U.S. patent number 3,644,054 [Application Number 05/044,034] was granted by the patent office on 1972-02-22 for compressor base and intercoolers.
This patent grant is currently assigned to Carrier Corporation. Invention is credited to Karol Pilarczyk.
United States Patent |
3,644,054 |
Pilarczyk |
February 22, 1972 |
COMPRESSOR BASE AND INTERCOOLERS
Abstract
A base containing a pair of identical heat exchangers, demisters
and separators has rigidly mounted thereon a cast multistage
compressor casing provided with integral air inlet and discharge
passages in direct communication with corresponding passages in the
top wall of the base for providing the intercooling between stages.
Fluid passes through the intercoolers by moving downwardly through
the heat exchangers, downwardly through restricted nozzles and
reversely upwardly for separating condensation, upwardly through
the demisters and through central partition walls forming central
manifold chambers. The liquid connections for the intercoolers may
be uncoupled at one end for sliding the intercoolers off shelves
from the opposite end. A telescopic resilient coupling between the
casing inlet to the rotor and an inlet housing rigidly coupled to a
fluid supply will prevent transmission of forces therebetween. The
base further mounts the drive structure for the compressor and
carries an oil sump below the drive structure.
Inventors: |
Pilarczyk; Karol (Loudonville,
NY) |
Assignee: |
Carrier Corporation (Syracuse,
NY)
|
Family
ID: |
21930172 |
Appl.
No.: |
05/044,034 |
Filed: |
June 8, 1970 |
Current U.S.
Class: |
415/179; 165/47;
417/375; 417/243 |
Current CPC
Class: |
F04D
29/582 (20130101); F04D 29/5826 (20130101) |
Current International
Class: |
F04D
29/58 (20060101); F04c 029/58 (); F24h
009/08 () |
Field of
Search: |
;415/179,201,199,219
;417/375 ;165/47,76 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Raduazo; Henry F.
Claims
What is claimed is:
1. A multistage compressor, comprising: a base; a compressor rotor
having at least two impellers; casing means rigidly secured on said
base and rotatably supporting said compressor rotor for providing
at least two compression stages, said casing means having an
integral fluid outlet for the first stage and an integral fluid
inlet for the second stage; said base including an upper wall,
sidewalls, and a lower wall forming therebetween a substantially
closed intercooler chamber; and said upper wall having an integral
chamber inlet in fluid communication directly with said first-stage
fluid outlet, and an integral chamber outlet in direct fluid
communication with said second-stage fluid inlet.
2. The compressor of claim 1, wherein said casing means includes a
one-piece cast casing having an axially through cylinder bore
receiving concentrically therein said compressor rotor and a
downwardly facing horizontally planar surface; said casing means
inlets and outlets extending between said bore and said planar
surface, with their respective ends opening upwardly and
downwardly; said base upper wall having an upwardly facing
substantially horizontally planar surface engaging the entire
casing planar surface.
3. The compressor of claim 1, including liquid gas heat exchanger
means mounted in said intercooler chamber in fluid communication
between said chamber fluid inlet and said chamber fluid outlet; and
chamber partition means forming a constricted passage for the fluid
downstream of said heat exchanger means for passing the fluid
downwardly and sharply reversing the fluid upwardly to discharge
condensed liquid therefrom.
4. The compressor of claim 3, including demister means mounted in
said intercooler chamber downstream of said separator.
5. The compressor of claim 1, wherein said compressor rotor has
three impellers and said casing means provides three compression
stages; said casing means further has an integral fluid outlet for
the second stage and an integral fluid inlet for the third stage;
said upper wall further has an integral chamber fluid inlet in
direct fluid communication with said third-stage fluid inlet; and
including two separate heat exchangers in said intercooler chamber,
means mounting one of said heat exchangers fluid interposed between
said first-stage fluid outlet and said second-stage fluid inlet,
and the other of said heat exchangers fluid interposed between said
second-stage fluid outlet and said third-stage fluid inlet.
