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51. 发明公开

EP3173325A1 AN AIRFRAME FOR AN AIR VEHICLE 审中-公开
标题翻译：一种用于空气车辆的机身
公开(公告)号：EP3173325A1
公开(公告)日：2017-05-31
申请号：EP15196707.2
申请日：2015-11-27
申请人： BAE Systems PLC
发明人： The designation of the inventor has not yet been filed
IPC分类号： B64C1/00 , B64C1/12 , B64G1/14 , B64G1/58 , A63H27/00
CPC分类号： B64C1/00 , B64C1/12 , B64G1/14 , B64G1/58
摘要： An airframe (10) for an air vehicle comprising an outer skin layer (12) and a support layer (13) defining a fuselage of said air vehicle, wherein said outer skin layer (12) is magnetically coupled to said support layer (13).
摘要翻译：一种用于飞行器的机身（10），其包括限定所述飞行器的机身的外蒙皮层（12）和支撑层（13），其中所述外蒙皮层（12）磁性耦合到所述支撑层（13）。

52. 发明公开

EP2981461A1 DISPOSITIF DE CONTRÔLE DE LA VITESSE D'UN AVION SPATIAL LORS DE LA TRANSITION D'UNE PHASE DE VOL SPATIAL VERS UNE PHASE DE VOL AÉRONAUTIQUE ET PROCÉDÉ DE TRANSITION ASSOCIÉ 有权
标题翻译：一种用于控制空间飞行器的速度在某一阶段太空飞行过渡到一个阶段期间和相应的过渡过程
公开(公告)号：EP2981461A1
公开(公告)日：2016-02-10
申请号：EP14713144.5
申请日：2014-03-28
申请人： Airbus Defence and Space SAS
发明人： FERREIRA, Eugénio , SANTERRE, Angélique , FAURE, Benjamin , CHEVROLLIER, Samuel , PARPAITE, Pierre , FAVRE, Christophe
IPC分类号： B64C9/32 , B64G1/14 , B64C25/16
CPC分类号： B64G1/62 , B64C9/323 , B64C25/10 , B64C25/16 , B64G1/14 , Y02T50/32
摘要： A spaceplane (10) suitable for aeronautical flight comprising a body and a wing (15) defining a lower airfoil surface in addition to attitude control means that comprise one or a plurality of shutters (11) disposed under the lower airfoil surface of same and manoeuvrable between a stowed position and an inclined extended position for aerodynamic braking during the transition from a phase of space flight to a phase of aeronautical flight of the aircraft.

53. 发明授权

EP2580125B1 MODULE REUTILISABLE SIMPLIFIE POUR LANCEUR 有权转让
标题翻译：简化可重复使用的模块一开始UNIT
公开(公告)号：EP2580125B1
公开(公告)日：2014-10-29
申请号：EP11724636.3
申请日：2011-06-10
申请人： Astrium SAS
发明人： PRAMPOLINI, Marco
IPC分类号： B64G1/00 , B64G1/14 , B64G1/40 , B64G1/62
CPC分类号： B64G1/401 , B64G1/002 , B64G1/40 , B64G1/62

54. 发明授权

EP1976761B1 ROCKET-POWERED VEHICLE RACING SYSTEM 失效
标题翻译： SYSTEM FOR火箭驱动的车辆RACE
公开(公告)号：EP1976761B1
公开(公告)日：2012-12-05
申请号：EP06850515.5
申请日：2006-10-03
申请人： Rocket Racing, Inc.
发明人： DIAMANDIS, Peter, H. , WHITELAW, Granger, B. , D'ANGELO, Michael, R.
IPC分类号： B64D27/02 , B64G1/00 , B64G1/14 , B64G3/00 , A63K3/00 , B64G1/36
CPC分类号： B64G1/00 , A63K3/00 , B64D27/023 , B64G1/14 , B64G1/36 , B64G3/00 , H04H20/04 , H04H60/07

55. 发明公开

EP1735212A4 REVERSABLE SPACE PLANE 有权转让
标题翻译：可逆RAUMFLUGZEUG
公开(公告)号：EP1735212A4
公开(公告)日：2009-07-15
申请号：EP05722476
申请日：2005-01-21
申请人： JANEKE CHARL E
发明人： JANEKE CHARL E
IPC分类号： B64G1/14 , F02K9/42
CPC分类号： B64G1/14 , F02K9/42
摘要： A reversible aerospace plane includes an air intake at a first end of the aerospace plane, at least one heat exchanger disposed in the aerospace plane, an engine at a second end of the aerospace plane, wherein the aerospace plane is configured to accelerate in a first direction and configured to glide and land in a second direction, wherein the second direction is substantially in a reverse direction from the first direction.

