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1. 发明申请

WO2010053607A3 SMART FUZE GUIDANCE SYSTEM WITH REPLACEABLE FUZE MODULE 审中-公开
标题翻译：带可更换引信模块的智能引信系统
公开(公告)号：WO2010053607A3
公开(公告)日：2010-07-01
申请号：PCT/US2009052176
申请日：2009-07-30
申请人： RAYTHEON CO , GESWENDER CHRIS E , BENNETT STEPHEN E , ZAMORA MATTHEW A , SANCHEZ CESAR
发明人： GESWENDER CHRIS E , BENNETT STEPHEN E , ZAMORA MATTHEW A , SANCHEZ CESAR
IPC分类号： F42B10/46 , F42C19/02
CPC分类号： F42C19/02 , F42B10/46
摘要： A smart fuze system (12) includes a radome (60) used to hold a replaceable smart fuze module (24) in place. An internally-threaded collar (66) screws onto threads on the main body (42) of the smart fuze system. Pressure from the radome presses the smart fuze module against electrical connections (48) in the main body. The smart fuze module may thereby be held in place without potting material, allowing different types of fuzes to be swapped into place. The different types of fuzes may include a type that communicates height of burst (HOB) information a type that communicates telemetry, and a type that communicates both HOB and telemetry information.
摘要翻译：智能引信系统（12）包括用于将可替换的智能引信模块（24）保持在适当位置的天线罩（60）。内螺纹环（66）拧到智能引信系统主体（42）上的螺纹上。来自天线罩的压力将智能引信模块按压在主体中的电连接（48）上。智能引信模块因此可以在没有灌封材料的情况下被保持在适当位置，从而允许不同类型的引信被交换到位。不同类型的引信可以包括传达突发的高度（HOB）信息，传达遥测的类型和传送HOB和遥测信息的类型的类型。

2. 发明申请

WO2009140412A4 METHODS AND APPARATUS FOR AIR BRAKE RETENTION AND DEPLOYMENT 审中-公开
标题翻译：空气制动器保持和部署的方法和装置
公开(公告)号：WO2009140412A4
公开(公告)日：2010-01-07
申请号：PCT/US2009043826
申请日：2009-05-13
申请人： RAYTHEON CO , GESWENDER CHRIS E , STREETER JAMES D , ZAMORA MATTHEW A , FINK JASON J , EISENBACHER MATTHEW O
发明人： GESWENDER CHRIS E , STREETER JAMES D , ZAMORA MATTHEW A , FINK JASON J , EISENBACHER MATTHEW O
IPC分类号： F42B10/50
CPC分类号： F42B10/50
摘要： Methods and apparatus for an air brake system [210] for a projectile [100] according to various aspects of the present invention comprises a pivot and a protrusion [212] mounted on the pivot. The protrusion is adapted to selectively translate outward from the longitudinal axis of the projectile. The methods and apparatus may further operate in conjunction with an actuation system [214] engaging the protrusion, wherein the actuation system is configured to selectively facilitate the translation of the protrusion.
摘要翻译：根据本发明的各个方面的用于射弹的空气制动系统[210]的方法和装置包括安装在枢轴上的枢轴和突起[212]。该突起适于从弹丸的纵向轴线向外选择性地平移。所述方法和装置还可以与接合突出部的致动系统214结合操作，其中致动系统构造成选择性地促进突起的平移。

3. 发明申请

WO2008091362A3 METHODS AND APPARATUS FOR MISSILE AIR INLET 审中-公开
标题翻译：用于空气入口的方法和装置
公开(公告)号：WO2008091362A3
公开(公告)日：2009-01-08
申请号：PCT/US2007072233
申请日：2007-06-27
申请人： RAYTHEON CO , GESWENDER CHRIS E
发明人： GESWENDER CHRIS E
IPC分类号： F42B10/00
CPC分类号： F02K7/10 , F02K7/105 , F02K7/18 , F42B10/38 , F42B15/10
摘要： Methods and apparatus for delivering a missile may operate in conjunction with a missile comprising an outer skin. The missile may be configured in a closed position and an open position. In the open position, an aperture is opened in the outer skin, for example to supply air to an air-breathing engine. In the closed position, the aperture is closed.
摘要翻译：用于传送导弹的方法和装置可以与包括外部皮肤的导弹一起操作。导弹可以配置在关闭位置和打开位置。在打开位置时，在外皮中开孔，例如将空气供给到空气呼吸引擎。在关闭位置，孔关闭。

4. 发明申请

WO2005022075B1 MISSILE WITH ODD SYMMETRY FINS 审中-公开
公开(公告)号：WO2005022075B1
公开(公告)日：2005-09-15
申请号：PCT/US2004015795
申请日：2004-05-20
申请人： RAYTHEON CO , GESWENDER CHRIS E , HARLINE SHAWN B , BLAHA GEORGE A
发明人： GESWENDER CHRIS E , HARLINE SHAWN B , BLAHA GEORGE A
IPC分类号： F42B10/06 , F42B10/26
CPC分类号： F42B10/06
摘要： A missile (10), either a powered missile or an unpowered projectile, includes a freely-rolling tail assembly (14) having an odd number of fins (32). Having an odd number of fins may reduce oscillations caused by the rotation of the freely-rotating tail. This may make a more stable platform for a seeker (22), such as an uncooled focal point array or other imaging infrared (IIR) or millimeter wave radio frequency (MMW) seeker, in the body of the missile. Also, minimizing oscillation by using an odd number of fins may facilitate control of the missile.

