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31. 发明专利

JP2008247378A Aircraft 有权
标题翻译：飞机
公开(公告)号：JP2008247378A
公开(公告)日：2008-10-16
申请号：JP2008049880
申请日：2008-02-29
申请人： Eads Deutschland Gmbh , イーエイーディーエス、ドイチュラント、ゲゼルシャフト、ミット、ベシュレンクテル、ハフツングEads Deutschland Gmbh
发明人： SCHWARZ MICHAEL
IPC分类号： B64D27/14
CPC分类号： B64D27/20 , B64C39/024 , B64C2201/021 , B64C2201/048
摘要： PROBLEM TO BE SOLVED: To provide an aircraft having improved aerodynamical characteristics and excellent in direction stability.
SOLUTION: In the aircraft having a first drive unit 4 in which an air taking-in port 10 is formed on an upper side of a body 2 of the aircraft 1 and a second drive unit 5 in which an air taking-in port 10 is formed on a lower side of the body 2 of the aircraft 1, the body of the aircraft 1 has a recession part 12 for storing the drive units 4, 5, and the recession part 12 is arranged such that the first and second drive units 4, 5 are vertically superposed/arranged on a plane where a vertical axis and a perpendicular axis of the aircraft 1 are laid. The drive units 4, 5 include an engine 14, a housing 11 provided with the air taking-in port 10, a means 8 for removably fixing the drive units 4, 5 to the body 2 of the aircraft 1, and a means 9 for removably bonding an electricity feed wire, a data circuit and a fuel pipe between the drive units 4, 5 and the body 2 of the aircraft 1.
COPYRIGHT: (C)2009,JPO&INPIT
摘要翻译：要解决的问题：提供具有改善的空气动力特性和优异的方向稳定性的飞机。解决方案：在具有第一驱动单元4的飞行器中，在飞行器1的主体2的上侧形成有吸气口10，其中空气吸入口端口10形成在飞行器1的主体2的下侧，飞行器1的主体具有用于存储驱动单元4,5的凹陷部12，并且凹部12被布置成使得第一和第二驱动单元4,5垂直叠加/布置在飞行器1的垂直轴和垂直轴线的平面上。驱动单元4,5包括发动机14，设置有吸气口10的壳体11，用于将驱动单元4,5可拆卸地固定到飞行器1的主体2的装置8和用于在驱动单元4,5和飞行器1的主体2之间可拆卸地连接供电线，数据电路和燃料管。（C）2009年，JPO和INPIT

32. 发明授权

EP1590239B1 AUTOMATED CARGO TRANSPORTATION SYSTEM 有权
标题翻译： AUTOMATED货运系统
公开(公告)号：EP1590239B1
公开(公告)日：2014-08-13
申请号：EP04701733.0
申请日：2004-01-13
申请人： Boxair Engineering, LLC
发明人： STUPAKIS, John, S.
IPC分类号： B64C1/00
CPC分类号： B64C39/024 , B64C39/02 , B64C2201/048 , B64C2201/086 , B64C2201/104 , B64C2201/128 , B64C2201/141 , B64C2201/165 , B64C2201/187 , B64C2211/00 , B64D2011/0046 , Y10S244/903

33. 发明公开

EP2147858A3 Ducted fan core for use with an unmanned aerial vehicle 失效
标题翻译：涵道的核心用在无人导弹
公开(公告)号：EP2147858A3
公开(公告)日：2012-04-11
申请号：EP09160870.3
申请日：2009-05-21
申请人： Honeywell International Inc.
发明人： Collette, Daniel Ross
IPC分类号： B64C27/20 , B64C39/02
CPC分类号： B64C39/024 , B64C27/20 , B64C2201/027 , B64C2201/048 , B64C2201/088 , B64C2201/108 , B64C2201/126 , B64C2201/162
摘要： A ducted fan core for an unmanned aerial vehicle is provided that accommodates a wide variety of payloads. The ducted fan core comprises a frame (190), attached to which are an engine (120), gearbox assembly, fan, and a plurality of control vanes (130). A first surface on the frame comprises a plurality of connects or electrical traces. The plurality of connects are used to removably attach a variety of pods (240) carrying various payloads. Thus, a wide variety of payloads may be delivered using the same unmanned aerial vehicle, simply by removing and attaching different pods to a fixed vehicle core. These pods may be shaped so as to form part of the vehicle exterior, and when the pods are attached to the frame, they enhance the aerodynamics of the vehicle.

