WO2006137863A2 - Variable area diffuser for a radial c0mpress0r - Google Patents

Variable area diffuser for a radial c0mpress0r Download PDF

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Publication number
WO2006137863A2
WO2006137863A2 PCT/US2005/032928 US2005032928W WO2006137863A2 WO 2006137863 A2 WO2006137863 A2 WO 2006137863A2 US 2005032928 W US2005032928 W US 2005032928W WO 2006137863 A2 WO2006137863 A2 WO 2006137863A2
Authority
WO
WIPO (PCT)
Prior art keywords
shroud
backing plate
vanes
variable area
vane
Prior art date
Application number
PCT/US2005/032928
Other languages
French (fr)
Other versions
WO2006137863A3 (en
Inventor
Christopher Mcauliffe
Craig Beers
Brent Merritt
Robert Telakowski
Original Assignee
Hamilton Sundstrand Corporation
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hamilton Sundstrand Corporation filed Critical Hamilton Sundstrand Corporation
Priority to EP05858134A priority Critical patent/EP1792054B1/en
Priority to DE602005021373T priority patent/DE602005021373D1/en
Priority to JP2007532457A priority patent/JP4708431B2/en
Publication of WO2006137863A2 publication Critical patent/WO2006137863A2/en
Publication of WO2006137863A3 publication Critical patent/WO2006137863A3/en

Links

Classifications

    • 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
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/165—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line
    • 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
    • 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

