Dispensed guided submunition
    71.
    发明授权
    Dispensed guided submunition 失效
    分配导弹子弹药

    公开(公告)号:US4554871A

    公开(公告)日:1985-11-26

    申请号:US553677

    申请日:1983-11-21

    Inventor: Richard G. Nixon

    Abstract: A missile such as a projectile (11) carries at least two submunitions (13, 14) each of which has an active guidance capability. Each submunition (13, 14) has a forward end (21) which is slanted, creating an asymmetric shape for the submunition (13, 14). When the projectile (11) reaches a predetermined point in its trajectory, the submunitions (13, 14) are dispensed in a manner which causes the submunitions (13, 14) to acquire different flight paths. The guidance system on each submunition (13, 14) relies on the asymmetrical shape of the submunition (13, 14) to cause the submunition (13, 14) to precess about its center axis, thus creating an appropriate search pattern, such as a rosette search pattern. The asymmetric shape of the submunitions (13, 14) can also be used to control the flight path of the submunition (13, 14) after a suitable target has been acquired by the submunition's guidance system. The inventive arrangement gives the submunitions (13, 14) the ability to search, acquire, track, hit and defeat in a package with minimum dimensions and with minimum complexity.

    Abstract translation: 诸如射弹(11)的导弹至少携带两个子弹药(13,14),每个弹药具有积极的引导能力。 每个子弹药(13,14)具有倾斜的前端(21),为子弹药(13,14)产生非对称形状。 当弹丸(11)到达其轨迹中的预定点时,子弹药(13,14)以使得子弹药(13,14)获取不同飞行路径的方式被分配。 每个子弹药(13,14)的引导系统依赖于子弹药(13,14)的不对称形状,使子弹药(13,14)进入其中心轴线,从而形成适当的搜索模式,如 玫瑰花搜索模式。 子弹药(13,14)的不对称形状也可用于在子弹药引导系统获得合适目标之后,控制子弹药(13,14)的飞行路径。 本发明的布置使子弹药(13,14)能够以最小尺寸和最小的复杂性在包装中搜索,获取,追踪,打击和失败。

    Process and apparatus for transporting and dropping a plurality of
charges contained in a single container and container equipped with
such an apparatus
    72.
    发明授权
    Process and apparatus for transporting and dropping a plurality of charges contained in a single container and container equipped with such an apparatus 失效
    用于运送和丢弃容纳在装有这种装置的单个容器和容器中的多个电荷的方法和装置

    公开(公告)号:US4372215A

    公开(公告)日:1983-02-08

    申请号:US151669

    申请日:1980-05-20

    Applicant: Roger Crepin

    Inventor: Roger Crepin

    CPC classification number: F42B12/62 B64D1/04 F42B10/56 F42C15/295

    Abstract: The invention concerns a process and apparatus for transporting and dropping a plurality of charges contained in a single container. Within the shell of the container is arranged a plurality of modules, the bodies of which contain a charge, which may particularly be military; said modules are extracted one by one, upon command, through the rear of the shell. This extraction can take place only if a general mechanical control element has moved from a position called the "safety" position to a position called the "cocked" position, a movement which can take place only when the means for fastening the container has been released from the lug holding it to the carrier vehicle. The invention is applied particularly to modular bombs having fragmentable modules designed for neutralization of relatively widespread ground targets.

    Abstract translation: 本发明涉及一种用于运送和放下包含在单个容器中的多个电荷的方法和装置。 在容器的外壳内布置有多个模块,其中的主体包含电荷,其可以是军事的; 说明的模块是按照命令一个一个的提取,通过后壳。 只有当一般的机械控制元件从称为“安全”位置的位置移动到称为“准备”位置的位置时才能进行该提取,只有当用于紧固容器的装置已被释放时才能发生的移动 从将其固定到载体车辆的接头。 本发明特别适用于具有设计用于中和相对广泛的地面目标的可分割模块的模块式炸弹。

    Two stage parachute fuze recovery system
    73.
    发明授权
    Two stage parachute fuze recovery system 失效
    双级降落伞引信恢复系统

    公开(公告)号:US4333400A

    公开(公告)日:1982-06-08

    申请号:US117702

    申请日:1980-02-01

    CPC classification number: F42B10/56 F42C21/00

    Abstract: A two stage parachute recovery system for use in recovering fuzes or otherensitive equipment from a projectile that has been launched from a gun barrel wherein explosive means are successively detonated by a timing mechanism and by centrifugal force imparted to the projectile respectively so as to deploy each of the said parachutes and to thereby recover the fuze before impact.

