Engine mounting assembly

Details Engine mounting assembly Engine mounting assembly

2005-07-25

2010-10-05

Collins, Timothy D (Department: 3644)

Aeronautics and astronautics

Aircraft power plants

Mounting

C244S05300R, C248S554000, C248S555000, C248S556000

Reexamination Certificate

active

07806363

ABSTRACT:
An engine mounting assembly for an engine, e.g. a gas turbine engine comprises a plurality of carrying arrangements. Each carrying arrangement comprises a rear load absorbing assembly. Each load absorbing assembly provides a rear mounting point for an engine carrier. Each carrying arrangement further comprises first and second stabilising members extending forwardly from the rear mounting point of the rear load absorbing assembly to first and second spaced forward mounting points for an engine carrier.

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Fig. 23-11 Typical turbo-jet engine mountings; ‘The Jet Engine’, Rolls-Royce plc 1986 5th Edition, pp248.
Applicant's Trent 800 mounting system which essentially is a more detailed version of the left hand figure of Fig. 23-11.

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