Structure for eliminating lift load bending in engine core of tu

Details Structure for eliminating lift load bending in engine core of tu Structure for eliminating lift load bending in engine core of tu

1991-09-26

1992-12-29

Peters, Jr., Joseph F.

Aeronautics and astronautics

Aircraft power plants

Mounting

248554, 60 3931, B64D 2700

Patent

active

051745259

ABSTRACT:
A structure for removing bending caused by an inlet lift load in the engine core of an aircraft having a support frame which is attached to a frame mount which connects to the pylon floor. The frame mount is located between a forward mount and a rear mount and to the front of the engine core. As a result of the frame mount, the moment created by the inlet lift load is not reacted through the engine core so engine performance is not affected.

REFERENCES:
patent: 2978209 (1961-04-01), Kerry
patent: 3318554 (1967-05-01), Ward et al.
patent: 3750983 (1973-08-01), Morris
patent: 3844115 (1974-10-01), Freid
patent: 4013246 (1977-03-01), Nightingale
patent: 4037809 (1977-07-01), Legrand
patent: 4044973 (1977-08-01), Moorehead
patent: 4266741 (1981-05-01), Murphy
patent: 4326682 (1982-04-01), Nightingale
patent: 4361296 (1982-11-01), Hall et al.
patent: 4458863 (1984-07-01), Smith
patent: 4471609 (1984-09-01), Porter et al.
patent: 4560122 (1985-12-01), Parkinson et al.
patent: 4603821 (1986-08-01), White
patent: 4683717 (1987-08-01), Naud
patent: 4742975 (1988-05-01), Pachomoff et al.
patent: 4766723 (1988-08-01), Newton
patent: 4854525 (1989-08-01), Chee
patent: 4940196 (1990-07-01), Lardellier

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