Aircraft main landing gear connecting structure

The utility model particularly relates to an aircraft main landing gear connecting structure, which comprises two main landing gear outer side joints, two main landing gear outer side connecting holes, two main landing gear outer side connecting holes, two main landing gear outer side connecting hol...

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Bibliographische Detailangaben
Hauptverfasser:	ZHANG JIANHUA, PAN XIAOQUAN, WANG YU, NIE RONGHUA, JIAO BINCHANG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	The utility model particularly relates to an aircraft main landing gear connecting structure, which comprises two main landing gear outer side joints, two main landing gear outer side connecting holes, two main landing gear outer side connecting holes, two main landing gear outer side connecting holes, two main landing gear outer side connecting holes and two main landing gear outer side connecting holes, the two main undercarriage inner side joints are provided with main undercarriage inner side connecting holes, are oppositely arranged, are connected between a front supporting frame and a rear supporting frame of the aircraft and are positioned between the two main undercarriage outer side joints; a supporting column of each tubular spring type main undercarriage correspondingly penetrates through one main undercarriage outer side connecting hole and extends into the main undercarriage inner side connecting hole close to the corresponding main undercarriage outer side connecting hole; each roller is corresp