56. 发明公开

EP1957366A1 KLAPPBARE RAUMFÄHRE 有权
标题翻译：折叠空间SHUTTLE
公开(公告)号：EP1957366A1
公开(公告)日：2008-08-20
申请号：EP06817464.8
申请日：2006-11-27
申请人： Sharif, Issam
发明人： Sharif, Issam
IPC分类号： B64G1/00 , B64G1/14 , B64B1/06
CPC分类号： B64G1/14 , B64B1/06 , B64B2201/00 , B64G1/002
摘要： The invention relates to an airship which can be unfolded and folded up automatically on the ground and during flight and which can be operated as an aircraft or as a reusable space shuttle, having a combined collapsible gas cell (400), a grid network (600) which provides the shape, an aircraft body (200) comprising a cockpit (210), a cargo bay (220), a machine bay (230) and collapsible wheels (240), components for aircraft navigation control (300), two rocket motors (500L, 500R) which can be rotated, a collapsible rudder wing (700) and a mechanism (100) for operation of the collapsible rudder wing. The combined collapsible gas cell (400) comprises an envelope (402) which can be folded and a housing (401) which cannot be folded. The housing (401) which cannot be folded is mounted on the inner walls and the bottom of the cargo bay (220). The gas cell (400) is filled with helium or hydrogen in the unfolded state, and is completely empty in the collapsed state. The envelope (402) which can be folded is held by the grid network (600) which provides the shape when in the unfolded state, and is located in the internal area of the housing (401), which cannot be folded, in the collapsed state.

57. 发明公开

EP1460048A8 HEAT-RESISTANT MATERIAL AND HOT STRUCTURE MEMBER BOTH FOR SPACE SHUTTLE, SPACE SHUTTLE, AND METHOD FOR PRODUCING HEAT-RESISTANT MATERIAL FOR SPACE SHUTTLE 审中-公开
标题翻译：耐热材料和部件温度航天飞机，航天飞机及其制备方法耐热材料航天飞机
公开(公告)号：EP1460048A8
公开(公告)日：2005-01-19
申请号：EP02793375.3
申请日：2002-12-25
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： OGURI, Kazuyuki Mitsubishi Heavy Industries, Ltd. , SEKIGAWA, Takahiro Mitsubishi Heavy Industries,Ltd
IPC分类号： C04B35/58 , B64G1/58 , B64G1/14
CPC分类号： C04B41/87 , B64G1/14 , B64G1/226 , B64G1/288 , B64G1/363 , B64G1/365 , B64G1/58 , B64G1/62 , C04B35/58078 , C04B41/009 , C04B41/5042 , C04B2111/00982 , C04B2235/3826 , C04B2235/80 , C04B2235/9684 , C04B41/0072 , C04B41/4556 , C04B35/58
摘要： An inexpensive high temperature oxidation resistant material for spacecraft, having a higher heat resistance than a conventional oxidation resistant material of a silicon carbide coating system, which may be readily formed into a desired shape, a hot structure part including the oxidation resistant material for spacecraft, a spacecraft provided with the hot structure part, and a method for producing the oxidation resistant material for spacecraft are provided. The oxidation resistant material for spacecraft includes a ceramic material in which silicon carbide is included in zirconium boride. The method for producing the oxidation resistant material for spacecraft includes the steps of including SiC in zirconium boride, and molding by means of a normal pressure sintering method.

