US3478955A - Variable area diffuser for compressor - Google Patents
Variable area diffuser for compressor Download PDFInfo
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- US3478955A US3478955A US712114A US3478955DA US3478955A US 3478955 A US3478955 A US 3478955A US 712114 A US712114 A US 712114A US 3478955D A US3478955D A US 3478955DA US 3478955 A US3478955 A US 3478955A
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- wall
- wall part
- compressor
- diffuser
- ring
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
- F01D17/143—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path the shiftable member being a wall, or part thereof of a radial diffuser
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/46—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/462—Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps
- F04D29/464—Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps adjusting flow cross-section, otherwise than by using adjustable stator blades
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/50—Inlet or outlet
- F05D2250/52—Outlet
Definitions
- a centrifugal compressor having a vaneless diffuser, one wall of which is defined by an annular member movable relative to the other wall to reduce or increase the width of the diffuser passage.
- the annular wall is mounted on four posts which extend through openings in the compressor casing and guide the reciprocating movement of the wall.
- the opposite ends of the posts are operatively coupled to helical cams in an annular control member mounted for rotation on the casing. Oscillation of the control member, by means of any suitable control mechanism, effects corresponding reciprocating movement of the movable annular wall.
- One approach for extending the range of volume flow at which a constant speed centrifugal compressor will operate at peak efiiciency and for lowering the design flow rate point at which surge will occur is to provide a diffuser having a variable flow area which can be adjusted in accordance with the demanded fiow rate through the compressor. It is known to provide vaneless diffusers wherein one wall of the diffuser passage is an annular member which may be moved relative to the other to vary the diffuser width.
- An object of this invention is to provide a centrifugal compressor having a vaneless diffuser with one variable wall defined by an annular member, and an improved mechanism for adjusting the position of the movable wall in accordance with desired conditions.
- a centrifugal compressor is provided with a vaneless annular diffuser passage or channel which communicates the compression chamber with the discharge chamber, one of the opposing walls of the diffuser chamber being defined by an annular wall 3,478,955 Patented Nov. 18, 1969 member movable relative to the opposing wall.
- the annular wall member is supported and guided for reciprocating movement in the compressor casing by parallel posts.
- the posts are coupled at their opposite ends to an annular control member, mounted for rotation on the compressor casing, having cams for effecting reciprocation of the wall member in response to oscillation of the control member.
- FIG. 1 is a sectional view of a centrifugal compressor in a plane through the impeller axis
- FIG. 2 is a fragmentary view of the compressor looking toward the inlet side thereof, along the line 2-2 of FIG. 1;
- FIG. 3 is a sectional view of a portion of the control assembly as viewed along the line 3-3 of FIG. 2.
- centrifugal compressor 10 having a casing defined by casing portions 10 and 11, secured together adjacent the outer peripheries by suitable bolts.
- the compressor casing defines a compression chamber between the inlet nozzle 12, in the casing portion 10, and the annular discharge chamber 13, adjacent to the outer periphery of the casing.
- An im peller 14 having blades 15 to mounted for rotation within the compression chamber, being secured to a suitable shaft 16 which extends through an opening 17 in the casing portion 11.
- the opening 17 may accommodate suitable seal or bearing housings for the impeller shaft.
- a vaneless diffuser Surrounding the impeller 14 is a vaneless diffuser which is an annular radially directed passage 20 communicating the outer periphery of the impeller 14 and the discharge chamber 13.
- a fixed wall of the diffuser passage is defined by the casing portion 11; and a movable wall 21 of the diffuser passage is defined by an annular member which is disposed in an annular groove 22 in the casing portion 10 concentric with the axis of rotation of the impeller.
- the movable wall member is generally rectangular in cross section, with the surface defining the diffuser wall surface being contoured for smooth air flow.
- the annular groove 22 is generally rectangular in cross section, and is dimensioned to receive the movable wall member with a relatively close fit.
