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DE69426601D1 - Axial öffnendes zylindrisches abblasventil - Google Patents

Axial öffnendes zylindrisches abblasventil

Info

Publication number
DE69426601D1
DE69426601D1 DE69426601T DE69426601T DE69426601D1 DE 69426601 D1 DE69426601 D1 DE 69426601D1 DE 69426601 T DE69426601 T DE 69426601T DE 69426601 T DE69426601 T DE 69426601T DE 69426601 D1 DE69426601 D1 DE 69426601D1
Authority
DE
Germany
Prior art keywords
valve
axial opening
opening cylindrical
cylindrical blow
blow
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
DE69426601T
Other languages
English (en)
Other versions
DE69426601T2 (de
Inventor
Alan Kostka
Vittorio Bruno
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Pratt and Whitney Canada Corp
Original Assignee
Pratt and Whitney Canada Corp
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 Pratt and Whitney Canada Corp filed Critical Pratt and Whitney Canada Corp
Publication of DE69426601D1 publication Critical patent/DE69426601D1/de
Application granted granted Critical
Publication of DE69426601T2 publication Critical patent/DE69426601T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control
    • F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
    • F04D27/0215—Arrangements therefor, e.g. bleed or by-pass valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control
    • F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
    • F04D27/023—Details or means for fluid extraction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00—Geometry
    • F05B2250/20—Geometry three-dimensional
    • F05B2250/23—Geometry three-dimensional prismatic
    • F05B2250/231—Geometry three-dimensional prismatic cylindrical

Landscapes

  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Lift Valve (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Self-Closing Valves And Venting Or Aerating Valves (AREA)
DE69426601T 1993-10-13 1994-10-13 Axial öffnendes zylindrisches abblasventil Expired - Fee Related DE69426601T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/135,710 US5380151A (en) 1993-10-13 1993-10-13 Axially opening cylindrical bleed valve
PCT/CA1994/000558 WO1995010709A1 (en) 1993-10-13 1994-10-13 Axially opening cylindrical bleed valve

Publications (2)

Publication Number Publication Date
DE69426601D1 true DE69426601D1 (de) 2001-02-22
DE69426601T2 DE69426601T2 (de) 2001-05-31

Family

ID=22469300

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69426601T Expired - Fee Related DE69426601T2 (de) 1993-10-13 1994-10-13 Axial öffnendes zylindrisches abblasventil

Country Status (6)

Country Link
US (1) US5380151A (de)
EP (1) EP0723630B1 (de)
JP (1) JP3682976B2 (de)
DE (1) DE69426601T2 (de)
RU (1) RU2126492C1 (de)
WO (1) WO1995010709A1 (de)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6048171A (en) * 1997-09-09 2000-04-11 United Technologies Corporation Bleed valve system
US6106227A (en) * 1998-02-27 2000-08-22 United Technologies Corporation Roller assembly for guiding an actuating ring
US6086326A (en) * 1998-02-27 2000-07-11 United Technologies Corporation Stator structure for a track opening of a rotary machine
US6370772B1 (en) * 1998-02-27 2002-04-16 United Technologies Corporation Method of forming a track for an axial flow gas turbine
US6212770B1 (en) * 1998-02-27 2001-04-10 United Technologies Corporation Method of forming a roller assembly
US6092987A (en) * 1998-02-27 2000-07-25 United Technologies Corporation Stator assembly for a rotary machine
JPH11294189A (ja) * 1998-02-27 1999-10-26 United Technol Corp <Utc> 回転機械用のステ―タ構造体
DE19834530A1 (de) * 1998-07-31 2000-02-03 Bmw Rolls Royce Gmbh Anordnung eines als Abblaseventil eines Axialverdichters fungierenden Blendenringes
US6183195B1 (en) 1999-02-04 2001-02-06 Pratt & Whitney Canada Corp. Single slot impeller bleed
GB9918072D0 (en) 1999-07-30 1999-10-06 Alliedsignal Ltd Turbocharger
US6695578B2 (en) 2001-12-19 2004-02-24 Sikorsky Aircraft Corporation Bleed valve system for a gas turbine engine
US6755025B2 (en) 2002-07-23 2004-06-29 Pratt & Whitney Canada Corp. Pneumatic compressor bleed valve
US6899513B2 (en) * 2003-07-07 2005-05-31 Pratt & Whitney Canada Corp. Inflatable compressor bleed valve system
US7197881B2 (en) 2004-03-25 2007-04-03 Honeywell International, Inc. Low loss flow limited feed duct
US7624581B2 (en) * 2005-12-21 2009-12-01 General Electric Company Compact booster bleed turbofan
US7946104B2 (en) * 2006-05-12 2011-05-24 Rohr, Inc. Bleed air relief system for engines
US7850419B2 (en) * 2006-11-30 2010-12-14 Pratt & Whitney Canada Corp. Bleed valve actuating system for a gas turbine engine
FR2925130B1 (fr) 2007-12-14 2012-07-27 Snecma Dispositif de prelevement d'air dans un compresseur de turbomachine
US8105012B2 (en) * 2008-03-12 2012-01-31 Opra Technologies B.V. Adjustable compressor bleed system and method
US8092153B2 (en) * 2008-12-16 2012-01-10 Pratt & Whitney Canada Corp. Bypass air scoop for gas turbine engine
US8167551B2 (en) * 2009-03-26 2012-05-01 United Technologies Corporation Gas turbine engine with 2.5 bleed duct core case section
GB2470050B (en) * 2009-05-07 2015-09-23 Cummins Turbo Tech Ltd A compressor
FR2987874B1 (fr) * 2012-03-09 2015-10-09 Snecma Couvercle pour compresseur, compresseur et turboreacteurs associes
US9068506B2 (en) 2012-03-30 2015-06-30 Pratt & Whitney Canada Corp. Turbine engine heat recuperator system
US9638201B2 (en) 2012-06-20 2017-05-02 United Technologies Corporation Machined aerodynamic intercompressor bleed ports
US9103283B2 (en) * 2012-06-20 2015-08-11 United Technologies Corporation Spherical-link end damper system with near constant engagement
US9322337B2 (en) 2012-06-20 2016-04-26 United Technologies Corporation Aerodynamic intercompressor bleed ports
US9328735B2 (en) 2012-09-28 2016-05-03 United Technologies Corporation Split ring valve
US9752587B2 (en) * 2013-06-17 2017-09-05 United Technologies Corporation Variable bleed slot in centrifugal impeller
US9651053B2 (en) * 2014-01-24 2017-05-16 Pratt & Whitney Canada Corp. Bleed valve
DE102015220333A1 (de) * 2015-10-19 2017-04-20 Rolls-Royce Deutschland Ltd & Co Kg Vorrichtung zur Einstellung eines Spaltes zwischen dem Gehäuse eines Laufrades und dem Laufrad in einem Radialverdichter und eine Turbomaschine
US10934943B2 (en) 2017-04-27 2021-03-02 General Electric Company Compressor apparatus with bleed slot and supplemental flange
US11346240B2 (en) * 2019-06-07 2022-05-31 Raytheon Technologies Corporation Gas turbine engine bleed valve damping guide link

