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公开(公告)号：US4685377A
公开(公告)日：1987-08-11
申请号：US831309
申请日：1986-02-20
申请人： Guy Mace , Andre Anglard , Andre Insa
发明人： Guy Mace , Andre Anglard , Andre Insa
摘要： A missile launcher comprises a supporting structure a bearing shoe connected to a supporting structure by links articulated so as to form a deformable parallelogram. A fluid pressure cylinder releases a locking system securing the missile on the structure and actuates the links in a direction causing the shoe to push the missile away. The shoe has a sufficient length for determining the distance between the missile and the aircraft at the end of its stroke and also the angular position of the missile. With that arrangement, the position and angular speed of the missile when the thrust of the shoe ceases may be accurately determined.
摘要翻译： 导弹发射器包括支撑结构，轴承瓦通过铰接而形成可变形平行四边形的连杆连接到支撑结构。 流体压力缸释放一个将导弹固定在结构上的锁定系统，并在导致鞋子推动导弹的方向上致动连杆。 该鞋具有足够的长度来确定在其行程结束时导弹和飞机之间的距离以及导弹的角度位置。 通过这种安排，可以准确地确定当鞋的推力停止时导弹的位置和角速度。
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公开(公告)号：US4679751A
公开(公告)日：1987-07-14
申请号：US857004
申请日：1986-04-29
申请人： Paul F. Peterson
发明人： Paul F. Peterson
CPC分类号： B64D7/08
摘要： The invention is a weapon dispensing system for an aircraft. The system includes a weapon positioning assembly for positioning the weapon in a stored position and a release position. The weapon positioning assembly comprises a weapon support rack and a pair of fore and aft links having first and second ends. The first ends of the links are pivotally coupled to the aircraft and the second ends are pivotally coupled to the rack. An actuator assembly is coupled by its first end to the aircraft and by its second end to the weapon positioning assembly. It is adapted to move the positioning assembly from the stored position to the release position. Fore and aft weapon attaching devices for releasably locking the weapon to the rack is attached to the weapon positioning assembly. The weapon releasing devices are adapted to lock the weapon to the rack when the weapon position assembly is in the stored position and to only unlock the weapon from the positioning assembly when it is in the release position. Thus, upon actuation, the rack with the weapon locked thereto is rotated in a downward and forward direction and automatically released when the release position is reached.
摘要翻译： 本发明是用于飞行器的武器分配系统。 该系统包括用于将武器定位在存储位置和释放位置的武器定位组件。 武器定位组件包括武器支撑架和具有第一和第二端的一对前后链节。 链节的第一端枢转地联接到飞行器，并且第二端枢转地联接到齿条。 致动器组件通过其第一端连接到飞机并且其第二端连接到武器定位组件。 它适于将定位组件从存储位置移动到释放位置。 用于将武器可释放地锁定到机架的前后武器附接装置附接到武器定位组件。 武器释放装置适于当武器位置组件处于存储位置时将武器锁定到机架上，并且当武器处于释放位置时仅从定位组件解锁武器。 因此，一旦致动，装有武器的机架锁定在其上，向下和向前方向旋转，并且在达到释放位置时自动释放。
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公开(公告)号：US4489638A
公开(公告)日：1984-12-25
申请号：US474994
申请日：1983-03-14
摘要： A missile launching system adapted for installation in a standard commercial aircraft without modification of the aircraft structure. The system comprises a plurality of frame members, linear tracks which are movable longitudinally relative to the frame members, a plurality of launch tubes for storing the missiles, an exit port for installation in an pre-established aircraft fuselage opening, and associated equipment for selectively launching the missiles from the launch tubes through the exit port. The entire system is assembled from individual components, all of which are sized to be placed on board the aircraft through a standard passenger door opening. In preparation for installing the system in a commercial aircraft, the passenger seats and related equipment conventionally installed in the interior of such an aircraft are removed. The frame members of the system are then mounted to the standard seat tracks in the floor of the aircraft. The remaining portions of the system are thereafter assembled and installed on the frame. The frame is inclined to support the launch tubes at an angle extending upward and forward so that when a missile is ejected from the launch tube, it is given a trajectory which carries it clear of the aircraft wing and empennage.
