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公开(公告)号：US3883097A
公开(公告)日：1975-05-13
申请号：US42335173
申请日：1973-12-10
申请人： RAFAUT & CIE
发明人： BILLOT JEAN
CPC分类号： B64D1/06
摘要： A device for picking up and ejecting loads arranged under the girder of a carrier, such as an airplane. The device comprises two identical assemblies intended to cooperate with bore holes provided in the load to be carried, each assembly comprising wedge coupling means, lifting means for bringing the load against the girder, a single locking control, and means actuated by gases to uncouple the load and eject it.
摘要翻译： 用于拾取和排出布置在诸如飞机的载体的梁下方的载荷的装置。 该装置包括两个相同的组件，其旨在与设置在待承载的负载中的钻孔配合，每个组件包括楔形联接装置，用于将负载抵靠在大梁上的提升装置，单个锁定控制装置，以及由气体致动的装置， 加载并弹出。
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公开(公告)号：US3771416A
公开(公告)日：1973-11-13
申请号：US3771416D
申请日：1971-09-22
申请人： US NAVY
发明人： ACKERMAN W , FISCHER E , CARUSO G
CPC分类号： B64D1/06
摘要： A removable weapons rail which is adaptable for bomb racks or missile launchers. Standard couplings mount the rail to an aircraft. A hoist system for moving the loaded or unloaded rail to or from mounting position is internally contained in the rail.
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公开(公告)号：US3756545A
公开(公告)日：1973-09-04
申请号：US3756545D
申请日：1971-10-06
申请人： ALKAN R & CIE
发明人： COUTIN P
摘要： In this retractable jettisoning device the ejection piston, whether single or telescopic, mounted in a cylinder of conventional type, is hollow and its inner cavity comprises a tubular distributor close at its outer end but provided adjacent this end with lateral ports adapted to co-act with an inner surface of the piston end for causing its inner space and the rear end of the piston to communicate with the atmosphere when this tubular distributor emerges from the ejection piston at the end of an expansion stroke of the ejection piston whereas the same movement of the tubular distributor uncovers lateral ports formed at the rear end of the piston to cause the fluid pressure in the chamber formed between the piston and the tubular distributor to act against the lower end of the fluid-tight portion of the piston in its cylinder, in order to move the piston upwards.
摘要翻译： 在这种可收缩的放弃装置中，安装在常规类型的气缸中的喷射活塞是单一的或可伸缩的，是中空的，并且其内腔包括在其外端处靠近但在该端附近设置的管状分配器，侧向端口适于共同作用 具有活塞端的内表面，用于使得其内部空间和活塞的后端与气体连通，当该弹性活塞在弹射活塞的膨胀冲程结束时，该管状分配器从喷射活塞露出，而相同的运动 管状分配器露出形成在活塞的后端处的侧向端口，以使形成在活塞和管状分配器之间的腔室中的流体压力在其气缸中作用在活塞的流体密封部分的下端， 为了向上移动活塞。
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公开(公告)号：US3738222A
公开(公告)日：1973-06-12
申请号：US3738222D
申请日：1971-05-12
申请人： US NAVY
CPC分类号： B64D1/06
摘要： A safety pin system for bomb racks including a pair of spring releasable pin lock and retraction assemblies interconnected via a load dividing pulley reciprocated by a push-pull cable operated by a single release latch with a contoured flag visible when the pins are lockable in the inserted position.
摘要翻译： 一种用于炸弹架的安全销系统，包括一对弹簧可释放的销锁定和缩回组件，该组件通过负载分配滑轮相互连接，该负载分配滑轮通过一个由单个释放闩锁操作的推拉电缆往复运动， 位置。
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95.发明授权
公开(公告)号：US3721415A
公开(公告)日：1973-03-20
申请号：US3721415D
申请日：1970-06-01
申请人： UNITED AIRCRAFT CORP
发明人： CHAPKOVICH J , LEE D
CPC分类号： F16M13/00 , B64D1/06 , F16M11/14 , F16M13/02 , F16M2200/022
摘要： A universally movable mounting mechanism in which the mounting mechanism is connected to a fixed ball by spherically shaped friction cups which are spring biased toward one another to lock the mounting mechanism in fixed position on the ball and which can be selectively moved away from one another to either totally eliminate the friction between the friction cups and the ball to thereby free the mounting mechanism for universal motion in response to actuation by a pilot operated handle or in which the friction between the friction cups and the fixed ball is selectively reduced so as to maintain a desired mount positioning force in accordance with operator feel as he moves the mounting mechanism through handle motion.
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96.发明授权Apparatus for loading on an airplane goods to be dropped off or tilted out of the plane 失效装载在飞机上的装置将被丢弃或倾倒在飞机上
公开(公告)号：US3613498A
公开(公告)日：1971-10-19
申请号：US3613498D
申请日：1969-01-07
发明人： RICCIUS ROLF , WEITKAMP GUNTER
摘要： An apparatus for loading loads on an airplane which are releasable from the airplane when the latter is in flight, which includes frame means detachably arranged in a loading chamber in the fuselage of an airplane preferably within the region of the center of gravity of the airplane, while said frame means has displaceably mounted thereon carriage means for suspending a load thereon, said carriage means being adapted to be locked to said frame means in a desired position of said carriage means on said frame means.
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公开(公告)号：US3611865A
公开(公告)日：1971-10-12
申请号：US3611865D
申请日：1969-02-05
发明人： SCHALLERT JOSEPH M
CPC分类号： B64D1/06
摘要： A mount for securing weapons and other stores to an aircraft and including a housing projecting into the aircraft, an ejector rack on the housing for securing a load partially within the housing, and an inflatable seal which engages the load and conforms to its contours. When the load is detached from the rack the seal extends across the cavity formed by the housing and is generally flush with the exterior surface of the aircraft so that an uninterrupted moldline exists.
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公开(公告)号：US3569912A
公开(公告)日：1971-03-09
申请号：US3569912D
申请日：1969-05-29
申请人： US NAVY
CPC分类号： H01R13/562 , B64D1/06 , H01B7/04 , Y10S439/919
摘要： An electrical connector including a flexible armored sheath having an insulated conductor threaded therethrough and electrically connected between a plug unit and a breech cap which is adapted for applying a firing signal to a pyrotechnic cartridge and which has flanged spring pins formed to function both as ground contacts and as spent cartridge extracting means. A braided sheath encircles the armored sheath and is mechanically connected at one end to the breech cap and at the other end through a turnbucklelike sheath stretching assembly to the plug unit. The stretching assembly enables the braided sheath to be longitudinally stretched so that it tightly grips the armored sheath and forms therewith a more rigid conduit.
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