  • This application relates to a variable area diffuser.
  • this application relates to a variable area, vane-type-diffuser suitable for use in a compressed air system for an air conditioning pack.
  • Variable area diffusers utilize multiple vanes that are rotated between different angular positions to vary the throat size of the diffuser.
  • Variable area diffusers can be used in conjunction with, for example, superchargers to vary the flow through an air conditioning system of an aircraft at various altitudes.
  • the variable area diffuser may be subjected to very high stresses, for example, as the compressor is driven at high speed.
  • the diffuser structure must pass a containment test in which the compressor rotor is rotated at very high speeds until the rotor disintegrates.
  • the debris must stay within its housing so that the debris does not create a hazard to surrounding areas, components or personnel.
  • Another problem with the diffuser operation is that the structure adjacent to the vanes, such as a backing plate and/or shroud, deflects. It is desirable to maintain a clearance of only a few thousandths on either side of the vane throughout the operation of the diffuser. Deflection of the structure surrounding the vanes can create a binding condition compromising the operation of the diffuser
  • variable area diffuser with improved operation under applied loads and improved containment of debris in the event of rotor failure.
  • the present invention provides a compressed air unit that includes a housing having a shroud.
  • An electric motor driven compressor rotor is arranged in the housing and including rotor blades.
  • a variable area diffuser is arranged in the housing and is in fluid communication with the compressor.
  • the diffuser includes multiple vanes arranged circumferentially around the rotor. The vanes rotate to multiple positions about pivot pins to change the flow through the compressed air system.
  • a mounting plate is secured to the housing by a retainer and supports a backing plate. The vanes are arranged between the backing plate and the shroud.
  • the pivot pins are in a slip fit relationship with the backing plate, vanes and shroud and are threadingly received by bosses in the mounting plate. With the mounting plate and pivot pin arrangement of the present invention, the backing plate and shroud are better able to remain parallel with one another during loading
  • protrusions and/or fasteners extend from between the backing plate and shroud through apertures in the vanes to better contain the vanes in the event of a catastrophic failure.
  • Multiple protrusions and bolts are used to act as a barrier to debris, in the example shown. Accordingly, the invention provides an improved variable area diffuser with improved operation under deflection and improved containment of debris in the event of vane failure.
  • Figure 1 is a cross-sectional view of a compressed unit system having the inventive variable area diffuser.
  • Figure 2 is a partially broken view of the inventive diffuser, broken at several planes and viewed in the direction of the arrows 2-2 in Figure 3.
  • Figure 3 is an enlarged cross-sectional view of the inventive diffuser shown in Figure 1.
  • a compressed air unit 10 is shown in Figure 1.
  • the unit 10 includes a compressor rotor 12 driven by an electric motor 14. It should be understood, however, that the inventive diffuser may be used in other, non-electric motor applications.
  • the compressor rotor 12 and electric motor 14 are contained within the housing 16, which may be constructed from multiple housing portions secured to one another.
  • the housing 16 provides an inlet 18 for providing air to the compressor 12.
  • a motor rotor 20 is disposed within a motor stator 19 and is rotatable about an axis A.
  • the rotor 20 supports compressor rotor with blades 21.
  • a diffuser assembly 22 is arranged radially outward of the blades 21. Air drawn through the inlet 18 is pumped radially outwardly to an outlet 24 by the blades 21 through the diffuser 22.
  • An actuator 26 cooperates with the diffuser 22 to vary the inlet throat
  • the unit 10 provides pressurized air to an air cycle air conditioning pack of an aircraft.
  • the diffuser 22 includes a backing plate 28 that is isolated from deflection D.
  • the backing plate 28 is secured directly to the housing 16 contributing to the diffuser vanes binding.
  • the inventive diffuser 22 employs a mounting plate 30 that supports the backing plate 28.
  • the inner and outer periphery of the backing plate 28 is supported by the mounting plate 30, but is also permitted to move axially independently of the mounting plate 30.
  • the mounting plate 30 is secured to the housing 16 by a retainer 32 and fasteners 34.
  • a shroud 36 is supported by the housing 16 and may deflect axially under load.
  • Multiple vanes 38 are retained between the backing plate 28 and shroud 36 and, typically, a few thousandths of an inch of clearance is provided between the vane 38 and the backing plate 28 and shroud 36. In the example system shown, there are 23 vanes that are modulated between full open and 40% of full open.
  • the vanes 38 include an inlet end 48 and an outlet end 50.
  • the inlet end 48 provides an adjustable throat 52, shown in Figure 2, which is provided by pivoting the vanes 38.
  • the present invention includes an aperture 44 arranged between the inlet and outlet ends 48 and 50.
  • the aperture is elongated in the direction of the length of the vane 38.
  • Protrusions 46 extend from the backing plate 28 through the aperture 44. In the example shown, the protrusions 46 are integral with the backing plate 28 and extend to engage the shroud 36.
  • Bolts 40 shown in Figure 2, extend through the aperture 44 to secure the vane 38 between the shroud 36 and backing plate 28. The additional bolts 40 and protrusions 46 of the present invention provide improved containment of the vanes 38 in the event of a failure.
  • the mounting plate 30 includes a boss 42 for each vane 38.
  • Each vane 38 includes a hole 55 for receiving a pivot pin 54.
  • the pivot pin 54 extends through an opening in the shroud to the mounting plate 30 to secure the vane 38 between the shroud 36 and backing plate 28. An end of the pivot pin 54 is secured into the boss 42. Openings in the backing plate 28, vane 38 and shroud 36 are in a slip fit relationship relative to the pivot pin 54 to permit the shroud 36 and backing plate 28 to deflect axially without binding the vane 38.
  • the shroud 36 is shown broken along planes J, K and L in Figure 2 to better illustrate the interrelationship of diffuser components.
  • the vanes 38 include a slot 60 that receives a drive pin 58.
  • the drive pins 58 are mounted on a drive ring 56 that is rotated by the actuator 26 to rotate the vanes 38 about the pivot pins 54.
  • the drive ring 56 includes a bearing 57 supporting the drive ring 56 in the housing 16.
  • the drive pin 58 is received in a slot in the shroud 36 that defines the positional limits of the vanes 38.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A diffuser includes multiple vanes rotatable about pivot pins between multiple positions. A mounting plate supports a backing plate. The vanes are arranged between the backing plate and the shroud. The pivot pins are in a slip fit relationship with the backing plate, vanes and shroud and are threadingly received by bosses in the mounting plate. The mounting plate and pivot pin arrangement better enables the backing plate and shroud to remain parallel with one another during deflection of the backing plate and/or shroud. Structure, such as integral protrusions and/or bolts, extend from between the backing plate and shroud through apertures in the vanes to better contain the vanes in the event of a catastrophic failure.

