公开(公告)号：US5605043A

公开(公告)日：1997-02-25

申请号：US462567

申请日：1995-06-05

申请人： Ivan H. Dimmock

发明人： Ivan H. Dimmock

IPC分类号： B64D1/06 ,  F15B13/04 ,  F15B13/043 ,  F15B13/044 ,  F16D31/02 ,  G05D11/00

CPC分类号： F15B13/044 ,  B64D1/06 ,  F15B13/0405 ,  F15B13/0431 ,  Y10T137/261

摘要： A gas operated release or ejection system which compensates for changes in pressure applied to a load being ejected. The pressure regulator compensates for decreases in pressure through a pressure regulating valve, and compensates for increases in pressure through a pressure relief valve.

摘要翻译： 气体释放或喷射系统，其补偿施加到被喷射的负载的压力变化。 压力调节器通过压力调节阀补偿压力降低，并通过压力释放阀补偿压力增加。

公开(公告)号：US4905568A

公开(公告)日：1990-03-06

申请号：US331520

申请日：1989-03-30

申请人： Walter Hetzer ,  Erwin Goellner

发明人： Walter Hetzer ,  Erwin Goellner

IPC分类号： B64D1/06

CPC分类号： B64D1/06

摘要： An ejecting mechanism for an ammunition body is operated by pressurized gas from a high pressure bottle for pressurizing a double piston, which controls two ejectors through a hydraulic valve system. The pressurized gas is heated by a heater surrounding the high pressure bottle to keep the bottle and its content at a temperature that corresponds approximately to the highest outer temperature under which the ejector mechanism is expected to operate. Thus, the pressurized gas has the same energy content at all expected external operating temperatures. After an ammunition body has been ejected, the ejector pistons are pushed back again under an electrical control signal from a control which controls the valve system, whereby the hydraulic oil is pressed back into a hydraulic reservoir. The ejector pistons are of the stepped type to facilitate the intended operation. A high pressure pump pumps the hydraulic oil back into the double piston cylinder device, whereby the respective double piston drives the working or driving gas back into the high pressure bottle, thereby reactivating the system for the next ejection.

摘要翻译： 用于弹药体的排出机构由来自高压瓶的加压气体操作，用于对通过液压阀系统控制两个喷射器的双重活塞加压。 加压气体被围绕高压瓶的加热器加热，以保持瓶子及其内容物的温度大致相当于预期喷射器机构运行的最高外部温度。 因此，在所有预期的外部操作温度下，加压气体具有相同的能量含量。 在弹药体被弹出之后，喷射器活塞在控制阀系统的控制器的电控制信号下被再次推回，由此将液压油压回到液压储存器中。 喷射器活塞是阶梯式的，以便于预期的操作。 高压泵将液压油抽回到双活塞缸装置中，由此相应的双活塞将工作或驱动气体驱动回高压瓶，从而重新启动系统以进行下一次喷射。

