Mounting arrangement for a gas turbine engine

Details Mounting arrangement for a gas turbine engine Mounting arrangement for a gas turbine engine

1996-11-01

1998-07-07

Mojica, Virna Lissi

Aeronautics and astronautics

Aircraft power plants

Mounting

248555, 248556, 248557, B64D 2726, F16M 100

Patent

active

057756384

ABSTRACT:
A linkage arrangement (20) joins a nacelle (12) enclosing a gas turbine engine (10) and a pylon (18) suspended from an aircraft wing. The linkage arrangement (20) counteracts the deflections of the nacelle (12) with respect to the free air stream due to the aerodynamic load. The linkage arrangement (20) includes a plurality of links (22, 24, 32, 34) that substantially duplicate the motion of a four bar linkage mechanism.

REFERENCES:
patent: 3003718 (1961-10-01), Peterson
patent: 4326682 (1982-04-01), Nightingale
patent: 4458863 (1984-07-01), Smith
patent: 4560122 (1985-12-01), Parkinson et al.
patent: 4717094 (1988-01-01), Chee
patent: 5078342 (1992-01-01), Langley et al.
patent: 5181675 (1993-01-01), Lardellier et al.
patent: 5197692 (1993-03-01), Jones et al.
patent: 5227382 (1993-07-01), Seelen et al.
patent: 5320307 (1994-06-01), Spofford et al.

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