    Abstract translation: 一种双级降落伞恢复系统,用于从枪管发射的射弹中回收fuzes或其他敏感设备,其中爆炸装置通过定时机构相继引爆,并通过离心力分别施加到射弹, 的降落伞,从而在冲击之前恢复引信。

    Surface-launched fuel-air explosive minefield clearance round
    74.
    发明授权
    Surface-launched fuel-air explosive minefield clearance round 失效
    燃油表面喷射爆炸雷区清扫

    公开(公告)号:US4273048A

    公开(公告)日:1981-06-16

    申请号:US24132

    申请日:1979-03-26

    CPC classification number: F42B10/56 F41H11/12 F42B12/52

    Abstract: A fuel-air explosive weapon launched from a remote distance is used for clearing minefields. A set timing pattern in the operation of the minefield clearance round permits varied range through retarding the length of time that a programed sequence of events occurs at the launch site. Upon flight, the round follows a predetermined pattern in deployment of a parachute, firing cloud detonators and initiation of a burster charge. An extendable probe at the front of the round permits detonation at a predetermined level above ground. The descent by parachute provides a relatively stable launching platform for cloud detonators if they are fired prior to the burster charge detonation for dispersal of the fuel-air cloud.

    Abstract translation: 从远处发射的燃油爆炸武器用于清雷雷区。 排雷周期运行中的设定时间模式允许通过延迟发射现场发生的编程顺序事件的时间长短来改变范围。 在飞行中,圆形按照预定的方式进行降落伞的部署,发射云雷管并引发爆胎。 在圆形前部的可伸缩探头允许在地面以上预定水平的爆震。 降落伞的下降为云雷管提供了一个相对稳定的发射平台,如果它们在燃烧空气云散布爆炸炸药爆炸之前被射击。

    Short range guided missile
    75.
    发明授权
    Short range guided missile 失效
    短距离引导的MISSILE

    公开(公告)号:US3827655A

    公开(公告)日:1974-08-06

    申请号:US32813163

    申请日:1963-12-04

    Applicant: US NAVY

    CPC classification number: F41G7/36 F42B10/56 F42B15/20 F42B15/22 F42B17/00

    Abstract: A submarine launched missile having a solid propellant rocket motor portion and a weapon portion is adapted for guidance from the water through the air and after motor burn out, followed by motor and weapon separation, aerodynamic steering of the weapon to the target point by a terminal guidance system for control of movable surfaces on the weapon.

    Abstract translation: 潜艇发射具有固体推进剂火箭发动机部分的导弹和武器部分适于从水中通过空气引导并且在电动机燃烧之后,随后进行电动和武器分离,由终端将武器气动转向目标点 用于控制武器上活动表面的指导系统。

    Parachute pack with release mechanism
    76.
    发明授权
    Parachute pack with release mechanism 失效
    PARACHUTE包装与释放机制

    公开(公告)号:US3817179A

    公开(公告)日:1974-06-18

    申请号:US56733566

    申请日:1966-07-21

    Applicant: US NAVY

    Inventor: LUDTKE W PETERSON C

    CPC classification number: F42B10/56

    Abstract: 1. A parachute assembly for an aircraft launched mine comprising, A RUPTURABLE CASING WHEREIN THE PARACHUTE IS INITIALLY DISPOSED IN A FOLDED CONDITION, A STATIC LINE CONNECTED BETWEEN SAID PARACHUTE AND THE AIRCRAFT, MEANS FOR RETAINING SAID STATIC LINE IN A FOLDED CONDITION UNTIL AFTER MINE LAUNCHING AND THEN RELEASING SAID STATIC LINE TO PERMIT MAXIMUM EXTENSION THEREOF, A RELEASE MECHANISM INITIALLY CONNECTED TO THE MINE, A RISER LINE CONNECTED BETWEEN SAID PARACHUTE AND SAID RELEASE MECHANISM FOR EFFECTING SPACING OF SAID RELEASE MECHANISM AND MINE FROM SAID PARACHUTE, MEANS FOR RETAINING SAID RISER LINE IN A FOLDED CONDITION UNTIL AFTER MINE LAUNCHING AND THEN RELEASING SAID RISER LINE TO PERMIT MAXIMUM EXTENSION THEREOF, AND MEANS FORMED ON SAID CASING FOR EFFECTING RUPTURING THEREOF UPON MAXIMUM EXTENSION OF SAID RISER LINE AND SAID STATIC LINE THEREBY EFFECTING RELEASE OF SAID PARACHUTE FROM SAID CONTAINER BY SAID STATIC LINE.