- the movable wall 21 is supported and guided for reciprocating axial movement on four cylindrical posts 23 which extend through cylindrical bores 24 in the casing portion 10, these bores being parallel to each other and being circumferentially equally spaced concentric with the impeller axis.
- the posts 23 are dimensioned for a close sliding fit within the respective bores 24; and the posts are provided with threaded studs 25 and 26 projecting from opposite ends thereof.
- the posts 23 are rigidly secured to the movable wall 21 by the threaded engagement of the studs 25 in suitable threaded holes in the movable wall member.
- sealing devices are provided at the inner and outer peripheries of the wall member.
- An inner piston type seal ring 27 is disposed in a suitable annular groove in the inner cylindrical wall of the annular groove 22 to provide a seal between this cylindrical wall and the inner cylindrical wall of the wall member 21.
- An outer seal ring 28 is disposed in an annular groove in the outer cylindrical wall of the movable wall member 21 to provide a seal between this cylindrical wall and the outer cylindrical wall of the annular groove 22.
- vent this trapped pocket there is created a trapped pocket or space between the movable wall member and the bottom of the annular groove 22. It is desirable to vent this trapped pocket; and this is accomplished by providing one or more vent passages 29 through the movable wall member. Preferably, these vent passages open to the diffuser side of the wall member at a precise radial location, again because of the pressure gradient across the movable wall member.
- the radial location is selected so that the pressure extant in the trapped pocket and acting on the movable wall member corresponds to the average pressure acting on the diffuser side of the movable wall, that is that the forces acting on the opposite sides of the movable wall are balanced so as not to effect the positioning of the movable wall by the means to be described,
- O-ring seals are disposed in suitable annular grooves in the cylindrical walls of the posts 23 for sealing engagement with the walls of the bores 24.
- the movable diffuser wall 21 is mounted and guided for reciprocating axial movement relative to the fixed diffuser wall, is prevented from rotation relative to the casing, and is gastightly sealed in the casing.
- the reciprocating movement of the movable diffuser wall 21 is controlled by a control member 32, which is an annular ring member mounted for rotation on the exterior of the casing portion concentric with the impeller axis.
- the inlet nozzle 12 of the casing portion 10 defines an outer cylindrical surface within which is provided an external ball race 33; and the inner cylindrical surface of the control ring 32 is provided with a complementary ball race 34. With suitable balls 42, then, the control ring 32 is rotatably secured to the housing portion 10 and prevented from relative axial movement.
- the control rin 32 provides angularly equally spaced helical cams 35 wh ch are defined by inclined arcuate webs 36, the webs being divided radially by arcuate slots 37 concentric with the axis of rotation of the control ring.
- the helical cams 35 are so related to the posts 23 that the post studs 26 extend through the respective slots 37.
- the opposite faces of the webs 36 are engaged by bearing members 38 in the form of wedge-shaped washers having bosses 39 which extend into the slots 37, two of which are positioned over each of the respective threaded studs 26 and secured thereon by means of suitable nuts.
- These bearing members may be fabricated of a suitable bearing material such as oilite bronze, and function as followers of the helical cams.
- Each of the helical cams has the same relation to the plane of rotation of the control ring 32 so that as the control ring is oscillated the movable diffuser wall is positioned in selected parallel planes relative to the fixed diffuser wall.
- a control arm 40 is suitably secured to the control ring 32; and this may be actuated by any suitable control mechanism to oscillate the control ring in response to the operating conditions of the compressor, for example.
- the above described mechanism provides a very positive and precise control for varying the width of the diffuser passage 20.
