GB843359A - Improvements in or relating to power plant installations for aircraft - Google Patents

Improvements in or relating to power plant installations for aircraft

Info

Publication number
GB843359A
GB843359A GB27689/57A GB2768957A GB843359A GB 843359 A GB843359 A GB 843359A GB 27689/57 A GB27689/57 A GB 27689/57A GB 2768957 A GB2768957 A GB 2768957A GB 843359 A GB843359 A GB 843359A
Authority
GB
United Kingdom
Prior art keywords
fairing
engine
housed
aircraft
auxiliary units
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
GB27689/57A
Inventor
Thomas Henry Kerry
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 GB27689/57A priority Critical patent/GB843359A/en
Publication of GB843359A publication Critical patent/GB843359A/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
    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)

Abstract

843,359. Aircraft. ROLLS-ROYCE Ltd. Aug. 15, 1958 [Sept. 2, 1957], No. 27689/57. Class 4. [Also in Group XXVI] A jet-propulsion engine is mounted on an aircraft wing by a faired strut, wherein is housed all of the engine driven auxiliary units. The wing spars 10 carry a structure 19 enclosed within a fairing 26 and having detachable connections 19a, 19b for a gas turbine engine 13 housed within a nacelle 18. The engine has a readily-disconnected connection to a shaft 32 driving auxiliary units which are housed in the fairing 26 instead of the more usual location within fairing 18. Such auxiliary units comprise a main fuel pump 27, a booster pump 28, an electric motor 29 and a tachometer 30, grouped about and mounted on a gearbox 31 driven by shaft 32. A fuel supply control unit 33, also mounted in the fairing 26, supplies fuel to the engine through a readily-disconnected pipe 34. An engine oil sump 20a is mounted in the front portion of fairing 18 adjacent air intake 18a. In an alternative embodiment, the fairing 18 is dispensed with and the engine casing constitutes the nacelle wall.
GB27689/57A 1957-09-02 1957-09-02 Improvements in or relating to power plant installations for aircraft Expired GB843359A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB27689/57A GB843359A (en) 1957-09-02 1957-09-02 Improvements in or relating to power plant installations for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB27689/57A GB843359A (en) 1957-09-02 1957-09-02 Improvements in or relating to power plant installations for aircraft

Publications (1)

Publication Number Publication Date
GB843359A true GB843359A (en) 1960-08-04

Family

ID=10263702

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27689/57A Expired GB843359A (en) 1957-09-02 1957-09-02 Improvements in or relating to power plant installations for aircraft

Country Status (1)

Country Link
GB (1) GB843359A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4318516A (en) * 1978-05-30 1982-03-09 Greenmeadow Engineers Limited Attachment of masses to aircraft and spacecraft
EP2065585A2 (en) 2007-11-30 2009-06-03 United Technologies Corporation Gas turbine engine with pylon mounted accessory drive
EP2009261A3 (en) * 2007-06-28 2012-01-11 United Technologies Corporation Engine accessory drive system for a gasturbine
RU2522208C1 (en) * 2012-01-17 2014-07-10 Юнайтед Текнолоджис Корпорейшн Gas turbine engine pylon assembly and gas turbine engine system
EP2872762A4 (en) * 2012-07-13 2015-08-12 United Technologies Corp Mid-turbine frame with oil system mounts
CN117382890A (en) * 2023-10-24 2024-01-12 湖南山河华宇航空科技有限公司 Aeroengine mounting frame and aircraft

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4318516A (en) * 1978-05-30 1982-03-09 Greenmeadow Engineers Limited Attachment of masses to aircraft and spacecraft
EP2009261A3 (en) * 2007-06-28 2012-01-11 United Technologies Corporation Engine accessory drive system for a gasturbine
EP2065585A2 (en) 2007-11-30 2009-06-03 United Technologies Corporation Gas turbine engine with pylon mounted accessory drive
EP2065585A3 (en) * 2007-11-30 2012-06-06 United Technologies Corporation Gas turbine engine with pylon mounted accessory drive
US9719428B2 (en) 2007-11-30 2017-08-01 United Technologies Corporation Gas turbine engine with pylon mounted accessory drive
RU2522208C1 (en) * 2012-01-17 2014-07-10 Юнайтед Текнолоджис Корпорейшн Gas turbine engine pylon assembly and gas turbine engine system
EP2872762A4 (en) * 2012-07-13 2015-08-12 United Technologies Corp Mid-turbine frame with oil system mounts
CN117382890A (en) * 2023-10-24 2024-01-12 湖南山河华宇航空科技有限公司 Aeroengine mounting frame and aircraft

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