exhaust pistons and the power-compression pistons being
alternately placed. Therefore, combustion takes place in every
other combustion chamber and occurs again in the same chamber once
for every two turns of the chamber rotor. In consequence thereof,
combustion takes place in a suitable sequence in 11 combustion
chambers, thereby causing a uniform heating of the chamber rotors.
From each chamber, in which the combustion process has just taken
place, the residual combustion gases are expelled, and then, during
the second turn of the chamber rotor, this chamber is filled with
cold air. Consequently, cooling and scavenging are obtained. The
foregoing factors have an advantageous effect particularly on the
life expectancy of the engine and on the improvement of its other
performances, among while others, they contribute to a more
complete combustion and to a decrease of the impurity content of
the combustion gases.
The number of the chamber rotors depends upon the ultimate purpose
of the engine. On this number are dependent e.g., the frequency of
the individual working cycles, the multiple of utilization of the
geometrical working volume of the engine, its specific power,
dimensions, weight etc. For instance, the multiple of utilization
of the geometrical working capacity of the engine is, in the case
of four chamber rotors, approximately twice as large as in the case
of two said rotors. This means that also the specific engine power,
at the same rotational speed, will be approximately twice as large.
The working cycle frequency accruing to dependent upon one rotation
of the piston rotor is in such a case, also twice as large. This
also means obtaining of a more uniform torque, and consequently
e.g., a smoother operation.
The cover plates affixed to the two frontal surfaces of the piston
rotor although appearing to be unessential, are, however, of rather
essential importance to the overall construction of the engine.
Above all, they make it possible to exactly arrange the afore-said
combustion gas outlet passages , and furthermore, they facilitate
the sealing of the individual working spaces, while they simplify
the axial setting of multi-chamber rotors.
On the frontal and rear sides of each chamber rotor there may be
provided a passage for connecting the suitable working space and
the cylindrical seat of that rotor. The passages on the frontal
sides of the chamber rotors assure a correct sequence of the air
compression processes in each working space of the engine. The
passages on the rear sides of the rotors assure a correct sequence
of the combustion gases expansion processes. This is possible due
to the fact that through each of these passages there occurs the
equilization of the pressures between the working space and the
corresponding combustion chamber, and this both during the initial
compression phase -- before connecting the given chamber units with
the compression space -- and during the end compression phase --
when such a chamber is already disconnected from the expansion
space. This determines above all the general efficiency of the
engine, and also the specific rate of fuel comsumption.
The passages in the middle part of the cylindrical seats of the
chamber rotors may be open or closed, as required. Residual
combustion gases rejected by the centrifugal force may escape
through these passages, and during the next operating turn of the
chamber rotor -- the scavenging air may flow out. This provides for
improved scavenging of the engine and more intensive cooling, which
results in improving the cleanliness of the combustion gases.
The remaining improved constructional features of the engine are,
perhaps, not as essential, but they basically result from
constructional reasons or they are more self-evident and as such
are described moe superficially or are completely omitted.
Glow plugs or sparking plugs are placed e.g., in power-compression
pistons for the purpose of rendering possible the regulation of the
ignition advance in any suitably large limits. The access to these
plugs is easy -- at the disclosed constructional embodiment of the
engine, and simultaneously -- the construction and the arrangement
of the ignition device may be very simple.
The distribution of the fuel injectors in the crankcase of the
engine, near the penetration edges of the cylindrical seats of the
chamber rotors with the cylindrical seat of the piston rotor, is
dictated by the possibility of obtaining a fuel injection sequence
lasting sufficiently long during each air compression cycle in the
working spaces of the engine. It is intended to avail oneself
entirely of the advantage of a direct, timed fuel injection. In
case of an even number of chambers, in each chamber rotor there may
be applied continuous fuel injection into the central air inlet to
the engine, or to a carburetor supply.
The method of blocking any toothed wheels on the pins of the
chamber rotors is intended to create, above all, for conditions of
unitary production of the engine or its prototypes, or for
conditions in which the production takes place with a partial
interchangeability of parts.
