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公开(公告)号：EP1594736B1
公开(公告)日：2012-12-19
申请号：EP04809283.7
申请日：2004-02-19
Applicant: AAI CORPORATION
Inventor： MILLER, Stephen, W. , VELAZQUEZ, Matthew, T.
IPC: B64F1/04
CPC classification number: B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/084 , B64C2201/102 , B64C2201/165 , B64C2201/201 , B64C2201/203 , B64F1/06
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公开(公告)号：EP2121437A2
公开(公告)日：2009-11-25
申请号：EP08727924.6
申请日：2008-01-18
Applicant: Arlton, Paul E. , Arlton, David J.
Inventor： Arlton, Paul E. , Arlton, David J.
IPC: B64C27/08
CPC classification number: B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/082 , B64C2201/108 , B64C2201/127 , B64C2201/201
Abstract: A rotary wing vehicle includes a body structure having an elongated tubular backbone or core and a counter-rotating coaxial rotor system having rotors. The rotor system is used to move the rotary wing vehicle in directional flight.
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公开(公告)号：EP1799545A1
公开(公告)日：2007-06-27
申请号：EP05789189.7
申请日：2005-02-14
Applicant: RAYTHEON COMPANY
Inventor： CORDER, David, A. , KOESSLER, Jeffrey, H. , WEBB, George, R.
IPC: B64C39/02
CPC classification number: B64C3/56 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/082 , B64C2201/102 , B64C2201/123 , B64C2201/127 , B64C2201/141 , B64C2201/145 , B64C2201/165 , B64C2201/201
Abstract: An air-launched aircraft (10) includes deployable wings (16, 18), elevons (20, 22), and vertical fins (26, 28) that deploy from a fuselage (12) during flight. The aircraft may include a control system for operating the elevons, a communication system, and batteries for powering the systems. In addition, the aircraft may include a payload module (14) that mates with an interface in the fuselage. The payload module may include any of a variety of payloads, including cameras, sensors, and/or radar emitters. The aircraft may be powered or unpowered, and may be very small, for example, less than on the order of 10 kg (22 pounds). The deployable surfaces of the aircraft may be configured to deploy in a pre-determined order, allowing the aircraft automatically to enter controlled flight after being launched in a tumbling mode.
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公开(公告)号：EP1761430A2
公开(公告)日：2007-03-14
申请号：EP05761246.7
申请日：2005-04-14
Applicant: Arlton, Paul E. , Arlton, David J.
Inventor： Arlton, Paul E. , Arlton, David J.
IPC: B64C27/10
CPC classification number: B64C27/10 , B64C27/22 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/082 , B64C2201/102 , B64C2201/108 , B64C2201/141 , B64C2201/146 , B64C2201/165 , B64C2201/201 , B64C2201/203 , B64C2201/205
Abstract: A rotary wing vehicle includes a body structure having an elongated tubular backbone or core, and a counter-rotating coaxial rotor system having rotors with each rotor having a separate motor to drive the rotors about a common rotor axis of rotation. The rotor system is used to move the rotary wing vehicle in directional flight.
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公开(公告)号：EP1628878B1
公开(公告)日：2007-03-07
申请号：EP04734053.4
申请日：2004-05-20
Applicant: QinetiQ Limited
CPC classification number: B64C37/02 , B64C39/024 , B64C39/026 , B64C2201/021 , B64C2201/022 , B64C2201/042 , B64C2201/088 , B64C2201/101 , B64C2201/104 , B64C2201/123 , B64C2201/127 , B64C2201/128 , B64C2201/146 , B64C2201/148 , B64C2201/201 , B64D5/00
Abstract: A heavier-than-air air vehicle (1), particularly a long endurance, solar powered, unmanned aerial vehicle (UAV) intended for 'perpetual' flight within the stratosphere, is carried to its operational altitude suspended on a tether (14) from a helium balloon (16). The tether is attached at or towards a tip of the UAV's wing (3) so that it is carried in effectively a 90° banked attitude. At the desired altitude the UAV's powerplant is started and it flies on its tether in an upwardly-spiralling path relative to the balloon until a level or near level attitude is attained, when the tether is released and the UAV is permitted to assume free flight.
