发明名称 Counterbalance mechanism for inwardly and upwardly opening plug-type airplane cargo doors
摘要 A counterbalance mechanism (10) counters the weight of a door in an airplane. The door hingedly mounts to the fuselage of the airplane, and rotates upward and inward relative to the fuselage along a hinge axis. The counterbalance mechanism includes a housing (12) for affixing the counterbalance mechanism to the fuselage of the airplane. A guide tube (14) rotatably mounts to the housing for swinging movement about an axis of rotation generally parallel to the hinge axis of the door. The guide tube includes a rod (40) that extends outwardly from the guide tube. Compression springs (34) within the guide tube oppose outward movement of the rod. A linkage assembly that includes a bell crank (50) and a push rod (56) connects the guide tube to the door via rod (40) to assert counterbalancing force during the door opening and closing sequence of the door.
申请公布号 US5704569(A) 申请公布日期 1998.01.06
申请号 US19950440230 申请日期 1995.05.12
申请人 THE BOEING COMPANY 发明人 DANIELS, DYRK L.
分类号 B64C1/14;(IPC1-7):B64C1/14 主分类号 B64C1/14
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