The hereinafter described method of reducing the rotational speed
of the engine by applying a gear wheel with an inner indentation,
engaging simultaneously all gear wheels of the chamber rotors, is
especially convenient for tractive applications of the engine and
for all other cases in which small dimensions and little weight are
required. Transmission ratios between the rotational speed of the
piston rotor and the transmission shaft of the engine of : 3; 2,5;
2; 1 and others are obtainable. The application of the solution
makes it also possible to remove clearances in the transmission
synchronizing the rotation of the chamber rotors and the piston
rotor.
The method of embedding the bearing of the piston rotor and of the
chamber rotors is been correlated as advantageously as possible
with the overall construction of the novel engine. The outrigger
support of the piston rotor in the rolling bearings is dictated by
technological and assembling reasons, and also by the possibility
of obtaining a long lasting and reliable operation of the engine.
The same reasons recommend a bilateral support for to the chamber
rotors e.g., in slide bearings separately mounted in ports of the
crankcase of the engine.
Having in mind the hereinbefore mentioned reasons, the crankcase of
the engine is preferably designed as a one-part-member which
provides its great advantage. In the embodiments disclosed by way
of example, it is technologically extremely simple and accommodated
to large-scale production. The cylindrical seats of the chamber
rotors have a constant diameter along the whole width of the
crankcase and may be made out of one piece jointly with the
cylindrical seat of the piston rotor. The cooling of the crankcase
may be effected by air or by fluid, according to the purpose of the
engine. The latter cooling method is more convenient to traction
applications. When a high unit power of the engine is required,
viz. if it is necessary to receive a great quantity of heat for a
small size of the engine, a fluid cooling system is closed
circulation with evaporation is provided.
Gap, labyrinth and opening seals of the working chambers of the
engine are used for several reasons. It is intended to increase the
highest rotational limit of the engine, and consequently its unit
power , and above all to decrease considerably the sliding friction
while distinctly improving the mechanical efficiency of the engine.
Seals of such a type do not require intensive lubrication, whereby
the oil consumption is considerably reduced. Burning of lubrication
oil is also reduced and consequently, no intensive carbon deposit
formation occurs whereby purer combustion gases are obtained.
The effectiveness of the seals of this type becomes sufficient on
account of the hereinabove already partly mentioned properties of
the novel engine, viz.: not too high and symmetrical heat loading
of fundamental elements of the engine, simple rotational movement
of its rotor at small considerable rotational speed, low and short
lasting pressure differential on both sides of the piston, and
relatively small or, in some cases, no mechanical load from gaseous
forces and inertia.
In some applications it becomes advisable to use sliding seals.
This mainly pertains to cases where the rotational speed of the
piston rotor must be relatively low, and consequently also to
engines in which the Diesel cycle is employed.
The device for infinitely variable adjustment of the compression
ratio has been designed with the intention of making a research
version of the engine or for cases where different types of fuel is
required.
Generally taking, the rotary internal combustion engine in its
construction is provided with e.g., a four-piston-rotor and four
three-chamber-rotors and has, in comparison with other engines of
this type, -- a series of advantages. Above all it is characterized
by an exceptionally simple and very compact construction and small
dimensions. Its unit power, at a rotational speed of 10,000 r.p.m.,
may be 400 - 800 B.H.P./l. A conveniently designed and properly
made engine of this type will have a high overall efficiency rate
of the order of 0.4 - 0.5 and a low fuel consumption -- within the
limits of: 0.12 - 1.16 kg/BHP hour. The rotational speed range
about: 3,000 - 20,000 r.p.m. -- without seals of the sliding type,
and with sliding type seals: 500 - 8,000 r.p.m. Output range: 10 -
10,000 HP. The engine is characterized by a quiet and uniform run,
and a high operating reliability. Moreover, the engine will have
good driving properties, viz. such features as: easy starting and
stopping, relatively advantageous traction performance, easy
acceleration and deceleration. The engine is characterized by a
large range of power and torque control due to the possibility of
disengaging any of its chamber rotors. A feature of this engine
lies also in the fact that it can be supplied with light fuel or
natural gas, or it may easily be constructed for multifuel use.