6. The compressor of claim 5, including partition wall means in
said base forming three aligned manifold subchambers, with the two
outside manifold subchambers being in fluid communication with said
second-stage fluid inlet and the middle manifold subchamber being
in fluid communication with said third-stage inlet.
7. The compressor of claim 5, including generally vertical
partition wall means in said base forming at least two manifolds
extending vertically for substantially the entire height of said
intercooler chamber and being respectively in direct fluid
communication through said upper wall with said second-stage fluid
inlet and said third-stage fluid inlet.
8. The compressor of claim 7, including said partition wall means
further dividing said intercooler chamber into a separate first
intercooler subchamber on one side of said manifolds and a separate
second intercooler subchamber on the other side of said manifolds,
with said first-stage fluid outlet discharging downwardly directly
into said first intercooler subchamber and said second-stage fluid
outlet discharging downwardly directly into said second intercooler
subchamber; and passage means interconnecting respective
intercooler subchambers and manifolds.
9. The compressor of claim 8, wherein said heat exchangers are
identical; said base having shelf means mounting each of said heat
exchangers for relative horizontal sliding in the same direction
for removal and assembly; said base having one sidewall being
perpendicular to said direction and being removable to provide
access for assembly and withdrawal of said heat exchangers; rigid
inlet and outlet liquid conduits on the other side of said heat
exchangers opposite from said one sidewall having releasable
coupling means fluid connecting them respectively to said heat
exchangers; and said base having removable wall means on said other
side for providing access to said releasable couplings.
10. The compressor of claim 9, including demister means operatively
mounted in each of said intercooler subchambers respectively
downstream from said heat exchangers; and fluid guide means for
respectively directing fluid from said heat exchangers downwardly
and then reversely upwardly through said demister means.
11. The compressor of claim 10, wherein said fluid guide means each
have a narrow vertically extending nozzle passage for accelerating
and directing the fluid downwardly closely adjacent the bottom of
each intercooler subchamber and then upwardly through said demister
means to constitute condensate separators.
12. The compressor of claim 10, wherein each of said heat
exchangers is mounted above the corresponding interconnecting
passage means and each of said demister means is mounted below the
corresponding interconnecting passage means.
Description
BACKGROUND OF THE INVENTION
Intercooler structure has heretofore been one of the largest
components of a multistage compressor, which not only increases the
cost of the compressor but of more importance increases the space
required for mounting the compressor unit. The intercooler
structure of the patent to Schierl, U.S. Pat. No. 3,001,692, issued
Sept. 26, 1961, overcomes some of the problems in the prior art but
still employs a rather large base in comparison to the size of the
heat exchangers used and employs a considerable amount of piping
between stages and waste space within the base.
The air connections for the Olmstead et al. patent, U.S. Pat. No.
2,849,960, issued Sept. 2, 1958, have advantages with respect to
force transmittal, but present a rather complicated structure that
must be assembled at the use location and does not provide any
rigid support for the adjacent piping extending away from the
pump.
CROSS-REFERENCE TO RELATED APPLICATIONS
The features of the invention of this application may be used in
combination with the features of the inventions in applicant's
following related applications of the same filing date and assignee
as the present application, the disclosures of which are
incorporated herein in their entirety by reference: "Compressor
Barrel Assembly," Ser. No 44,446; "Compressor Power Recovery," Ser.
No. 44,463; "Interchangeable Compressor Drive," Ser. No. 44,403;
"Variable Capacity Compressor," Ser. No. 44,263.
BRIEF DESCRIPTION OF THE DRAWING
Further objects, features and advantages in the present invention
will become more clear from the following detailed description of a
preferred embodiment as shown in the attached drawing, in
which:
FIG. 1 is a perspective view of a multistage centrifugal
compressor;
FIG. 2 is a schematic flow diagram showing the relationship of the
compressor stages and intercoolers;
FIG. 3 is a partial cross section side elevation view, with the
cross sections being taken in a vertical plane passing through the
axes of rotation of the compressor rotor and drive assembly;
FIG. 4 is a partial cross section and exploded view of a portion of
the structure as shown in FIG. 1; and
FIG. 5 is a cross-sectional view taken on line 5--5 in FIG. 3
showing the air discharge manifold of the intercoolers.