- a centrifugal compressor comprising a casing defining a compression chamber and an annular discharge chamber; an impeller disposed in said compression chamber;
- annular diffuser passage communicating said compression chamber and said discharge chamber, defined by confronting walls at least one of which is movable relative to the other to enlarge or restrict said diffuser passage;
- said movable wall comprising a ring member disposed for axial movement relative to said casing; said ring member being supported on a plurality of posts which extend in a direction parallel to the axis of said impeller; means on said casing for" guiding the rectilinear movement of said posts parallel to the axis of said impeller;
- control member mounted for rotation on said casing in axial alignment with said movable wall and parallel thereto; said control member defining a plurality of cams, each of said cams being defined by opposed surfaces of said control member inclined along an are relative to the plane of rotation of said control member;
- a centrifugal compressor as set forth in claim 3 including sliding seal rings for the adjoining cylindrical surfaces of said movable wall and said annular groove.
- a centrifugal compressor as set forth in claim 3 including seal means between the inner walls of said annular groove and said movable wall member, and between the outer walls of said annular groove and said movable wall member for preventing gas flow radially through said annular groove.
- a centrifugal compressor as set forth in claim 5 including vent means through said movable wall for venting the annular space between said wall and the bottom of said annular groove; said vent means opening to the diffuser side of said movable wall at a predetermined radial position, such that the forces acting on the opposite sides thereof are controlled.
- each of said posts includes an axially extending stud extending through an arcuate slot in said control member; and a pair of bearing members supported on said stud for sliding engagement with the opposite faces of the associated cam web.
Abstract
1,231,152. Centrifugal compressors. DRESSER INDUSTRIES Inc. March 3, 1969 [March 11, 1968], No.11256/69. Heading F1C. In a centrifugal compressor comprising an annular diffuser passage 20, Fig. 1, between the impeller 14 and a discharge chamber 13, a wall part 21 is movable to vary the axial width of the diffuser passage. The wall part 21 is connected via four cylindrical posts 23 to a control ring 32 which can be partially rotated in either direction on ball bearings 42 to control the axial position of the wall part 21. Each post 23 is slidably connected to a cam in the form of a helical web 36 extending circumferentially around parts of the ring 32 and having an arcuate slot 37 which receives a stud 26 carrying a pair of washer-like bearing members 38, e.g. of bronze, having bosses (39), Fig.3 (not shown), extending into the slot. The ring 32 is moved by an arm 40, e.g. in accordance with a compressor operating condition. Gas circulation around the back of the wall part 21 is prevented by seal rings 27, 28. Pressure balancing passages 29 are provided through the wall part 21.
Description
Nov. 18, 1969 F. K. KUNDERMAN VARIABLE AREA DIFFUSER FOR COMPRESSOR 2 Sheets-Sheet 1 Filed March 11, 1968 IIHIIH fir:.-..i
Nov. 18, 1969 F. K. KUNDERMAN 3,478,955
VARIABLE AREA DIFFUSER FOR COMPRESSOR Filed March 11, 1968 2 Sheets-Sheet ILL/ I W56 56 INVENTOR. FEM K Xu/wE/eM/m y z w United States Patent O US. Cl. 230-114 9 Claims ABSTRACT OF THE DISCLOSURE A centrifugal compressor having a vaneless diffuser, one wall of which is defined by an annular member movable relative to the other wall to reduce or increase the width of the diffuser passage. The annular wall is mounted on four posts which extend through openings in the compressor casing and guide the reciprocating movement of the wall. The opposite ends of the posts are operatively coupled to helical cams in an annular control member mounted for rotation on the casing. Oscillation of the control member, by means of any suitable control mechanism, effects corresponding reciprocating movement of the movable annular wall.
Background of the invention In the design of compressors or compressor systems for supplying plant air, that is compressed air for the operation of air-powered tools for example, provision must be made for fluctuating demands which is characteristic of this type of load; and it is a characteristic of constant speed centrifugal compressors that they operate at peak efficiency for a relatively narrow range of volume flow. Surge or pulsation is an unstable operating condition of centrifugal compressors which occurs when the flow rate in the compressor has been reduced to some value below a designated operating point of the machine. Intensity of surge can be such that it produces violent shocks which may be damaging to the machine.