Description

Description
VARIABLE AREA DIFFUSER
The present application claims priority to United States Provisional Application Serial No. 60/612,303, filed September 22, 2004.
Technical Field
This application relates to a variable area diffuser. In particular, this application relates to a variable area, vane-type-diffuser suitable for use in a compressed air system for an air conditioning pack.
Variable area diffusers utilize multiple vanes that are rotated between different angular positions to vary the throat size of the diffuser. Variable area diffusers can be used in conjunction with, for example, superchargers to vary the flow through an air conditioning system of an aircraft at various altitudes. The variable area diffuser may be subjected to very high stresses, for example, as the compressor is driven at high speed. The diffuser structure must pass a containment test in which the compressor rotor is rotated at very high speeds until the rotor disintegrates. The debris must stay within its housing so that the debris does not create a hazard to surrounding areas, components or personnel. Another problem with the diffuser operation is that the structure adjacent to the vanes, such as a backing plate and/or shroud, deflects. It is desirable to maintain a clearance of only a few thousandths on either side of the vane throughout the operation of the diffuser. Deflection of the structure surrounding the vanes can create a binding condition compromising the operation of the diffuser.
What is needed is an improved variable area diffuser with improved operation under applied loads and improved containment of debris in the event of rotor failure.
Disclosure of Invention
The present invention provides a compressed air unit that includes a housing having a shroud. An electric motor driven compressor rotor is arranged in the housing and including rotor blades. A variable area diffuser is arranged in the housing and is in fluid communication with the compressor. The diffuser includes multiple vanes arranged circumferentially around the rotor. The vanes rotate to multiple positions about pivot pins to change the flow through the compressed air system. A mounting plate is secured to the housing by a retainer and supports a backing plate. The vanes are arranged between the backing plate and the shroud.
The pivot pins are in a slip fit relationship with the backing plate, vanes and shroud and are threadingly received by bosses in the mounting plate. With the mounting plate and pivot pin arrangement of the present invention, the backing plate and shroud are better able to remain parallel with one another during loading
Structure, such as protrusions and/or fasteners (such as bolts), extend from between the backing plate and shroud through apertures in the vanes to better contain the vanes in the event of a catastrophic failure. Multiple protrusions and bolts are used to act as a barrier to debris, in the example shown. Accordingly, the invention provides an improved variable area diffuser with improved operation under deflection and improved containment of debris in the event of vane failure.
These and other features of the present invention can be best understood from the following specification and drawings, the following of which is a brief description.
Brief Description of Drawings
Figure 1 is a cross-sectional view of a compressed unit system having the inventive variable area diffuser. Figure 2 is a partially broken view of the inventive diffuser, broken at several planes and viewed in the direction of the arrows 2-2 in Figure 3.
Figure 3 is an enlarged cross-sectional view of the inventive diffuser shown in Figure 1.
Best Mode for Carrying Out the Invention
A compressed air unit 10 is shown in Figure 1. The unit 10 includes a compressor rotor 12 driven by an electric motor 14. It should be understood, however, that the inventive diffuser may be used in other, non-electric motor applications. The compressor rotor 12 and electric motor 14 are contained within the housing 16, which may be constructed from multiple housing portions secured to one another. The housing 16 provides an inlet 18 for providing air to the compressor 12. A motor rotor 20 is disposed within a motor stator 19 and is rotatable about an axis A. The rotor 20 supports compressor rotor with blades 21. A diffuser assembly 22 is arranged radially outward of the blades 21. Air drawn through the inlet 18 is pumped radially outwardly to an outlet 24 by the blades 21 through the diffuser 22. An actuator 26 cooperates with the diffuser 22 to vary the inlet throat
(shown at 52 in Figure 2) to vary the flow rate through the unit 10. In one example, the unit 10 provides pressurized air to an air cycle air conditioning pack of an aircraft.
Referring to Figures 2 and 3, the diffuser 22 includes a backing plate 28 that is isolated from deflection D. In conventional devices, the backing plate 28 is secured directly to the housing 16 contributing to the diffuser vanes binding. Instead, the inventive diffuser 22 employs a mounting plate 30 that supports the backing plate 28. The inner and outer periphery of the backing plate 28 is supported by the mounting plate 30, but is also permitted to move axially independently of the mounting plate 30. The mounting plate 30 is secured to the housing 16 by a retainer 32 and fasteners 34.
A shroud 36 is supported by the housing 16 and may deflect axially under load. Multiple vanes 38 are retained between the backing plate 28 and shroud 36 and, typically, a few thousandths of an inch of clearance is provided between the vane 38 and the backing plate 28 and shroud 36. In the example system shown, there are 23 vanes that are modulated between full open and 40% of full open.
The vanes 38 include an inlet end 48 and an outlet end 50. The inlet end 48 provides an adjustable throat 52, shown in Figure 2, which is provided by pivoting the vanes 38. To provide improved containment, the present invention includes an aperture 44 arranged between the inlet and outlet ends 48 and 50. The aperture is elongated in the direction of the length of the vane 38. Protrusions 46 extend from the backing plate 28 through the aperture 44. In the example shown, the protrusions 46 are integral with the backing plate 28 and extend to engage the shroud 36. Bolts 40, shown in Figure 2, extend through the aperture 44 to secure the vane 38 between the shroud 36 and backing plate 28. The additional bolts 40 and protrusions 46 of the present invention provide improved containment of the vanes 38 in the event of a failure.
The mounting plate 30 includes a boss 42 for each vane 38. Each vane 38 includes a hole 55 for receiving a pivot pin 54. The pivot pin 54 extends through an opening in the shroud to the mounting plate 30 to secure the vane 38 between the shroud 36 and backing plate 28. An end of the pivot pin 54 is secured into the boss 42. Openings in the backing plate 28, vane 38 and shroud 36 are in a slip fit relationship relative to the pivot pin 54 to permit the shroud 36 and backing plate 28 to deflect axially without binding the vane 38.
The shroud 36 is shown broken along planes J, K and L in Figure 2 to better illustrate the interrelationship of diffuser components. The vanes 38 include a slot 60 that receives a drive pin 58. The drive pins 58 are mounted on a drive ring 56 that is rotated by the actuator 26 to rotate the vanes 38 about the pivot pins 54. The drive ring 56 includes a bearing 57 supporting the drive ring 56 in the housing 16. The drive pin 58 is received in a slot in the shroud 36 that defines the positional limits of the vanes 38. Although a preferred embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.