5. 发明申请

WO2011014287A3 LOW COST, HIGH STRENGTH ELECTRONICS MODULE FOR AIRBORNE OBJECT 审中-公开
标题翻译：低成本，高强度电子模块用于AIRBORNE对象
公开(公告)号：WO2011014287A3
公开(公告)日：2011-04-07
申请号：PCT/US2010034383
申请日：2010-05-11
申请人： RAYTHEON CO , GESWENDER CHRIS E
发明人： GESWENDER CHRIS E
IPC分类号： H05K7/14
CPC分类号： H05K1/144 , F42B15/08 , F42B30/006 , F42C19/06 , H05K7/1434 , H05K2201/09027 , H05K2201/10378 , H05K2201/2018
摘要： An electronics module is provided for utilization on board an airborne object. In one embodiment, the electronics module includes a housing having a cavity therein, a first printed circuit board (PCB) disposed in the cavity, a second PCB disposed in the cavity above the first PCB, and a supportive interconnect structure. The supportive interconnect structure includes a substantially annular insulative body and a plurality of vias. The substantially annular insulative body extends around an inner circumferential portion of the housing between the first PCB and the second PCB to support the second PCB and to axially space the second PCB from the first PCB. The plurality of vias is formed through the substantially annular insulative body and electrically couples the first PCB to the second PCB.
摘要翻译：提供电子模块用于机载物体上的利用。在一个实施例中，电子模块包括其中具有空腔的壳体，设置在空腔中的第一印刷电路板（PCB），布置在第一PCB上方的空腔中的第二PCB以及支撑互连结构。支撑互连结构包括基本环形的绝缘体和多个通孔。基本上环形的绝缘体围绕第一PCB和第二PCB之间的壳体的内圆周部分延伸以支撑第二PCB并使第二PCB从第一PCB轴向空间。多个通孔通过大体上环形的绝缘体形成，并将第一PCB电耦合到第二PCB。

6. 发明申请

WO2008105894A3 METHODS AND APPARATUS FOR PROJECTILE DATA LINK SYSTEM 审中-公开
标题翻译：投弹数据链系统的方法和设备
公开(公告)号：WO2008105894A3
公开(公告)日：2008-11-20
申请号：PCT/US2007072242
申请日：2007-06-27
申请人： RAYTHEON CO , GESWENDER CHRIS E
发明人： GESWENDER CHRIS E
IPC分类号： F42C19/06
CPC分类号： F42C17/04
摘要： Methods and apparatus for a data link system according to various aspects of the present invention may be incorporated into a cartridge system. The cartridge system may comprise a case and a projectile. The data link system may be connected to the case and the projectile to provide signals. The data link system a first connection point and a second connection point disposed on the case and an electrical connector connected to the first connection point and the second connection point
摘要翻译：根据本发明的各个方面的用于数据链路系统的方法和设备可以被结合到盒子系统中。盒体系统可以包括壳体和抛射体。数据链系统可以连接到壳体和射弹以提供信号。数据连接系统设置在壳体上的第一连接点和第二连接点以及连接到第一连接点和第二连接点的电连接器

7. 发明申请

WO2005022075A2 MISSILE WITH ODD SYMMETRY FINS 审中-公开
标题翻译：与ODD对称FINS的MISSILE
公开(公告)号：WO2005022075A2
公开(公告)日：2005-03-10
申请号：PCT/US2004015795
申请日：2004-05-20
申请人： RAYTHEON CO , GESWENDER CHRIS E , HARLINE SHAWN B , BLAHA GEORGE A
发明人： GESWENDER CHRIS E , HARLINE SHAWN B , BLAHA GEORGE A
IPC分类号： F42B10/06 , F42B10/26
CPC分类号： F42B10/06
摘要： A missile (10), either a powered missile or an unpowered projectile, includes a freely-rolling tail assembly (14) having an odd number of fins (32). Having an odd number of fins may reduce oscillations caused by the rotation of the freely-rotating tail. This may make a more stable platform for a seeker (22), such as an uncooled focal point array or other imaging infrared (IIR) or millimeter wave radio frequency (MMW) seeker, in the body of the missile. Also, minimizing oscillation by using an odd number of fins may facilitate control of the missile.
摘要翻译：导弹（10），动力导弹或无动力射弹，包括具有奇数个鳍片（32）的自由滚动的尾翼组件（14）。具有奇数数量的翅片可以减少由自由旋转的尾部的旋转引起的振荡。这可以为导弹（22）的导弹的身体中的诸如未冷却的焦点阵列或其他成像红外（IIR）或毫米波射频（MMW）探测器的平台提供更稳定的平台。此外，通过使用奇数的翅片来最小化振荡可以有助于控制导弹。

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