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1. 发明申请

WO2010147910A1 MODULAR DIVERT AND ATTITUDE CONTROL SYSTEM 审中-公开
公开(公告)号：WO2010147910A1
公开(公告)日：2010-12-23
申请号：PCT/US2010/038547
申请日：2010-06-14
申请人： RAYTHEON COMPANY , OLDEN, Thomas A. , CAVALLERI, Robert J.
发明人： OLDEN, Thomas A. , CAVALLERI, Robert J.
IPC分类号： F42B15/00
CPC分类号： F42B15/01 , F02K9/18 , F02K9/26 , F05D2240/40 , F42B10/661
摘要： There is disclosed a vehicle and methods for maneuvering the vehicle. The vehicle may include a plurality of multiple-impulse rocket motors, each of which comprises a plurality of independently ignitable solid fuel propellant charges, and a processor that generates at least one command to ignite at least one solid fuel propellant charge of at least one of the plurality of multiple-impulse rocket motors.
摘要翻译：公开了用于操纵车辆的车辆和方法。车辆可以包括多个多冲程火箭发动机，每个多冲程火箭发动机包括多个独立可点燃的固体燃料推进剂装料，以及处理器，其产生至少一个命令以点燃至少一个固体燃料推进剂装料多个多冲程火箭发动机。

2. 发明专利

CA1306228C LOW FRICTIONAL LOSS ROTARY VANE GAS COMPRESSOR HAVING SUPERIOR LUBRICATION CHARACTERISTICS 未知
公开(公告)号：CA1306228C
公开(公告)日：1992-08-11
申请号：CA482593
申请日：1985-05-28
申请人： CAVALLERI ROBERT J , CLARK WILLIAM E
发明人： CAVALLERI ROBERT J , CLARK WILLIAM E
IPC分类号： F04C29/02
摘要： A low frictional loss, rotary vane gas compressor utilizing a housing having a generally elliptical cavity therein, and a rotor disposed in the cavity, with the axis of rotation of the rotor being offset from the central axis of the cavity. The housing has an inlet passage and a discharge passage, each in contact with the cavity, with the rotor having a plurality of radial slots in equally spaced relation about its periphery. A slidable vane is disposed in each of these slots, with the outer tip of each vane being in close proximity to an inner stator wall that defines the outer boundary of the cavity. The vanes serve to define a plurality of chambers in the cavity, which chambers undergo significant volume changes as they move about the cavity during rotation of the rotor, the vanes thus cooperating with the inner stator wall to compress gas entering the inlet passage, such that as it leaves through the discharge passage, it is at a higher pressure. Means provide a film of lubricant on the inner stator wall, with the outer tips of the vanes each possessing a compound contour that interacts with the film of lubricant to effect a good seal with the inner stator wall, while minimizing friction.

3. 发明专利

CA2016172A1 SELF-MACHINING SEAL RING LEAKAGE PREVENTION ASSEMBLY FOR ROTARY VANE DEVICE 未知
公开(公告)号：CA2016172A1
公开(公告)日：1991-11-07
申请号：CA2016172
申请日：1990-05-07
申请人： CAVALLERI ROBERT J
发明人： CAVALLERI ROBERT J
IPC分类号： F04C18/00 , F04C27/00
摘要： A low internal leakage, rotary vane gas compressor utilizing a housing having a generally elliptical cavity, whose outer boundary is defined by an inner stator wall. A shaft mounted rotor is disposed offset from the central axis of the cavity, with an end plate secured on each end of the housing. Each end plate has a centrally mounted hole for rotatably supporting the respective side of the rotor shaft. The housing has inlet and discharge passages, each in contact with the cavity. The rotor has a plurality of radial slots in equally spaced relation about its periphery, in each of which slots a slidable vane of minimal weight is disposed. Each vane is approximately the width of the rotor, and the outer tip of each vane is in close proximity to the inner stator wall. These vanes define a plurality of chambers which undergo significant volume changes during rotation of the rotor. The vanes thus cooperate with the inner stator wall and the end plates to compress gas entering the inlet passage, such that the gas thereafter leaving through the discharge passage is at a higher pressure. Advantageously, a seal ring of particularly hard, tough steel is mounted in each end plate, and biased into contact with the respective side of the rotor to effect an essentially zero gap therewith. Each seal ring has a tapered cross section, such that the initial footprint area is small, but with rotor wear, the small contact area desirably becomes a surface contact.

