Lifting type installation device for helicopter piston engine

The embodiment of the invention provides a lifting type installation device for a helicopter piston engine. The lifting type installation device includes an upper installation component, a main installation component and a bottom installation component. The upper installation component includes an u...

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Bibliographische Detailangaben
Hauptverfasser:	CHEN LONG, ZHU YANGZHENG, DUAN YONGLIANG, LIN SENSHI
Format:	Patent
Sprache:	chi ; 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:	The embodiment of the invention provides a lifting type installation device for a helicopter piston engine. The lifting type installation device includes an upper installation component, a main installation component and a bottom installation component. The upper installation component includes an upper shock absorber, an upper connecting rod, a first mounting hole and a first fastener. One end ofthe upper connecting rod is connected to one end of the upper shock absorber, and the first mounting hole and the first fastener are arranged at the other end of the upper connecting rod. The main installation component includes a main body bracket, main body shock absorbers, second installation holes and second fasteners. The main installation component is installed on a structural beam throughthe main body shock absorbers, and the main installation component is fixed to the center of gravity of the engine. The bottom installation component includes a bottom bracket, a shock absorber shell,third installation holes a