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公开(公告)号：US4736669A
公开(公告)日：1988-04-12
申请号：US17777
申请日：1987-02-20
Applicant: Kenneth R. Long , Gary D. Poole , David A. Witt , Ronald L. Dale
Inventor： Kenneth R. Long , Gary D. Poole , David A. Witt , Ronald L. Dale
Abstract: A missile launcher is disclosed having an elongate planar platform (28) formed integral with the body of the launcher (26). Plural bomb rack fasteners (34, 36) and pylon mounting lugs (38, 40) are fixed to the platform surface (28) to accommodate different aircraft types. Plural sway braces (46) are removably fixed to the side edges of the platform surface (28). Each sway brace (46) can be fixed to desired positions along the side edges of the platform surface (28) to also accommodate different aircraft type mounting apparatus.
Abstract translation: 公开了一种具有与发射器（26）的主体一体形成的细长平面平台（28）的导弹发射器。 多个炸弹架紧固件（34,36）和塔架安装凸耳（38,40）固定到平台表面（28）以适应不同的飞机类型。 多个摇摆支架（46）可移除地固定到平台表面（28）的侧边缘。 每个摆动支架（46）可以沿着平台表面（28）的侧边缘固定到期望的位置，以适应不同的飞机型安装装置。
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公开(公告)号：US4448373A
公开(公告)日：1984-05-15
申请号：US216460
申请日：1980-12-15
Applicant: Jack R. Bates , John W. Holtrop
Inventor： Jack R. Bates , John W. Holtrop
Abstract: An elastomeric sway bracing and ejector system for aircraft is provided bywo different apparatus. In one, an elastomeric cushion is placed on the aircraft in a position to be crushed by a carried aircraft store. In the other, an elastomeric bladder is filled with gas, which is compressed to the sway brace store. This acts as a cushion between the aircraft and the store. In both apparatus, the release of the store permits it to be ejected by the compressed force of the elastomeric material. Insertion of pressurized sections in the elastomeric cushion permit both the cushion and the bladder to be inflated by different air pressures to control the resilient force exerted against the store.
Abstract translation: 用于飞机的弹性摇摆支撑和喷射器系统由两种不同的装置提供。 在一个中，弹性垫子被放置在飞机上被被携带的飞机商店压碎的位置。 另一方面，弹性气囊被气体填充，气体被压缩到摇摆支架存储器。 这作为飞机和商店之间的坐垫。 在两个装置中，商店的释放允许其通过弹性体材料的压缩力而被弹出。 在弹性垫中插入加压部分允许衬垫和气囊通过不同的气压膨胀以控制施加在商店上的弹性力。
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23.发明授权Device for suspending under aircraft miscellaneous loads with variable distance between centers 失效用于在飞机之间悬挂的装置，中心之间的距离可变
公开(公告)号：US4395003A
公开(公告)日：1983-07-26
申请号：US272845
申请日：1981-06-12
Applicant: Pierre F. Coutin
Inventor： Pierre F. Coutin
CPC classification number: B64D7/08
Abstract: Device for carrying under aircraft multiple loads disposed at variable distances between centers, the modification of the distance between centers being obtained by rotating load supports about longitudinal axes by means of bearings provided in the frame structure of the carrier device. Each load support may be rigid with circular sets of teeth engaged by matching teeth formed on arms fulcrumed by means of eccentric pins on the frame structure and controlled for a same load support by cam device rigid with a common shaft.
Abstract translation: 用于在飞行器下承载多个负载在中心之间可变距离的负载的装置，通过借助于设置在承载装置的框架结构中的轴承使负载支撑件围绕纵向轴线旋转来获得中心之间的距离的修改。 每个负载支撑件可以是刚性的，圆形组的齿通过匹配在由框架结构上的偏心销支撑的臂上形成的齿啮合，并且通过与公共轴刚性的凸轮装置控制相同的负载支撑。
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公开(公告)号：US4356770A
公开(公告)日：1982-11-02
申请号：US92898
申请日：1979-11-09
Applicant: John V. Atanasoff , W. Kenneth Clark , David Henderson , Kenneth W. Wreghitt
Inventor： John V. Atanasoff , W. Kenneth Clark , David Henderson , Kenneth W. Wreghitt
CPC classification number: B64D7/08 , F42B10/26 , F42B12/04 , F42B12/10 , F42B15/105
Abstract: In a munitions system, a cylindrical canister is fired over a target. The canister carries a target sensing infrared device and, when a target is detected, a projectile is fired downward from the bottom of the overflying missile. A spinning motion is imparted to the missile to stabilize its flight, and a wobbling motion is imparted to the missile to provide a larger target area. The projectile forms a concave lower end to the missile and is fired by an explosive charge.