One approach for extending the range of volume flow at which a constant speed centrifugal compressor will operate at peak efiiciency and for lowering the design flow rate point at which surge will occur is to provide a diffuser having a variable flow area which can be adjusted in accordance with the demanded fiow rate through the compressor. It is known to provide vaneless diffusers wherein one wall of the diffuser passage is an annular member which may be moved relative to the other to vary the diffuser width.
Summary of the invention An object of this invention is to provide a centrifugal compressor having a vaneless diffuser with one variable wall defined by an annular member, and an improved mechanism for adjusting the position of the movable wall in accordance with desired conditions.
According to the invention, a centrifugal compressor is provided with a vaneless annular diffuser passage or channel which communicates the compression chamber with the discharge chamber, one of the opposing walls of the diffuser chamber being defined by an annular wall 3,478,955 Patented Nov. 18, 1969 member movable relative to the opposing wall. The annular wall member is supported and guided for reciprocating movement in the compressor casing by parallel posts. The posts are coupled at their opposite ends to an annular control member, mounted for rotation on the compressor casing, having cams for effecting reciprocation of the wall member in response to oscillation of the control member.
Brief description of the drawing The invention is embodied in apparatus illustrated in the accompanying drawings in which:
FIG. 1 is a sectional view of a centrifugal compressor in a plane through the impeller axis;
FIG. 2 is a fragmentary view of the compressor looking toward the inlet side thereof, along the line 2-2 of FIG. 1; and
FIG. 3 is a sectional view of a portion of the control assembly as viewed along the line 3-3 of FIG. 2.
Description of the preferred embodiment Referring to the drawings, there is shown a centrifugal compressor 10 having a casing defined by casing portions 10 and 11, secured together adjacent the outer peripheries by suitable bolts. The compressor casing defines a compression chamber between the inlet nozzle 12, in the casing portion 10, and the annular discharge chamber 13, adjacent to the outer periphery of the casing. An im peller 14 having blades 15 to mounted for rotation within the compression chamber, being secured to a suitable shaft 16 which extends through an opening 17 in the casing portion 11. The opening 17 may accommodate suitable seal or bearing housings for the impeller shaft.
Surrounding the impeller 14 is a vaneless diffuser which is an annular radially directed passage 20 communicating the outer periphery of the impeller 14 and the discharge chamber 13. A fixed wall of the diffuser passage is defined by the casing portion 11; and a movable wall 21 of the diffuser passage is defined by an annular member which is disposed in an annular groove 22 in the casing portion 10 concentric with the axis of rotation of the impeller. The movable wall member is generally rectangular in cross section, with the surface defining the diffuser wall surface being contoured for smooth air flow. correspondingly, the annular groove 22 is generally rectangular in cross section, and is dimensioned to receive the movable wall member with a relatively close fit.
The movable wall 21 is supported and guided for reciprocating axial movement on four cylindrical posts 23 which extend through cylindrical bores 24 in the casing portion 10, these bores being parallel to each other and being circumferentially equally spaced concentric with the impeller axis. The posts 23 are dimensioned for a close sliding fit within the respective bores 24; and the posts are provided with threaded studs 25 and 26 projecting from opposite ends thereof. The posts 23 are rigidly secured to the movable wall 21 by the threaded engagement of the studs 25 in suitable threaded holes in the movable wall member.
In order to prevent circulation of gas around the movable wall member 21, that is radially through the groove 22, which may occur because of the pressure gradient which exists across the diffuser wall during normal operation of the compressor, sealing devices are provided at the inner and outer peripheries of the wall member. An inner piston type seal ring 27 is disposed in a suitable annular groove in the inner cylindrical wall of the annular groove 22 to provide a seal between this cylindrical wall and the inner cylindrical wall of the wall member 21. An outer seal ring 28 is disposed in an annular groove in the outer cylindrical wall of the movable wall member 21 to provide a seal between this cylindrical wall and the outer cylindrical wall of the annular groove 22.