公开(公告)号：US4850553A

公开(公告)日：1989-07-25

申请号：US26039

申请日：1987-03-16

申请人： Earl K. Takata ,  Ben E. Paul ,  John P. Nordhaus

发明人： Earl K. Takata ,  Ben E. Paul ,  John P. Nordhaus

IPC分类号： B64D1/06 ,  F15B15/16 ,  F15B15/26

CPC分类号： B64D1/06 ,  F15B15/16 ,  F15B15/261

摘要： An ejector arrangement for aircraft store racks that are carried by military type aircraft and the like for releasably attaching to the aircraft stores such as conventional or nuclear weapons, in which the ejector arrangement is duplicated in mirror image form at the usual fore and aft positions of the rack, with each ejector arrangement being in the form of an elongated housing with which the usual fore and aft sway braces are respectively integral, which ejector housing internally defines an elongate internal chamber in which are mounted an outer cylinder and inner cylinder that in the dormant relation of the ejector are in substantially telescoped coaxial relation with like ends of same disposed adjacent one end of the housing to which the rack ballistic gas is supplied, with the ejector cylinders at their other ends being exposed externally of the other end of the housing and keyed for sequential movement to their extended relations under the action of the ballistic gas involved, to thrust the store which at the same time has been released from the aircraft, beyond the aircraft's air stream envelope; the inner and outer cylinders of the rack ejectors, in moving from the ejector dormant relation to the ejector extended relation, act under the ballistic gas pressure released within the respective rack ejectors, to apply to the store the needed unbalanced force, and in a more or less uniform, sequential manner, to effect application to the store of maximized release thrust during the thrust stroke of the rack ejectors.

摘要翻译： 用于飞机存储架的喷射器装置，其由军用飞机等承载，用于可释放地附接到诸如常规或核武器的飞机存储器，其中喷射器装置以镜像形式复制在通常的前后位置 每个喷射器装置为细长壳体的形式，通常的前后摇摆支架分别与其一体，该喷射器壳体内部限定细长的内部腔室，其中安装有外筒和内筒， 喷射器的休眠关系基本上是伸缩的同轴关系，其中相同的端部设置在与壳体弹性气体供给的壳体的一端相邻的位置，其顶端的喷射器筒体在壳体的另一端的外侧露出 并指出在涉及的弹道气的作用下顺序移动到他们的扩大关系 o推动同时从飞机上释放的商店，超出飞机的气流信封; 齿条喷射器的内部和外部气缸从喷射器休眠关系移动到喷射器延伸关系，在相应的齿条喷射器内释放的弹道气体压力下作用，以向存储器施加所需的不平衡力，并且在更多 或更小的均匀，连续的方式，以在机架喷射器的推力冲程期间施加到存储最大化的释放推力。

公开(公告)号：US4702145A

公开(公告)日：1987-10-27

申请号：US875422

申请日：1986-06-17

申请人： John T. Kannapell ,  Haig Asdurian ,  Robert F. Buttles

发明人： John T. Kannapell ,  Haig Asdurian ,  Robert F. Buttles

IPC分类号： B64D1/06 ,  F41A9/76 ,  F41F3/06 ,  B64D1/02

CPC分类号： F41F3/06 ,  B64D1/06 ,  F41A9/76

摘要： A stores handling system for an aircraft having a fuselage including a chamber for enclosing the stores handling system proximate an area openable through said fuselage through which stores may be loaded into and ejected from the aircraft. The handling system comprises a magazine arranged substantially vertically within the chamber for storing and positioning ejectable stores and including a flexible drive having stores holding shoes spaced apart thereon for engaging and retaining stores against movement within the aircraft, and for lifting and/or lowering stores within the magazine; and a launching mechanism for receiving stores individually from said magazine drive, and including an actuator having hands pivotable between a first closed position and a second open position for engaging the lowermost store to preclude ejecting movement when said hands are in said first position, and for engaging said stores to eject same from the aircraft when said hands are in said second position.

摘要翻译： 一种用于具有机身的飞机的商店处理系统，所述机身包括用于将商店处理系统封闭的室，靠近可通过所述机身打开的区域，所述机构可以通过所述区域装载和从所述飞机弹出。 该处理系统包括一个在该腔室内基本垂直地布置的仓，用于存储和定位可弹出式储存器，并且包括一个柔性驱动器，该弹性驱动器具有在其上间隔开的用于接合和保持储存器的货架，以防止在飞行器内移动， 该杂志; 以及用于从所述仓库驱动器单独接收存储器的启动机构，并且包括具有在第一关闭位置和第二打开位置之间枢转的手的致动器，用于接合最下面的存储器，以防止当所述手位于所述第一位置时弹出移动，并且 当所述手位于所述第二位置时，使所述商店从所述飞机弹出。

