FR2324874A1 - Dispositif pour soutirer de l'air d'un compresseur - Google Patents

Dispositif pour soutirer de l'air d'un compresseur

Info

Publication number
FR2324874A1
FR2324874A1 FR7627840A FR7627840A FR2324874A1 FR 2324874 A1 FR2324874 A1 FR 2324874A1 FR 7627840 A FR7627840 A FR 7627840A FR 7627840 A FR7627840 A FR 7627840A FR 2324874 A1 FR2324874 A1 FR 2324874A1
Authority
FR
France
Prior art keywords
compressor
supplying air
supplying
air
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.)
Granted
Application number
FR7627840A
Other languages
English (en)
Other versions
FR2324874B1 (fr
Inventor
Wayne Myron Brown
Joseph Carmen Manente
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Publication of FR2324874A1 publication Critical patent/FR2324874A1/fr
Application granted granted Critical
Publication of FR2324874B1 publication Critical patent/FR2324874B1/fr
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • 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
FR7627840A 1975-09-19 1976-09-16 Dispositif pour soutirer de l'air d'un compresseur Granted FR2324874A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/614,807 US4008977A (en) 1975-09-19 1975-09-19 Compressor bleed system

Publications (2)

Publication Number Publication Date
FR2324874A1 true FR2324874A1 (fr) 1977-04-15
FR2324874B1 FR2324874B1 (fr) 1982-09-17

Family

ID=24462783

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7627840A Granted FR2324874A1 (fr) 1975-09-19 1976-09-16 Dispositif pour soutirer de l'air d'un compresseur

Country Status (4)

Country Link
US (1) US4008977A (fr)
CA (1) CA1050775A (fr)
FR (1) FR2324874A1 (fr)
GB (1) GB1524139A (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2610783C3 (de) * 1976-03-15 1978-08-31 Kraftwerk Union Ag, 4330 Muelheim Einrichtung zur Stabilisierung der Strömung durch Radialbohrungen in rotierenden Hohlzylindern, insbesondere in Hohlwellen von Gasturbinen
DE2633291C3 (de) * 1976-07-23 1981-05-14 Kraftwerk Union AG, 4330 Mülheim Gasturbinenanlage mit Kühlung durch zwei unabhängige Kühlluftströme
GB1561229A (en) * 1977-02-18 1980-02-13 Rolls Royce Gas turbine engine cooling system
FR2401320A1 (fr) * 1977-08-26 1979-03-23 Snecma Perfectionnements au refroidissement des turbines a gaz
DE3424139C2 (de) * 1984-06-30 1996-02-22 Bbc Brown Boveri & Cie Gasturbinenrotor
US4674955A (en) * 1984-12-21 1987-06-23 The Garrett Corporation Radial inboard preswirl system
FR2609500B1 (fr) * 1987-01-14 1991-04-12 Snecma Disque de compresseur de turbomachine avec accelerateur centripete pour l'aspiration d'air de refroidissement de la turbine
GB2207465B (en) * 1987-07-18 1992-02-19 Rolls Royce Plc A compressor and air bleed arrangement
IT1317538B1 (it) * 2000-05-15 2003-07-09 Nuovo Pignone Spa Dispositivo per il controllo dei flussi di refrigerazione delleturbine a gas
DE102008014957A1 (de) * 2008-03-19 2009-09-24 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenverdichter mit Zapfluftentnahme
DE102010063071A1 (de) * 2010-12-14 2012-06-14 Rolls-Royce Deutschland Ltd & Co Kg Kühlvorrichtung für ein Strahltriebwerk
US9032738B2 (en) 2012-04-25 2015-05-19 Siemens Aktiengeselischaft Gas turbine compressor with bleed path
US9528391B2 (en) 2012-07-17 2016-12-27 United Technologies Corporation Gas turbine engine outer case with contoured bleed boss

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3043561A (en) * 1958-12-29 1962-07-10 Gen Electric Turbine rotor ventilation system
DE2633291A1 (de) * 1976-07-23 1978-01-26 Kraftwerk Union Ag Gasturbinenanlage mit kuehlung durch zwei getrennte kuehlluftstroeme
DE2633222A1 (de) * 1976-07-23 1978-01-26 Kraftwerk Union Ag Gasturbinenanlage mit kuehlung der turbinenteile

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE488010A (fr) * 1947-03-11 1900-01-01
US2618433A (en) * 1948-06-23 1952-11-18 Curtiss Wright Corp Means for bleeding air from compressors
US2858101A (en) * 1954-01-28 1958-10-28 Gen Electric Cooling of turbine wheels
US2830751A (en) * 1954-04-01 1958-04-15 Bristol Aero Engines Ltd Gas turbine engines
DE1098959B (de) * 1959-06-05 1961-02-09 Licentia Gmbh Dampfturbinenlaeufer-Drehvorrichtung mit auf dem Laeufer angeordneter Drehturbine
US3099134A (en) * 1959-12-24 1963-07-30 Havilland Engine Co Ltd Combustion chambers
CH487337A (de) * 1968-01-10 1970-03-15 Sulzer Ag Anordnung für den Durchtritt von Gas durch den Mantel eines hohlen Rotors

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3043561A (en) * 1958-12-29 1962-07-10 Gen Electric Turbine rotor ventilation system
DE2633291A1 (de) * 1976-07-23 1978-01-26 Kraftwerk Union Ag Gasturbinenanlage mit kuehlung durch zwei getrennte kuehlluftstroeme
DE2633222A1 (de) * 1976-07-23 1978-01-26 Kraftwerk Union Ag Gasturbinenanlage mit kuehlung der turbinenteile

Also Published As

Publication number Publication date
CA1050775A (fr) 1979-03-20
GB1524139A (en) 1978-09-06
US4008977A (en) 1977-02-22
FR2324874B1 (fr) 1982-09-17

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Legal Events

Date Code Title Description
ST Notification of lapse