DETAILED DESCRIPTION OF THE DRAWING
The base 1 as shown in FIG. 1 has mounted rigidly thereon an fluid
inlet housing 2 by means of a plurality of bolts (not shown)
passing through bolt holes 3, a one-piece cast compressor casing 4
by means of a plurality of bolts 5, a gear housing 6 by means of a
plurality of bolts 7, an electric drive motor 8 by means of
resilient pads 9, and a control panel 10 by any conventional
means.
The inlet housing 2 is provided with an annular flange 11 provided
with a plurality of peripherally arranged holes 12 for rigidly
securing thereto an inlet fluid pipe when assembling the compressor
at the use location. An upwardly extending integral mounting arm 13
is provided on the flange 11 for mounting thereto by means of
bolts, or the like, a support bracket 14 that carries the diaphragm
control mechanism 15 of an inlet valve member 16, with the
interposition of a suitable linkage 17. The inlet valve mechanism
15, 16, 17 is conventional per se for throttling the inlet fluid on
partial load and for density control in a known manner. The
diaphragm control is provided with a pressure feedback tube 18 for
this purpose. The multistage impeller rotor and fluid guide
structure is contained within the one-piece cast casing 4, which
casing is provided with an axially through cylindrical bore 19, a
downwardly facing planar surface 20 engaging the correspondingly
planar upper surface of the top wall 21 of the base 1, and with an
upwardly extending boss 22 that is bored for fluid communication
with the outlet of the last compressor stage. As will be described
later, a resilient coupling for vibration and load isolation is
provided between the fluid inlet housing 2 and the compressor
casing 4.
The drive assembly for the compressor may be of any type, but
preferably employs the electric motor 8 that drives a gearset
within the gear housing 6. Particularly, the drive structure may be
of the type mentioned in one of applicant's previously identified
applications wherein the structure is set forth in detail.
Welded steel fabrication is used for constructing the base 1,
preferably from stock sheet and plate steel. The front wall 23 is
provided with oppositely opening doors 24, which lead to a control
and auxiliary component compartment having therein the inlet and
outlet water couplings for the intercoolers. The supply 25 and
outlet 26 water pipes for the intercoolers extend permanently
through the sidewall 27 and are provided at their outer ends with
suitable couplings to be connected during installation at the site
of use.
The basic fluid flow for the compressor is shown in FIG. 2 wherein
the impeller of a first stage 28 passes fluid downwardly through a
first intercooler 29. Thereafter, the fluid passes through the
second stage impeller 30, which directs it downwardly through the
second intercooler 31. Finally, the fluid passes upwardly and
through the third stage impeller 32 for discharge to the point of
use. The impellers 28, 32, 30 form an integral rotor drivingly
connected with a spur helical pinion gear 33 that is driven by
means of a drive helical gear 34 mounted on a parallel axis gear
drive input shaft 35.
The inlet connection is shown in more detail in FIG. 3. A
cylindrical mounting portion 36 of the inlet housing 2 is
telescopically received over a cylindrical mounting portion 37 with
the interposition of an O-ring 38. From the drawing, it is seen
that the adjacent cylindrical surfaces of mounting portions 36, 37
are radially spaced from each other so that the O-ring 38 provides
the only engaging connection between the inlet housing 2 and the
compressor casing 4, while sealing these structures. Thus, the
inlet housing 2 is independently supported on the base 1 to prevent
transmittal of inlet housing vibration, canting, axial movement,
radial movement and rotational movement to the compressor casing 4.
