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41. 发明授权

US5743492A Payload housing and assembly joint for a launch vehicle 失效
标题翻译：运载火箭的有效载荷和组装接头
公开(公告)号：US5743492A
公开(公告)日：1998-04-28
申请号：US511170
申请日：1995-08-04
申请人： Allan L. Chan , Robert M. Heath , Steven D. Mettler , Chau N. Pham , Douglas B. Pereyda , Robert J. MacDonald , Kenneth W. Epstein , David P. Kennon
发明人： Allan L. Chan , Robert M. Heath , Steven D. Mettler , Chau N. Pham , Douglas B. Pereyda , Robert J. MacDonald , Kenneth W. Epstein , David P. Kennon
IPC分类号： B64F1/04 , B64G1/00 , B64G1/40 , B64G1/64 , B64G5/00 , F02K9/34 , B64G1/22
CPC分类号： B64F1/04 , B64G1/002 , B64G1/007 , B64G1/401 , B64G1/641 , B64G5/00 , F02K9/343 , F42B15/36 , F42B15/38 , B64G1/402 , B64G1/403 , B64G2001/1092 , B64G2005/005
摘要： A launch vehicle payload housing and assembly joint for a launch vehicle, the housing comprising a shroud having first and second shell sections, and a frusto-conical payload adapter mounted in the shroud. The shell sections are connected together to form a housing. A peripherally extending explosive seam and a pair of longitudinally extending explosive seams hold the shell sections together. Each seam comprises a plurality of seam elements which include a pair of brackets attached to opposed ends of those parts of the shell abutting the longitudinally and peripherally extending seams. The brackets are spaced from one another to define a cavity. The cavity accommodates a deformable tube which houses explosive material in the form of an explosive cord. Detonation of the explosive material causes the shell sections to separate from one another. Longitudinally acting thrustor springs and transverse acting assistor springs urge the shell sections apart to pivot about hinges between the shell sections and a base ring. The hinges comprise brackets which are separable from one another when the shell sections are in their separated open state. This allows the shell sections automatically to be discarded once fully opened. The assembly joint for connecting a shroud and a payload adapter to a final stage motor of a launch vehicle comprises a flange defined by a lower end of a wall of the shroud, an adapter bracket secured to a lower end of the adapter, the adapter bracket defining a flange aligned with the flange of the shroud wall, and a motor bracket secured to an outer wall of the final stage motor. The motor defines a flange aligned with the flange of the adapter bracket. The three flanges define axially extending aligned holes for receiving bolts to secure the flanges to one another.
摘要翻译：一种用于运载火箭的运载火箭有效载荷壳体和组装接头，所述壳体包括具有第一和第二壳体部分的护罩和安装在护罩中的截头圆锥形有效载荷适配器。外壳部分连接在一起形成外壳。外围延伸的爆炸缝和一对纵向延伸的爆炸接缝将壳体部分保持在一起。每个接缝包括多个接缝元件，这些接缝元件包括一对支架，该对支架附接到壳体的与纵向和周向延伸的接缝相邻的那些部分的相对端。支架彼此间隔开以限定空腔。空腔容纳可变形管，其容纳爆炸线形式的爆炸性材料。爆炸材料的爆炸导致壳体部分彼此分离。纵向作用的推力弹簧和横向作用的组合弹簧促使壳体分开以围绕壳体部分和基部环之间的铰链枢转。铰链包括当壳部分处于其分离打开状态时彼此分离的支架。这样一来，一旦完全打开，shell部分将自动被丢弃。用于将护罩和有效负载适配器连接到运载火箭的最终级马达的组装接头包括由护罩的壁的下端限定的凸缘，固定到适配器的下端的适配器支架，适配器支架限定与护罩壁的凸缘对准的凸缘，以及固定到最终级电动机的外壁的电动机支架。电机定义与适配器支架的凸缘对齐的凸缘。三个凸缘限定轴向延伸的对准的孔，用于接收用于将凸缘彼此固定的螺栓。

42. 发明授权

US4266742A Ram wing aircraft launch platform system 失效
标题翻译：拉姆翼飞机发射平台系统
公开(公告)号：US4266742A
公开(公告)日：1981-05-12
申请号：US85662
申请日：1979-10-17
申请人： David J. Perez , Kenneth P. Schwartz
发明人： David J. Perez , Kenneth P. Schwartz
IPC分类号： B64F1/04
CPC分类号： B64F1/04
摘要： A launch platform for conventional landing gear aircraft having the launch platform configured as a ram wing structure with wheel latches secured to the platform. The platform is secured to the aircraft by means of the wheel latches. The wheel latches are released to permit the aircraft to leave the platform by pilot command. A parachute system is provided for platform deceleration after aircraft take-off. Spoilers are provided on the ram wing for stabilization of the ram wing during rotation.
摘要翻译：具有发射平台的传统起落架飞机的发射平台，其配置为具有固定到平台的轮锁的冲压翼结构。平台通过车轮锁扣固定在飞机上。车轮闩锁被释放以允许飞机通过驾驶员指令离开平台。飞机起飞后降落伞系统提供平台减速。在公转翼上设有防盗器，用于在旋转过程中使压头翼稳定。

