FR1396944A - Dispositif de commande d'entrée d'air, notamment pour aéronefs supersoniques - Google Patents

Dispositif de commande d'entrée d'air, notamment pour aéronefs supersoniques

Info

Publication number
FR1396944A
FR1396944A FR976586A FR976586A FR1396944A FR 1396944 A FR1396944 A FR 1396944A FR 976586 A FR976586 A FR 976586A FR 976586 A FR976586 A FR 976586A FR 1396944 A FR1396944 A FR 1396944A
Authority
FR
France
Prior art keywords
control device
air intake
intake control
supersonic aircraft
supersonic
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
FR976586A
Other languages
English (en)
Inventor
Milton Marcus
David Raymond Pearl
Robert Dwight Porter
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 Aircraft 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 Aircraft Corp filed Critical United Aircraft Corp
Application granted granted Critical
Publication of FR1396944A publication Critical patent/FR1396944A/fr
Expired 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/057—Control or regulation
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S367/00—Communications, electrical: acoustic wave systems and devices
    • Y10S367/906—Airborne shock-wave detection

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Fluid-Driven Valves (AREA)
FR976586A 1964-05-15 1964-05-30 Dispositif de commande d'entrée d'air, notamment pour aéronefs supersoniques Expired FR1396944A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB20259/64A GB1059465A (en) 1964-05-15 1964-05-15 Control system for the variable aperture air inlet of an air breathing engine

Publications (1)

Publication Number Publication Date
FR1396944A true FR1396944A (fr) 1965-04-23

Family

ID=10143032

Family Applications (1)

Application Number Title Priority Date Filing Date
FR976586A Expired FR1396944A (fr) 1964-05-15 1964-05-30 Dispositif de commande d'entrée d'air, notamment pour aéronefs supersoniques

Country Status (3)

Country Link
US (1) US3181818A (fr)
FR (1) FR1396944A (fr)
GB (1) GB1059465A (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3533238A (en) * 1968-12-23 1970-10-13 Gen Electric Inlet control system
US4879895A (en) * 1988-08-29 1989-11-14 Mcdonnell Douglas Corporation Normal shock locator
US5806301A (en) * 1995-12-11 1998-09-15 United Technologies Corporation Ramjet/scramjet inlet isolator unstart prevention
US6209821B1 (en) 1999-09-14 2001-04-03 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Apparatus and method for measuring air temperature ahead of an aircraft for controlling a variable inlet/engine assembly
GB0510440D0 (en) 2005-05-21 2005-06-29 Rolls Royce Plc An instrumentation rake
GB201307004D0 (en) * 2013-04-18 2013-05-29 Rolls Royce Plc An air intake and a method of controlling the same
FR3023871B1 (fr) * 2014-07-18 2019-03-29 Safran Aircraft Engines Procede de commande d'un actionneur bistable pour moteur d'aeronef
US9878778B2 (en) * 2014-08-14 2018-01-30 Gulfstream Aerospace Corporation System and method for controlling a pressure field around an aircraft in flight

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2638738A (en) * 1951-03-22 1953-05-19 Jr Robert M Salter Ramjet engine having inlet cone diffuser automatically adjustable as to length and cone angle
US2969939A (en) * 1956-07-30 1961-01-31 North American Aviation Inc Asymmetrically variable supersonic inlet system
US2920446A (en) * 1957-04-23 1960-01-12 United Aircraft Corp Shock positioning means
US2934893A (en) * 1957-05-06 1960-05-03 Westinghouse Electric Corp Air intake structure for an aircraft engine
US2997843A (en) * 1958-04-23 1961-08-29 Bendix Corp Inlet control system for supersonic aircraft
US2971328A (en) * 1958-07-22 1961-02-14 United Aircraft Corp Control system for air inlet bypass
US3102387A (en) * 1959-04-20 1963-09-03 Curtiss Wright Corp Shock positioning control system

Also Published As

Publication number Publication date
GB1059465A (en) 1967-02-22
US3181818A (en) 1965-05-04

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