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1. 发明公开

EP1283164A2 Vorrichtung zum Überschalltransport 有权
标题翻译： Vorrichtung zumÜberschall运输
公开(公告)号：EP1283164A2
公开(公告)日：2003-02-12
申请号：EP02015965.3
申请日：2002-07-18
申请人： Astrium GmbH
发明人： van der Velden, Alexander , Stockfleth, Holger
IPC分类号： B64C37/02 , B64D25/12
CPC分类号： B64D25/12 , B64C37/02 , B64C39/02 , B64D2011/0046 , B64D2201/00
摘要： Bei einer Vorrichtung zum Überschalltransport von Passagieren mit einem als Kampfflugzeug ausgebildeten Hochleistungsflugzeug (1) wird vorgeschlagen, daß ein Passagiermodul (2) als autarke Zusatzkabine einschließlich Versorgungseinrichtungen mit dem Kampfflugzeug in der Art eines Nutzlastbehälters verbunden ist.
摘要翻译：使用设计为作战飞机的高性能飞机的超音速乘客运输装置（1）包括设计为自给自足的附加舱室的乘客模块（2）和以装载容器的形式连接到作战飞机的供应装置。优选特征：战斗机还附加设置位置控制喷嘴（3）和/或火箭助推器（4）。乘客模块使用分离元件可拆卸地保持在战斗平面上，并使用降落伞系统从作战飞机上分离和落下。

2. 发明授权

EP0127246B1 Capsule and rocket extraction system 失效
标题翻译：胶囊和口腔提取系统
公开(公告)号：EP0127246B1
公开(公告)日：1987-09-30
申请号：EP84300070.4
申请日：1984-01-05
申请人： Stencel Aero Engineering Corp.
发明人： Peck, Walter R.
IPC分类号： B64D25/12
CPC分类号： B64D25/12

3. 发明公开

EP3418187A1 TRANSPORTATION SYSTEM AND METHOD FOR POD ASSEMBLY SELECTIVELY ATTACHABLE TO AIRCRAFT 审中-实审
公开(公告)号：EP3418187A1
公开(公告)日：2018-12-26
申请号：EP18186939.7
申请日：2016-08-25
申请人： Bell Helicopter Textron Inc.
发明人： McCULLOUGH, John Richard , OLDROYD, Paul K.
IPC分类号： B64C17/02 , B64C29/02 , B64C39/02 , B64C27/26 , B64D25/12 , G08G5/00 , G05D1/10 , B64C39/08 , B64C27/30 , B64D17/80
CPC分类号： B64C29/0033 , B64C1/28 , B64C1/32 , B64C11/28 , B64C17/02 , B64C27/26 , B64C27/28 , B64C27/30 , B64C29/02 , B64C39/024 , B64C39/08 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/128 , B64C2201/185 , B64C2211/00 , B64D17/80 , B64D25/12 , G08G5/0065 , G08G5/0069 , G08G5/025
摘要： The present disclosure relates to a transportation system and services method including receiving, at a transportation services provider system, a request for transportation of a pod assembly (170) having a current location and a destination; uploading a flight plan to a flight control system of a flying frame (112) including an airframe and a propulsion system; dispatching the flying frame (112) to the current location of the pod assembly (170); coupling the flying frame (112) to the pod assembly (170) at the current location of the pod assembly (170); transporting the pod assembly (170) by air from the current location of the pod assembly (170) to the destination of the pod assembly (170); and decoupling the pod assembly (170) from the flying frame (112) at the destination of the pod assembly (170).

4. 发明授权

EP1747990B1 Fluggerät mit einem Rettungslandesystem 有权转让
标题翻译：飞机救援着陆系统
公开(公告)号：EP1747990B1
公开(公告)日：2009-02-11
申请号：EP06013983.9
申请日：2006-07-06
申请人： EADS Deutschland GmbH
发明人： Christof, Horst
IPC分类号： B64D17/80 , B64D25/12
CPC分类号： B64D25/12 , B64D17/80 , Y10S244/902