34. 发明公开

EP2147858A2 Ducted fan core for use with an unmanned aerial vehicle 失效
标题翻译： Mantelstromkern zur Verwendung在einem unbemanntenFlugkörper
公开(公告)号：EP2147858A2
公开(公告)日：2010-01-27
申请号：EP09160870.3
申请日：2009-05-21
申请人： Honeywell International Inc.
发明人： Collette, Daniel Ross
IPC分类号： B64C27/20 , B64C39/02
CPC分类号： B64C39/024 , B64C27/20 , B64C2201/027 , B64C2201/048 , B64C2201/088 , B64C2201/108 , B64C2201/126 , B64C2201/162
摘要： A ducted fan core for an unmanned aerial vehicle is provided that accommodates a wide variety of payloads. The ducted fan core comprises a frame (190), attached to which are an engine (120), gearbox assembly, fan, and a plurality of control vanes (130). A first surface on the frame comprises a plurality of connects or electrical traces. The plurality of connects are used to removably attach a variety of pods (240) carrying various payloads. Thus, a wide variety of payloads may be delivered using the same unmanned aerial vehicle, simply by removing and attaching different pods to a fixed vehicle core. These pods may be shaped so as to form part of the vehicle exterior, and when the pods are attached to the frame, they enhance the aerodynamics of the vehicle.
摘要翻译：提供用于无人驾驶飞行器的管道风扇芯，其容纳各种有效载荷。风管风扇芯包括附接到发动机（120），齿轮箱组件，风扇和多个控制叶片（130）的框架（190）。框架上的第一表面包括多个连接或电迹线。多个连接件用于可移除地附接承载各种有效载荷的各种吊舱（240）。因此，简单地通过将不同的荚移除并附接到固定的车辆核心，可以使用相同的无人驾驶飞行器来传送各种有效载荷。这些荚可以成形为形成车辆外部的一部分，并且当荚被附接到框架时，它们增强了车辆的空气动力学。

35. 发明公开

EP1590239A2 AUTOMATED CARGO TRANSPORTATION SYSTEM 有权
标题翻译： AUTOMATED货运系统
公开(公告)号：EP1590239A2
公开(公告)日：2005-11-02
申请号：EP04701733.0
申请日：2004-01-13
申请人： Boxair Engineering, LLC
发明人： STUPAKIS, John, S.
IPC分类号： B64C1/00
CPC分类号： B64C39/024 , B64C39/02 , B64C2201/048 , B64C2201/086 , B64C2201/104 , B64C2201/128 , B64C2201/141 , B64C2201/165 , B64C2201/187 , B64C2211/00 , B64D2011/0046 , Y10S244/903
摘要： A modular automated air transport system comprising an unmanned autonomous aircraft having a selectively detachable control systems portion and a structural air frame portion, wherein the structural air frame portion contains an interior cargo hold, aerodynamic members having control surfaces and at least one propulsion device attached to the structural air frame portion; and wherein the control system portion includes a control computer for autonomously controlling the flight of said air transport system from one known location to a second known location.

36. 发明公开

EP3402718A1 HYBRID PROPULSION VERTICAL TAKE-OFF AND LANDING AIRCRAFT 有权
公开(公告)号：EP3402718A1
公开(公告)日：2018-11-21
申请号：EP17701961.9
申请日：2017-01-12
申请人： Aurora Flight Sciences Corporation
发明人： GIANNINI, Francesco , GOMEZ, Martin , COTTRELL, Dan , LEDE, Jean-Charles , ROBERTS, Tom , SCHAEFER, Carl, Jr. , COLAS, Dorian , WHIPPLE, Brian , NUHFER, Tim , HUNTER, Herb , GROHS, Jonathon , PETULLO, Steve
IPC分类号： B64C3/38 , B64C5/04 , B64C5/16 , B64C29/00 , B64C39/12 , B64D27/02 , B64D27/24
CPC分类号： B64C29/0033 , B64C3/385 , B64C5/04 , B64C5/16 , B64C39/024 , B64C39/12 , B64C2201/021 , B64C2201/042 , B64C2201/048 , B64D27/24 , B64D29/02 , B64D2027/026 , Y02T50/14 , Y02T50/44 , Y02T50/64
摘要： A hybrid propulsion aircraft is described having a distributed electric propulsion system. The distributed electric propulsion system includes a turbo shaft engine that drives one or more generators through a gearbox. The generator provides AC power to a plurality of ducted fans (each being driven by an electric motor). The ducted fans may be integrated with the hybrid propulsion aircraft's wings. The wings can be pivotally attached to the fuselage, thereby allowing for vertical take-off and landing. The design of the hybrid propulsion aircraft mitigates undesirable transient behavior traditionally encountered during a transition from vertical flight to horizontal flight. Moreover, the hybrid propulsion aircraft offers a fast, constant-altitude transition, without requiring a climb or dive to transition. It also offers increased efficiency in both hover and forward flight versus other VTOL aircraft and a higher forward max speed than traditional rotorcraft.