Claims

1. A variable area diffuser comprising: a backing plate and a shroud spaced apart from the backing plate; a vane arranged between the backing plate and shroud, the vane adjustable between multiple positions, the vane including an aperture; and structure extending from the backing plate towards the shroud through the aperture.
2. The variable area diffuser according to claim 1, wherein the vane includes a hole, and a pivot pin arranged within the hole, the hole spaced from the aperture, the vane rotatable about the pivot pin between the multiple positions.
3. The variable area diffuser according to claim 2, wherein the structure includes a protrusion integral with the backing plate.
4. The variable area diffuser according to claim 3, wherein the structure includes a fastener extending through the aperture proximate to the protrusion.
5. The variable area diffuser according to claim 4, wherein the structure includes multiple protrusions and fasteners.
6. The variable area diffuser according to claim 2, wherein a mounting plate supports the backing plate, the pivot pin extending from the shroud into the mounting plate, the pivot pin in a slip fit relationship with the shroud, vane and backing plate.
7. The variable area diffuser according to claim 6, wherein the mounting plate includes a boss receiving a threaded end of the pivot pin.
8. The variable area diffuser according to claim 2, wherein a drive ring having a drive pin rotates the vane about the pivot pin, the drive pin received in a slot in the vane.
9. A compressed air unit comprising: a housing having a shroud; a compressor arranged in the housing and including rotor blades; a variable area diffuser arranged in the housing and in fluid communication with the compressor rotor, the diffuser including multiple vanes arranged circumferentially and outward of the rotor blades, the vanes rotatable about pivot pins between multiple positions, a mounting plate secured to the housing and supporting a backing plate, the vanes arranged between the backing plate and the shroud.
10. The system according to claim 9, wherein a retainer is secured to the housing with fasteners, the mounting plate arranged between the retainer and the housing
11. The system according to claim 9, wherein the mounting plate includes bosses, and the vanes include holes, pivot pins extending from the shroud though the holes and into the bosses.
12. The system according to claim 11, wherein the pivot pins are in a slip fit relationship with the backing plate, vanes and shroud.
13. The system according to claim 9, wherein the vanes include apertures and structure extends from the backing plate through the apertures to the shroud.
14. The system according to claim 13, wherein the structure includes protrusions and fasteners proximate to the protrusions.
15. The system according to claim 9, wherein a drive ring is supported by the housing on a bearing, the drive ring including drive pins received by slots in the vanes, and an actuator operatively connected to the drive ring for moving the vanes between the multiple positions.
16. The system according to claim 9, wherein an electric motor is arranged within the housing, the electric motor driving the compressor.
17. The system according to claim 9, wherein the shroud and backing plate are arranged parallel to one another transverse to an axis of rotation of the compressor.
PCT/US2005/032928 2004-09-22 2005-09-15 Variable area diffuser for a radial c0mpress0r WO2006137863A2 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP05858134A EP1792054B1 (en) 2004-09-22 2005-09-15 Radial variable area diffuser for a radial compressor
DE602005021373T DE602005021373D1 (en) 2004-09-22 2005-09-15 RADIAL VARIABLE FLAT DIFFUSER
JP2007532457A JP4708431B2 (en) 2004-09-22 2005-09-15 Variable area diffuser