With these seals and the seals for the post 23 to be described, there is created a trapped pocket or space between the movable wall member and the bottom of the annular groove 22. It is desirable to vent this trapped pocket; and this is accomplished by providing one or more vent passages 29 through the movable wall member. Preferably, these vent passages open to the diffuser side of the wall member at a precise radial location, again because of the pressure gradient across the movable wall member. The radial location is selected so that the pressure extant in the trapped pocket and acting on the movable wall member corresponds to the average pressure acting on the diffuser side of the movable wall, that is that the forces acting on the opposite sides of the movable wall are balanced so as not to effect the positioning of the movable wall by the means to be described,
To prevent a leakage of gas from the trapped pocket to the exterior of the casing 12, O-ring seals are disposed in suitable annular grooves in the cylindrical walls of the posts 23 for sealing engagement with the walls of the bores 24.
From the foregoing it will be seen that the movable diffuser wall 21 is mounted and guided for reciprocating axial movement relative to the fixed diffuser wall, is prevented from rotation relative to the casing, and is gastightly sealed in the casing.
The reciprocating movement of the movable diffuser wall 21 is controlled by a control member 32, which is an annular ring member mounted for rotation on the exterior of the casing portion concentric with the impeller axis. The inlet nozzle 12 of the casing portion 10 defines an outer cylindrical surface within which is provided an external ball race 33; and the inner cylindrical surface of the control ring 32 is provided with a complementary ball race 34. With suitable balls 42, then, the control ring 32 is rotatably secured to the housing portion 10 and prevented from relative axial movement.
The control rin 32 provides angularly equally spaced helical cams 35 wh ch are defined by inclined arcuate webs 36, the webs being divided radially by arcuate slots 37 concentric with the axis of rotation of the control ring.
The helical cams 35 are so related to the posts 23 that the post studs 26 extend through the respective slots 37. The opposite faces of the webs 36 are engaged by bearing members 38 in the form of wedge-shaped washers having bosses 39 which extend into the slots 37, two of which are positioned over each of the respective threaded studs 26 and secured thereon by means of suitable nuts. These bearing members may be fabricated of a suitable bearing material such as oilite bronze, and function as followers of the helical cams. Each of the helical cams has the same relation to the plane of rotation of the control ring 32 so that as the control ring is oscillated the movable diffuser wall is positioned in selected parallel planes relative to the fixed diffuser wall.
A control arm 40 is suitably secured to the control ring 32; and this may be actuated by any suitable control mechanism to oscillate the control ring in response to the operating conditions of the compressor, for example. The above described mechanism provides a very positive and precise control for varying the width of the diffuser passage 20.
4 The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:
1. A centrifugal compressor comprising a casing defining a compression chamber and an annular discharge chamber; an impeller disposed in said compression chamber;
an annular diffuser passage, communicating said compression chamber and said discharge chamber, defined by confronting walls at least one of which is movable relative to the other to enlarge or restrict said diffuser passage; said movable wall comprising a ring member disposed for axial movement relative to said casing; said ring member being supported on a plurality of posts which extend in a direction parallel to the axis of said impeller; means on said casing for" guiding the rectilinear movement of said posts parallel to the axis of said impeller;
an annular control member mounted for rotation on said casing in axial alignment with said movable wall and parallel thereto; said control member defining a plurality of cams, each of said cams being defined by opposed surfaces of said control member inclined along an are relative to the plane of rotation of said control member;
and means coupling said posts to respective control member cams whereby oscillation of said control member relative to said casing effects rectilinear movement of said posts relative to said casing and corresponding rectilinear movement of said movable diffuser wall.
2. A centrifugal compressor as set forth in claim 1 wherein said casing is provided with a plurality of bores extending parallel to the axis of rotation of the impeller; said bores being dimensioned to receive said posts with a sliding fit for supporting and guiding said movable wall.
3. A centrifugal compressor as set forth in claim 1 wherein the casing portion, opposite from the portion defining the fixed diffuser wall, is provided with an annular groove having a generally rectangular cross section; and wherein said movable diffuser wall is generally rectangular in cross section and dimensioned to be received within said annular groove with a relatively close fit; and said movable wall being fully received within said groove, in the maximum flow position of said movable wall, whereby the movable wall and the adjacent casing portion define a smooth diffuser wall surface.
