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1. 发明公开

EP3066006A2 CARGO AIRSHIP 无效
标题翻译： FRACHTLUFTSCHIFF
公开(公告)号：EP3066006A2
公开(公告)日：2016-09-14
申请号：EP14863047.8
申请日：2014-11-03
申请人： LTA Corporation
发明人： GOELET, John , KAPITAN, Loginn , HOCHSTETLER, Ron
IPC分类号： B64B1/22 , B64D1/22 , B64D9/00
CPC分类号： B64B1/08 , B64B1/10 , B64B1/20 , B64B1/22 , B64B1/32 , B64B1/34 , B64B1/58 , B64B1/70 , B64D1/02 , B64D1/22 , B64D9/003 , Y02T50/46
摘要： A cargo airship is disclosed. The cargo airship may include a hull configured to contain a gas and at least one propulsion assembly coupled to the airship and including a propulsion device. The cargo airship may further include a payload bay comprising an external cargo area located outside of the hull. The cargo airship may also include a cargo handling system including at least one hoisting mechanism configured to lift cargo into the external cargo area while the airship is hovering.
摘要翻译：披露了一艘货船。货物飞艇可以包括构造成容纳气体的船体和联接到飞艇的至少一个推进组件，并且包括推进装置。货物飞艇还可以包括有效载荷舱，其包括位于船体外部的外部货物区域。货物飞艇还可以包括货物处理系统，其包括至少一个起重机构，其构造成在飞艇盘旋时将货物提升到外部货物区域中。

2. 发明授权

EP2143610B1 Retracting Air Cushioned Landing System for Air Vehicles 有权
标题翻译：起落架的收放系统，气垫飞行器
公开(公告)号：EP2143610B1
公开(公告)日：2012-09-05
申请号：EP09164336.1
申请日：2009-07-01
申请人： Lockheed Martin Corporation
发明人： Morehead, John , Greiner, Douglas , Pasman, Renee , Boyd, Robert
IPC分类号： B64B1/06 , B64B1/32 , B60V3/08
CPC分类号： B60V3/08 , B64B1/06 , B64B1/32 , B64B2201/00

3. 发明授权

EP1160156B1 Antriebseinheit mit zumindest einem eine Propellernabe aufweisenden Propeller 失效
标题翻译：驱动单元与具有螺旋桨至少一个螺旋桨
公开(公告)号：EP1160156B1
公开(公告)日：2006-06-07
申请号：EP01122153.8
申请日：1998-01-02
申请人： Künkler, Hermann , IABG Industrieanlagen-Betriebsgesellschaft mbH
发明人： Künkler, Hermann
IPC分类号： B64C27/52 , B64C29/00 , B64C27/28 , B64C27/41
CPC分类号： B64C29/0033 , B63H5/125 , B64B1/32 , B64B2201/00 , B64C11/02 , B64C27/28 , B64C27/52 , B64D35/00

4. 发明公开

EP1209076A2 Hybrid aircraft 失效
标题翻译：混合飞机
公开(公告)号：EP1209076A2
公开(公告)日：2002-05-29
申请号：EP02075631.8
申请日：1996-10-24
申请人： Bothe, Hans-Jurgen
发明人： Bothe, Hans-Jurgen
IPC分类号： B64C29/00 , B64C1/00 , B64C39/00
CPC分类号： B64C39/00 , B64B1/06 , B64B1/08 , B64B1/18 , B64B1/32 , B64B1/34 , B64B2201/00 , B64C27/52 , B64C29/00 , B64C29/0033 , B64C39/10 , B64C2001/0063 , B64C2001/0072 , B64C2001/0081 , Y02T50/12 , Y02T50/43
摘要： A hybrid aircraft having VTOL R-VTOL and S-STOL capabilities having a lifting body hull (1) and four wing sections (20) arranged in tandem which are pivotally moveable about their neutral axis. Each wing section has mounted thereon a pivotal propeller-rotor (21) assembly for providing thrust substantially in a range between horizontal and vertical. The wings and propellers are integrated to the hull by an outrigger designed to be very stiff and to distribute forces from the wings and propellers from the hull. The hull is shaped to provide aerodynamic lift in an airstream and to facilitate construction by minimizing the number of panels of differing curvature required. The hull is formed of a pressure tensioned frame covered with semi-rigid panels, a lower cladding frame and bow and stem cladding nose cones. The semi-rigid panels covering the frame are formed of gas-tight and abrasion resistant laminate material and are connected to the frame by means of an interface rib and latch system. The frame is formed of a plurality of curved elongate segments arranged in series orthogonal to the long axis of the hull and connected by means of torsion members. A turbo-electric drive system can be used to drive the aircraft. An advanced hybrid aircraft is also described having about 8 to 12 high speed fans in place of the propeller-rotors.
摘要翻译：具有VTOL R-VTOL和S-STOL能力的混合动力飞机具有提升体壳体（1）和四个前后布置的机翼部分（20），所述机翼部分（20）可围绕其中性轴线枢转地移动。每个翼段在其上安装有枢转螺旋桨 - 转子（21）组件，用于提供基本上在水平和垂直之间范围内的推力。机翼和螺旋桨通过设计成非常坚硬的支腿与船体相结合，并从机身和螺旋桨上分配来自船体的力。船体成形为在气流中提供气动升力，并通过最小化所需曲率不同的面板的数量来促进施工。船体由压力张紧框架形成，覆盖有半刚性面板，下覆层框架以及弓形和杆状覆层鼻锥体。覆盖框架的半刚性面板由气密和耐磨层压材料形成，并通过接口肋和闩锁系统连接到框架。该框架由多个弯曲的细长段形成，该多个弯曲的细长段与船体的长轴线正交地排列并通过扭转构件连接。可以使用涡轮驱动系统来驱动飞机。还描述了一种高级混合动力飞机，其具有大约8至12个高速风扇来代替螺旋桨转子。

