CH320997A - Einrichtung zum Befestigen eines Triebwerkes aussen an einem Flugzeugteil - Google Patents

Einrichtung zum Befestigen eines Triebwerkes aussen an einem Flugzeugteil

Info

Publication number
CH320997A
CH320997A CH320997DA CH320997A CH 320997 A CH320997 A CH 320997A CH 320997D A CH320997D A CH 320997DA CH 320997 A CH320997 A CH 320997A
Authority
CH
Switzerland
Prior art keywords
attaching
engine
outside
aircraft part
aircraft
Prior art date
Application number
Other languages
English (en)
Inventor
Hector Kent Nelson
Original Assignee
Rolls Royce
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 filed Critical Rolls Royce
Publication of CH320997A publication Critical patent/CH320997A/de

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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
CH320997D 1953-03-04 1954-03-04 Einrichtung zum Befestigen eines Triebwerkes aussen an einem Flugzeugteil CH320997A (de)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
GB320997X 1953-03-04
GB319069X 1953-03-12
GB130753X 1953-07-13
GB260254X 1954-02-26

Publications (1)

Publication Number Publication Date
CH320997A true CH320997A (de) 1957-04-15

Family

ID=27448178

Family Applications (1)

Application Number Title Priority Date Filing Date
CH320997D CH320997A (de) 1953-03-04 1954-03-04 Einrichtung zum Befestigen eines Triebwerkes aussen an einem Flugzeugteil

Country Status (2)

Country Link
CH (1) CH320997A (de)
GB (1) GB743205A (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4422288A (en) * 1981-03-02 1983-12-27 General Electric Company Aft mounting system for combustion transition duct members
FR3058127B1 (fr) 2016-10-28 2022-02-25 Safran Aircraft Engines Assemblage entre un pylone d'aeronef et une turbomachine

Also Published As

Publication number Publication date
GB743205A (en) 1956-01-11

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