BE756363A - Systeme d'echappement pour compresseurs de moteurs a turbine a gaz - Google Patents

Systeme d'echappement pour compresseurs de moteurs a turbine a gaz

Info

Publication number
BE756363A
BE756363A BE756363DA BE756363A BE 756363 A BE756363 A BE 756363A BE 756363D A BE756363D A BE 756363DA BE 756363 A BE756363 A BE 756363A
Authority
BE
Belgium
Prior art keywords
compressors
gas turbine
exhaust system
turbine engines
engines
Prior art date
Application number
Other languages
English (en)
French (fr)
Inventor
T L Hampton
Original Assignee
Gen Electric
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.)
Publication date
Publication of BE756363A publication Critical patent/BE756363A/xx

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE756363D 1969-09-30 Systeme d'echappement pour compresseurs de moteurs a turbine a gaz BE756363A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US86219669A 1969-09-30 1969-09-30

Publications (1)

Publication Number Publication Date
BE756363A true BE756363A (fr) 1971-03-01

Family

ID=25337899

Family Applications (1)

Application Number Title Priority Date Filing Date
BE756363D BE756363A (fr) 1969-09-30 Systeme d'echappement pour compresseurs de moteurs a turbine a gaz

Country Status (5)

Country Link
US (1) US3588268A (xx)
BE (1) BE756363A (xx)
DE (1) DE2045983A1 (xx)
FR (1) FR2068282A5 (xx)
GB (1) GB1319348A (xx)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2410139C3 (de) * 1974-03-02 1981-10-15 Klöckner-Humboldt-Deutz AG, 5000 Köln Gasturbinenanlage
US4086761A (en) * 1976-04-26 1978-05-02 The Boeing Company Stator bypass system for turbofan engine
FR2569783B1 (fr) * 1984-09-06 1986-09-12 Snecma Structure d'anneau et dispositif de decharge de compresseur comportant cet anneau
FR2569785B1 (fr) * 1984-09-06 1986-09-12 Snecma Disposit
US5505587A (en) * 1995-01-05 1996-04-09 Northrop Grumman Corporation RAM air turbine generating apparatus
US6048171A (en) * 1997-09-09 2000-04-11 United Technologies Corporation Bleed valve system
US6899379B1 (en) 1999-10-22 2005-05-31 Mack Trucks, Inc. Modular sleeping compartment for trucks
US6899513B2 (en) * 2003-07-07 2005-05-31 Pratt & Whitney Canada Corp. Inflatable compressor bleed valve system
WO2006091138A1 (en) * 2005-02-25 2006-08-31 Volvo Aero Corporation A bleed structure for a bleed passage in a gas turbine engine
US7624581B2 (en) * 2005-12-21 2009-12-01 General Electric Company Compact booster bleed turbofan
DE102011101331A1 (de) * 2011-05-12 2012-11-15 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinentriebwerk mit Zapfluftentnahmevorrichtung
WO2013102098A1 (en) * 2011-12-29 2013-07-04 Rolls-Royce North American Technologies, Inc. Vavle for gas turbine engine
US9328735B2 (en) * 2012-09-28 2016-05-03 United Technologies Corporation Split ring valve
US10393128B2 (en) 2015-05-26 2019-08-27 Pratt & Whitney Canada Corp. Translating gaspath bleed valve
US20230212989A1 (en) * 2022-01-05 2023-07-06 General Electric Company Bleed valve assemblies
US11619170B1 (en) * 2022-03-07 2023-04-04 Rolls-Royce North American Technologies Inc. Gas turbine engine with radial turbine having modulated fuel cooled cooling air

Also Published As

Publication number Publication date
DE2045983A1 (de) 1971-04-15
FR2068282A5 (xx) 1971-08-20
US3588268A (en) 1971-06-28
GB1319348A (en) 1973-06-06

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