公开(公告)号：US4520711A

公开(公告)日：1985-06-04

申请号：US448997

申请日：1982-11-10

申请人： Paul R. Robinson

发明人： Paul R. Robinson

IPC分类号： B64D1/06 ,  F41F5/02 ,  B64D1/04

CPC分类号： B64D1/06

摘要： A loop retention device for hook operated bomb arming solenoids (13) in which when effecting unarmed release a telescopic plunger (4-6) is displaced by spring means (14) when the bomb release hooks (3) move including the armature (12) of the solenoid (13) which is de-energized to completely release a lanyard, but when a bomb is to be armed the solenoid (13) remains energized and the telescopic member (4-6) acts to lock the armature (12) of the solenoid (13) and the release control pin (2) in a holding position irrespective of whether the solenoid (13) is energized or not.

摘要翻译： PCT No.PCT / AU82 / 00025 Sec。 371日期：1982年11月10日 102（e）1982年11月10日日期PCT提交1982年3月12日PCT公布。 公开号WO82 / 03272 日本1982年9月30日。一种用于挂钩操作的炸弹布防螺线管（13）的回路保持装置，其中当释放弹簧释放钩（3）时，通过弹簧装置（14）使伸缩式活塞（4-6）进行非手动释放时， 包括被断电的螺线管（13）的电枢（12）以完全释放挂绳，但是当一个炸弹被布防时，螺线管（13）保持通电，并且伸缩构件（4-6）作用于 无论螺线管（13）是否通电，都将螺线管（13）的电枢（12）和释放控制销（2）锁定在保持位置。

公开(公告)号：US4498392A

公开(公告)日：1985-02-12

申请号：US384098

申请日：1982-06-01

申请人： Alain A. Billard ,  Hubert C. Calmettes ,  Roland C. Encoyand

发明人： Alain A. Billard ,  Hubert C. Calmettes ,  Roland C. Encoyand

IPC分类号： B64D1/06 ,  F42B5/15 ,  F42B4/22 ,  F41F5/02 ,  F42B4/24

CPC分类号： F42B5/15 ,  B64D1/06

摘要： An infrared decoy member is provided with a pyrotechnic chain for ejection and ignition incorporated in a unit. The ejection charge is mounted to slide in a cavity which allows the ejection of the unit as well as of adjacent infrared charges. A slide, which can be released when an acceleration threshold is crossed and on condition of ejection could ensure the transmission of fire to a transverse channel leading to useful charges. A second fire-transmitting chain which is independent, makes it possible to excite previously a similar decoy member located below.

摘要翻译： 一个红外诱饵构件设置有一个用于排出和点燃的烟火链，并入一个单元中。 喷射装置被安装成在允许单元以及相邻红外线电荷的弹出的腔中滑动。 当加速度阈值越过并且在排出状态下可以释放的滑块可以确保火焰传递到横向通道，导致有用的费用。 独立的第二个防火传输链，可以激发以前类似的位于下方的诱饵成员。

公开(公告)号：US4233883A

公开(公告)日：1980-11-18

申请号：US2734

申请日：1979-01-11

申请人： Richard J. Miko

发明人： Richard J. Miko

IPC分类号： B64D1/04 ,  B64D1/06 ,  F41F5/02

CPC分类号： B64D1/06

摘要： A swaybrace system includes one or more pairs of opposing swaybrace arms that pivot in relation to aircraft structure, each arm with a pad thereon automatically being biased by a spring-loaded wedge or the like to cause the pad to contact with the store under all load conditions. Each arm in one embodiment is bifurcated into upper and lower portions capable of flexing, the store-contacting pad being attached to the lower portion, with the lower portion flexing with respect to the upper portion through a predetermined distance Sa for pad loads between zero and a predetermined pre-load. The upper portion, together with the lower portion and pad, flexes about the wedge through a predetermined distance Sb for pad loads between the predetermined pre-load and a predetermined maximum load. An alternate embodiment utilizes resilient means between the pad and arm to allow the pad to move through the predetermined distance Sa with respect to the arm, the arm together with the pad flexing about the wedge through the predetermined distance Sb, all under corresponding load conditions. Distance Sa equals distance SB in each embodiment. Each embodiment automatically loads itself to obtain adequate but not excessive store pre-loads at each pad, to properly restrain the store but limit maximum hook loads.

