公开(公告)号：US07786417B2

公开(公告)日：2010-08-31

申请号：US11636922

申请日：2006-12-11

申请人： Harold R. Sells, II

发明人： Harold R. Sells, II

IPC分类号： B64D1/04 ,  F42B30/00 ,  F42B15/10 ,  F42B15/00

CPC分类号： F41H13/0006 ,  F41H11/02 ,  F42B12/68

摘要： An article for neutralizing an enemy weapon comprising an interceptor and a deployable net attached to the interceptor, said deployable net remaining attached to the interceptor upon deployment, is disclosed. A method of neutralizing an airborne enemy weapon comprising launching an interceptor, with a capture sock, towards the enemy weapon and deploying the capture sock just prior to the interceptor encountering the enemy weapon is also disclosed. The capture sock remains attached to the interceptor upon deployment.

摘要翻译： 公开了一种用于中和敌方武器的文章，该武器包括拦截器和连接到拦截器的可部署网络，所述部署网在部署时保持附着到拦截器。 还公开了一种中和空中敌方武器的方法，其中包括在拦截者遇到敌方武器之前，向敌方武器发射拦截器和捕获袜子，并部署捕获袜子。 捕获袜子在部署时仍然附着在拦截器上。

公开(公告)号：US07540226B2

公开(公告)日：2009-06-02

申请号：US11260558

申请日：2005-10-28

申请人： Jamie J. Childress ,  Edward C. Marques

发明人： Jamie J. Childress ,  Edward C. Marques

IPC分类号： B64D1/04

CPC分类号： B64D27/00 ,  B64D29/00 ,  F41J2/02

摘要： A thermal radiation-generating decoy mounted adjacent an aircraft engine structure, such as an engine nacelle, includes a heat source inside of an aerodynamic enclosure with a mounting interface to attach the enclosure to the engine structure. The decoy can further be located at the lower extreme of and adjacent the forward-most portion of the engine nacelle in order to attract an infrared-seeking threat to the vicinity of the fan containment portion of the engine nacelle. The decoy can be designed to have a thermal signature that mimics a scaled overall aircraft thermal signature. In addition, the decoy can include a fuse shield adjacent the enclosure to detonate a threat in the case that the threat approach trajectory is imprecise and the threat bypasses the enclosure within an aspect of the fuse shield as viewed from the approach direction of the threat.

摘要翻译： 安装在诸如发动机机舱的飞机发动机结构附近的热辐射产生诱饵包括在空气动力学外壳内部的热源，具有将外壳附接到发动机结构的安装界面。 诱饵可以进一步位于发动机舱的最前部并邻近发动机机舱的最前部，以便引发对发动机机舱的风扇容纳部分附近的红外线寻求威胁。 诱饵可以设计成具有模拟飞机热标签整体的热签名。 此外，鉴于威胁进近轨迹不精确，威胁绕过保险丝屏蔽的一个方面，威胁将从威胁的进场方向观察，旁路装置可以包括邻近外壳的保险丝屏蔽以引爆威胁。

公开(公告)号：US07478578B2

公开(公告)日：2009-01-20

申请号：US11165975

申请日：2005-06-24

申请人： Philip L. Kirkpatrick

发明人： Philip L. Kirkpatrick

IPC分类号： B64D1/04

CPC分类号： F41H11/02 ,  F41J2/02 ,  F42B12/70

摘要： A commercial airliner (100) controls and is flown in formation with a drone aircraft (200) that includes missile detection and diversion equipment (215) capable of protecting the airliner from a man portable missile (130).

摘要翻译： 商用客机（100）通过无人机（200）来控制和飞行，其中包括能够保护客机不受人类便携式导弹（130）的导弹探测和引导设备（215）的影响。

公开(公告)号：US07444918B2

公开(公告)日：2008-11-04

申请号：US11761160

申请日：2007-06-11

申请人： Masato Hirooka ,  Mikio Yabuta

发明人： Masato Hirooka ,  Mikio Yabuta

IPC分类号： B64D1/04

CPC分类号： F42B3/006 ,  B60R21/017 ,  B60R21/26 ,  F15B15/19 ,  F42B3/04 ,  Y10T137/1647

摘要： The present invention relates to a pyrotechnic actuator, containing: a housing, a piston slidable inside the housing, an igniter disposed within the housing and causing the piston to slide, the piston including a piston head having a pressure-receiving surface with which a combustion product, produced by actuation of the igniter, collides, a piston rod extending from the piston head and further, a resin portion provided at least in a part of the piston, the resin portion being disposed in contact with a member including the housing, the piston being fixed by contacting the resin portion to the member including the housing, and the piston being prevented from moving before activation of the igniter.