43. 发明授权

US4103849A Catapult restraint/release system 失效
标题翻译：弹射器限制/释放系统
公开(公告)号：US4103849A
公开(公告)日：1978-08-01
申请号：US833415
申请日：1977-09-15
申请人： Lloyd J. Holt , Clayton E. Panlaqui
发明人： Lloyd J. Holt , Clayton E. Panlaqui
IPC分类号： B64F1/04 , B64F1/16
CPC分类号： B64F1/04 , Y10T24/45466 , Y10T403/1633 , Y10T403/22
摘要： Apparatus for restraining an aircraft against the combined forces of a cault launching shuttle and aircraft takeoff power during a catapult assisted takeoff until a predetermined combined force level has been reached. Release of the aircraft is triggered by the relative movement of a central piston within a housing which causes disengagement of gripping lugs from a tensile bar attached to the aircraft. The relative movement is enabled by the compressibility of hydraulic oil confined within the apparatus and loaded by the combined forces.
摘要翻译：用于在弹射器辅助起飞期间限制飞机抵抗弹射器发射梭和飞机起飞力的组合力的装置，直到达到预定的组合力水平。飞机的释放由中心活塞在壳体内的相对运动触发，这导致抓紧爪从连接到飞行器的拉力杆脱离。相对运动由限制在设备内并被组合力加载的液压油的压缩性所实现。

44. 发明授权

US3552688A Helicopter landing means 失效
标题翻译：直升机登陆手段
公开(公告)号：US3552688A
公开(公告)日：1971-01-05
申请号：US3552688D
申请日：1969-03-10
申请人： FAIREY CANADA LTD
发明人： BAEKKEN ASBJORN
IPC分类号： B64F1/04 , B64F1/12
CPC分类号： B64F1/04 , B64F1/125
摘要： Trap means, for grasping a probe carried by a helicopter and used on board ship to secure a helicopter to the ship at the instant of touchdown, comprise a hydraulic system arranged to move together two arresting beams which trap the probe and hold it in trapped position.

45. 发明授权

US3198459A Imposion thrust engine and vehicle 失效
标题翻译：投影推力发动机和车辆
公开(公告)号：US3198459A
公开(公告)日：1965-08-03
申请号：US12120561
申请日：1961-06-30
申请人： MILFORD GEARY
发明人： MILFORD GEARY
IPC分类号： B64D27/10 , B64F1/04 , F02K7/12
CPC分类号： F02K7/12 , B64F1/04

46. 发明授权

US3163380A Aircraft launching apparatus 失效
标题翻译：飞机发射装置
公开(公告)号：US3163380A
公开(公告)日：1964-12-29
申请号：US11451461
申请日：1961-06-02
申请人： BRODIE JAMES H
发明人： BRODIE JAMES H
IPC分类号： B64F1/04
CPC分类号： B64F1/04

47. 发明授权

US3132710A Vehicle ground guidance system 失效
标题翻译：车辆地面导向系统
公开(公告)号：US3132710A
公开(公告)日：1964-05-12
申请号：US4731960
申请日：1960-08-03
申请人： BLISS E W CO
发明人： PETRELLA JOSEPH L , STRANCE JOHN S
IPC分类号： B64F1/00 , B64F1/04 , G05D1/00 , G05D1/02
CPC分类号： G05D1/0083 , B64F1/00 , B64F1/002 , B64F1/04 , G05D1/0265

48. 发明授权

US3077110A System for monitoring the take-off performance of an aircraft 失效
标题翻译：监控飞机起飞性能的系统
公开(公告)号：US3077110A
公开(公告)日：1963-02-12
申请号：US82375359
申请日：1959-06-29
申请人： SPERRY RAND CORP
发明人： THEODORE GOLD
IPC分类号： B64F1/04 , G05D1/00 , G06G7/70
CPC分类号： G05D1/0083 , B64F1/04 , G06G7/70

49. 发明授权

US2592873A Apparatus for landing rockets and rocket ships 失效
标题翻译：用于着陆火箭和火箭船的装置
公开(公告)号：US2592873A
公开(公告)日：1952-04-15
申请号：US13885750
申请日：1950-01-16
申请人： DRISKILL DALLAS B
发明人： DRISKILL DALLAS B
IPC分类号： B64F1/04
CPC分类号： B64F1/04

50. 发明授权

US2441505A Reciprocal actuator 失效
标题翻译：互动执行器
公开(公告)号：US2441505A
公开(公告)日：1948-05-11
申请号：US68080646
申请日：1946-07-01
申请人： BENDIX AVIAT CORP
发明人： LEONARD OCHTMAN
IPC分类号： B60K23/00 , B64F1/04 , G05G15/04
CPC分类号： G05G15/04 , B60K23/00 , B60K2700/02 , B64F1/04 , Y10T74/18688 , Y10T74/2063 , Y10T477/3225

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