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公开(公告)号：US5169260A
公开(公告)日：1992-12-08
申请号：US717026
申请日：1991-06-18
CPC分类号： F16B1/00 , B64G1/641 , Y10T403/595 , Y10T403/7007
摘要： Device for linking two objects, one of these objects (1) bearing sections of mobile bayonets (3) connected by connecting rods (4) to enable them to be controlled simultaneously. The other object bears fixed bayonet sections. Mobile bayonet sections (3) are preferably composed of two concentric rings (7) and (9) connected by a freeable ratchet mechanism (12) for breaking up the movement into one phase for establishing the link by the bayonets and one wedge clamping phase. The rotation of the bayonets is only authorized if the action of a locking system (20) is interrupted. Application for the linking of portions of aeronautical, space or submarine vehicles.
摘要翻译： 用于链接两个物体的装置，其中一个物体（1）通过连杆（4）连接的移动刺刀（3）的轴承部分，以使它们能够被同时控制。 另一个对象承载固定的卡口部分。 移动式卡口部分（3）优选地由两个同心圆环（7）和（9）构成，该两个同心环通过可自由的棘轮机构（12）连接，用于将运动分解成一个相，用于通过卡口和一个楔形夹紧相建立连杆。 如果锁定系统（20）的动作中断，则卡口的旋转仅被授权。 连接航空，空间或潜艇车辆部分的申请。
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2.发明授权公开(公告)号：US09290279B2
公开(公告)日：2016-03-22
申请号：US13376231
申请日：2010-05-28
CPC分类号： B64G1/62 , B64G2001/1071
摘要： A landing system of a body and a space probe provided with such a system for landing on a bearing ground. The landing system includes landing legs (5), each with a footpad (6) at the end thereof, intended for braking the landing impact of the body when coming into contact with the ground and for supporting the body on the ground after landing. The footpads (6) are not coplanar.
摘要翻译： 身体的一个着陆系统和一个设有这样一个系统的空间探针，用于在轴承地面上着陆。 着陆系统包括着陆腿（5），每个脚蹬在其末端具有足垫（6），用于在与地面接触时制动身体的着陆冲击，并在着陆后将身体支撑在地面上。 脚垫（6）不共面。
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3.发明申请SYSTEM COMPRISING A SPATIAL MOTHER PROBE FORMING A SPATIAL CARRIER VEHICLE AND A PLURALITY OF SPATIAL DAUGHTER PROBES 有权包括形成空间载体车厢和空间大气探头的空间主体的空间系统的系统公开(公告)号：US20120210808A1
公开(公告)日：2012-08-23
申请号：US13320307
申请日：2010-05-07
IPC分类号： G01D21/00
CPC分类号： B64G1/105 , B64G1/641 , B64G2001/643
摘要： A system includes a mother probe forming a carrier space vehicle (1) and a plurality of daughter probes (2a, 2b, 2c) aligned in a longitudinal axis (A) of the mother probe, in which the attachment of the daughter probes to the mother probe is carried out by a plurality of probe-supporting annular segments (5a, 5b, 5c) each provided with an annular collar (3a, 3b, 3c) for attaching a daughter probe.
摘要翻译： 系统包括形成载体空间载体（1）的母体探针和在母体探针的纵向轴线（A）上对准的多个子探针（2a，2b，2c），其中将子探针附接到 母体探针通过多个探针支承环形部分（5a，5b，5c）进行，每个环形部分设置有用于附接子探针的环形套环（3a，3b，3c）。
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4.发明申请LANDING DEVICE FOR A SPACE PROBE, AND LANDING METHOD FOR A PROBE PROVIDED WITH SUCH A DEVICE 审中-公开用于空间探测器的着陆装置以及用这种装置提供的探测器的接地方法公开(公告)号：US20120080562A1
公开(公告)日：2012-04-05
申请号：US13257267
申请日：2010-03-05
CPC分类号： B64G1/62 , B64G1/16 , B64G1/58 , B64G2001/1064 , B64G2001/1071
摘要： A space probe including a descent module with a mobile exploration vehicle, wherein the descent module is a landing module inside which the mobile exploration vehicle is fastened, the landing module being provided with landing legs which can be deployed under the lower level of the mobile exploration vehicle.