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1862289A (en) * 1929-03-29 1932-06-07 American Blower Corp Apparatus and method of controlling fans
US2092961A (en) * 1936-05-01 1937-09-14 Chain Belt Co Discharge gate mechanism for concrete transportation conduits
US2473620A (en) * 1944-12-05 1949-06-21 Bendix Aviat Corp Valve
US2645244A (en) * 1948-08-06 1953-07-14 Amiel F Klickman Close-off device for pipe lines
US2693904A (en) * 1950-11-14 1954-11-09 A V Roe Canada Ltd Air bleed for compressors
US2702665A (en) * 1951-03-07 1955-02-22 United Aircraft Corp Stator construction for axial flow compressors
US2850227A (en) * 1954-12-03 1958-09-02 Gen Motors Corp Compressor air bleed-off valve
US3030006A (en) * 1958-05-27 1962-04-17 United Aircraft Corp Circumferential bleed valve
US3360189A (en) * 1965-10-11 1967-12-26 United Aircraft Canada Bleed arrangement for gas turbine engines
US3398928A (en) * 1966-03-11 1968-08-27 Otis Eng Co Valves
US3638428A (en) * 1970-05-04 1972-02-01 Gen Electric Bypass valve mechanism
GB1365491A (en) * 1971-01-02 1974-09-04 Dowty Rotol Ltd Gas turbine ducted fan engines and fans therefor
DE2247400C2 (de) * 1972-09-27 1975-01-16 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Vorrichtung zum Abblasen von verdichteter Luft aus einem Verdichter eines Gasturbinenstrahltriebwerks
US3941498A (en) * 1974-04-08 1976-03-02 Chandler Evans Inc. Variable geometry collector for centrifugal pump
US4050240A (en) * 1976-08-26 1977-09-27 General Motors Corporation Variable air admission device for a combustor assembly
US4120156A (en) * 1977-06-08 1978-10-17 The Garrett Corporation Turbocharger control
US4280678A (en) * 1978-11-29 1981-07-28 Pratt & Whitney Aircraft Of Canada, Limited Bleed valve
US5136840A (en) * 1982-09-30 1992-08-11 General Electric Company Gas turbine engine actuation system
US4522592A (en) * 1983-08-01 1985-06-11 Johnson W Grant Valve structure for an oral evacuator system
US4715779A (en) * 1984-12-13 1987-12-29 United Technologies Corporation Bleed valve for axial flow compressor
US4998562A (en) * 1986-05-23 1991-03-12 Halkey-Roberts Corporation Flow control valve
US4827713A (en) * 1987-06-29 1989-05-09 United Technologies Corporation Stator valve assembly for a rotary machine
DE3734386A1 (de) * 1987-10-10 1989-04-20 Daimler Benz Ag Abgasturbolader fuer eine brennkraftmaschine

Also Published As

Publication number Publication date
RU2126492C1 (ru) 1999-02-20
WO1995010709A1 (en) 1995-04-20
EP0723630B1 (de) 2001-01-17
US5380151A (en) 1995-01-10
DE69426601T2 (de) 2001-05-31
EP0723630A1 (de) 1996-07-31
JP3682976B2 (ja) 2005-08-17
JPH09503568A (ja) 1997-04-08

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee