BE743399A - - Google Patents

Info

Publication number
BE743399A
BE743399A BE743399DA BE743399A BE 743399 A BE743399 A BE 743399A BE 743399D A BE743399D A BE 743399DA BE 743399 A BE743399 A BE 743399A
Authority
BE
Belgium
Application number
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 filed Critical
Publication of BE743399A publication Critical patent/BE743399A/xx

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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]
    • Y10T137/0645—With condition responsive control means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)
BE743399D 1968-12-23 1969-12-19 BE743399A (xx)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US78607768A 1968-12-23 1968-12-23

Publications (1)

Publication Number Publication Date
BE743399A true BE743399A (xx) 1970-05-28

Family

ID=25137529

Family Applications (1)

Application Number Title Priority Date Filing Date
BE743399D BE743399A (xx) 1968-12-23 1969-12-19

Country Status (5)

Country Link
US (1) US3533238A (xx)
BE (1) BE743399A (xx)
DE (1) DE1964056A1 (xx)
FR (1) FR2026964A1 (xx)
GB (1) GB1285086A (xx)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113945355A (zh) * 2021-09-21 2022-01-18 中国航空工业集团公司西安飞机设计研究所 一种冲击波下的进气道风洞试验模拟系统

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4025008A (en) * 1973-11-27 1977-05-24 Messerschmitt-Bolkow-Blohm Gmbh Intake control for air utilizing aircraft engines
US3911260A (en) * 1974-05-30 1975-10-07 Nasa Shock position sensor for supersonic inlets
US4186556A (en) * 1975-05-29 1980-02-05 General Electric Company Compressor bleed biased acceleration schedule
JPS51143117A (en) * 1975-06-04 1976-12-09 Toyota Motor Corp Surge control system of gas turbine engine
US3977182A (en) * 1975-06-20 1976-08-31 General Motors Corporation Gas turbine control
US4130872A (en) * 1975-10-10 1978-12-19 The United States Of America As Represented By The Secretary Of The Air Force Method and system of controlling a jet engine for avoiding engine surge
US4509325A (en) * 1978-12-28 1985-04-09 The United States Of America As Represented By The Secretary Of The Navy Turbine engine cold temperature starting system
FR2698911B1 (fr) * 1992-12-09 1995-01-06 Snecma Agencement de moteur d'avion.
US5437151A (en) * 1993-08-20 1995-08-01 United Technologies Corporation Detecting and controlling supersonic airflow normal shock pattern position in an aircraft jet engine assembly
FR2879564B1 (fr) * 2004-12-20 2008-05-16 Airbus France Sas Agencement d'entree d'air de ventilation a element d'obturation mobile
US9957060B2 (en) * 2012-03-21 2018-05-01 Hamilton Sundstrand Corporation Deployable inlet scoop for an inboard ram air turbine
US20140331682A1 (en) * 2012-11-08 2014-11-13 Mark Bovankovich High-speed-launch ramjet booster

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2989846A (en) * 1958-02-12 1961-06-27 Lear Inc Shock wave sensing device
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
US2971330A (en) * 1959-07-20 1961-02-14 United Aircraft Corp Air-inlet shock controller
US2971329A (en) * 1959-07-20 1961-02-14 United Aircraft Corp Air-inlet controller
US3139922A (en) * 1959-10-19 1964-07-07 Bendix Corp Compensated controller
GB932844A (en) * 1960-03-07 1963-07-31 Rolls Royce Improvements in or relating to air intakes for supersonic aircraft
GB1042140A (en) * 1962-11-12 1966-09-14 Dehavilland Aircraft Improvements in or relating to pulse train generators
US3172622A (en) * 1962-12-19 1965-03-09 United Aircraft Corp Air inlet control with afterburner anticipator
US3181818A (en) * 1964-05-15 1965-05-04 United Aircraft Corp Shock wave position controller

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113945355A (zh) * 2021-09-21 2022-01-18 中国航空工业集团公司西安飞机设计研究所 一种冲击波下的进气道风洞试验模拟系统
CN113945355B (zh) * 2021-09-21 2024-01-30 中国航空工业集团公司西安飞机设计研究所 一种冲击波下的进气道风洞试验模拟系统

Also Published As

Publication number Publication date
US3533238A (en) 1970-10-13
GB1285086A (en) 1972-08-09
FR2026964A1 (xx) 1970-09-25
DE1964056A1 (de) 1970-07-02

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