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US61230304P 2004-09-22 2004-09-22
US60/612,303 2004-09-22
US11/108,286 US7407367B2 (en) 2004-09-22 2005-04-18 Variable area diffuser
US11/108,286 2005-04-18

Publications (2)

Publication Number Publication Date
WO2006137863A2 true WO2006137863A2 (en) 2006-12-28
WO2006137863A3 WO2006137863A3 (en) 2007-08-09

Family

ID=36074193

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2005/032928 WO2006137863A2 (en) 2004-09-22 2005-09-15 Variable area diffuser for a radial c0mpress0r

Country Status (5)

Country Link
US (1) US7407367B2 (en)
EP (1) EP1792054B1 (en)
JP (2) JP4708431B2 (en)
DE (1) DE602005021373D1 (en)
WO (1) WO2006137863A2 (en)

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JP4930151B2 (en) * 2007-03-29 2012-05-16 株式会社Ｉｈｉ Expansion turbine with variable nozzle mechanism
JP4930150B2 (en) * 2007-03-29 2012-05-16 株式会社Ｉｈｉ Expansion turbine with variable nozzle mechanism
US20080276613A1 (en) * 2007-05-09 2008-11-13 Phillipe Noelle Discrete variable geometry compressor
US9080578B2 (en) * 2008-09-02 2015-07-14 Hamilton Sundstrand Corporation Compact drive for compressor variable diffuser
US20100170262A1 (en) * 2009-01-06 2010-07-08 Kaslusky Scott F Aircraft power and thermal management system with electric co-generation
US8839625B2 (en) 2010-06-08 2014-09-23 Hamilton Sunstrand Corporation Gas turbine engine diffuser having air flow channels with varying widths
US8834097B2 (en) 2010-06-09 2014-09-16 Hamilton Sundstrand Corporation Compressor diffuser vane damper
US8864449B2 (en) 2010-11-02 2014-10-21 Hamilton Sundstrand Corporation Drive ring bearing for compressor diffuser assembly
US8864456B2 (en) 2011-09-19 2014-10-21 Hamilton Sundstrand Corporation Turbine nozzle for air cycle machine
US9341193B2 (en) * 2013-04-04 2016-05-17 Hamilton Sundstrand Corporation Cabin air compressor diffuser vane drive ring
US9890793B2 (en) * 2014-09-23 2018-02-13 Hamilton Sundstrand Corporation Variable diffuser vane
DE102015219556A1 (en) 2015-10-08 2017-04-13 Rolls-Royce Deutschland Ltd & Co Kg Diffuser for radial compressor, centrifugal compressor and turbo machine with centrifugal compressor
US10174765B2 (en) 2016-01-14 2019-01-08 Hamilton Sundstrand Corporation Outlet housing for cabin air compressor
WO2019060754A2 (en) * 2017-09-25 2019-03-28 Johnson Controls Technology Company Two piece split scroll for centrifugal compressor
FR3085720B1 (en) * 2018-09-06 2020-08-07 Liebherr-Aerospace Toulouse Sas DISTRIBUTOR OF A TURBOMACHINE RADIAL TURBINE, TURBOMACHINE INCLUDING SUCH A DISTRIBUTOR AND AIR CONDITIONING SYSTEM INCLUDING SUCH A TURBOMACHINE
US11098730B2 (en) 2019-04-12 2021-08-24 Rolls-Royce Corporation Deswirler assembly for a centrifugal compressor
US11286952B2 (en) 2020-07-14 2022-03-29 Rolls-Royce Corporation Diffusion system configured for use with centrifugal compressor
US11441516B2 (en) 2020-07-14 2022-09-13 Rolls-Royce North American Technologies Inc. Centrifugal compressor assembly for a gas turbine engine with deswirler having sealing features
US11578654B2 (en) 2020-07-29 2023-02-14 Rolls-Royce North American Technologies Inc. Centrifical compressor assembly for a gas turbine engine

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Also Published As

Publication number Publication date
US20060062666A1 (en) 2006-03-23
DE602005021373D1 (en) 2010-07-01
JP4708431B2 (en) 2011-06-22
JP2008513674A (en) 2008-05-01
EP1792054B1 (en) 2010-05-19
JP5160656B2 (en) 2013-03-13
JP2011080481A (en) 2011-04-21
EP1792054A2 (en) 2007-06-06
US7407367B2 (en) 2008-08-05
WO2006137863A3 (en) 2007-08-09

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