专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

2. 发明授权

US4395172A Cargo restraint system with spring fuse 失效
标题翻译：带弹簧保险丝的货物约束系统
公开(公告)号：US4395172A
公开(公告)日：1983-07-26
申请号：US215613
申请日：1980-12-12
申请人： Dieter W. Hoener , Neville L. Lambert , Erwin V. Schweizer
发明人： Dieter W. Hoener , Neville L. Lambert , Erwin V. Schweizer
IPC分类号： B64D9/00 , B64D1/10
CPC分类号： B64D9/003
摘要： A cargo restraint and delivery system for an aircraft having a cargo-receiving and delivery opening for cargo secured to pallets. The cargo is moved backwardly and out of the rear cargo-delivery opening under either the pull of the parachute when the aircraft is airborne or by the force developed by the rapid acceleration of the aircraft for combat off-loading of cargo onto the ground. One of two spaced-apart guide rails for the pallets supports locks to releasably hold the pallets. A logistics control includes a lever at a loadmaster station to move a logistics control cable extending along the rail supporting the locks to move them into a first position where the pallet locks will release the pallets for movement either forward or aft of the aircraft and a second position where the pallet locks will prevent either forward or aft movement of a pallet. A system of levers coupled to each of the locks is controlled by a chain system extending to the loadmaster station and operating on cam members to sequentially actuate each system of levers. The levers move the pallet locks into a third position wherein the locks will prevent forward movement of a pallet but will permit aft movement of a pallet against a biasing force of a spring acting on the lever system thereof. The control for the pallet locks is mounted below the floor of an aircraft and the guide rails are mounted to pivot into troughs to form a flush relation with the floor of the aircraft.
摘要翻译：一种用于飞机的货物约束和运送系统，其具有固定在托盘上的货物的货物接收和运送开口。当飞机空降时，由于飞机的快速加速所产生的力量，货物在货物运送到地面上作战将货物卸载后，货物在降落伞的拉力之下向后移动并离开后货物运送开口。用于托盘的两个间隔开的导轨中的一个支撑锁定以可释放地保持托盘。物流控制包括在负载主站站处的杠杆，用于移动沿着支撑锁的轨道延伸的物流控制电缆，以将它们移动到第一位置，在该位置托盘锁将释放托盘以使飞行器向前或向后移动，托盘锁的位置将防止托盘的向前或向后移动。耦合到每个锁的杠杆系统由延伸到负载主站站的链系统控制，并且在凸轮构件上操作以顺序地致动每个系统系统。杠杆将托盘锁移动到第三位置，其中锁将防止托盘的向前移动，但将允许托板抵抗作用在其杠杆系统上的弹簧的偏置力的后运动。托盘锁的控制安装在飞机的地板下方，并且导轨安装成使槽枢转以与飞机的地板形成平齐的关系。

IPRDB

热门服务

关于我们

友情链接

联系方式