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1. 发明授权

US4512537A Canard control assembly for a projectile 失效
标题翻译：卡达控制组件为弹丸
公开(公告)号：US4512537A
公开(公告)日：1985-04-23
申请号：US392716
申请日：1973-08-10
申请人： George Sebestyen , Ronald R. Sinclair , John A. Smith , Timothy B. Sands , Theodore J. Nussdorfer
发明人： George Sebestyen , Ronald R. Sinclair , John A. Smith , Timothy B. Sands , Theodore J. Nussdorfer
IPC分类号： F41G7/22 , F42B13/28 , F42B15/02
CPC分类号： F41G7/222 , F41G7/2253 , F41G7/2293
摘要： Control is provided to conventional gun-fired projectiles by substituting for the standard fuze thereof a device comprising a canard frame and a main housing, which threads into the fuze well of the projectile, with the canard frame being rotatable with respect to the main housing and having deflectable canards thereon for providing vernier correction on the trajectory to the projectile.
摘要翻译：通过用标准引信代替标准的引信来对包括一个卡车框架和主壳体在内的装置进行控制，该装置将螺纹连接到射弹的引信井中，其中挡板相对于主壳体可旋转，在其上具有可偏转的挡板，用于在弹道的轨迹上提供游标校正。

2. 发明授权

US3741125A Stabilized rocket head 失效
标题翻译：稳定的摇篮头
公开(公告)号：US3741125A
公开(公告)日：1973-06-26
申请号：US3741125D
申请日：1960-11-22
申请人： US NAVY
发明人： LA POINTE A
IPC分类号： F42B12/70 , F42B13/28 , F42B13/42
CPC分类号： F42B12/70
摘要： 1. A rocket head for attachment to a spin stabilized rocket motor, said rocket head comprising, a body tube, means at the rearward end of said tube for closing said body tube and adapted for attachment to a rocket motor, a removable tube closure assembly attached to the forward end of said body tube means actuated by rotation of the rocket head for releasing said removable tube closure, a plurality of packages of loosely packed radar reflective material removably contained within said body tube; and ejection means within the tube body for ejecting said packages one at a time with a time delay therebetween upon removal from said body tube of said removable tube closure assembly from the forward end of the body tube.

3. 发明授权

US3572249A High efficiency rocket munition 失效
标题翻译：高效率摇篮运动
公开(公告)号：US3572249A
公开(公告)日：1971-03-23
申请号：US3572249D
申请日：1968-09-11
申请人： US AIR FORCE
发明人： DAVIS DALE M
IPC分类号： F42B12/20 , F42B15/00 , F42B13/28 , F42B15/24
CPC分类号： F42B12/204 , F42B15/00
摘要： A HIGH EFFICIENCY ROCKET MUNITION WHICH UTILIZES THE MOTOR CASE AS THE WARHEAD FRAGMENTATION CASE. THE WARHEAD EXPLOSIVE IS INSTALLED INSIDE THE MOTOR CASE AND PROTECTED FROM THE MOTOR HEAT BY A THIN INSULATOR. THE LETHALITY OF THE ROCKET MINITON IS INCREASED BY THE USE OF UNBURNED PORTION OF THE ROCKET MOTOR AS AN EXPLOSIVE IN THE EVENT IMPACT BEFORE BURN-OUT AND THE STABILITY OF THE SPIN STABILIZED ROCKET IS INCREASED BY DISTRIBUTING THE WEIGHT SO THAT THE AXIAL MOMENT OF INERTIA IS INCREASED WHILE THE LATERAL MOMENT OF INERTIA IS DECREASED.

4. 发明授权

US3546997A Small arms weapon 失效
标题翻译：小型武器
公开(公告)号：US3546997A
公开(公告)日：1970-12-15
申请号：US3546997D
申请日：1965-02-11
申请人： MBASSOCIATES
发明人： GOULD BERT B , BIEHL ARTHUR T , MAINHARDT ROBERT , BARTON WILLIAM D
IPC分类号： F02K9/97 , F42B13/28
CPC分类号： F02K9/97 , F42B5/025 , F42B10/04 , F42B10/06 , F42B10/08 , F42B15/00