Abstract translation: 在一个弹药系统中，一个圆柱形罐被射出一个目标。 所述罐携带目标感测红外线装置，并且当检测到目标时，从所述飞越的底部向下射出射弹。 向导弹传递旋转动作以稳定其飞行，并且向导弹施加摆动的动作以提供更大的目标区域。 射弹形成导弹的凹下端，并被炸药引爆。
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公开(公告)号：US4299157A
公开(公告)日：1981-11-10
申请号：US106790
申请日：1979-12-26
Applicant: Dallas D. Burns , Jack D. Brannan
Inventor： Dallas D. Burns , Jack D. Brannan
CPC classification number: B64D7/08
Abstract: An arming wire extractor controlled tension device for an aircraft delive weapon comprising a controlled tension device which comprises a coil of wound wire with a straight end that is pulled through an orifice that allows the application of a force for extracting the arming wire such that it yields a relatively constant force and the angle of pull through the orifice is not a significant variable in firing.
Abstract translation: 一种用于飞行器提供的武器的布线提拉器控制的张紧装置，包括受控张力装置，该张力装置包括卷绕的线圈，该线圈具有直的端部，该直线线圈允许施加用于提取布线的力，使得其产生 相对恒定的力和通过孔的拉动角度在烧制中不是重要的变量。
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Patent Agency Ranking
公开(公告)号：US4202576A
公开(公告)日：1980-05-13
申请号：US949484
申请日：1978-10-06
Applicant: Jean H. Hasquenoph , Pierre F. Coutin
Inventor： Jean H. Hasquenoph , Pierre F. Coutin
CPC classification number: B64D7/08
Abstract: This device for locking on fixed support loads carried under aircraft comprises, between the suspension rings or saddles of the load and the fixed structure of the aircraft, a pair of spaced pivot pins having fulcrumed thereon a pair of symmetrically opposed bell-crank levers having in turn one arm pivotally connected to a suspension hook and the other arm pivotally connected to a common stretching device, the fulcri of the levers having each also pivoted thereto a radial link having its free end pivoted to a pair of links connected the one to a central rocker and the other to the relevant hook, the rocker being responsive to a detent-positioning device. Due to the provision of adequate extensions of the stretching device and of the hooks, completed by another pair of links, another pair of hooks disposed externally and in coplanar relationship to the first pair may be provided for accommodating indifferently loads having either suspension rings or saddles disposed at one standard distance between centers or other suspension rings or saddles disposed at another standard distance between centers.
Abstract translation: 用于锁定在飞机下承载的固定支撑载荷上的该装置包括在悬挂环或负载的鞍座和飞行器的固定结构之间的一对间隔开的枢轴销，其上支撑有一对对称的相对的钟形曲柄杆， 转动一个可枢转地连接到悬挂钩的臂，另一个臂可枢转地连接到一个共同的拉伸装置上，杠杆的每一个都具有一个径向连杆，该自由端枢转到一对连杆， 摇杆和另一个到相关的钩子，摇杆响应于定位装置。 由于提供了由另一对链节完成的拉伸装置和钩子的适当延伸，可以提供另外一对布置在外部并且与第一对共同关系的钩，以容纳具有悬挂环或鞍座的无差异载荷 设置在中心之间的一个标准距离处，或设置在中心之间另一标准距离处的其他悬挂环或鞍座。
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27.发明授权
公开(公告)号：US4168047A
公开(公告)日：1979-09-18
申请号：US866899
申请日：1978-01-04
Applicant: Jean H. Hasquenoph , Pierre F. Coutin
Inventor： Jean H. Hasquenoph , Pierre F. Coutin
Abstract: This hoisting device for loads to be carried under aircraft is incorporated partially or completely in a load carrier system without requiring any lateral access, the connection between the hoisting device and the load being eliminated automatically once the load is properly anchored to the carrier system. The device comprises one or two ropes, as the case may be, and comprises an anchoring member rigid with the load and formed with an internal groove engageable by a set of balls carried by a socket in which an end piece crimped to the rope end is adapted to travel axially through a limited extent. Slackening the rope will free the load which is then retained by the carrier system.