摘要翻译： 一种适合安装在标准商用飞机上而不改装飞机结构的导弹发射系统。 该系统包括多个框架构件，相对于框架构件可纵向移动的线性轨道，用于存储导弹的多个发射管，用于安装在预先建立的飞行器机身开口中的出口，以及用于选择性地设置的相关设备 通过出口将发射管的导弹发射出去。 整个系统由单个部件组装，所有这些部件的尺寸都通过标准乘客门开口放置在飞机上。 为了准备将该系统安装在商用飞机中，除去常规安装在这种飞行器内部的乘客座椅和相关设备。 然后将系统的框架构件安装到飞机地板上的标准座椅轨道上。 此后系统的其余部分组装并安装在框架上。 框架倾向于以向上和向前延伸的角度支撑发射管，使得当导弹从发射管弹出时，它被给予一个轨迹，其使飞机机翼和尾翼远离。
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公开(公告)号：US4399968A
公开(公告)日：1983-08-23
申请号：US150465
申请日：1980-05-16
CPC分类号： B64D7/08
摘要： An actuator for ejecting a store from an aircraft, with a pre-selected force vs stroke profile, is disclosed. The actuator comprises a cylinder and a fixed tubular member coupled to a source of fluid under pressure having a first array of orifices for flowing fluid into the cylinder. A piston assembly is provided, which is adapted to engage and eject the store. The iston assembly is slidably mounted within the cylinder and telescopically movable over the fixed tubular member from a first position, wherein the piston assembly covers a portion of the first array of orifices, to a second position, wherein the first array of orifices is uncovered. Typically, the pressure level of the source of fluid varies, generally as a function of the flow into the cylinder during the stroke of the piston assembly. Thus, the cross-sectional area and spacing of each of the orifices of the first array is selected to maintain a desired pre-selected pressure vs stroke profile within the cylinder upon the application of the fluid to the fixed tubular member, as the initially covered portion of the first array of orifices are uncovered during the stroke. Therefore, upon initiation of fluid flow, the first array of orifices meters the fluid into the cylinder at a rate sufficient to maintain the pre-selected pressure vs stroke profile therein.A system for varying the magnitude of the pressure vs stroke profile within the cylinder is provided, which comprises an adjustable tubular member coupled to the source of fluid, rotatably mounted in a bore within the fixed tubular member. The adjustable tubular member incorporates a second array of orifices which are in a one-to-one relationship with the first array of orifices. Preferably, an electric motor is provided to rotate the adjustable tubular member varying the overlap of the first and second array of orifices, such that the magnitude of the pre-selected pressure vs stroke profile can be varied.
摘要翻译： 公开了一种用于从飞机上弹出存储器的致动器，其具有预选的力与行程曲线。 致动器包括气缸和固定管状构件，其连接到压力下的流体源，具有用于将流体流入气缸的第一阵列孔。 提供活塞组件，其适于接合和弹出商店。 所述组件可滑动地安装在所述气缸内并且可从第一位置可伸缩地移动到所述固定管状构件上方，其中所述活塞组件将所述第一阵列阵列的一部分覆盖到第二位置，其中所述第一阵列的孔未被覆盖。 通常，流体源的压力水平通常在活塞组件的冲程期间作为流入气缸的流动的函数而变化。 因此，选择第一阵列的每个孔的横截面面积和间距，以便在将流体施加到固定管状构件上时保持在气缸内的期望的预选压力与行程轮廓，如初始覆盖 第一阵列的孔的一部分在中风期间未被覆盖。 因此，在开始流体流动时，第一阵列的孔将流体以足以维持其中预选压力与冲程曲线的速率将流体计量到气缸中。 提供了用于改变气缸内的压力与行程轮廓的大小的系统，其包括联接到流体源的可调节管状构件，其可旋转地安装在固定管状构件中的孔中。 可调管状构件包括与第一孔阵列成一对一关系的第二孔阵列。 优选地，提供电动马达以使可调管状构件旋转，改变第一和第二孔阵列的重叠，使得可以改变预先选择的压力与行程曲线的大小。
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公开(公告)号：US4347777A
公开(公告)日：1982-09-07
申请号：US194148
申请日：1980-10-06
CPC分类号： B64D7/08
摘要： A store carrier having automatic sway bracing which includes two sway braces located symmetrically at a span larger than a pair of inner suspension hooks and smaller than a pair of outer suspension hooks. When a store is loaded on either the inner or outer pair of hooks and the hooks close, a pair of spring loaded tapered wedges on each side of vertically moveable sway brace supporting columns are released to slide and wedge against mating tapered surfaces on the sway brace column thereby locking the sway braces against the loaded store. The wedges are compliant in that they are spring biased against the sliding surface so as to avoid unloading the wedge when subjected to vibratory loads. The wedges are thus prevented from excessive tightening when subject to vibration. At hook opening the tapered wedges are driven with the hooks to cocked positions ready to accept the next store.
