GB612272A - Improvements in or relating to mountings for gas-turbine power plants for aircraft - Google Patents

Improvements in or relating to mountings for gas-turbine power plants for aircraft

Info

Publication number
GB612272A
GB612272A GB15545/46A GB1554546A GB612272A GB 612272 A GB612272 A GB 612272A GB 15545/46 A GB15545/46 A GB 15545/46A GB 1554546 A GB1554546 A GB 1554546A GB 612272 A GB612272 A GB 612272A
Authority
GB
United Kingdom
Prior art keywords
gear
compressor
rods
shaft
box
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
GB15545/46A
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 GB15545/46A priority Critical patent/GB612272A/en
Publication of GB612272A publication Critical patent/GB612272A/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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/10—Aircraft characterised by the type or position of power plant of gas-turbine type
    • B64D27/12—Aircraft characterised by the type or position of power plant of gas-turbine type within or attached to wing

Abstract

612,272. Gas turbine plant. BRISTOL AEROPLANE CO., Ltd., MARCHANT, F. C. I., and MORGAN, W. G. May 22, 1946, No. 15545. [Class 110 (iii)] Two gas turbine units mounted side by side drive a shaft 10 through a gear-box 6 and the shaft 10 drives oppositely-rotating air-screws 13 through speed-reducing gear 11. The units are secured together by the gear-box and by bridge-pieces 17 between the compressor casings and the whole is supported in the wing of an aeroplane by four rods 20 pivotally attached to the units in the same transverse plane and pivotally attached to the wing ribs 9. A bracket 28 bolted to one compressor casing has a sliding engagement, with both radial and transverse freedom, with one of two pillars 29 secured to the ribs 9 and a bracket 27, Fig. 2, secured to the other compressor casing carries a pin 31 having lengthwise freedom in the other pillar 29. The gear-box structure 11 which supports the forward end of the shaft 10 and the air-screw shafts is carried by rods 24 pivoted to the structure 11 and to the compressor casings. The pivotal connections of all the rods to the compressor casings may be by means of trough-shaped rings bolted to and embracing the flanges of the compressor casings.
GB15545/46A 1946-05-22 1946-05-22 Improvements in or relating to mountings for gas-turbine power plants for aircraft Expired GB612272A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB15545/46A GB612272A (en) 1946-05-22 1946-05-22 Improvements in or relating to mountings for gas-turbine power plants for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB15545/46A GB612272A (en) 1946-05-22 1946-05-22 Improvements in or relating to mountings for gas-turbine power plants for aircraft

Publications (1)

Publication Number Publication Date
GB612272A true GB612272A (en) 1948-11-10

Family

ID=10061034

Family Applications (1)

Application Number Title Priority Date Filing Date
GB15545/46A Expired GB612272A (en) 1946-05-22 1946-05-22 Improvements in or relating to mountings for gas-turbine power plants for aircraft

Country Status (1)

Country Link
GB (1) GB612272A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7806363B2 (en) 2004-08-19 2010-10-05 Rolls-Royce Plc Engine mounting assembly

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7806363B2 (en) 2004-08-19 2010-10-05 Rolls-Royce Plc Engine mounting assembly

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