Thus, the complete compressor may be supplied to a user and the
user may rigidly couple his inlet fluid pipes directly to the inlet
housing 2, without fear that forces relating to the coupling and
inlet pipes will be transmitted to the compressor casing. Further,
the stresses due to tightening of the connections between the inlet
casing and fluid supply pipes will not be transferred to the
compressor casing.
The removable barrel structure of the compressor includes separate
shrouds, diffusers, and annular fluid guide elements all received
in a stacked relationship within the cylindrical bore 19 of the
one-piece compressor casing 4. The compressor casing 4 is provided
with integrally cast passages extending between the barrel assembly
and the base 1. Particularly, a first passage 39 extends between
the bore 19 and the planar surface 20 to conduct fluid from the
discharge of the first stage, second passage 40 extends from the
bore 19 to the planar surface 20 to conduct the fluid into the
third-stage inlet, third passage 41 extends from the bore 19 to the
planar surface 20 to conduct fluid discharged from the second stage
and fourth passage 42 extends from the bore 19 to the planar
surface 20 to conduct fluid to the inlet of the second stage. The
base 1 is provided with a top wall 21, opposed sidewalls 27 and 43,
opposed front and back walls 23 and 44, and a bottom wall 45, which
together form a substantially closed main chamber containing the
intercooler structure. The top wall 21 is provided with a plurality
of passages, also shown in FIG. 4, extending between the passages
39-42 and the intercooler main chamber. Particularly, the top plate
21 is provided with holes 46 that align with passages 39, holes 47
that align with passage 42, hole 48 that aligns with passage 40 and
hole 49 that aligns with passage 41.
Two parallel partition walls 50, which are parallel to the walls
27, 43, extend completely from the top wall 21 to the bottom wall
45 and extend from the front wall 23 to the backwall 44 to form a
central manifold chamber 51. Additional partition walls 52
subdivide the manifold chamber into three aligned subchambers, with
the outside subchambers 53 being in fluid communication between the
holes 47 in the top wall and correspondingly aligned holes in the
left-hand partition wall 50, and with the inside subchamber 54
being in fluid communication between the hole 48 and a hole 55 in
the right-hand partition wall 50 as shown in FIG. 3. In this
manner, the main intercooler chamber is further divided into a
first intercooler chamber 55 to the left of the partition walls 50
and a second intercooler chamber 56 to the right of the partition
walls 50, as seen in FIG. 3. Identical and interchangeable parallel
tube fluid heat exchangers 57 are mounted on shelves 58 within
their respective intercooler chambers 55, 56 so that they may be
horizontally slid into and out of the base 1 after the releasably
secure back wall 44 is removed. For this purpose, the pipes 25, 26
are provided with releasable couplings 59 for uncoupling the heat
exchangers, without affecting the location of the pipes 25, 26.
It is seen from FIG. 3, that fluid discharged respectively from the
first stage and the second stage will pass through passages 39, 41
and holes 46, 49 downwardly into intercooler chambers 55, 56 to
pass through their corresponding heat exchangers 57. Thereafter,
the thus cooled fluid will be directed by baffle plates 60 through
vertically extending restricted nozzle-type passages 61 where the
flow of fluid will approach sonic velocity. The high-speed fluid
then passes through a sharp acute angle and upwardly through
demisters 62. Thus, it is seen that the baffles 60 formed in the
nozzle-type passages 61 constitute separators that will take the
cooled fluid from the heat exchangers having condensed droplets
therein, accelerate this cooled fluid and substantially reverse the
flow of the accelerated cooled fluid to separate the condensate.
Further, moisture will be removed from this separated fluid by
means of demister 62. Thereafter, the relatively dry fluid will
pass through respective holes in the partition walls 50 so that the
fluid from the intercooler chamber 55 will pass into the
submanifold chambers 53 and fluid from the intercooler 56 will pass
into the submanifold chamber 54. It is noted that the left-hand
passage 61 is substantially larger than the right-hand passage 61
as shown in FIG. 3, which difference is proportional to the
difference in volume of fluid handled by the two intercoolers due
to compression. For this same reason, two submanifold chambers 53
are provided for returning fluid to the second stage, while only
one submanifold chamber is provided for returning fluid to the
third stage.