58. 发明公开

EP1436196A1 ESD COATINGS FOR USE WITH SPACECRAFT 审中-公开
标题翻译： ESD涂料，空间车辆使用
公开(公告)号：EP1436196A1
公开(公告)日：2004-07-14
申请号：EP02759693.1
申请日：2002-09-17
申请人： Eikos, Inc.
发明人： GLATKOWSKI, Paul, J. , CONNELL, John, W. , LANDIS, David, H., Jr. , SMITH, Joseph, G., Jr. , PICHE, Joseph, W.
IPC分类号： B64G1/00 , B64G1/14 , C01B31/00 , B05D1/12
CPC分类号： B82Y30/00 , B64G1/226 , B82Y10/00 , C08J5/005 , C09D5/24 , H01B1/24
摘要： Spacecraft with electrostatic dissipative surfaces are disclosed herein. The surface has layer which includes a plurality of carbon nanotubes to incorporate electrical conductivity into space durable polymeric layers without degrading optical transparency, solar absorptivity or mechanical properties.

59. 发明公开

EP1163152A4 PAYLOAD CARRY AND LAUNCH SYSTEM 有权
标题翻译：系统换着穿，启动有效载荷
公开(公告)号：EP1163152A4
公开(公告)日：2004-03-03
申请号：EP99972835
申请日：1999-12-29
申请人： SPACE ACCESS L L C , SCOTT HARRY , WURST STEPHEN G
发明人： SCOTT HARRY , WURST STEPHEN G
IPC分类号： B64C30/00 , B64G1/00 , B64G1/14 , B64G1/40 , F02K7/10 , F02K7/12 , F02K9/50 , F02K9/80
CPC分类号： B64G1/401 , B64G1/005 , B64G1/007 , B64G1/14 , B64G1/402 , F02K7/10 , F02K7/12 , Y02T50/672
摘要： The reusable space launch system (1) embodiment has a first stage vehicle or aerospacecraft (50), a second stage vehicle or reusable spacecraft (51) and a third stage vehicle or reusable orbit transfercraft (52). All the stages have the basic aerodynamic vehicle elements of a fuselage, wings, and tail, with the incorporation of control surfaces to supply lift, stability and control. The aerospacecraft (50) is configured to use ejector ramjet engines (18) for powered flight and includes equipment to capture air to supplement oxidizer for the ejector ramjet engine (18) during take-off and extreme high altitude. In order to optimize aerospacecraft (50) performance in a pull up movement to exit the sensible atmosphere, the aerospacecraft (50) may include auxiliary ascent rocket engines (116).

60. 发明公开

EP0778200A2 Mehrstufiges Raumfahrt-Transportsystem und Verfahren zum Horizontalstart 失效
标题翻译： Mehrstufiges Raumfahrt-Transportsystem und Verfahren zum Horizontalstart
公开(公告)号：EP0778200A2
公开(公告)日：1997-06-11
申请号：EP96118411.6
申请日：1996-11-16
申请人： Daimler-Benz Aerospace Aktiengesellschaft
发明人： Stockfleth, Holger, Dipl.-Ing. , Spies, Johann, Dipl.-Ing.
IPC分类号： B64G1/14
CPC分类号： B64G1/14 , B64G1/005 , B64G1/401 , B64G1/402 , F02K9/766
摘要： Es ist vorgesehen, ein absetzbares Fluggerät (2) mit einem wiederverwendbaren aerodynamischen Trägergerät (1) zu verbinden, wobei das Fluggerät (2) eine Antriebsanlage (5) als Alleinantrieb für die Gesamtanordnung aufweist. Hierbei sind im Trägergerät (1) als Start- und Landevorrichtung Treibstofftanks für die Versorgung der Antriebsanlage (5) angeordnet.
摘要翻译：运输系统由具有可重复使用的气动载体模块（1）的飞行模块（2）组成。飞行模块具有驱动单元，特别是火箭，（5）是组合模块的唯一驱动器。载体模块具有向火箭提供燃料和氧化剂的罐。承载模块具有起落架（4）。燃料箱在供应管线（9,10）中具有分离阀，用于可拆卸地连接到飞行模块中的火箭。飞行模块可以在起落架区域内的载体模块下方悬挂。

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