FR1012339A - Improvements made to axial compressors, in particular those for aviation turbo-machines - Google Patents

Improvements made to axial compressors, in particular those for aviation turbo-machines

Info

Publication number
FR1012339A
FR1012339A FR1012339DA FR1012339A FR 1012339 A FR1012339 A FR 1012339A FR 1012339D A FR1012339D A FR 1012339DA FR 1012339 A FR1012339 A FR 1012339A
Authority
FR
France
Prior art keywords
machines
particular those
improvements made
axial compressors
aviation turbo
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
Application number
Other languages
French (fr)
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 Transmission Systems SAS
Societe dExplotation des Materiels Hispano Suiza
Original Assignee
Societe dExplotation des Materiels Hispano Suiza
Hispano Suiza SA
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 dExplotation des Materiels Hispano Suiza, Hispano Suiza SA filed Critical Societe dExplotation des Materiels Hispano Suiza
Application granted granted Critical
Publication of FR1012339A publication Critical patent/FR1012339A/en
Expired 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1012339D 1949-07-13 1949-07-13 Improvements made to axial compressors, in particular those for aviation turbo-machines Expired FR1012339A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1012339T 1949-07-13

Publications (1)

Publication Number Publication Date
FR1012339A true FR1012339A (en) 1952-07-08

Family

ID=9570742

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1012339D Expired FR1012339A (en) 1949-07-13 1949-07-13 Improvements made to axial compressors, in particular those for aviation turbo-machines

Country Status (1)

Country Link
FR (1) FR1012339A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2850227A (en) * 1954-12-03 1958-09-02 Gen Motors Corp Compressor air bleed-off valve
US2915262A (en) * 1957-09-26 1959-12-01 Douglas Aircraft Co Inc Vortex inhibitor for aircraft jet engines
US2945672A (en) * 1956-10-05 1960-07-19 Marquardt Corp Gas turbine unit
US3057541A (en) * 1958-06-03 1962-10-09 United Aircraft Corp Circumferential bleed valve
US3074432A (en) * 1958-05-15 1963-01-22 Rolls Royce Valve for gas turbine engines
US3142438A (en) * 1961-04-21 1964-07-28 Rolls Royce Multi-stage axial compressor
US3297307A (en) * 1963-01-30 1967-01-10 Krantz H Multi-stage circulators
US4155680A (en) * 1977-02-14 1979-05-22 General Electric Company Compressor protection means
US5209633A (en) * 1990-11-19 1993-05-11 General Electric Company High pressure compressor flowpath bleed valve extraction slot
WO1999051866A2 (en) * 1998-02-26 1999-10-14 Allison Advanced Development Company Compressor endwall bleed system
EP2305960A1 (en) * 2009-09-28 2011-04-06 Techspace Aero S.A. Purging valve in a primary duct of a compressor and corresponding process to suppress the surge effect
EP2987967A1 (en) * 2014-08-20 2016-02-24 Siemens Aktiengesellschaft Compressor housing for a gas turbine

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2850227A (en) * 1954-12-03 1958-09-02 Gen Motors Corp Compressor air bleed-off valve
US2945672A (en) * 1956-10-05 1960-07-19 Marquardt Corp Gas turbine unit
US2915262A (en) * 1957-09-26 1959-12-01 Douglas Aircraft Co Inc Vortex inhibitor for aircraft jet engines
US3074432A (en) * 1958-05-15 1963-01-22 Rolls Royce Valve for gas turbine engines
US3057541A (en) * 1958-06-03 1962-10-09 United Aircraft Corp Circumferential bleed valve
US3142438A (en) * 1961-04-21 1964-07-28 Rolls Royce Multi-stage axial compressor
US3297307A (en) * 1963-01-30 1967-01-10 Krantz H Multi-stage circulators
US4155680A (en) * 1977-02-14 1979-05-22 General Electric Company Compressor protection means
US5209633A (en) * 1990-11-19 1993-05-11 General Electric Company High pressure compressor flowpath bleed valve extraction slot
WO1999051866A2 (en) * 1998-02-26 1999-10-14 Allison Advanced Development Company Compressor endwall bleed system
WO1999051866A3 (en) * 1998-02-26 2001-07-19 Allison Advanced Dev Co Compressor endwall bleed system
US6428271B1 (en) 1998-02-26 2002-08-06 Allison Advanced Development Company Compressor endwall bleed system
EP2305960A1 (en) * 2009-09-28 2011-04-06 Techspace Aero S.A. Purging valve in a primary duct of a compressor and corresponding process to suppress the surge effect
US8753074B2 (en) 2009-09-28 2014-06-17 Techspace Aero S.A. Aspirator insert for a boundary layer in a fluid, a wall and a compressor equipped with said insert
EP2987967A1 (en) * 2014-08-20 2016-02-24 Siemens Aktiengesellschaft Compressor housing for a gas turbine

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