FR1295287A - Auxiliary compressor installed near the air intake of a turbo-engine - Google Patents

Auxiliary compressor installed near the air intake of a turbo-engine

Info

Publication number
FR1295287A
FR1295287A FR868356A FR868356A FR1295287A FR 1295287 A FR1295287 A FR 1295287A FR 868356 A FR868356 A FR 868356A FR 868356 A FR868356 A FR 868356A FR 1295287 A FR1295287 A FR 1295287A
Authority
FR
France
Prior art keywords
turbo
engine
air intake
installed near
auxiliary compressor
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
FR868356A
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to FR868356A priority Critical patent/FR1295287A/en
Application granted granted Critical
Publication of FR1295287A publication Critical patent/FR1295287A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/12—Plants including a gas turbine driving a compressor or a ducted fan characterised by having more than one gas turbine
FR868356A 1961-07-19 1961-07-19 Auxiliary compressor installed near the air intake of a turbo-engine Expired FR1295287A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR868356A FR1295287A (en) 1961-07-19 1961-07-19 Auxiliary compressor installed near the air intake of a turbo-engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR868356A FR1295287A (en) 1961-07-19 1961-07-19 Auxiliary compressor installed near the air intake of a turbo-engine

Publications (1)

Publication Number Publication Date
FR1295287A true FR1295287A (en) 1962-06-01

Family

ID=8759603

Family Applications (1)

Application Number Title Priority Date Filing Date
FR868356A Expired FR1295287A (en) 1961-07-19 1961-07-19 Auxiliary compressor installed near the air intake of a turbo-engine

Country Status (1)

Country Link
FR (1) FR1295287A (en)

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