摘要翻译： 滑行系统包括一对或多对相对于飞行器结构枢转的相对的滑行臂，每个臂上具有一个垫，其上由弹簧加载的楔形物等自动地偏置，以使该垫在所有载荷下与储存器接触 条件。 一个实施例中的每个臂分叉成能够弯曲的上部和下部，储存接触垫附接到下部，下部相对于上部弯曲预定距离Sa，用于在0和 预定的预加载。 上部与下部和垫一起围绕楔形物弯曲预定距离Sb，用于在预定预载荷和预定最大载荷之间的载荷。 替代实施例利用垫和臂之间的弹性装置，以允许衬垫相对于臂移动超过预定距离Sa，臂与焊盘一起在楔形件周围穿过预定距离Sb，全部在相应的负载条件下移动。 距离Sa等于每个实施例中的距离SB。 每个实施例自动加载自身以在每个焊盘处获得足够但不是过度的存储预加载，以适当地限制存储，但限制最大挂钩负载。

公开(公告)号：US4050656A

公开(公告)日：1977-09-27

申请号：US687283

申请日：1976-05-17

申请人： Paul F. Peterson

发明人： Paul F. Peterson

IPC分类号： B64D1/06 ,  B64D1/02

CPC分类号： B64D1/06

摘要： An ejector rack that is attachable to an aircraft and is for supporting and selectively releasing and/or ejecting a store that is carried internal of the aircraft, i.e., in a bomb bay. The store can be released from the ejector rack, and from the aircraft, in either of two ways, namely: by pushing on a manually operated release handle; or, by forced ejection, the only way used during flight of the aircraft. Forced ejection is achieved by sending an electrical impulse to either or both of two cartridges in the breech of the ejector rack, igniting the cartridge(s). Gas is generated thereby; and, the resultant pressure that is built up in a gas system in the rack provides force that acts upon an unlocking piston, causing the piston to move out of its "locked" position. In turn, the moving piston provides a force on a slide, rotating a latch that allows the main linkage bellcrank to rotate and thus to open two hooks which are holding the store, thereby releasing the suspended store. Concurrently, gas pressure is manifolded to two sway brace ejection piston cylinders, and the ejection pistons therein are forcefully extended, causing positive and forcible ejection of the store by the ejection pistons. Unlike prior art devices, this ejector rack incorporates: a fully automatic sway brace system; a counterbalance assembly with a counterweight that prevents vibration loads from causing the inadvertent release of the store from the rack; and, a safety lock that automatically closes and also latches the hook linkage when the lock is moved to the locked position.

摘要翻译： 一种可附接到飞行器并且用于支撑和选择性地释放和/或喷射在飞行器内部携带的商店（即在炸弹舱中）的喷射器架。 商店可以从喷射器架和从飞行器以两种方式中的一种释放，即：通过推动手动操作的释放手柄; 或者通过强制弹射，在飞机飞行中使用的唯一方式。 通过向喷射器架的后膛中的两个盒中的任一个或两个发送电脉冲来点燃盒，来实现强制喷射。 从而产生气体; 并且在机架中的气体系统中建立的合成压力提供作用在解锁活塞上的力，导致活塞移出其“锁定”位置。 反过来，移动的活塞在滑动件上提供力，旋转一个闩锁，允许主联动曲拐转动，从而打开两个保持储存器的钩，从而释放悬挂的储存器。 同时，两个摆动支架弹出活塞气缸的气体压力分歧，其中的喷射活塞被强力地延伸，从而引起喷射活塞的存储器的正向和强制的喷射。 与现有技术的设备不同，该喷射器机架包括：全自动摇摆支架系统; 具有配重的平衡组件，其防止振动负载导致商店从机架的意外释放; 以及当锁移动到锁定位置时，自动关闭的安全锁还锁定钩连杆。

