FR2083468B3 - - Google Patents

Info

Publication number
FR2083468B3
FR2083468B3 FR7109814A FR7109814A FR2083468B3 FR 2083468 B3 FR2083468 B3 FR 2083468B3 FR 7109814 A FR7109814 A FR 7109814A FR 7109814 A FR7109814 A FR 7109814A FR 2083468 B3 FR2083468 B3 FR 2083468B3
Authority
FR
France
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
FR7109814A
Other versions
FR2083468A3 (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.)
MINI AVIAT SUPPLY
Original Assignee
MINI AVIAT SUPPLY
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 MINI AVIAT SUPPLY filed Critical MINI AVIAT SUPPLY
Publication of FR2083468A3 publication Critical patent/FR2083468A3/fr
Application granted granted Critical
Publication of FR2083468B3 publication Critical patent/FR2083468B3/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • 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
FR7109814A 1970-03-20 1971-03-19 Expired FR2083468B3 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1357670 1970-03-20

Publications (2)

Publication Number Publication Date
FR2083468A3 FR2083468A3 (fr) 1971-12-17
FR2083468B3 true FR2083468B3 (fr) 1973-12-28

Family

ID=10025475

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7109814A Expired FR2083468B3 (fr) 1970-03-20 1971-03-19

Country Status (3)

Country Link
US (1) US3726087A (fr)
FR (1) FR2083468B3 (fr)
GB (1) GB1315856A (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4315405A (en) * 1978-12-09 1982-02-16 Rolls-Royce Limited Combustion apparatus
GB2118710B (en) * 1981-12-31 1985-05-22 Secr Defence Improvements in or relating to combustion chamber wall cooling
US5131221A (en) * 1989-12-21 1992-07-21 Sundstrand Corporation Injector carbon screen
US5113648A (en) * 1990-02-28 1992-05-19 Sundstrand Corporation Combustor carbon screen
US5918465A (en) * 1995-02-03 1999-07-06 Bmw Rolls-Royce Gmbh Flow guiding body for a gas turbine combustion chamber
DE19503567A1 (de) * 1995-02-03 1996-08-08 Bmw Rolls Royce Gmbh Ringdiffusor für eine Gasturbinen-Brennkammer
DE19720786A1 (de) * 1997-05-17 1998-11-19 Abb Research Ltd Brennkammer
US9366438B2 (en) * 2013-02-14 2016-06-14 Siemens Aktiengesellschaft Flow sleeve inlet assembly in a gas turbine engine

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR393022A (fr) * 1908-08-07 1908-12-11 Simon Mery Dispositifs de sécurité pour éviter l'inflammation des milieux combustibles par les gaz d'échappement des moteurs à explosion
FR674840A (fr) * 1928-09-21 1930-02-03 Air Securite Ets Dispositif empêchant la propagation des flammes dans les conduites d'aspiration des moteurs à explosion et autres applications
US2616257A (en) * 1946-01-09 1952-11-04 Bendix Aviat Corp Combustion chamber with air inlet means providing a plurality of concentric strata of varying velocities
FR1006128A (fr) * 1947-11-19 1952-04-21 Dispositif d'alimentation et de combustion pour turbines à gaz et turbo-réacteurs
NL71705C (fr) * 1947-12-04
US2547959A (en) * 1948-01-27 1951-04-10 Westinghouse Electric Corp Centrifugal fuel feeding system for annular combustion chambers
US2716330A (en) * 1950-06-24 1955-08-30 Westinghouse Electric Corp Combustion apparatus having primary air preheating ducts
US2825203A (en) * 1951-08-03 1958-03-04 Snecma Aerodynamic valves
US2775094A (en) * 1953-12-03 1956-12-25 Gen Electric End cap for fluid fuel combustor
US3058306A (en) * 1961-03-24 1962-10-16 Schlumbohm Peter Gas turbine motor and inlet wall structure therefor
US3516253A (en) * 1967-07-31 1970-06-23 Davies Allport Combustion system for producing high temperature and high pressure gas
DE1932881C3 (de) * 1969-06-28 1978-06-29 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Brennkammer für Gasturbinentriebwerke

Also Published As

Publication number Publication date
US3726087A (en) 1973-04-10
GB1315856A (en) 1973-05-02
FR2083468A3 (fr) 1971-12-17

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Legal Events

Date Code Title Description
ST Notification of lapse