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FR1356718A - Improvements to the installation of jet engines in engine spans - Google Patents

Improvements to the installation of jet engines in engine spans

Info

Publication number
FR1356718A
FR1356718A FR934631A FR934631A FR1356718A FR 1356718 A FR1356718 A FR 1356718A FR 934631 A FR934631 A FR 934631A FR 934631 A FR934631 A FR 934631A FR 1356718 A FR1356718 A FR 1356718A
Authority
FR
France
Prior art keywords
installation
jet engines
spans
engine
engine spans
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
FR934631A
Other languages
French (fr)
Inventor
Ernest Edward Chilvers
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
Priority claimed from GB18948/62A external-priority patent/GB969806A/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to FR934631A priority Critical patent/FR1356718A/en
Application granted granted Critical
Publication of FR1356718A publication Critical patent/FR1356718A/en
Expired legal-status Critical Current

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
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/0058—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors with vertical jet
    • 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
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR934631A 1962-05-16 1963-05-13 Improvements to the installation of jet engines in engine spans Expired FR1356718A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR934631A FR1356718A (en) 1962-05-16 1963-05-13 Improvements to the installation of jet engines in engine spans

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB18948/62A GB969806A (en) 1962-05-16 1962-05-16 Improvements relating to the installation of jet engines in engine bays
FR934631A FR1356718A (en) 1962-05-16 1963-05-13 Improvements to the installation of jet engines in engine spans

Publications (1)

Publication Number Publication Date
FR1356718A true FR1356718A (en) 1964-03-27

Family

ID=26201292

Family Applications (1)

Application Number Title Priority Date Filing Date
FR934631A Expired FR1356718A (en) 1962-05-16 1963-05-13 Improvements to the installation of jet engines in engine spans

Country Status (1)

Country Link
FR (1) FR1356718A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3043751A1 (en) * 2015-11-12 2017-05-19 Snecma SUPPORTING AND GUIDING MEMBER OF AN AIRCRAFT TURBOMACHINE DURING ITS INSTALLATION OR REMOVAL

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3043751A1 (en) * 2015-11-12 2017-05-19 Snecma SUPPORTING AND GUIDING MEMBER OF AN AIRCRAFT TURBOMACHINE DURING ITS INSTALLATION OR REMOVAL

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