公开(公告)号：US3936019A

公开(公告)日：1976-02-03

申请号：US443250

申请日：1974-02-19

申请人： Samuel W. Craigie

发明人： Samuel W. Craigie

IPC分类号： B64D1/06 ,  B64D1/02

CPC分类号： B64D1/06

摘要： This invention is concerned with an ejection release unit for releasing and projecting a store from an aircraft. The unit comprises a releasable latching mechanism for supporting the store, a pair of telescopic ejection guns for projecting the store from the aircraft, a breech for one or more cartridges which, on ignition, produce pressure gas which causes the latching mechanism to release the store and also acts on a piston which indirectly transmits the resultant force to a body of hydraulic fluid, which, in its turn, operates the ejection gun at each side. Preferably, there are two oppositely acting pistons, each of which pistons transmits pressure to a separate body of hydraulic fluid for operating a respective ejection gun. The breeches may be formed in a removable unit which also defines the cylinders within which the pistons work.

摘要翻译： 本发明涉及一种用于从飞行器释放和投影商店的排出装置。 该单元包括用于支撑商店的可释放的闩锁机构，一对用于从飞行器上投射商店的伸缩式弹射枪，用于一个或多个弹药筒的臀部，其在点燃时产生压力气体，其使闩锁机构释放商店 并且还作用于间接地将合力传递到液压流体的活塞上，该液压流体又在每一侧操作喷射枪。 优选地，存在两个相对作用的活塞，每个活塞中的每一个活塞将压力传递到用于操作相应喷射枪的单独的液压流体。 马桶可以形成在可移动单元中，该单元还限定活塞在其中工作的气缸。

公开(公告)号：US3898909A

公开(公告)日：1975-08-12

申请号：US44781274

申请日：1974-03-04

申请人： ML AVIATION CO LTD

发明人： CRAIGIE SAMUEL W

IPC分类号： B64D1/06 ,  B64D1/12

CPC分类号： B64D1/06

摘要： This invention is concerned with an ejector release unit for releasing and projecting a store from an aircraft. The unit comprises a pair of telescopic ejection guns for projecting the store from the aircraft and a releasable latching mechanism for supporting the store, having an inner pair of pivoted hooks located between the ejection guns which are swung from their operative positions by means of links controlled by a central toggle mechanism, and an outer pair of hooks located outside the ejection guns, each of the hooks being held in its operative position by a separate toggle linkage which is released by means of a link controlled from the central toggle linkage, which is so located in a lateral direction as to pass to one side of the respective ejection gun. Each of the separate toggle linkages are preferably braced in a position just past dead-centre and is released by turning one of the links through the dead-centre position by means of a short connecting arm fixed to the link in question and acted on by the link controlled from the central toggle linkage.

摘要翻译： 本发明涉及一种用于从飞行器释放和投射商店的喷射器释放单元。 该单元包括一对用于从飞行器上投射商店的可伸缩喷射枪和用于支撑商店的可释放的闩锁机构，其具有位于弹射枪之间的内部一对枢转钩，所述旋转钩从其操作位置通过连杆控制 通过中央肘节机构和位于喷射枪外部的外部一对钩，每个钩通过单独的肘节连杆保持在其操作位置，该肘节联动装置通过从中心肘节连杆机构控制的连杆释放， 所以位于横向方向上以便通过相应喷射枪的一侧。 每个单独的肘节连杆件优选地被支撑在刚好超过死角的位置，并且通过借助于固定到所讨论的连杆的短连接臂将链节中的一个转过死点位置来释放，并且由 从中央拨动连杆控制的连杆。