Beneath the drive assembly 8, 6, the base 1 is provided with an oil
sump 63, which is in direct communication with the interior of the
gear housing 6.
From the above, it is seen that the compressor base of the present
invention separately and rigidly mounts a rigid compressor casing
and a rigid fluid inlet casing, and provides a telescopic coupling
therebetween having only a flexible interengagement by means of the
O-ring 38. With this coupling, the user's rigid fluid inlet pipes
may be rigidly connected directly to the fluid inlet casing 2 for
support thereof, without fear that the stresses produced by the
rigid supply coupling will be transmitted to the compressor casing
4. Also, any vibrations, thermal expansion, settling, misalignment,
etc. associated with the user's fluid supply pipes will be
transmitted only to the heavy rigid base and not transmitted
directly to the compressor casing. Further, this O-ring seal 38 and
flexible coupling will accommodate misalignment and tolerances as
between the casings 2 and 4, as well as preventing force
transmittal therebetween because of the considerable radial spacing
between the telescoping cylindrical portions 36, 37. Further, the
inlet casing may be advantageously used for a conventional type of
inlet valve, without fear that forces associated with the inlet
valve will be transmitted to the compressor casing.
The compressor casing is of a one-piece cast construction with
integral fluid passages between stages communicating between each
stage and intercoolers within the base, respectively, so that no
bulky, costly and cumbersome external piping connections are
required. For this purpose, the base has a top compressor
supporting wall that is provided with integral passages aligned
respectively in fluid communication with the compressor casing
integral passages so that fluid is conducted from the first and
second stages downwardly into the intercooler chambers and upwardly
from the intercooler chambers into the second and third stages.
The base is further of a compact construction in that it requires
very little extra room over that of the plan view dimensions
associated with the compressor casing and inlet fluid casing, with
respect to its enclosure for housing intercoolers, centrifugal
separators, and demisters. The intercoolers are identical and the
demisters are identical to provide for interchangeability and
inexpensive manufacture. Also, the separators are formed by baffles
that are identical although assembled in mirror image fashion. The
fluid flows downwardly through the intercoolers through a
restricted passage formed by the separator baffles so that the
cooled fluid approaches or reaches sonic velocity before it is
sharply and reversely guided upwardly through the demisters, so
that during this reversal, droplets of condensate will be
discharged downwardly where they will be collected and removed if
desired. The fluid moving upwardly through demisters is further
directed upwardly through submanifold chambers located centrally
between the two intercooler chambers for discharge through the top
wall of the base. Construction of the base is rigid and relatively
inexpensive in that it is of welded steel fabrication employing
only planar sheets and plates, with the partition walls forming the
submanifold chambers considerably contributing to the rigidity of
the entire structure by providing cross bracing.
The portion of the base under the drive mechanism, particularly an
electric motor and gear train, is of relatively shallow
construction due to the greater height of these components and
forms a sump for the oil lubrication system. Preferably this sump
is in direct communication with the gear housing.
The intercoolers are mounted within their respective intercooler
chambers by means of shelves so that they may be slid horizontally
in one direction out of the base, after the removal of the adjacent
releasably mounted wall. The wall opposite from the releasably
mounted wall is provided with access means so that rigid cooling
liquid supply and exhaust pipes may be quickly coupled and
uncoupled from the intercoolers. In a like manner, the demisters
are mounted on respective shelves to be horizontally slid out of
their respective intercooler chambers in the same direction as the
heat exchangers, for purposes of repair, replacement or the
like.
While a preferred embodiment of the present invention has been
specifically described with respect to specific advantageous
features, it is to be realized that the invention, in its broader
aspects, includes further modifications, embodiments and
variations.
* * * * *