Aircraft engine mounting

Details Aircraft engine mounting Aircraft engine mounting

2005-03-29

2005-03-29

Carone, Michael J. (Department: 3641)

Aeronautics and astronautics

Aircraft power plants

Mounting

C244S055000

Reexamination Certificate

active

06871820

ABSTRACT:
An aircraft engine mounting installation uses an overall partially focalized or convergent mount configuration with a combination of individual, or paired, axial mounts and individual, or paired, inclined mounts. When paired, the axial mount axes are parallel to the engine thrust axis. The respective axes of the axial and inclined mounts, or planes through paired similar mounts, converge at, or ahead of, the engine center of gravity in order to brace engine weight, engine thrust and torque reaction loads, without undue complexity in mount geometry.

REFERENCES:
patent: 5409184 (1995-04-01), Udall et al.
patent: 6123293 (2000-09-01), Breitbach et al.
patent: 6398161 (2002-06-01), Jule et al.
patent: 6581874 (2003-06-01), Lemire et al.
patent: 554860 (1942-10-01), None
patent: 548527 (1943-07-01), None

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