Horizontally opposed trunnion forward engine mount system suppor

Aeronautics and astronautics – Aircraft power plants – Mounting

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Details

248554, B64D 2700

Patent

active

061261106

ABSTRACT:
The present invention relates to an engine mount assembly for supporting an aircraft engine in aft-cantilevered position beneath the aircraft wing. The assembly includes a pair forward engine mounts positioned on opposite sides of an integrally formed yoke member wrapped about the upper half of the engine casing. Each side of the yoke is preferably configured as an A-shaped frame member with the bottom portions joining each other and the pylon. To prevent "backbone bending" of the engine trunnion assembly, the forward engine mounts supported at opposite ends of the yoke engage the casing along its centerline. The trunnion assembly is preferably constructed of high strength titanium machined and/or forged.

REFERENCES:
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patent: 5238206 (1993-08-01), Pachomoff
patent: 5474258 (1995-12-01), Taylor et al.

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