37. 发明授权

EP2844556B1 HYBRIDFLUGZEUG 有权
公开(公告)号：EP2844556B1
公开(公告)日：2016-04-27
申请号：EP13724566.8
申请日：2013-05-16
申请人： Siemens Aktiengesellschaft
发明人： ANTON, Frank , GEDIGA, Swen , WOLLENBERG, Johannes
IPC分类号： B64C31/024 , B64D27/24 , B64D27/02
CPC分类号： B64D27/24 , B64C31/024 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64D2027/026 , Y02T50/64 , Y10S903/903

38. 发明公开

EP2844556A1 HYBRIDFLUGZEUG 有权
标题翻译： HYBRID飞机
公开(公告)号：EP2844556A1
公开(公告)日：2015-03-11
申请号：EP13724566.8
申请日：2013-05-16
申请人： Siemens Aktiengesellschaft
发明人： ANTON, Frank , GEDIGA, Swen , WOLLENBERG, Johannes
IPC分类号： B64C31/024 , B64D27/24 , B64D27/02
CPC分类号： B64D27/24 , B64C31/024 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64D2027/026 , Y02T50/64 , Y10S903/903
摘要： The invention relates to a hybrid aircraft (F). According to the invention, a suitable position for mounting an energy generation unit (14) in the aircraft is identified, said energy generation unit comprising an internal combustion engine (34) and an electric generator (30) that is coupled thereto via a shaft. Independently of the position of the energy generation unit (14), a position is also identified for a thrust generation unit (12) comprising an electric motor (24) and a propeller (20) that is coupled thereto via a shaft (22). When the aircraft (F) is built, the thrust generation unit (12) and the energy generation unit (14) are disposed in the positions identified therefor. The generator (30) is then coupled to the electric motor (24) via an electric transmission device (16).

39. 发明公开

EP2720948A1 SELF-SUSTAINING DRONE AIRCRAFT FREIGHT AND OBSERVATION SYSTEM 审中-公开
标题翻译：自治区货运和观测SYSTEM FOR无人机
公开(公告)号：EP2720948A1
公开(公告)日：2014-04-23
申请号：EP11867771.5
申请日：2011-06-17
申请人： Sing, Robert, L.
发明人： Sing, Robert, L.
IPC分类号： B64F1/22 , B64D9/00 , B64F1/28 , B64D45/00 , B64C13/18
CPC分类号： B64D9/00 , B64C39/024 , B64C2201/021 , B64C2201/048 , B64C2201/084 , B64C2201/104 , B64C2201/128 , B64C2201/145 , B64C2201/187
摘要： The self-sustaining drone aircraft freight and observation system (5) comprises a fleet of jet-powered drone aircraft (10) designed to carry freight (12) only. The drones (10) operate from a separate airfield in outlying areas to decrease land costs and to avoid disturbing residential and business areas. Navigation is automated using guidance from GPS satellites (16), and the aircraft (10) can be assisted by a hydraulic catapult (13) during takeoff to reduce the fuel payload. The observation component (18) includes sensors that can observe weather conditions and emergency signals from boats, ships and other sources. The system (5) may include a large-scale energy production center and multi-acre vegetable, herb and flower production center (26). The energy production center includes solar panels (30), fuel cells (38), and batteries (44). Thus, the system (5) does not need to be connected to the public utility electrical grid.

40. 发明公开

EP1784331A1 UNMANNED AIR VEHICULES AND METHOD OF LANDING SAME 审中-公开
标题翻译：无人驾驶飞机登陆方式为同一
公开(公告)号：EP1784331A1
公开(公告)日：2007-05-16
申请号：EP05759026.7
申请日：2005-07-06
申请人： ELBIT SYSTEMS LTD.
发明人： SIRKIS, Omri
IPC分类号： B64C39/02
CPC分类号： B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64C2201/086 , B64C2201/104 , B64C2201/167 , B64C2201/187
摘要： There is provided an Unmanned Air Vehicule (uav) (2) including an engine (4) and an airframe (6), including means for performing a deep stall maneouvre; at least one inflatable sleeve (12) connected or connectable to the airframe (6), and means for inflating the sleeve (12) during flight, wherein the inflated sleeve (12) extends along the lower side of the airframe (6) so as to protect same during deep stall landing. A method for operating an Unmanned Air Vehicle (UAV), including an engine and an airframe is also provided.

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