5. 发明授权

EP0854821B1 HYBRID AIRCRAFT 失效
标题翻译： HYBRID飞机
公开(公告)号：EP0854821B1
公开(公告)日：2002-05-02
申请号：EP96934255.9
申请日：1996-10-24
申请人： Bothe, Hans-Jurgen
发明人： Bothe, Hans-Jurgen
IPC分类号： B64C29/00 , B64C1/00 , B64C39/00
CPC分类号： B64C39/00 , B64B1/06 , B64B1/08 , B64B1/18 , B64B1/32 , B64B1/34 , B64B2201/00 , B64C27/52 , B64C29/00 , B64C29/0033 , B64C39/10 , B64C2001/0063 , B64C2001/0072 , B64C2001/0081 , Y02T50/12 , Y02T50/43
摘要： A hybrid aircraft having VTOL R-VTOL and S-STOL capabilities having a lifting body hull (1) and four wing sections (20) arranged in tandem which are pivotally moveable about their neutral axis. Each wing section has mounted thereon a pivotal propeller-rotor (21) assembly for providing thrust substantially in a range between horizontal and vertical. The wings and propellers are integrated to the hull by an outrigger designed to be very stiff and to distribute forces from the wings and propellers from the hull. The hull is shaped to provide aerodynamic lift in an airstream and to facilitate construction by minimizing the number of panels of differing curvature required. The hull is formed of a pressure tensioned frame covered with semi-rigid panels, a lower cladding frame and bow and stem cladding nose cones. The semi-rigid panels covering the frame are formed of gas-tight and abrasion resistant laminate material and are connected to the frame by means of an interface rib and latch system. The frame is formed of a plurality of curved elongate segments arranged in series orthogonal to the long axis of the hull and connected by means of torsion members. A turbo-electric drive system can be used to drive the aircraft. An advanced hybrid aircraft is also described having about 8 to 12 high speed fans in place of the propeller-rotors.

6. 发明公开

EP0854821A2 HYBRID AIRCRAFT 失效
标题翻译： HYBRID飞机
公开(公告)号：EP0854821A2
公开(公告)日：1998-07-29
申请号：EP96934255.0
申请日：1996-10-24
申请人： Bothe, Hans-Jurgen
发明人： Bothe, Hans-Jurgen
IPC分类号： B64B1 , B64C1 , B64C27 , B64C29 , B64C39
CPC分类号： B64C39/00 , B64B1/06 , B64B1/08 , B64B1/18 , B64B1/32 , B64B1/34 , B64B2201/00 , B64C27/52 , B64C29/00 , B64C29/0033 , B64C39/10 , B64C2001/0063 , B64C2001/0072 , B64C2001/0081 , Y02T50/12 , Y02T50/43
摘要： A hybrid aircraft having VTOL R-VTOL and S-STOL capabilities having a lifting body hull (1) and four wing sections (20) arranged in tandem which are pivotally moveable about their neutral axis. Each wing section has mounted thereon a pivotal propeller-rotor (21) assembly for providing thrust substantially in a range between horizontal and vertical. The wings and propellers are integrated to the hull by an outrigger designed to be very stiff and to distribute forces from the wings and propellers from the hull. The hull is shaped to provide aerodynamic lift in an airstream and to facilitate construction by minimizing the number of panels of differing curvature required. The hull is formed of a pressure tensioned frame covered with semi-rigid panels, a lower cladding frame and bow and stem cladding nose cones. The semi-rigid panels covering the frame are formed of gas-tight and abrasion resistant laminate material and are connected to the frame by means of an interface rib and latch system. The frame is formed of a plurality of curved elongate segments arranged in series orthogonal to the long axis of the hull and connected by means of torsion members. A turbo-electric drive system can be used to drive the aircraft. An advanced hybrid aircraft is also described having about 8 to 12 high speed fans in place of the propeller-rotors.