    Abstract translation: 1.一架飞机发射的降落伞组件,包括:在可折叠的状态下初始处置的“可拆卸的空挡”,与“飞机之间”相连的静止线,用于在矿井之后保持折叠状态下的静止线 发射,然后释放使静止线达到最大延伸范围,初始连接到矿井的释放机构,用于影响同位置释放机构和地雷的同位素和同位素释放机构之间连接的上升线,用于保留所述 在启动后,经过折叠状态的上升线,然后释放使得上升器允许最大延伸,并且意味着在最大限度地延长上升线和上述静态线之间进行遏制,从而有效地释放所述的附件 通过标准静态线的集装箱。

    Chaff dispenser, method of dispersing chaff
    77.
    发明授权
    Chaff dispenser, method of dispersing chaff 失效
    CHAFF分配器,分配方法

    公开(公告)号:US3797394A

    公开(公告)日:1974-03-19

    申请号:US3797394D

    申请日:1972-09-11

    Inventor: THURSTON J ADAMS G

    CPC classification number: F42B10/56 F42B12/70

    Abstract: A chaff dispenser for signals and other uses, which ejects from a moving craft and disperses the signal material after a pre-set delay time, comprises an outer case, a canister holding the chaff and explosive charge, a timer, and a parachute. Upon ejection, the timer measures the delay time, releases itself and the parachute which pulls the canister from the outer case. The canister explodes to disperse the chaff. The invention herein described was made in the course of or under contract with the U.S. Air Force (Contract F33657-72-C-0136).

    Abstract translation: 用于信号和其他用途的谷壳分配器,其从移动的工艺喷射并在预设的延迟时间之后分散信号材料,包括外壳,容纳谷壳和炸药的罐,定时器和降落伞。 在弹出时,定时器测量延迟时间,释放自身和从外壳拉出罐的降落伞。 罐子爆炸分散谷壳。 本文所述的发明是在与美国空军(合同F33657-72-C-0136)的合同或合同下进行的。

    Parachute retarding tail assembly for bomb
    78.
    发明授权
    Parachute retarding tail assembly for bomb 失效
    BOMB的PARACHUTE延迟尾料总成

    公开(公告)号:US3749017A

    公开(公告)日:1973-07-31

    申请号:US3749017D

    申请日:1971-12-07

    Applicant: US NAVY

    Inventor: PETERSON C

    CPC classification number: F42B10/56

    Abstract: A drop bomb usable in a retarded and an unretarded mode at the option of the aircraft pilot, having tail fins and a parachute within a cannister in the tail section. The parachute may be deployed for the retarded mode by retaining at the aircraft a lanyard attached to an arming wire associated with a ball lock release mechanism which holds a spring loaded cover on the parachute cannister. For the unretarded deployment, the lanyard is not retained at the aircraft, but falls with the bomb and the ball lock mechanism is not activated.

    Controlled descent system
    79.
    发明授权
    Controlled descent system 失效
    控制系统

    公开(公告)号:US3730099A

    公开(公告)日:1973-05-01

    申请号:US3730099D

    申请日:1970-12-17

    Applicant: US NAVY

    Inventor: SCHOPP L

    CPC classification number: F42B10/56

    Abstract: A descent retarding system for an airdropped store is provided by a multistage canister allowing timed, sequential deployment of a parachute and parawing. Following ejection of the store, split half rings and a cover are removed from one end for deployment of a deceleration parachute. After a delay provided by a mechanical or pyrotechnic timer, a retaining member is removed from a parawing compartment allowing resilient, longitudinal finger-like sections of the compartment housing to spring outwardly allowing rapid deployment of an accordion-folded parawing. The parachute is jettisoned once the parawing has inflated.

    Abstract translation: 用于空投储存器的下降延迟系统由多级罐提供,允许定时,顺序地部署降落伞和解码。 在商店出售之后,从一端拆下分开的半环和盖子,以部署减速伞。 在由机械或烟火计时器提供的延迟之后,将保持构件从变形隔间移除,允许隔室壳体的弹性的纵向手指状部分向外弹出,允许快速展开手风琴折叠的解码。 一旦解剖膨胀,降落伞就会被抛弃。

    Method and apparatus for suppression of antiaircraft fire
    80.
    发明授权
    Method and apparatus for suppression of antiaircraft fire 失效
    用于抑制抗病毒灭火的方法和装置

    公开(公告)号:US3727861A

    公开(公告)日:1973-04-17

    申请号:US3727861D

    申请日:1970-03-05

    Applicant: US NAVY

    Inventor: SWANN E

    CPC classification number: F42B12/625 F42B10/56

    Abstract: An aerial weapon is provided for the suppression of antiaircraft artillery fire against an air attack. This concept has been called various names in the past, notably AFIRM standing for Anti-Flak InfraRed Missile. A first rocket delivers the missile which descends on a parachute until the heat of an antiaircraft gun is sensed. A second rocket propels the missile to target under control of heat sensing guidance and control unit.

    Abstract translation: 提供一种空中武器,用于制止高射炮击打空袭。 这个概念在过去被称为各种名称,特别是AFIRM代表Anti-Flak InfraRed导弹。 第一枚火箭提供在降落伞下降的导弹,直到感觉到高射炮的热量。 第二枚火箭推动导弹在热敏指导和控制单位的控制下。

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