Finally, the engine is characterized not only by relatively low
production costs -- due to its simple and technological
construction, but above all by low operating costs. In the
disclosed embodiment, a running-in period is unnecessary. The life
of the engine is many times longer in comparison with that of other
known rotary engines. Overhauls are practically unnecessary
The engine of the invention is shown by way of examples in the
following descriptions in conjunction with the drawings in which
the individual Figures represent:
FIG. 1 - a longitudinal section of the engine with a
four-piston-rotor and four three-chamber rotors, the section being
taken along the line B -- B in FIG. 2;
FIG. 2 - a cross-sectional view of the engine of FIG. 1, the
section being taken along the line A -- A in FIG. 1;
FIG. 3 - a longitudinal section along the axis of symmetry of the
engine shown without the transmission gear for decreasing the
rotations, and provided with a device for infinitely variable
adjustment of the compression ratio;
FIG. 4 - a cross-sectional view of a three-chamber -rotor of the
engine of FIG. 3;
FIG. 5 - a cross-sectional view of the engine with a
two-piston-rotor and one single-chamber rotor;
FIG. 6 - a cross-sectional view of the engine with a two-piston
rotor and two single-chamber rotors;
FIG. 7 - a cross-sectional view of the engine with a two-piston
rotor and three single-chamber rotors;
FIG. 8 - the cross-sectional view of the engine with a four-piston
rotor and three three-chamber rotors;
FIG. 9 - a cross-sectional view of the engine with a four-piston
rotor and four three-chamber rotors;
FIG. 10 - a cross-sectional view of the engine with a four-piston
rotor and five three-chamber rotors;
FIG. 11 - a radial seal for the pistons and the frontal seal of the
piston rotor;
FIG. 12 - showing seals for the cylindrical surfaces of the rotors;
and
FIG. 13 - seals for the frontal surfaces of the chamber rotors and
seals for the pistons along the edges of the combustion
chambers.
The rotary internal combustion engine according to the invention in
an embodiment provided e.g., with a four-piston rotor and four
three-chamber rotors as shown in FIGS. 1 and 2 - is constructed as
hereinafter described. In the central part of a crankcase 1 there
is a four-piston rotor 2, and around it there are disposed four
three-chamber rotors 3 which are kinematically coupled with the
rotor 2 by means of a gear wheel 4 and four gear wheels 5. The
internal surface of the crankcase 1 is formed by five
interpenetrating, parallel extending circular cylinders of
different size, the largest, central circular cylinder being the
seat 6 of the four-piston rotor 2, while the remaining four
circular cylinders are the seats 7 of the three-chamber rotors
3.
The four-chamber rotor 2 which on the cylindrical surface thereof
is provided with two suction-exhaust pistons 8 and two
power-compression pistons 9, and on the frontal surfaces with cover
plates 10 and 11, is cantilever-like mounted in the bearings 12 and
in the bearing 13 in the crankcase 1. The pistons 8 and 9 are
mounted in a dovetail manner in the four-piston rotor 2 and are
designed so that in a plane which is perpendicular to the axis of
said rotor, the profile of their frontal and rear surfaces, in
relation to the direction of movement of the pistons is
epicycloidal, whereas the profile of the outer surface of the
pistons which lies on the opposite side of the lock, is a circular
one having conveniently shaped grooves forming the seal 14. In the
rear surface of each suction-exhaust piston 8 there is the outlet
for the suction passage 15. These passages lead to a common central
inlet 16 in the four-piston rotor 2. At the front surface of each
of the said pistons 8, and in the frontal cover plate 10 of the
four-piston rotor 2 there is provided the combustion gases outlet
passage 17 leading to the annular collector 18 in the crankcase
1.
The two power-compression pistons 9 are equipped with glow or spark
plugs 19, the axes of which extend parallel to the axis of the
four-piston rotor 2. In the frontal cover plates 10 and 11 of the
four-piston rotor 2 there are provided labyrinth seals 20 and 21.