摘要翻译： 烟火致动器技术领域本发明涉及一种烟火致动器，其包括壳体，可在壳体内滑动的活塞，设置在壳体内并引起活塞滑动的点火器，活塞包括具有压力接收表面的活塞头，燃烧器 通过致动点火器产生的产品碰撞从活塞头延伸的活塞杆，另外，至少设置在活塞的一部分中的树脂部分，树脂部分设置成与包括壳体的构件接触， 活塞通过将树脂部分接触到包括壳体的构件而被固定，并且在启动点火器之前防止活塞移动。

公开(公告)号：US07415918B2

公开(公告)日：2008-08-26

申请号：US10562262

申请日：2004-06-30

申请人： Lothar Alwin Paul

发明人： Lothar Alwin Paul

IPC分类号： B64D1/04 ,  F41F5/00

CPC分类号： F41A13/08

摘要： This invention relates to a fume extractor (10) for extracting fumes from a bore (12) of a barrel (14) of a gun and comprising an annular main reservoir (16); an annular inlet reservoir (18); and an annular auxiliary reservoir (20), all concentrically surrounding the barrel (14) and being in communication with each other and the bore (12). The inlet reservoir (18) is sandwiched between the main reservoir (16) and the barrel (14). The auxiliary reservoir (20) is sandwiched between the main reservoir (16) and the barrel (14) and is located adjacent the inlet reservoir (18) on a muzzle brake end thereof. The arrangement is such that the main reservoir (16) is pressurized when the gun is fired and such that the fumes in the bore (12) are extracted by the release of pressure in the main and auxiliary reservoirs (16) and (20), after the projectile has left the barrel (14). The communication between the inlet reservoir (18) and main reservoir (16) consists of plurality of ports (24) distributed circumferentially each port being provided with a check valve (30).

摘要翻译： 本发明涉及一种用于从枪的枪管（14）的孔（12）中提取烟雾并包括环形主贮器（16）的抽烟器（10）。 环形入口容器（18）; 以及环形辅助容器（20），所有环形辅助容器（20）全部同心地围绕所述筒体（14）并且彼此连通和所述孔（12）。 入口储存器（18）夹在主储存器（16）和桶（14）之间。 辅助储存器（20）夹在主储存器（16）和桶（14）之间，并且位于入口储存器（18）的枪口制动端附近。 这种布置使得当枪被击发时主容器（16）被加压，并且通过在主和辅助储存器（16）和（20）中释放压力来提取孔（12）中的烟雾， 射弹射出枪管后（14）。 入口储存器（18）和主储存器（16）之间的连通件由沿圆周方向分布的多个端口（24）组成，每个端口设有止回阀（30）。

公开(公告)号：US20070152101A1

公开(公告)日：2007-07-05

申请号：US11326677

申请日：2005-12-19

申请人： David Bittle ,  Gary Jimmerson ,  Julian Cothran

发明人： David Bittle ,  Gary Jimmerson ,  Julian Cothran

IPC分类号： B64D1/04

CPC分类号： F42B3/04 ,  F42B12/62

摘要： The Variable-Force Payload Ejecting System, residing within an air vehicle, utilizes multiple pressure generators, one or more of which may be activated, to produce variable levels of force. A controlling computer within the air vehicle determines when and how much pressure needs to be generated to eject a given item, such as a submunition, from the vehicle. In its determination, the computer factors in the vehicle's forward velocity and height over the intended target at the time of ejection and the characteristics of the particular submunition to be ejected. An activating mechanism activates one or more pressure generators to produce the determined amount of pressure. The pressure thusly generated acts on an inflatable tube that inflates and expels the selected submunition. The result is a more precise delivery of the submunitions onto the intended targets.

摘要翻译： 驻留在空中车辆中的可变力有效载荷弹出系统利用多个压力发生器，其中一个或多个可以被激活，以产生可变的等级的力。 航空器内的控制计算机确定何时以及从车辆中弹出诸如子弹药的给定物品需要多少压力。 在其决定中，计算机在弹出时对车辆前进速度和高度超过预定目标的要素以及要弹出的特定子弹药的特性。 激活机构激活一个或多个压力发生器以产生确定的压力量。 因此产生的压力作用在充气管上，该管充气并排出选定的子弹药。 结果是更准确地将子弹药递送到预期的目标。

公开(公告)号：US20060283315A1

公开(公告)日：2006-12-21

申请号：US11146254

申请日：2005-06-06

申请人： Rick Blackburn

发明人： Rick Blackburn

IPC分类号： B64D1/04 ,  B64D1/12

CPC分类号： F42C14/06 ,  B64D1/04 ,  F42C11/006 ,  F42C19/06

摘要： A weapons cable retention device is used for separating an electrical connection, and retaining a cable and an electrical connector coupled to an aircraft, when a munition, such as a bomb or a missile, is released from the aircraft. The cable retention device includes a structural coupling for coupling to the aircraft, a rod having an adjustment mechanism for adjusting the length of the rod, and an attachment mechanism for attaching to the electrical connector. The cable retention device provides a substantially rigid coupling to secure the electrical connector. The cable retention device may be configured so that the attachment mechanism engages lanyard holes of a standard electrical connector. According to one embodiment, the structural coupling may include a collar that receives a bail bar on the aircraft structure through a hole therein.

