DE69503719D1 - Abblassvorrichtung für Turbomaschine - Google Patents

Abblassvorrichtung für Turbomaschine

Info

Publication number
DE69503719D1
DE69503719D1 DE69503719T DE69503719T DE69503719D1 DE 69503719 D1 DE69503719 D1 DE 69503719D1 DE 69503719 T DE69503719 T DE 69503719T DE 69503719 T DE69503719 T DE 69503719T DE 69503719 D1 DE69503719 D1 DE 69503719D1
Authority
DE
Germany
Prior art keywords
turbomachinery
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 - Lifetime
Application number
DE69503719T
Other languages
English (en)
Other versions
DE69503719T2 (de
Inventor
Patrick Roger Jean Derouet
Michel Serge Guimier
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of DE69503719D1 publication Critical patent/DE69503719D1/de
Application granted granted Critical
Publication of DE69503719T2 publication Critical patent/DE69503719T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F01D17/105—Final actuators by passing part of the fluid
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sampling And Sample Adjustment (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
DE69503719T 1994-08-24 1995-08-23 Abblassvorrichtung für Turbomaschine Expired - Lifetime DE69503719T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9410237A FR2723981B1 (fr) 1994-08-24 1994-08-24 Dispositif de prelevement d'air auto-regule a la source pour turbomachine

Publications (2)

Publication Number Publication Date
DE69503719D1 true DE69503719D1 (de) 1998-09-03
DE69503719T2 DE69503719T2 (de) 1999-03-11

Family

ID=9466457

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69503719T Expired - Lifetime DE69503719T2 (de) 1994-08-24 1995-08-23 Abblassvorrichtung für Turbomaschine

Country Status (4)

Country Link
US (1) US5531566A (de)
EP (1) EP0698739B1 (de)
DE (1) DE69503719T2 (de)
FR (1) FR2723981B1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6695578B2 (en) 2001-12-19 2004-02-24 Sikorsky Aircraft Corporation Bleed valve system for a gas turbine engine
FR2884867B1 (fr) 2005-04-21 2007-08-03 Snecma Moteurs Sa Dispositif de regulation du debit d'air circulant dans un arbre rotatif d'une turbomachine
GB0618072D0 (en) * 2006-09-14 2006-10-25 Rolls Royce Plc Aeroengine nozzle
US8578716B2 (en) * 2008-03-22 2013-11-12 United Technologies Corporation Valve system for a gas turbine engine
US10041407B2 (en) 2011-03-29 2018-08-07 General Electric Company System and method for air extraction from gas turbine engines
WO2015030907A1 (en) * 2013-08-26 2015-03-05 Hamilton Sundstrand Corporation Variable pressure air supply
WO2015126551A1 (en) * 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine having minimum cooling airflow
GB201504010D0 (en) * 2015-03-10 2015-04-22 Rolls Royce Plc Gas bleed arrangement
GB201718796D0 (en) * 2017-11-14 2017-12-27 Rolls Royce Plc Gas turbine engine having an air-oil heat exchanger
US11053949B2 (en) 2018-08-03 2021-07-06 Hamilton Sundstrand Corporation Passively controlled inline bleed valves
US10975875B2 (en) 2018-08-03 2021-04-13 Hamilton Sundstrand Corporation Passive bleed valves with adjustable pressure threshold

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB113718A (de) * 1900-01-01
US2546432A (en) * 1944-03-20 1951-03-27 Power Jets Res & Dev Ltd Apparatus for deflecting a fuel jet towards a region of turbulence in a propulsive gaseous stream
FR1182604A (fr) * 1957-09-11 1959-06-26 Moteur à combustion perfectionné
GB906541A (en) * 1958-07-18 1962-09-26 Richardsons Westgarth & Co Improvements in or relating to blowers and compressors
NO119851B (de) * 1967-01-30 1970-07-13 Nordisk Ventilator
US3909152A (en) * 1973-09-27 1975-09-30 United Aircraft Corp Variable size bleed port for jet engines
US3915587A (en) * 1973-09-27 1975-10-28 United Technologies Corp Variable size bleed port for jet engines
US5113649A (en) * 1990-05-11 1992-05-19 General Electric Company Passive bypass valve assembly
GB2259328B (en) * 1991-09-03 1995-07-19 Gen Electric Gas turbine engine variable bleed pivotal flow splitter

Also Published As

Publication number Publication date
FR2723981A1 (fr) 1996-03-01
EP0698739A1 (de) 1996-02-28
FR2723981B1 (fr) 1996-09-20
US5531566A (en) 1996-07-02
DE69503719T2 (de) 1999-03-11
EP0698739B1 (de) 1998-07-29

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: SNECMA MOTEURS, PARIS, FR

8327 Change in the person/name/address of the patent owner

Owner name: SNECMA, PARIS, FR