Aircraft engine mounting assembly

A mounting assembly ( 10 ) for mounting a gas turbine engine on an aircraft. The assembly ( 10 ) comprising four equispaced hydraulic piston and cylinder thrust links ( 16 ) connecting between the engine fan case ( 12 ) and the air intake ( 14 ), which intake ( 14 ) is mounted to the airframe.

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Bibliographische Detailangaben
Hauptverfasser:	PETER BEARDSLEY, RICHARD GEOFFREY STRETTON, DAVID MICHAEL BEAVEN
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	A mounting assembly ( 10 ) for mounting a gas turbine engine on an aircraft. The assembly ( 10 ) comprising four equispaced hydraulic piston and cylinder thrust links ( 16 ) connecting between the engine fan case ( 12 ) and the air intake ( 14 ), which intake ( 14 ) is mounted to the airframe.