At the front part thereof, this rotor is equipped with a labyrinth
seal 22, whereas at its rear end, with a sliding seal 23. On the
side of the central inlet 16 the four-piston rotor 2 is closed by
means of a ring-shaped insert 24. The three-chamber rotors 3 are
provided in their cylindrical surfaces with three identical
combustion chambers 25. Each of these chambers has, in the plane
perpendicular to the axes of the multi-chamber rotors 3, a profile
which is a combination of e.g., a semicircle and two sections of a
straight line, and which is conformed to the shape of the pistons 8
and 9 in such a manner that when cooperating with the pistons, the
two edges of each combustion chamber 25 slide along corresponding
surfaces, i.e. the front surface and rear surface of the pistons 8
and 9.
All of the three-chamber rotors 3 are supported on both ends
through the intermediary of the pins 26 and 27 in slide bearings 28
and 29. These bearings are enabled to be set in a suitable axial
position allowing the three-chamber rotors 3 to be tightly closed
on the frontal surfaces.
Each three-chamber rotor 3 may be provided with a device for
controlling the compression ratio as shown in the embodiment of the
engine in FIGS. 3 and 4. This device comprises inserts 30 of
lenticular cross-section, elements 31 integrating these inserts,
and sleeves 32 mounted on the pins 26. These pins are provided with
oblong cavities 33 constituting an extension of the combustion
chambers 25. The inserts 30 are tightly fitted to the said cavities
33 and holes 34 in the elements 31, and also to the internal
surfaces of the sleeves 32. The inserts 30 are shiftable in the
axial direction of the chamber rotors 3 through the intermediary of
the bearings 35.
In the cylindrical surfaces of the three-chamber rotors 3, there
are provided, besides the combustion chambers 25 also the oblong
grooves of the labyrinth seal 36. In the crankcase 1 between the
three-chamber rotors 3 there are provided suitable passages 37 and
38 connecting the cylindrical seats 7 of the three-chamber rotors 3
to the cylindrical seat 6 of the four-piston rotor 2. These
passages are designed for equalizing the pressures between the
cooperative working spaces 39 and combustion chambers 25.
In the crankcase 1 there are also provided four passages 40 for
carrying the residual combustion gases and the scavenging air out
of the corresponding combustion chambers 25. In the circumferential
part of the crankcase 1 there are also located four fuel injectors
41, and from the central inlet 16 in the front part of the said
crankcase there extends the ignition control device 42. This device
is equipped with a commutator 43 connected by means of a jack shaft
44 to the four-piston rotor 2, the casing 45 of the commutator
together with carbon brushes adapted to be set in a convenient
angular position.
The gears 5 of four three-chamber rotors 3 are rotatably mounted on
pins 27 and are pressed down by nuts 47 against the frontal
surfaces of the straps 48 which are mounted on the key 49. These
gears are angularly locked in relation to the straps by means of
set screws 50. The crackcase 1 of the engine, which is formed by a
single piece, is cooled by a fluid and shaped so that the
cylindrical seats 7 under the three-chamber chamber rotors 3 are
made with a constant diameter, as port holes in this crankcase and
in the ring-shaped insert 24 which closes the cylindrical seat 6
containing the four-piston rotor 2. The space 51 of the crankcase 1
including the gear 4 and four gears 5 is closed by means of a
frontal cover 52 in which the bearings 13 and seal 53 are arranged.
In this space there may also be the gear 55 with internal
indentation, coupled simultaneously with all gears 5 of the
three-chamber rotors 3 and mounted on the transmission shaft 56.
The latter is rotationally mounted on the shaft 57 of the
four-piston rotor 2 by means of bearings 58 and is sealed in
relation to the shaft 56 with the aid of seal 59.
In the frontal cover 52 there are provided the outlets of the
drives of such devices as: starter, injection device, oil pump,
water pump, fan or possibly also the ignition device. The fittings
of the engine are driven by a gear 60 made in conjunction with the
transmission shaft of the engine and gears 61.
The construction of other embodiments of the rotary internal
combustion engine, FIGS. 5 - 10, is similar to that described
above. Differences in the construction relate only to the number of
pistons 8 and 9 of the chamber rotor 2, to the number of chamber
rotor 3 and combustion chambers 25 with which the rotors are
equipped, to the ratio of the diameters of the chamber rotors 3 and
of the piston rotor 2, to the size of the suction passages 15
exhaust passages 17, and to the number of fuel injectors 41, and to
the number of glow or spark plugs 19 etc.
