FR967640A - Mounting and fixing of a turbo-propeller in the airframe of an airplane - Google Patents

Mounting and fixing of a turbo-propeller in the airframe of an airplane

Info

Publication number
FR967640A
FR967640A FR967640DA FR967640A FR 967640 A FR967640 A FR 967640A FR 967640D A FR967640D A FR 967640DA FR 967640 A FR967640 A FR 967640A
Authority
FR
France
Prior art keywords
airframe
airplane
turbo
propeller
fixing
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
Other languages
French (fr)
Inventor
Hermann Oestrich
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
Application granted granted Critical
Publication of FR967640A publication Critical patent/FR967640A/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; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • 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
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR967640D 1948-06-03 1948-06-03 Mounting and fixing of a turbo-propeller in the airframe of an airplane Expired FR967640A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR967640T 1948-06-03

Publications (1)

Publication Number Publication Date
FR967640A true FR967640A (en) 1950-11-08

Family

ID=9500769

Family Applications (1)

Application Number Title Priority Date Filing Date
FR967640D Expired FR967640A (en) 1948-06-03 1948-06-03 Mounting and fixing of a turbo-propeller in the airframe of an airplane

Country Status (1)

Country Link
FR (1) FR967640A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1078878B (en) * 1956-07-30 1960-03-31 Snecma Device for mounting an engine
DE1126256B (en) * 1958-11-26 1962-03-22 Rolls Royce Bearing ring for a gas turbine jet engine
DE1162199B (en) * 1960-05-18 1964-01-30 Rolls Royce Turbine lift jet engine installed with vertical axis in the aircraft
US3352114A (en) * 1965-07-17 1967-11-14 Rolls Royce Mounting means for separately supporting a gas turbine engine and a jet pipe in an engine pod
US3675418A (en) * 1970-11-19 1972-07-11 United Aircraft Corp Jet engine force frame
FR2309402A1 (en) * 1975-04-29 1976-11-26 Gen Electric SYSTEM FOR MOUNTING AN ENGINE ON THE STRUCTURE OF AN AIRCRAFT
US4013246A (en) * 1974-12-24 1977-03-22 Rolls-Royce (1971) Limited Mounting bypass gas turbines engines on aircraft
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet
WO1996020111A1 (en) * 1994-12-23 1996-07-04 United Technologies Corporation A mounting arrangement for a gas turbine engine
JP2002173094A (en) * 2000-06-30 2002-06-18 General Electric Co <Ge> Link part for aircraft engine fixing system

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1078878B (en) * 1956-07-30 1960-03-31 Snecma Device for mounting an engine
DE1126256B (en) * 1958-11-26 1962-03-22 Rolls Royce Bearing ring for a gas turbine jet engine
DE1162199B (en) * 1960-05-18 1964-01-30 Rolls Royce Turbine lift jet engine installed with vertical axis in the aircraft
US3352114A (en) * 1965-07-17 1967-11-14 Rolls Royce Mounting means for separately supporting a gas turbine engine and a jet pipe in an engine pod
US3675418A (en) * 1970-11-19 1972-07-11 United Aircraft Corp Jet engine force frame
US4013246A (en) * 1974-12-24 1977-03-22 Rolls-Royce (1971) Limited Mounting bypass gas turbines engines on aircraft
FR2309402A1 (en) * 1975-04-29 1976-11-26 Gen Electric SYSTEM FOR MOUNTING AN ENGINE ON THE STRUCTURE OF AN AIRCRAFT
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet
WO1996020111A1 (en) * 1994-12-23 1996-07-04 United Technologies Corporation A mounting arrangement for a gas turbine engine
JP2002173094A (en) * 2000-06-30 2002-06-18 General Electric Co <Ge> Link part for aircraft engine fixing system

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