4. A centrifugal compressor as set forth in claim 3 including sliding seal rings for the adjoining cylindrical surfaces of said movable wall and said annular groove.
5. A centrifugal compressor as set forth in claim 3 including seal means between the inner walls of said annular groove and said movable wall member, and between the outer walls of said annular groove and said movable wall member for preventing gas flow radially through said annular groove.
6. A centrifugal compressor as set forth in claim 5 including vent means through said movable wall for venting the annular space between said wall and the bottom of said annular groove; said vent means opening to the diffuser side of said movable wall at a predetermined radial position, such that the forces acting on the opposite sides thereof are controlled.
7. A centrifugal compressor as, set forth in claim 1 wherein said control member is mounted on said housing by means of complementary ballraces formed respectively in a peripheral wall of an axially projecting portion of said casing and an inner wall of said annular control member; and said members being coupled together by means of balls disposed within said ballraces.
8. A centrifugal compressor as set forth in claim 1 wherein said cams are helical cams defined by angularly spaced inclined web portions of said control memher, said web portions having a uniform thickness and being radially divided by arcuate slots concentric with the axis of rotation;
and wherein said posts extend through said arcuate slots and are provided with follower means engaging both of the opposing surfaces of said web portions.
9. A centrifugal compressor as set forth in claim 8 wherein each of said posts includes an axially extending stud extending through an arcuate slot in said control member; and a pair of bearing members supported on said stud for sliding engagement with the opposite faces of the associated cam web.
Huitson. Jassniker. Dreesen et al. Beran et a1. Jassniker.
1O LEONARD H. GERIN, Primary Examiner U.S. Cl. X.R.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US71211468A | 1968-03-11 | 1968-03-11 |
Publications (1)
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US3478955A true US3478955A (en) | 1969-11-18 |
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US712114A Expired - Lifetime US3478955A (en) | 1968-03-11 | 1968-03-11 | Variable area diffuser for compressor |
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US (1) | US3478955A (en) |
DE (1) | DE1913048A1 (en) |
FR (1) | FR2003644A1 (en) |
GB (1) | GB1231152A (en) |
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CN105473956B (en) | 2013-08-27 | 2018-07-31 | 丹佛斯公司 | A kind of compressor including stream controller and electromagnetic actuators |
DE102015202375A1 (en) * | 2015-02-11 | 2016-08-11 | Robert Bosch Gmbh | Radial compressor, exhaust gas turbocharger and corresponding method for operating a centrifugal compressor |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2285976A (en) * | 1940-01-15 | 1942-06-09 | Gen Electric | Centrifugal compressor |
US3032259A (en) * | 1957-12-23 | 1962-05-01 | Sulzer Ag | Turbocompressor having a radial diffuser |
US3150650A (en) * | 1961-09-29 | 1964-09-29 | Caterpillar Tractor Co | Variable area diffuser for compressor |
US3349997A (en) * | 1965-05-05 | 1967-10-31 | Ckd Praha | Adjustable diffuser blades |
US3365120A (en) * | 1964-05-11 | 1968-01-23 | Sulzer Ag | Turbine radial diffuser |
-
1968
- 1968-03-11 US US712114A patent/US3478955A/en not_active Expired - Lifetime
-
1969
- 1969-03-03 GB GB1231152D patent/GB1231152A/en not_active Expired
- 1969-03-10 FR FR6906673A patent/FR2003644A1/fr not_active Withdrawn