摘要翻译： 武器电缆固定装置用于分离电气连接，并且当诸如炸弹或导弹的弹药从飞行器释放时，保持连接到飞行器的电缆和电连接器。 电缆保持装置包括用于联接到飞行器的结构联接件，具有用于调节杆的长度的调节机构的杆和用于附接到电连接器的附接机构。 电缆保持装置提供基本上刚性的联接以固定电连接器。 电缆保持装置可以被构造成使得附接机构接合标准电连接器的挂绳孔。 根据一个实施例，结构联接件可以包括通过其中的孔在飞行器结构上接收吊环的轴环。

公开(公告)号：US20060054012A1

公开(公告)日：2006-03-16

申请号：US11210915

申请日：2005-08-24

申请人： Otto Baumann ,  Rolf Mueller ,  Dietmar Saur ,  Helmut Heinzelmann

发明人： Otto Baumann ,  Rolf Mueller ,  Dietmar Saur ,  Helmut Heinzelmann

IPC分类号： B64D1/04

CPC分类号： B25D17/00 ,  B25D2250/065 ,  B25D2250/365

摘要： A hand power tool has a percussion bolt, a hammer barrel receiving the percussion bolt, a sealing element effecting sealing between the percussion bolt and the hammer barrel, a restraining element that retains the sealing element at a predetermined point along the hammer barrel, and a counterpart element fixing the restraining element in a longitudinal direction of the hammer barrel, wherein the restraining element is located on an outer face, toward the hammer barrel, of the sealing element.

摘要翻译： 手动工具具有冲击螺栓，接收冲击螺栓的锤子筒，影响冲击螺栓和锤筒之间的密封的密封元件，将密封元件保持在沿着锤筒的预定点处的限制元件，以及 对应元件将限制元件固定在锤筒的纵向方向上，其中限制元件位于密封元件的朝向锤筒的外表面上。

公开(公告)号：US20060048667A1

公开(公告)日：2006-03-09

申请号：US10969724

申请日：2004-10-20

申请人： Quenten Duden ,  Allan Mense

发明人： Quenten Duden ,  Allan Mense

IPC分类号： B64D1/04 ,  F42B14/06

CPC分类号： B64G1/641 ,  B64G1/002 ,  B64G1/22 ,  B64G2001/643 ,  C08K5/14 ,  F41H11/02 ,  F42B12/56 ,  F42B12/58 ,  F42B12/62 ,  F42B12/74 ,  F42B12/76 ,  F42B15/08 ,  Y10T428/249954

摘要： A high energy, e.g., ultraviolet (UV) catalyzed decomposing foam encapsulating kinetic media forms a payload to be boosted in space and provides an ultra-light weight means for intercepting an incoming missile or other target. The decomposed foam releases the kinetic media (at designed rates so as to preserve a required density of media on target) to intercept a target and destroy it. The use of the decomposing foam significantly lowers the weight and cost and improves the probability of success of destroying the target.

公开(公告)号：US06955111B1

公开(公告)日：2005-10-18

申请号：US10975631

申请日：2004-10-29

申请人： Terry L. Davis

发明人： Terry L. Davis

IPC分类号： F41A3/64 ,  B64D1/04

CPC分类号： F41A3/64

摘要： A method comprising the steps of lifting a stool-like device onto the recoil slide rails of a howitzer, sliding the device on the recoil slide rails of the howitzer until the device is centered under the breechblock of the howitzer, receiving and holding the breechblock on top of the device while permitting passage of the spindle through a hole in the device, and removing the spindle from the carrier without the breechblock dropping out of the carrier and causing bodily harm. After the spindle is removed, the breechblock can also be removed by raising the carrier and sliding the device out from under it.

摘要翻译： 一种方法包括以下步骤：将粪便状装置提升到榴弹炮的反冲滑轨上，将装置滑动在榴弹炮的反冲滑轨上，直到装置在榴弹炮的膛下居中，接收和保持枪闩 同时允许主轴通过装置中的孔，并且将主轴从载体上移除，而不会使后膛从载体中脱落并造成身体伤害。 在拆卸主轴后，也可以通过抬起托架并将设备从其下方滑出来移除后挡块。