FR1234559A - Improvements made to the inlets for fluids flowing at supersonic speeds, in particular to the air inlets for stato and turbo-reactors - Google Patents

Improvements made to the inlets for fluids flowing at supersonic speeds, in particular to the air inlets for stato and turbo-reactors

Info

Publication number
FR1234559A
FR1234559A FR804254A FR804254A FR1234559A FR 1234559 A FR1234559 A FR 1234559A FR 804254 A FR804254 A FR 804254A FR 804254 A FR804254 A FR 804254A FR 1234559 A FR1234559 A FR 1234559A
Authority
FR
France
Prior art keywords
inlets
stato
turbo
reactors
improvements made
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
FR804254A
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development Ltd
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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Application granted granted Critical
Publication of FR1234559A publication Critical patent/FR1234559A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
FR804254A 1958-09-04 1959-09-03 Improvements made to the inlets for fluids flowing at supersonic speeds, in particular to the air inlets for stato and turbo-reactors Expired FR1234559A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB28497/58A GB879956A (en) 1958-09-04 1958-09-04 Intakes for fluid flowing at supersonic velocities

Publications (1)

Publication Number Publication Date
FR1234559A true FR1234559A (en) 1960-10-18

Family

ID=10276572

Family Applications (1)

Application Number Title Priority Date Filing Date
FR804254A Expired FR1234559A (en) 1958-09-04 1959-09-03 Improvements made to the inlets for fluids flowing at supersonic speeds, in particular to the air inlets for stato and turbo-reactors

Country Status (3)

Country Link
DE (1) DE1112902B (en)
FR (1) FR1234559A (en)
GB (1) GB879956A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0810357A1 (en) * 1996-05-28 1997-12-03 Lockheed Martin Corporation Diverting boundary layer air

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8393158B2 (en) 2007-10-24 2013-03-12 Gulfstream Aerospace Corporation Low shock strength inlet

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0810357A1 (en) * 1996-05-28 1997-12-03 Lockheed Martin Corporation Diverting boundary layer air

Also Published As

Publication number Publication date
DE1112902B (en) 1961-08-17
GB879956A (en) 1961-10-11

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