GB638539A - Improvements in or relating to mounting structures for gas-turbine engines - Google Patents

Improvements in or relating to mounting structures for gas-turbine engines

Info

Publication number
GB638539A
GB638539A GB660448A GB660448A GB638539A GB 638539 A GB638539 A GB 638539A GB 660448 A GB660448 A GB 660448A GB 660448 A GB660448 A GB 660448A GB 638539 A GB638539 A GB 638539A
Authority
GB
United Kingdom
Prior art keywords
air
aeroplane
plant
nacelle
shell
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
GB660448A
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.)
Bristol Aeroplane Co Ltd
Original Assignee
Bristol Aeroplane Co Ltd
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 Bristol Aeroplane Co Ltd filed Critical Bristol Aeroplane Co Ltd
Priority to GB660448A priority Critical patent/GB638539A/en
Publication of GB638539A publication Critical patent/GB638539A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Supercharger (AREA)

Abstract

638,539. Mounting aero-engines. BRISTOL AEROPLANE CO., Ltd., and MARCHANT, F. C. I. March 2, 1948, No. 6604. [Class 4] [Also in Group XXVI] A gas turbine plant for aircraft is supported by a unitary tubular structure 21 which is bolted at its forward end to a flange 20 of the air compressor and is secured at its rearward end to the air frame. When the plant is carried by an aeroplane wing, Fig. 3, air is taken in through ports 32 in the leading edge and passes through ducts 31 and a semi-circular opening 33 in the end of the chamber 49. The plant is enclosed in a nacelle 19 eccentric to the shell 21 and air-coolers and an oil tank are housed in the space below the shell. A tunnel 44 is also provided in this space for electric cables and oil, fuel and air pipes. The aeroplane undercarriage retracts into the nacelle and is provided with two spaced wheels which lie on either side of a flattened exhaust pipe 18.
GB660448A 1948-03-02 1948-03-02 Improvements in or relating to mounting structures for gas-turbine engines Expired GB638539A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB660448A GB638539A (en) 1948-03-02 1948-03-02 Improvements in or relating to mounting structures for gas-turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB660448A GB638539A (en) 1948-03-02 1948-03-02 Improvements in or relating to mounting structures for gas-turbine engines

Publications (1)

Publication Number Publication Date
GB638539A true GB638539A (en) 1950-06-07

Family

ID=9817499

Family Applications (1)

Application Number Title Priority Date Filing Date
GB660448A Expired GB638539A (en) 1948-03-02 1948-03-02 Improvements in or relating to mounting structures for gas-turbine engines

Country Status (1)

Country Link
GB (1) GB638539A (en)

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