BE752584A - MULTI-STAGE COMPRESSOR TURBINE ENGINE WITH BETWEEN STAGE AIR LEAK SYSTEMS - Google Patents

MULTI-STAGE COMPRESSOR TURBINE ENGINE WITH BETWEEN STAGE AIR LEAK SYSTEMS

Info

Publication number
BE752584A
BE752584A BE752584DA BE752584A BE 752584 A BE752584 A BE 752584A BE 752584D A BE752584D A BE 752584DA BE 752584 A BE752584 A BE 752584A
Authority
BE
Belgium
Prior art keywords
stage
turbine engine
air leak
compressor turbine
systems
Prior art date
Application number
Other languages
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.)
Filing date
Publication date
Application filed by Gen Electric filed Critical Gen Electric
Publication of BE752584A publication Critical patent/BE752584A/en

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
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE752584D 1969-09-30 1970-06-26 MULTI-STAGE COMPRESSOR TURBINE ENGINE WITH BETWEEN STAGE AIR LEAK SYSTEMS BE752584A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US86219769A 1969-09-30 1969-09-30

Publications (1)

Publication Number Publication Date
BE752584A true BE752584A (en) 1970-12-01

Family

ID=25337901

Family Applications (1)

Application Number Title Priority Date Filing Date
BE752584D BE752584A (en) 1969-09-30 1970-06-26 MULTI-STAGE COMPRESSOR TURBINE ENGINE WITH BETWEEN STAGE AIR LEAK SYSTEMS

Country Status (5)

Country Link
US (1) US3632223A (en)
BE (1) BE752584A (en)
DE (1) DE2031612A1 (en)
FR (1) FR2060529A5 (en)
GB (1) GB1310401A (en)

Families Citing this family (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1291943A (en) * 1970-02-11 1972-10-04 Secr Defence Improvements in or relating to ducted fans
US3826084A (en) * 1970-04-28 1974-07-30 United Aircraft Corp Turbine coolant flow system
GB1342590A (en) * 1970-07-17 1974-01-03 Secr Defence Suppression of noise in gas turbine engines
US3945759A (en) * 1974-10-29 1976-03-23 General Electric Company Bleed air manifold
US3966355A (en) * 1975-06-24 1976-06-29 Westinghouse Electric Corporation Steam turbine extraction system
US3976394A (en) * 1975-07-18 1976-08-24 The United States Of America As Represented By The Secretary Of The Air Force Interstage bleed assembly
US4156344A (en) * 1976-12-27 1979-05-29 The Boeing Company Inlet guide vane bleed system
US4155681A (en) * 1977-02-14 1979-05-22 General Electric Company Manifold protection system
US4512715A (en) * 1980-07-22 1985-04-23 Electric Power Research Institute, Inc. Method and means for recapturing coolant in a gas turbine
GB2192229B (en) * 1986-07-04 1990-05-02 Rolls Royce Plc A compressor and air bleed system
US4979587A (en) * 1989-08-01 1990-12-25 The Boeing Company Jet engine noise suppressor
GB2251031B (en) * 1990-12-19 1995-01-18 Rolls Royce Plc Cooling air pick up
US5160241A (en) * 1991-09-09 1992-11-03 General Electric Company Multi-port air channeling assembly
US5351478A (en) * 1992-05-29 1994-10-04 General Electric Company Compressor casing assembly
US5327716A (en) * 1992-06-10 1994-07-12 General Electric Company System and method for tailoring rotor tip bleed air
DE4326799A1 (en) * 1993-08-10 1995-02-16 Abb Management Ag Device for extracting secondary air from an axial compressor
GB9709086D0 (en) * 1997-05-07 1997-06-25 Rolls Royce Plc Gas turbine engine cooling apparatus
JP2003517525A (en) 1998-02-26 2003-05-27 アリソン・アドバンスト・ディベロップメント・カンパニー Compressor end wall bleed system
US6109868A (en) * 1998-12-07 2000-08-29 General Electric Company Reduced-length high flow interstage air extraction
FR2823532B1 (en) * 2001-04-12 2003-07-18 Snecma Moteurs DISCHARGE SYSTEM FOR A TURBO-JET OR TURBO-PROPELLER WITH SIMPLIFIED CONTROL
US6438941B1 (en) 2001-04-26 2002-08-27 General Electric Company Bifurcated splitter for variable bleed flow
US20050141991A1 (en) * 2001-10-17 2005-06-30 Frutschi Hans U. Method for conditioning a compressor airflow and device therefor
US6732530B2 (en) * 2002-05-31 2004-05-11 Mitsubishi Heavy Industries, Ltd. Gas turbine compressor and clearance controlling method therefor
JP4893110B2 (en) * 2006-05-31 2012-03-07 株式会社Ｉｈｉ Axial fluid device
US8292567B2 (en) * 2006-09-14 2012-10-23 Caterpillar Inc. Stator assembly including bleed ports for turbine engine compressor
US8388308B2 (en) * 2007-10-30 2013-03-05 General Electric Company Asymmetric flow extraction system
US8307943B2 (en) 2010-07-29 2012-11-13 General Electric Company High pressure drop muffling system
GB201015029D0 (en) 2010-09-10 2010-10-20 Rolls Royce Plc Gas turbine engine
US8430202B1 (en) 2011-12-28 2013-04-30 General Electric Company Compact high-pressure exhaust muffling devices
US9399951B2 (en) 2012-04-17 2016-07-26 General Electric Company Modular louver system
US8511096B1 (en) 2012-04-17 2013-08-20 General Electric Company High bleed flow muffling system
US8550208B1 (en) 2012-04-23 2013-10-08 General Electric Company High pressure muffling devices
US20140338360A1 (en) * 2012-09-21 2014-11-20 United Technologies Corporation Bleed port ribs for turbomachine case
US9689315B2 (en) * 2015-02-13 2017-06-27 Hamilton Sundstrand Corporation Full-area bleed valves
US20180313364A1 (en) * 2017-04-27 2018-11-01 General Electric Company Compressor apparatus with bleed slot including turning vanes
US10934943B2 (en) * 2017-04-27 2021-03-02 General Electric Company Compressor apparatus with bleed slot and supplemental flange
US10626879B2 (en) * 2017-11-13 2020-04-21 United Technologies Corporation Gas turbine engine with mid-compressor bleed
US10823069B2 (en) * 2018-11-09 2020-11-03 Raytheon Technologies Corporation Internal heat exchanger system to cool gas turbine engine components
US11828226B2 (en) * 2022-04-13 2023-11-28 General Electric Company Compressor bleed air channels having a pattern of vortex generators

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US25253A (en) * 1859-08-30 Faucet
US2314058A (en) * 1941-06-23 1943-03-16 Edward A Stalker Pump
US2693904A (en) * 1950-11-14 1954-11-09 A V Roe Canada Ltd Air bleed for compressors
US2738921A (en) * 1950-11-22 1956-03-20 United Aircraft Corp Boundary layer control apparatus for compressors
GB869576A (en) * 1958-05-15 1961-05-31 Rolls Royce Improvements in compressors for gas turbine engines
US3142438A (en) * 1961-04-21 1964-07-28 Rolls Royce Multi-stage axial compressor

Also Published As

Publication number Publication date
DE2031612A1 (en) 1971-04-15
GB1310401A (en) 1973-03-21
US3632223A (en) 1972-01-04
FR2060529A5 (en) 1971-06-18

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