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Patent Agency Ranking
公开(公告)号：EP1628878A1
公开(公告)日：2006-03-01
申请号：EP04734053.4
申请日：2004-05-20
Applicant: Qinetiq Limited
CPC classification number: B64C37/02 , B64C39/024 , B64C39/026 , B64C2201/021 , B64C2201/022 , B64C2201/042 , B64C2201/088 , B64C2201/101 , B64C2201/104 , B64C2201/123 , B64C2201/127 , B64C2201/128 , B64C2201/146 , B64C2201/148 , B64C2201/201 , B64D5/00
Abstract: A heavier-than-air air vehicle (1), particularly a long endurance, solar powered, unmanned aerial vehicle (UAV) intended for 'perpetual' flight within the stratosphere, is carried to its operational altitude suspended on a tether (14) from a helium balloon (16). The tether is attached at or towards a tip of the UAV's wing (3) so that it is carried in effectively a 90° banked attitude. At the desired altitude the UAV's powerplant is started and it flies on its tether in an upwardly-spiralling path relative to the balloon until a level or near level attitude is attained, when the tether is released and the UAV is permitted to assume free flight.
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公开(公告)号：EP1594736A2
公开(公告)日：2005-11-16
申请号：EP04809283.7
申请日：2004-02-19
Applicant: AAI CORPORATION
Inventor： MILLER, Stephen, W. , VELAZQUEZ, Matthew, T.
IPC: B64B1/00
CPC classification number: B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/084 , B64C2201/102 , B64C2201/165 , B64C2201/201 , B64C2201/203 , B64F1/06
Abstract: A portable unmanned air vehicle and launcher system is provided that includes a foldable unmanned air vehicle having a pressure tube; a launch gas reservoir for holding launch gas; a launch tube operatively connected to the launch gas reservoir and having a free end that is positioned in the pressure tube of the air vehicle; a free piston positioned within the launch tube; and a free piston stop to prevent the free piston from leaving the launch tube. A first portion of the launch gas in the launch gas reservoir is released into the launch tube and forces the free piston from an initial position to an end position at which the free piston is stopped by the free piston stop.
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公开(公告)号：EP0184226B1
公开(公告)日：1988-09-14
申请号：EP85116421.0
申请日：1983-10-12
Applicant: DORNIER GMBH
Inventor： Friedel, Franz , Frühauf, Werner , Harms, Günter , Heise, Georg, Dipl.-Ing. , Lükewille, Heinrich, Dipl.-Ing.
CPC classification number: F42B10/64 , B64C39/024 , B64C2201/028 , B64C2201/044 , B64C2201/165 , B64C2201/201 , F16D7/021 , F42B15/105
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公开(公告)号：EP0184226A3
公开(公告)日：1987-05-06
申请号：EP85116421
申请日：1983-10-12
Applicant: DORNIER GMBH
Inventor： Friedel, Franz , Frühauf, Werner , Harms, Günter , Heise, Georg, Dipl.-Ing. , Lükewille, Heinrich, Dipl.-Ing.
CPC classification number: F42B10/64 , B64C39/024 , B64C2201/028 , B64C2201/044 , B64C2201/165 , B64C2201/201 , F16D7/021 , F42B15/105
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公开(公告)号：EP0184226A2
公开(公告)日：1986-06-11
申请号：EP85116421.0
申请日：1983-10-12
Applicant: DORNIER GMBH
Inventor： Friedel, Franz , Frühauf, Werner , Harms, Günter , Heise, Georg, Dipl.-Ing. , Lükewille, Heinrich, Dipl.-Ing.
CPC classification number: F42B10/64 , B64C39/024 , B64C2201/028 , B64C2201/044 , B64C2201/165 , B64C2201/201 , F16D7/021 , F42B15/105
Abstract: Unbemannter Flugkörper, der in einem Behälter transportiert und aus dem Behälter mittels eines Hilfsantriebes nach Lösung einer Arretierung gestartet wird und der während des Marschfluges durch ein Propellertriebwerk antreibbar ist, wobei eine Reibschlußkupplung (64, 65) am Flugkörper vorgesehen ist, die ohne Zuführung von Energie von aussen mittels des Antriebes (7) den innerhalb des Behälters (1') stillstehenden Propeller (6) mit dem bereits im Behälter laufenden Antriebsmotor (7) nach Verlassen des Behälters kuppelt.
Abstract translation: 这是在一个容器中的锁定机构的释放和后运送并从容器推出由辅助驱动装置无人驾驶飞机是由一个螺旋桨发动机，其特征在于，摩擦离合器（64，65）被设置在导弹，巡航飞行期间驱动其中没有能量的供给 从由所述驱动装置的外侧（7），所述容器（1“）的螺旋桨（6）与当前容器内部的固定到驱动马达（7）在离开容器后脱离。
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