7. 发明公开

EP2686238A1 SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS 有权
标题翻译：系统和方法，持续时间长AIR船舶营运
公开(公告)号：EP2686238A1
公开(公告)日：2014-01-22
申请号：EP12712014.5
申请日：2012-03-13
申请人： Heppe, Stephen
发明人： Heppe, Stephen
IPC分类号： B64B1/06 , B64C37/02
CPC分类号： B64B1/32 , B64B1/06 , B64C37/02 , B64C2201/022 , B64C2201/063
摘要： In one example, a long endurance airship system includes a payload airship and a first logistics airship mechanically joined to the payload airship to form a first combined airship, the payload airship and the logistics airship having design capabilities differing by at least a factor of two with regard to at least one of: power generation capability, propulsion capability, endurance capability, and lift capability, in which the first combined airship is free flying, lighter-than-air, and configured to maintain stationkeeping for greater than 30 days. Illustrative methods for long endurance airship operations are also provided.

8. 发明公开

EP2143610A3 Retracting Air Cushioned Landing System for Air Vehicles 有权
标题翻译：起落架的收放系统，气垫飞行器
公开(公告)号：EP2143610A3
公开(公告)日：2011-06-22
申请号：EP09164336.1
申请日：2009-07-01
申请人： Lockheed Martin Corporation
发明人： Morehead, John , Greiner, Douglas , Pasman, Renee , Boyd, Robert
IPC分类号： B60V3/08
CPC分类号： B60V3/08 , B64B1/06 , B64B1/32 , B64B2201/00
摘要： A hybrid air vehicle (100) is disclosed in which a cover is provided for a plurality of air cushioned landing pads (206) to reduce drag when airborne. The pad is inflatable to provide an air cushioned during touchdown and deflatable during flight of the air vehicle. The cover can include a first cover portion and a second cover portion. A first cover roller of the first cover portion and a matching second cover roller of the second cover portion abut to cover the corresponding pad. The first cover roller and the second cover roller, which are separate and free from a physical linkage there between, are separable in an eyelid fashion to expose the corresponding pad. A separation gap between the first cover roller and the second cover roller is increased or decreased by roller straps to cover or expose the corresponding pad.

9. 发明授权

EP1772374B1 Non-rigid airship with direct mounted propulsion 有权
标题翻译：非刚性飞艇具有直接连接驱动器
公开(公告)号：EP1772374B1
公开(公告)日：2010-07-07
申请号：EP06255086.8
申请日：2006-09-30
申请人： Lockheed Martin Corporation
发明人： Marimon, Thomas L. , Peritt, Jonathan , Houmard, James E.
IPC分类号： B64B1/30
CPC分类号： B64B1/32 , B64B1/02 , B64B1/42

10. 发明公开

EP2125506A2 LUFTSCHIFF 审中-公开
公开(公告)号：EP2125506A2
公开(公告)日：2009-12-02
申请号：EP08716573.4
申请日：2008-03-17
申请人： Technische Universität Chemnitz
发明人： KRAUSE, Thomas
IPC分类号： B64B1/32 , B64B1/02
CPC分类号： B64B1/32
摘要： The invention relates to an airship comprising a balloon and several drives for displacing the airship. Said invention can be used by dirigibles that are also known as autonomous airships or blimps, as well as for Zeppelins. The aim of the invention is to provide an airship of the above-mentioned type in which the airship can be prevented to a large extent from oscillating or tilting. Said aim is achieved as the drives of the airship are at least three drives and are arranged about the balloon in such a manner that a force vector or a torque vector generated by the drives can be produced thus varying the position thereof.
摘要翻译：飞艇技术领域本发明涉及一种飞艇，其包括气球以及用于使飞艇移位的多个驱动器。所述发明可以被称为自主飞艇或软式飞艇的飞船以及齐柏林飞艇所使用。本发明的目的是提供一种上述类型的飞艇，其中可以在很大程度上防止飞艇摆动或倾斜。由于飞艇的驱动器是至少三个驱动器并且以这样的方式围绕气囊布置，使得可以产生由驱动器产生的力矢量或转矩矢量，从而改变其位置，从而实现所述目标。

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