5. 发明授权

US4763127A Fiber under foil chaff coil 失效
标题翻译：纤维在箔糠线圈下
公开(公告)号：US4763127A
公开(公告)日：1988-08-09
申请号：US822127
申请日：1986-01-24
申请人： Bradley T. Sallee
发明人： Bradley T. Sallee
IPC分类号： F41J2/00 , H01Q15/14 , F42B13/28
CPC分类号： F42B12/70 , F41J2/00 , H01Q15/145
摘要： A chaff device for exoatmospheric deployment as a countermeasure to radar detection of exoatmospheric objects utilizes a plurality of elongated foil members and a plurality of elongated fiber members, each for providing a dipole. The foil dipole members are disposed in an end-to-end overlapping relationship and wrapped in a coil configuration. The fiber dipole members in a group are disposed adjacent one of the foil dipole members so as to be sandwiched between adjacent layers of coil wrapped foil dipole members.
摘要翻译：用于大气外部部署的谷壳装置作为对大气外物体的雷达检测的对策，利用多个细长的箔构件和多个细长的纤维构件，每个用于提供偶极子。箔偶极子构件以端对端的重叠关系设置并缠绕在线圈构型中。组中的纤维偶极构件邻近一个箔偶极子构件设置，以夹在相邻的线圈缠绕的箔偶极子构件之间。

6. 发明授权

US4455943A Missile deployment apparatus 失效
标题翻译：导弹部署装置
公开(公告)号：US4455943A
公开(公告)日：1984-06-26
申请号：US295164
申请日：1981-08-21
申请人： George T. Pinson
发明人： George T. Pinson
IPC分类号： F42B12/58 , F42B15/00 , F42B13/28 , F42B13/50
CPC分类号： F42B12/58
摘要： Apparatus for deploying one or more submissiles (15) from a carrier missile (25) whereby each submissile (15) is deployed into a flight path which is initially parallel to a streamline (20) of the fluid flow contiguous to the carrier missile (25). An ejection mechanism (45) has a submissile support member (105) oriented substantially parallel to the streamline (20) at the point where the submissile (15) is separated from the support member (105). The ejection mechanism (45) also provides a minimum side force to the submissile (15) which is proportional to a speed of the carrier vehicle (25). Provisions are also made to reduce or minimize any change in the aerodynamic characteristics of the carrier missile (25) after a submissile (15) has been deployed.
摘要翻译：用于从载体导弹（25）展开一个或多个下沉（15）的装置，由此每个突变体（15）被部署到最初平行于与载体导弹相邻的流体流的流线（20）的飞行路径（25 ）。弹出机构（45）具有在该突出部（15）与支撑构件（105）分离的点处基本上平行于流线（20）定向的副突起支撑构件（105）。排出机构（45）还向与该运载工具（25）的速度成比例的该副切片（15）提供最小的侧向力。还规定了减少或最小化部署后（15）的载体导弹（25）的空气动力特性的变化。

7. 发明授权

US4095528A Vehicle with combined fuel tank/warhead 失效
标题翻译：混合燃油箱/弹头的车辆
公开(公告)号：US4095528A
公开(公告)日：1978-06-20
申请号：US763318
申请日：1977-01-28
申请人： Donald McChesney Post
发明人： Donald McChesney Post
IPC分类号： F42B15/00 , F42B13/28
CPC分类号： F42B15/00 , Y10S102/705
摘要： A vehicle driven by a combustible fuel propulsion system, in which the fuelemaining upon arrival at the target is exploded to act as a warhead. The vehicle has a fuel tank incorporated into the structure, which will hold more than enough fuel to complete the mission. The residual fuel is atomized into the vacant space in the fuel tank and mixed with air or oxygen, which can be used as the driving agent for the atomization. The fuel/air mixture is then detonated. The fuel tank may be thin walled for maximum blast effect, or be of heavier structure which is grooved for fragmentation.
摘要翻译：由可燃燃料推进系统驱动的车辆，其中在到达目标时剩余的燃料被爆炸以用作弹头。该车辆具有结合在结构中的燃料箱，其将容纳足够的燃料以完成任务。残余燃料被雾化到燃料箱的空置空间中，与空气或氧气混合，可用作雾化的驱动剂。然后将燃料/空气混合物引爆。燃料箱可以是薄壁的，以获得最大的爆炸效果，或者是更重的结构，其被开槽以用于碎裂。