- 1969-03-11 DE DE19691913048 patent/DE1913048A1/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2285976A (en) * | 1940-01-15 | 1942-06-09 | Gen Electric | Centrifugal compressor |
US3032259A (en) * | 1957-12-23 | 1962-05-01 | Sulzer Ag | Turbocompressor having a radial diffuser |
US3150650A (en) * | 1961-09-29 | 1964-09-29 | Caterpillar Tractor Co | Variable area diffuser for compressor |
US3365120A (en) * | 1964-05-11 | 1968-01-23 | Sulzer Ag | Turbine radial diffuser |
US3349997A (en) * | 1965-05-05 | 1967-10-31 | Ckd Praha | Adjustable diffuser blades |
Cited By (59)
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FR2162466A1 (en) * | 1971-12-06 | 1973-07-20 | H R Electronics Co | |
US3941498A (en) * | 1974-04-08 | 1976-03-02 | Chandler Evans Inc. | Variable geometry collector for centrifugal pump |
US4544325A (en) * | 1980-10-22 | 1985-10-01 | Teledyne Industries, Inc. | Variable geometry device for turbine compressor outlet |
US4403914A (en) * | 1981-07-13 | 1983-09-13 | Teledyne Industries, Inc. | Variable geometry device for turbomachinery |
US4499731A (en) * | 1981-12-09 | 1985-02-19 | Bbc Brown, Boveri & Company, Limited | Controllable exhaust gas turbocharger |
US4557665A (en) * | 1982-05-28 | 1985-12-10 | Helset Engineering Company Limited | Variable inlet area turbine |
US4538410A (en) * | 1982-07-07 | 1985-09-03 | A/S Kongsberg Vapenfabrikk | Compressor diffuser non-return valve and method for starting gas turbine engines |
US4844690A (en) * | 1985-01-24 | 1989-07-04 | Carrier Corporation | Diffuser vane seal for a centrifugal compressor |
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US20050262841A1 (en) * | 2002-11-19 | 2005-12-01 | John Parker | Variable geometry turbine |
US20040128997A1 (en) * | 2002-11-19 | 2004-07-08 | John Parker | Variable geometry turbine |
US7658068B2 (en) | 2002-11-19 | 2010-02-09 | Cummins Inc. | Method of controlling the exhaust gas temperature for after-treatment systems on a diesel engine using a variable geometry turbine |
US7475540B2 (en) | 2002-11-19 | 2009-01-13 | Holset Engineering Co., Limited | Variable geometry turbine |
US6931849B2 (en) * | 2002-11-19 | 2005-08-23 | Holset Engineering Company, Limited | Variable geometry turbine |
US6872050B2 (en) | 2002-12-06 | 2005-03-29 | York International Corporation | Variable geometry diffuser mechanism |
JP2006509155A (en) * | 2002-12-06 | 2006-03-16 | ヨーク・インターナショナル・コーポレーション | Diffuser system for variable capacity centrifugal compressors |
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US20040216466A1 (en) * | 2003-03-12 | 2004-11-04 | Werner Bosen | Expansion turbine stage |
US20080089782A1 (en) * | 2005-06-07 | 2008-04-17 | Parker John F | Variable geometry turbine |
US8172516B2 (en) * | 2005-06-07 | 2012-05-08 | Cummins Turbo Technologies Limited | Variable geometry turbine |
US20080031732A1 (en) * | 2005-11-30 | 2008-02-07 | Dresser-Rand Company | Closure device for a turbomachine casing |
US7850427B2 (en) * | 2005-11-30 | 2010-12-14 | Dresser-Rand Company | Closure device for a turbomachine casing |
US20070196206A1 (en) * | 2006-02-17 | 2007-08-23 | Honeywell International, Inc. | Pressure load compressor diffuser |
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US7871243B2 (en) * | 2007-06-05 | 2011-01-18 | Honeywell International Inc. | Augmented vaneless diffuser containment |
US20080304953A1 (en) * | 2007-06-05 | 2008-12-11 | Chen Robert P | Augmented vaneless diffuser containment |
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Also Published As
Publication number | Publication date |
---|---|
GB1231152A (en) | 1971-05-12 |
FR2003644A1 (en) | 1969-11-14 |
DE1913048A1 (en) | 1970-02-26 |
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