The construction of the engine with sliding leak seals, FIGS. 11 -
13, does not require any detail description. Radial seals for the
pistons 8 and 9, or only for the pistons 9, are composed of one,
two or more flat inserts 62 which are seated in grooves formed
along the tops of the pistons. The length of the inserts 62 is
greater than the width of the piston rotor 2.
The frontal seals of the piston rotor 2 are composed of sliding
rings 63, located in grooves made about the circumference of the
frontal cover plates 11 and 12 of the rotor. The seals of the
cylindrical surfaces of the rotors are formed by flat packing
pieces 64 which are seated in grooves formed along the generating
lines of the cylindrical surface of the piston rotor 2. The length
of the packing pieces 64 is greater than the width of the piston
rotor 2, and the ends of the packing pieces are seated in openings
made in the frontal cover plates 10 and 11 of the rotor 2.
The seals of the pistons 8 and 9, particularly those of pistons 9
with the edges or surfaces of chambers 25, referring to FIGS. 4 and
13 of the drawings, include yawing inserts 65 located within each
combustion chamber 25. The yawing inserts 65 each include
projections or lug portions, as shown in FIG. 13, adapted to extend
into and be fastened with a plurality of flat cavities or recesses
68. The yawing inserts are designed in a manner whereby the
centrifugal force generated upon rotation of chamber rotors 3
deflects their edges cooperating with the pistons 8 and 9 outwards
from the pistons, while a suitably high pressure in the combustion
chambers 25 causes the yawing inserts 65 to be pressed towards the
pistons 8 and 9.
Similarly, the frontal seals of the chamber rotors 3 are formed by
elastic circumferential radial seals 66 which have projections
adapted to be positioned in a plurality of recesses or flat
cavities 67 formed in the frontal srufaces of the chamber rotors 3,
and seated on their pins 26 and 27.
In the chamber rotors 3, and possibly in the piston rotor 2 there
may additionally be provided passages 69 which are designed for
cooling of the rotors by means of oil supplied under suitable
pressure.
The performance of the rotary internal combustion engine results
from the description of the embodiments stated by way of example.
In all embodiments, the turn of the piston rotor 2 brings about
that all working spaces 39 of the engine from the rear side of the
pistons 8 and 9 become larger, while the spaces from the front side
of said pistons become smaller. Due to this fact, through the
central inlet 16, air is sucked in which when flowing then through
the suction passages 15 will be slightly compressed and forced into
the working spaces situated on the rear side of the suction-exhaust
pistons 8. At the same time, the front side of the pistons 8 pushes
out the combustion gases which have earlier been expanded by the
power-compression pistons 9. These combustion gases escape through
the passages 17 in the frontal cover plate 10 of the piston rotor 2
into the annular collector 18 from which they pass through the
passages 70 outwardly to the atmosphere.
The air sucked into the working spaces is then compressed by the
power-compression pistons 9. Towards the end of the compression,
before the pistons 9 will plunge into the corresponding combustion
chambers 25 of the chamber rotors 3, the fuel is injected by the
injectors 41. Then, when the pistons 9 are entirely plunged into
the combustion chambers 25, ignition takes place due to the glow or
spark plugs 19 seated in the pistons 9. The high pressure of the
combustion gases acting on the rear side of each of the pistons 9
forces the piston rotor to turn, whereby the working spaces on the
rear side of the pistons 9 are increased and the combustion gases
expand. At the same time, the front side of these power-compression
pistons 9 are compressing the air earlier sucked-in by the
suction-exhaust pistons 8. All working cycles occur in the engine
simultaneously and also in all working spaces 39. The action of the
engine is thus extremely harmonized. In all working spaces 39 the
suction-exhaust pistons 8 suck the air by their rear side, and
simultaneously, they push out by their front side the earlier
expanded combustion gases, while the power compression pistons 9
take over by their rear side the reaction of the combustion gases
and simultaneously they are compressing by their front side the
earlier sucked air. The suction, compression, expansion and
exhaustion process occurs continuously and lasts for one-fourth of
a turn of the piston rotor 2.