摘要翻译： 具有自动摇摆支撑的商店承载架，其包括两个摆动支架，所述两个摇摆支架对称地位于比一对内悬挂钩大的跨度处，并且小于一对外悬挂钩。 当一个商店装在内侧或外侧的一对钩子上并且钩子关闭时，在垂直移动的摇摆支架支柱的每一侧上的一对弹簧加载的锥形楔形件被释放以滑动并楔在摆动支架上的配合锥形表面 从而将摆动支架锁定在装载的商店上。 楔子是顺从的，因为它们被弹簧偏置在滑动表面上，以便在受到振动载荷时避免卸载楔形件。 因此，当受到振动时，楔形物被防止过度的紧固。 在钩子打开时，锥形楔形件由钩子驱动，以准备好接受下一个商店。
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56.发明授权
公开(公告)号：US4318561A
公开(公告)日：1982-03-09
申请号：US84347
申请日：1979-10-12
CPC分类号： B64D7/08
摘要： A device for suspending and wedging loads under aircraft ensures, through a central control, the wedging of a load carried under an aircraft at a level determined by a pair of suspension hooks subjected to balanced stresses. The central control is obtained by sleeves which slide vertically under the action of rotary shafts and bevel-tooth gears, the vertical translation of these sleeves ensuring the downward movement of parts of bearings engaging the load.
摘要翻译： 用于在飞机下悬挂和楔入负载的装置确保通过中央控制器在由平衡应力的一对悬挂钩确定的水平下承载在飞行器下的负载的楔入。 中央控制是通过在旋转轴和斜齿齿轮的作用下垂直滑动的套筒获得的，这些套筒的垂直平移确保了承载部件的向下运动。
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57.发明授权Ejector release unit for airborne stores having lockable sway brace assembly 失效用于具有可锁定摇摆支架组件的机载商店的推出器释放单元
公开(公告)号：US4196879A
公开(公告)日：1980-04-08
申请号：US877530
申请日：1978-02-13
申请人： Samuel W. Craigie
发明人： Samuel W. Craigie
CPC分类号： B64D7/08
摘要： An ejector release unit comprising a pair of hooks for supporting a store and an ejection device for ejecting a store supported by the hooks also includes, adjacent each hook, a sway brace assembly comprising a pair of pads for engagement with the upper surface of a store supported by the hooks, the pads being so mounted that during loading of a store they are free to yield, but at the completion of loading are locked firmly in position in contact with the surface of the store by way of irreversible mechanical connections exerting a thrust on the pads and resisting reverse movement. Each irreversible connection includes a slideable member having an end surface co-operating with a wedge-shaped surface on a vertically slideable member. The vertically slideable members may be held in an upper position against the effect of a downward bias by a latch engaging recesses in the sides of the members and withdrawn simultaneously by an interlock linkage coordinated with the locking of the hooks in the closed position, whereafter the members move downwardly to engage and lock the respective slideable members and hence the pads.