Abstract translation: 用于承载在飞行器下的负载的起重装置部分地或完全地并入载重系统中，而不需要任何横向进入，一旦载荷适当地锚定到载体系统，起重装置和载荷之间的连接就被自动消除。 该装置包括一个或两个绳索，视情况而定，并且包括与该负载刚性的锚定构件，并且形成有内凹槽，该内槽可由一套由一个插座承载的球接合，其中端部件压接到绳索端部 适于在有限程度上轴向行进。 松动绳索将释放载体系统所保留的载荷。
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公开(公告)号：US4132147A
公开(公告)日：1979-01-02
申请号：US828365
申请日：1977-08-29
Applicant: Attilio Contaldo
Inventor： Attilio Contaldo
CPC classification number: B64D7/08 , Y10T403/1624 , Y10T403/535 , Y10T403/583
Abstract: A retention and release mechanism utilizes a collet with deflectable fingers to allow assembly of the mechanism onto an object which is to be retained. Movement of the object toward the mechanism causes a force to be exerted on the bottom end of a plunger and movement of the plunger, which is coupled to a lockpin by a plurality of spherical balls and a split ring, from a released to a retained position. In the retained position, the balls secure the lockpin in a fixed position relative to the collet while mating tapered surfaces at the ends of the collet fingers and the lockpin cooperate to retain the object to which an expendable bushing has been attached, the bushing being part of the mechanism. To release the object, a force must be exerted on the top end of the plunger to move it to an axial position wherein the balls are released from their fixed position relative to the collet and the mating tapered surfaces move away from each other. The weight of the object causes the fingers to deflect inwardly, releasing the object.
Abstract translation: 保持和释放机构利用具有可偏转的手指的夹头，以允许机构组装到待保持的物体上。 物体朝向机构的运动导致作用在柱塞的底端上的力和柱塞的运动，柱塞通过多个球形球和分隔环联接到锁定销，从释放位置到保持位置 。 在保持位置中，滚珠将锁定销固定在相对于夹头的固定位置，同时在夹头和端子之间配合锥形表面配合以保持已安装有消耗性衬套的物体，衬套为零件 的机制。 为了释放物体，必须施加在柱塞的顶端上的力以将其移动到轴向位置，其中球相对于夹头从其固定位置释放，并且配合的锥形表面彼此远离。 物体的重量使手指向内偏转，释放物体。
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公开(公告)号：US3967528A
公开(公告)日：1976-07-06
申请号：US458141
申请日：1974-04-05
Applicant: Curtis K. Baker
Inventor： Curtis K. Baker
CPC classification number: B64D7/08
Abstract: A single station bomb rack includes two cantilevered sway brace arms each ovided with two oppositely placed sway bolts. The sway brace arms are shaped to accomodate a variety of store shapes and each of the sway brace arms acts in a spring-like fashion under loading. The sway bolts are each provided with internal springs which assure continuous pad-to-store contact. Each sway bolt is provided with a force indicating means which signals that sufficient force has been applied to the sway bolt thereby preventing unnecessary down-hook forces on the bomb rack hook.
Abstract translation: 单站炸弹架包括两个悬臂摆动支架臂，每个悬臂支架臂均设有两个相对放置的摇摆螺栓。 摆动支架臂被成形为适应各种商店形状，并且每个摆动支架臂在加载下以类似弹簧的方式起作用。 摇摆螺栓均设有内部弹簧，确保连续的垫到存储器的接触。 每个摇摆螺栓都设有一个力指示装置，该指示装置指示足够的力已经施加到摇摆螺栓上，从而防止炸弹架钩上不必要的下垂力。
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公开(公告)号：US3942409A
公开(公告)日：1976-03-09
申请号：US440886
申请日：1974-02-08
Applicant: Lawrence W. Baldwin , Avinoam S. Zerkowitz
Inventor： Lawrence W. Baldwin , Avinoam S. Zerkowitz
Abstract: A digital launch sequence timing network in a single rail launcher which interprets signals from the aircraft and generates the signals necessary to automatically prepare and launch a missile. In order to launch the missile, a number of signals must be sent from the launcher to the missile in a particular time sequence. The launcher must first send an activate pulse to the missile battery which lasts for a predetermined amount of time, until the missile battery reaches its operational condition. Next, the launcher delivers a pulse to activate the missile rocket motor to provide the propulsion needed by the missile when it leaves the launcher. The preparation steps needed to prepare and launch the missile must take place in an exact time sequence which is provided by the digital timing network, composed of several shift registers. The single rail launcher is used for carrying and launching the maverick missile.
Abstract translation: 在单轨发射器中的数字发射序列定时网络，其解释来自飞行器的信号并产生自动准备和发射导弹所需的信号。 为了发射导弹，必须以特定的时间顺序从发射器发送许多信号到导弹。 发射器必须首先向导弹电池发送激活脉冲，持续预定的时间，直到导弹电池达到其运行状态。 接下来，发射器发出一个脉冲来激活导弹火箭发动机，以便在离开发射器时提供导弹所需的推进。 准备和发射导弹所需的准备步骤必须以数字定时网络提供的确切时间顺序进行，数字定时网络由多个移位寄存器组成。 单轨发射器用于携带和发射特立独行导弹。
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