This invention relates to engine mountings and the object of the invention is to provide a resilient mounting positioned between an engine and its supporting frame and arranged to allow slight vertical and horizontal movement of the engine in relation to its frame. Another object of the invention...

An engine mounting system where an aft body mounted counter-rotation prop fan engine is mounted to aircraft structure. The engine is connected through a longitudinally extending beam to a mounting strut structure comprising a fore spar, a mid spar and a rear spar. Vertical loads and lateral loads are transmitted from the engine to the beam at forward and rear locations, and these vertical and lateral loads are in turn transmitted to the spars at forward and rear locations. The torque loads from the engine are transmitted at a selected location into the beam, and then transmitted through the beam to the spar or spars at a selected location or locations. The beam can initially be mounted to either the engine or to the spars of the aircraft.

Engine mounting assembly

A shock absorber strut that includes inner and outer tubes which slide one over the other in a telescopic relationship. In the space confined between closed ends of the tubes, a stack arrangement of compressible elastomeric material pad assemblies is provided to function as shock absorber medium. Each assembly has a pad of compressible material having a central opening, a metal plate having a corresponding central opening and abutting one end of the pad, and a flanged bearing through said openings and abutting the plate to the pad. The pad has ends provided with a series of different sized bores cooperating to define flow spaces for compressed elastomer material to avoid contact with the guide rod. A guide rod extends substantially through the strut through the bearings. The entire arrangement of the bearing provides a glide path for the guide rod. Each plate has a plurality of holes, sub-peripherally located, the holes having torn and jagged protrusions engageable with the pad end.

Heavy off-road large vehicle suspension strut

A mount system for an auxiliary component includes two side brackets and a top bracket for rigidly attaching an auxiliary component to an engine casing. Each side bracket defines mount segments, a deformable member and two retainer members between the mount segment. The deformable member plastically deforms during a fan-blade out event, thereby absorbing a majority of the high shock load experienced on the auxiliary component. The retainer members maintain the attachment between the auxiliary component and the engine casing subsequent to the fan-blade out event.

Gas turbine engine auxiliary component mount

Miniature vibration isolator

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Automobile engine mounting

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Automobile engine mounting

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Engine mounting assembly

Heavy off-road large vehicle suspension strut

Gas turbine engine auxiliary component mount

Miniature vibration isolator

Extractor basket drive

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