Aircraft engine mount

Aeronautics and astronautics – Aircraft power plants – Mounting

Patent

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Details

60 39031, 248555, 248554, B64D 2700, F02C 720

Patent

active

052753573

ABSTRACT:
An aircraft engine mount includes a frame fixedly joined in a gas turbine engine and a platform fixedly joined to an aircraft wing or tail pylon. A first beam is pivotally joined to the frame and the platform at first and second joints, respectively. The first beam is additionally joined to the platform at a third joint which allows longitudinal movement between the first beam and the platform at the third joint while preventing rotation of the first beam. A second beam is spaced from the first beam and is pivotally joined to the frame and platform at fourth and fifth joints, respectively, and is additionally joined to the platform at a sixth joint for allowing limited rotation of the second beam during normal operation while preventing rotation of the second beam upon a failure of the first beam to carry load.

REFERENCES:
patent: 3042349 (1962-07-01), Pirtle et al.
patent: 3809340 (1974-05-01), Dolgy et al.
patent: 4326682 (1982-04-01), Nightingale
patent: 4603822 (1986-08-01), Chee
patent: 4717094 (1988-01-01), Chee
patent: 4725019 (1988-02-01), White
patent: 4742975 (1988-05-01), Pachomoff et al.
patent: 4943013 (1990-07-01), Kapala et al.
patent: 5078342 (1992-01-01), Langley et al.
M. H. Schneider, GE Airline Review Team, GE 90 Nacelle Structures, Aftmount.
General Electric Company, CF6-80C2 aft engine mount drawing, in production for more than one year, single drawing sheet, FIG. 2.3.
Boeing, "777 Propulsion Design Review GE90 Strut Structure and Fairings," Feb. '91, five pages.

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