摘要翻译： 一种喷射器释放单元，包括一对用于支撑储存器的钩子和用于弹出由钩子支撑的商店的弹出装置，还包括在每个钩子附近的摇摆支架组件，该摇摆支架组件包括一对垫，用于与商店的上表面接合 由钩支撑，垫被安装成使得在商店的装载期间它们可以自由地产生，但是在装载完成时，通过不可逆的机械连接施加推力将其牢固地锁定在与储存器的表面接触的位置 在垫上并抵抗反向运动。 每个不可逆连接包括可滑动构件，其具有与竖直可滑动构件上的楔形表面配合的端面。 可垂直滑动的构件可以通过在构件的侧面中的闩锁接合凹部而被保持在上部位置，以抵抗向下偏置的作用，并且通过与钩在闭合位置中的锁定协调的联锁连杆同时撤回， 构件向下移动以接合和锁定相应的可滑动构件并因此锁定衬垫。
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公开(公告)号：US4122754A
公开(公告)日：1978-10-31
申请号：US822125
申请日：1977-08-05
申请人： Clayton E. Panlaqui , Lloyd J. Holt
发明人： Clayton E. Panlaqui , Lloyd J. Holt
CPC分类号： B64D7/08
摘要： Automatic sway brace mechanism for restraining stores mounted on an aircraft. Cam actuated paired sets of sway braces terminating in store engaging pads are arranged to provide a positive self-centering force equalization arrangement wherein said sway brace mechanism is automatically moved from a retracted to a store engaging position and back to a retracted position under positive control.
摘要翻译： 用于限制安装在飞机上的商店的自动摇摆支架机构。 凸轮致动的配对组终止于存储接合垫中的摆动支架被布置成提供正自动对中力均衡装置，其中所述摆动支架机构在正向控制下自动地从缩回位置移动到存储器接合位置并返回到缩回位置。
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公开(公告)号：US3982466A
公开(公告)日：1976-09-28
申请号：US497405
申请日：1974-08-14
申请人： Curtis K. Baker
发明人： Curtis K. Baker
CPC分类号： B64D7/08
摘要： A quick release mechanism for a single hook bomb rack which is arranged so that forced overlatch or hypersensitive triggering is minimized by inherent self-adjustment of the individual members comprising the quick release mechanism.The mechanism includes two initially vertically aligned links fixedly secured to an enclosing housing at a proximal end by a fixed pin and having an initially horizontally aligned array of three additional links extending to one side of the distal end of the two vertically aligned links. A member to be released has a tip bearing against an inner surface of the second of the horizontally aligned links and has a tension spring connected between a projecting ear of the released member and the third of the horizontally aligned links. A thrust link supplies force to the junction of the vertically aligned links causing them to toggle and assume a bent knee configuration; simultaneously the first two of the horizontally aligned links are urged to rotate upwardly as though these two links were one (by means of complementary shoulders at their abutting ends) to thereby free the member to be released. The unitary rotation of the first two of the horizontally aligned links also pulls the third of the horizontally aligned links towards the vertically aligned links and forces it to rotate upwardly also.
摘要翻译： 用于单钩炸弹架的快速释放机构，其被布置成使得通过包括快速释放机构的各个构件的固有自调节来最小化强制重叠或过敏触发。
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公开(公告)号：US3954233A
公开(公告)日：1976-05-04
申请号：US557980
申请日：1975-03-13
CPC分类号： B64D7/08
摘要： This device for automatically releasably hanging and holding against lateral oscillation load carried under aircrafts has load suspension hooks and holding members preventing the lateral oscillation of the load which project very moderately from the underface of a closed casing containing the actuating mechanism. This mechanism includes in combination linkage detents and springloaded devices disposed on either side of each load suspension hook. A certain delay is introduced into the action whereby when the load is lifted for engagement with the hooks, these are actuated to their load-supporting position and release with a predetermined time-lag the linkage holding the load against lateral oscillation to their operative position. To this end, each pivotally mounted hook is connected via a spring-loaded piston-and-cylinder actuator to a rocker controlling the movement of wedge members controlling in turn a lever supporting the holding members.
摘要翻译： 用于自动可拆卸地悬挂和保持在飞行器下承受的横向振荡负载的装置具有负载悬挂钩和保持构件，其防止负载的横向振荡，其从包含致动机构的封闭壳体的底部非常适度地突出。 该机构包括组合的联动棘爪和设置在每个负载悬挂钩的任一侧上的弹簧装置。 在该动作中引入一定的延迟，当负载被提升以与钩接合时，它们被致动到其负载支撑位置并且以预定的时间延迟释放以将负载横向振荡保持在其操作位置。 为此，每个枢转安装的钩通过弹簧加载的活塞和缸致动器连接到控制楔形构件运动的摇杆上，所述楔形构件又控制支撑保持构件的杆。
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