The working spaces located on both sides of each piston 8 and 9 are
separated at every moment by the labyrinth seal 14 of the external
side of the piston, which seal is sliding along the inner surface
of the seat 6 of the piston rotor 2, or by one of the generating
lines of the combustion chamber 25 of the chamber rotors 3, which
generating line is sliding along the back or front surface of the
pistons 8 and 9.
The engine acts as a four-stroke one. To two turns of a four-piston
rotor, 16 full four-stroke cycles accrue, whereby the action of
this engine can be compared -- as far as the working cycle
frequency is concerned -- with the action of a 16-cylinder-four
stroke engine. The pulsation of the torque is comparable with that
of an eight-cylinder four-stroke engine. During the two turns of a
four-piston rotor there occurs a quadruple utilization of the
working volume of the engine, whereby it is comparable -- as far as
the working volume is concerned -- with a four-stroke piston engine
having a four times greater swept volume. The action of less
essential elements of the engine results directly from the drawings
and description of the construction.
The action of an engine having a two-piston rotor 2 and one
single-chambered rotor 3, FIG. 5, is similar to the action of a
one-cylinder four-stroke engine. The utilization frequency of the
working volume during one turn of a two-piston rotor 2 amounts to
one-half.
The action of an engine having a two-piston rotor 2 and two
single-chambered rotors 3, FIG. 6, corresponds to the action of a
two-cylinder four-stroke engine with cranks shifted every
180.degree.. Utilization frequency of the working volume: 1 pro one
turn of a two-piston rotor 2.
The action of an engine having a two-piston rotor 2 and three
single-chamber rotors 3, FIG. 7, corresponds to the action of a
three-cylinder four-stroke engine with cranks shifted every
120.degree. with the difference that the suction and exhaust cycle
is shifted by 60.degree. in relation to the work and compression
cycle. Utilization frequency of the working volume: three-seconds
pro one turn of a two-piston rotor 2.
The action of an engine having a four-piston rotor 2 and three
three-chambered rotors 3, FIG. 8, is similar -- as far as the
frequency of working cycles is concerned -- to the action of a
12-cylinder four stroke engine with cranks shifted every
60.degree.. Utilization frequency of the working volume:
three-seconds - pro one turn of a four-piston rotor 2.
The action of an engine having a four-piston rotor 2 and four
rotors 3, FIG. 9, is hereinbefore described: analogy to a sixteen
cylinder four-stroke engine with cranks shifted every 90.degree..
Utilization frequency of the working volume: 2 - pro one turn of a
four-piston rotor 2.
The action of an engine having a four-piston rotor 2 and five
three-chambered rotors 3, FIG. 10, corresponds to the action of a
20-cylinder four-stroke engine with cranks shifted every 36.degree.
with the difference that the suction and exhaust cycle is shifted
by 18.degree. in relation to the working and compression cycle.
Utilization frequency of the working volume: five-seconds - pro one
turn of the four-piston rotor 2.
The action of an engine provided with sliding seals, FIGS. 11 -13,
does not require a separate description.
The described embodiments, given by way of example, of the rotary
internal combustion engine according to the invention do not
comprise, of course, all the possible details and modifications of
the solution, which might still develop the essence of the
invention.
The rotary internal combustion engine according to the invention
may e.g., act as a self-driven rotary internal combustion
compressor. In such a case it is of advantage using to this purpose
e.g., an engine provided with a four-piston rotor and four
three-chambered rotors, two of which, facing each other, being
chambered rotors of the rotary compressor, while the other two --
chambered rotors of a rotary internal combustion engine.
The rotary internal combustion engine according to the invention
may also be used as a blower, compressor or pump, and also as a
hydraulic, steam or gas engine. In such cases the piston rotor of
the given device is equipped on the circumference solely with
pistons provided with inlet and outlet passages. The action of such
a device does not require a separate description. It is only to be
mentioned that the direction of rotation of the piston rotor for
the application of the device as a blower, compressor or pump, is
reverse to that when the device is used as a hydraulic, steam or
gas engine. The direction of flow of the working medium is for the
above-mentioned applications also reverse.
* * * * *