8. 发明授权

US3521564A Miniature rocket 失效
标题翻译： MINIATURE ROCKET
公开(公告)号：US3521564A
公开(公告)日：1970-07-21
申请号：US3521564D
申请日：1965-10-22
申请人： MB ASSOC
发明人： GOULD BERT B , BIEHL ARTHUR T , MAINHARDT ROBERT , BARTON WILLIAM D
IPC分类号： F42B15/00 , F42B13/28
CPC分类号： F42B15/00 , F42B10/04 , F42B10/06 , F42B10/08

9. 发明授权

US3427977A Nose cone tip 失效
标题翻译： NOSE CONE提示
公开(公告)号：US3427977A
公开(公告)日：1969-02-18
申请号：US3427977D
申请日：1966-06-01
申请人： MOTT LAMBERT H
发明人： MOTT LAMBERT H
IPC分类号： F42B15/34 , F42B13/28
CPC分类号： F42B15/34

10. 发明授权

US4093154A Target seeking gyro for a missile 失效
标题翻译：目标寻找陀螺仪的导弹
公开(公告)号：US4093154A
公开(公告)日：1978-06-06
申请号：US583337
申请日：1956-05-07
申请人： William B. McLean
发明人： William B. McLean
IPC分类号： F41G7/22 , F42B13/28 , F41G7/10 , G01C19/28
CPC分类号： F41G7/2253 , F41G7/2213 , F41G7/2293 , Y10T74/125
摘要： 37. In combination in a missle guidance system, a target seeking apparatus having radiation responsive means including a scanner, a gyroscope having a rotor, said scanner being mounted on said rotor for picking up radiation from a target, means for precessing said gyroscope rotor to align its axis with the sight line to said target, said radiation responsive means producing a signal when the gyroscope rotor axis deviates from alignment with the sight line to said target, said signal having a time phase dependent on the radial direction of departure of said target from the gyro rotor axis, the precessing means embodying mechanism responsive to the phase of said signal whereby said gyro is precessed in the proper sense to align its axis with the line of sight to said target, a position sensing means included in said target seeking apparatus and mounted adjacent said gyro rotor for sensing the position of said gyro rotor, and servo means responsive to signals from said gyro rotor position sensing means for guiding said missile.38. A target seeking device for a guided missile comprising a gyroscopically stabilized means for optically scanning a limited region about a first coordinate axis for electromagnetic radiations emanating from a target source, said means including a permanent magnet rotor rotatable with said gyroscopic means about said first axis, the magnetic poles of said permanent magnet defining a second coordinate axis transverse to said first coordinate axis, a radiation sensitive means for producing electrical signal variations in response to variations in radiation incident on said radiaton sensitive means, said radiation sensitive means being fixedly positioned relative to said scanning means for receiving said radiations from said scanning means to cause said electrical signals generated thereby to vary in magnitude with the directional displacement of said target with respect to said first coordinate axis and in time phase with the polar angular position of said target with respect to the second coordinate axis, and means interacting with said permanent magnet rotor responsive to said signal for applying a magnetic force to said gyroscopically stabilized means having a component normal to said second axis and in a direction causing said gyroscopically stabilized means to precess through an angle and in a direction to bring said first coordinate axis into directional alignment with said target source.
摘要翻译： 37.一种在引导引导系统中的目标搜索装置，具有包括扫描器的放射线响应装置，具有转子的陀螺仪，所述扫描器安装在所述转子上用于拾取来自目标的辐射，用于将所述陀螺仪转子进动到将其轴线与瞄准线对准所述目标，所述辐射响应装置在陀螺仪转子轴线偏离与瞄准线对准所述目标时产生信号，所述信号具有取决于所述目标的径向离开方向的时间相位从陀螺仪转子轴，进动装置体现机构响应于所述信号的相位，由此所述陀螺仪在正确的意义上被进动以使其轴线与所述目标的视线对准，包括在所述目标寻找装置中的位置检测装置并且安装在所述陀螺仪转子附近，以感测所述陀螺仪转子的位置，以及响应于来自所述陀螺仪转子位置的信号的伺服装置用于引导所述导弹的感测装置。

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