摘要翻译： 一种包括具有移动探测车辆的下降模块的空间探测器，其中所述下降模块是其中所述移动探测车辆被固定的着陆模块，所述着陆模块设置有可以部署在所述移动探测器的较低水平下的着陆腿 车辆。
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5.发明授权Landing device for a space probe, and landing method for a probe provided with such a device 有权用于空间探针的着陆装置，以及具有这种装置的探针的着陆方法公开(公告)号：US08991764B2
公开(公告)日：2015-03-31
申请号：US13257267
申请日：2010-03-05
CPC分类号： B64G1/62 , B64G1/16 , B64G1/58 , B64G2001/1064 , B64G2001/1071
摘要： A space probe including a descent module with a mobile exploration vehicle, wherein the descent module is a landing module inside which the mobile exploration vehicle is fastened, the landing module being provided with landing legs which can be deployed under the lower level of the mobile exploration vehicle.
摘要翻译： 一种包括具有移动探测车辆的下降模块的空间探测器，其中所述下降模块是其中所述移动探测车辆被固定的着陆模块，所述着陆模块设置有可以部署在所述移动探测器的较低水平下的着陆腿 车辆。
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6.发明申请公开(公告)号：US20120153077A1
公开(公告)日：2012-06-21
申请号：US13376231
申请日：2010-05-28
CPC分类号： B64G1/62 , B64G2001/1071
摘要： A landing system of a body and a space probe provided with such a system for landing on a bearing ground. The landing system includes landing legs (5), each with a footpad (6) at the end thereof, intended for braking the landing impact of the body when coming into contact with the ground and for supporting the body on the ground after landing. The footpads (6) are not coplanar.
摘要翻译： 身体的一个着陆系统和一个设有这样一个系统的空间探针，用于在轴承地面上着陆。 着陆系统包括着陆腿（5），每个脚蹬在其末端具有足垫（6），用于在与地面接触时制动身体的着陆冲击，并在着陆后将身体支撑在地面上。 脚垫（6）不共面。
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7.发明授权System comprising a spatial mother probe forming a spatial carrier vehicle and a plurality of spatial daughter probes 有权包括形成空间载体载体的空间母体探针和多个空间子探针的系统公开(公告)号：US09073646B2
公开(公告)日：2015-07-07
申请号：US13320307
申请日：2010-05-07
CPC分类号： B64G1/105 , B64G1/641 , B64G2001/643
摘要： A system includes a mother probe forming a carrier space vehicle (1) and a plurality of daughter probes (2a, 2b, 2c) aligned in a longitudinal axis (A) of the mother probe, in which the attachment of the daughter probes to the mother probe is carried out by a plurality of probe-supporting annular segments (5a, 5b, 5c) each provided with an annular collar (3a, 3b, 3c) for attaching a daughter probe.
摘要翻译： 系统包括形成载体空间载体（1）的母体探针和在母体探针的纵向轴线（A）上对准的多个子探针（2a，2b，2c），其中将子探针附接到 母体探针通过多个探针支承环形部分（5a，5b，5c）进行，每个环形部分设置有用于附接子探针的环形套环（3a，3b，3c）。
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公开(公告)号：US5865025A
公开(公告)日：1999-02-02
申请号：US881353
申请日：1997-06-24
CPC分类号： F02K7/10 , Y02T50/672
摘要： A fuel injection stub (6) for a ramjet is designed to operate at a high Mach number. According to the invention, said stub includes a carbon-carbon composite body (10), in which a rail of elementary injectors is arranged, and a nose piece (11) consisting of a thin skin of carbon-carbon composite in at least approximately the shape of a dihedron, the edge (11A) of which has a radius of curvature (r) at most equal to 2 mm and the angle of which is at most equal to 15.degree.. Means (23, 27) for injecting a coolant into the sealed chamber (18) are arranged in said body (10), said injection means producing a number of jets of pressurized coolant striking the concave face of said skin (11).
摘要翻译： 用于冲压式喷气式燃料喷射柱（6）设计成以高马赫数运行。 根据本发明，所述短截线包括碳 - 碳复合体（10），其中布置有基本注射器的轨道，以及由至少大致为所述的碳 - 碳复合材料的薄皮层组成的鼻部件（11） 二面体的形状，其边缘（11A）具有最多等于2mm的曲率半径（r），其角度最大等于15°。 用于将冷却剂注入密封室（18）的装置（23,27）布置在所述主体（10）中，所述注射装置产生许多喷射到所述皮肤（11）的凹面上的加压冷却剂喷射。
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