4. 发明申请

WO2009151796A3 SOLID-FUEL PELLET THRUST AND CONTROL ACTUATION SYSTEM TO MANEUVER A FLIGHT VEHICLE 审中-公开
公开(公告)号：WO2009151796A3
公开(公告)日：2009-12-17
申请号：PCT/US2009/041240
申请日：2009-04-21
申请人： RAYTHEON COMPANY , OLDEN, Thomas, A. , CAVALLERI, Robert, J. , KINSEY, Lloyd, E.
发明人： OLDEN, Thomas, A. , CAVALLERI, Robert, J. , KINSEY, Lloyd, E.
IPC分类号： F42B10/64 , F42B10/66
摘要： A solid-fuel pellet thrust and control actuation system (PT-CAS) provides command authority for maneuvering flight vehicles (10) over subsonic and supersonic speeds and within the atmosphere and exo-atmosphere. The PT-CAS includes a chamber (26) of solid-fuel pellets (28) that are ignited to expel gas through a throat (30). The expelled gas (34) is directed at supersonic vehicle speeds in atmosphere to a cavity (19) between an aero control surface (12) and the airframe (13) to pressurize the cavity (19) and deploy the surface (12) or at subsonic speeds in atmosphere or any speed in exo-atmosphere allowed to flow out a through-hole (14) in the surface where the throat (30) and through-hole provide a virtual converging/diverging nozzle (72) to produce a supersonic divert thrust. A pellet and control actuation system (P-CAS) without the through-hole (14) provides command authority at supersonic speeds in atmosphere. A restrictor mechanism (42) controls the bleed of pressurized gas from the cavity (19) to the external environment to achieve a deployment time objective for either the PT-CAS or P-CAS.

5. 发明申请

WO2009151796A2 SOLID-FUEL PELLET THRUST AND CONTROL ACTUATION SYSTEM TO MANEUVER A FLIGHT VEHICLE 审中-公开
标题翻译：固体燃料盘阀和控制执行系统来控制飞行器
公开(公告)号：WO2009151796A2
公开(公告)日：2009-12-17
申请号：PCT/US2009041240
申请日：2009-04-21
申请人： RAYTHEON CO , OLDEN THOMAS A , CAVALLERI ROBERT J , KINSEY LLOYD E
发明人： OLDEN THOMAS A , CAVALLERI ROBERT J , KINSEY LLOYD E
IPC分类号： F42B10/64 , F42B10/66
CPC分类号： F42B10/64 , F42B10/668
摘要： A solid-fuel pellet thrust and control actuation system (PT-CAS) provides command authority for maneuvering flight vehicles over subsonic and supersonic speeds and within the atmosphere and exo-atmosphere. The PT-CAS includes a chamber of solid-fuel pellets that are ignited to expel gas through a throat. The expelled gas is directed at supersonic vehicle speeds in atmosphere to a cavity between an aero control surface and the airframe to pressurize the cavity and deploy the surface or at subsonic speeds in atmosphere or any speed in exo-atmosphere allowed to flow out a through-hole in the surface where the throat and through-hole provide a virtual converging/diverging nozzle to produce a supersonic divert thrust. A pellet and control actuation system (P-CAS) without the through-hole provides command authority at supersonic speeds in atmosphere. A restrictor mechanism controls the bleed of pressurized gas from the cavity to the external environment to achieve a deployment time objective for either the PT-CAS or P-CAS.
摘要翻译：固体燃料颗粒推力和控制致动系统（PT-CAS）为在亚音速和超音速下以及大气和大气中的机动飞行器提供了指挥权力。 PT-CAS包括一个固体燃料颗粒室，它被点燃以通过喉管排出气体。排出的气体以大气中的超音速车辆速度被引导到航空控制表面和机身之间的空腔，以对空腔加压并且将其表面或亚音速的速度在大气中或任何速度在外部气氛中流出，喉部和通孔的表面中的孔提供虚拟的会聚/发散喷嘴以产生超音速转向推力。没有通孔的颗粒和控制致动系统（P-CAS）在大气中以超音速速度提供命令权限。限流器机构控制加压气体从空腔排放到外部环境，以实现PT-CAS或P-CAS的部署时间目标。

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