5. 发明公开

EP1110861A1 Capsule ejection system for passenger aircraft 审中-公开
标题翻译： KapselrettungssystemfürPassagierluftfahrzeuge
公开(公告)号：EP1110861A1
公开(公告)日：2001-06-27
申请号：EP00126857.2
申请日：2000-12-07
申请人： Chiu, Chui-Wen
发明人： Chiu, Chui-Wen
IPC分类号： B64D25/12
CPC分类号： B64D25/12
摘要： Nowadays, travelling by airplanes has been well established, and air accident rate is on the whole very low. However, as the number of air flights increases, accidents with the fatality of more than one hundred people have occurred. With the occurrence of such accidents, it poses fear to tens of thousands of air travellers that catastrophe may fall upon them in any flight. Two hundred and thirty people died on August 20, 1997 aboard Transworld Airline Flight 800, and two hundred and ninety people perished on Swiss Airline Flight 111 on September 20, 1998, while two hundred and seventeen people died in the air disaster on Egypt Airline Flight 990 on October 31, 1999. These accidents occurred prior to my invention because the airplanes failed to provide the appropriate means for saving the lives of the travellers in these accidents. Soft pillows, woolen blankets, oxygen masks, seat belts and floatation jackets did not save any life in these accidents. The crux of this invention is to provide means for blasting the airplane body apart in an accident so as to enable separate passengers cabin sections to break away automatically from the airplane. The break away passengers cabin sections will formed independent sealed units similar to unhitched train carts passing through a tunnel so as to protect the passengers who may remain sitting in each cabin. With such safety provision, the lives of the passengers of the Transworld, Swiss, and Egypt Airlines accidents would have been saved; also, the fear of billion of air travel passengers would be dispelled.
摘要翻译：如今，飞机旅行已经很成熟，空中交通事故率处于非常低的水平。但随着航班数量的增加，死亡人数已达百人以上。随着这种事故的发生，恐怕数万名乘客在任何飞行中可能会遇到灾难。一九九七年八月二十日，二百三十人于一九九八年二月二十日在Transworld航空800班机上遇难，二百九十人于一九九八年九月二十日在瑞士航空111班机上丧生，二百一十七人在埃及航空公司 990年10月31日，这些事故发生在我的发明之前，因为飞机没有提供适当的方法来挽救这些事故中的旅客的生命。软枕头，羊毛毯，氧气面罩，安全带和漂浮夹克在这些事故中没有挽救生命。本发明的关键在于提供在事故中将飞机机体分开的装置，以使得能够使单独的乘客舱区段与飞机自动脱离。拆卸乘客舱部分将形成独立的密封单元，类似于穿过隧道的未开凿的火车车厢，以保护可能保持坐在每个客舱的乘客。有了这样的安全规定，Transworld，瑞士和埃及航空公司的乘客的生命将会得到挽救; 此外，恐怕十亿的航空旅客将被驱散。

6. 发明公开

EP3466813A1 TILTROTOR AIRCRAFT HAVING INTERCHANGEABLE PAYLOAD MODULES 有权
公开(公告)号：EP3466813A1
公开(公告)日：2019-04-10
申请号：EP18195580.8
申请日：2018-09-19
申请人： Bell Helicopter Textron Inc.
发明人： CAMPBELL, Kip Gregory
IPC分类号： B64C29/00
CPC分类号： B64D1/02 , B64C29/0033 , B64C2201/128 , B64D25/12 , B64D37/12
摘要： A tiltrotor aircraft (10) has a vertical takeoff and landing flight mode and a forward flight mode. The aircraft (10) includes an airframe (24) having a wing (14) with oppositely disposed wing tips (14c, 14d). Tip booms (16a, 16b) respectively extend longitudinally from the wing tips (14c, 14d). Forward rotors (28a, 28b) are coupled to the forward ends (18a, 18b) of the tip booms (16a, 16b) and aft rotors (28c, 28d) are coupled to the aft ends (20a, 20b) of the tip booms (16a, 16b). The forward rotors (28a, 28b) are reversibly tiltable between a vertical lift orientation, wherein the forward rotors (28a, 28b) are above the tip booms (16a, 16b), and a forward thrust orientation, wherein the forward rotors (28a, 28b) are forward of the tip booms (16a, 16b). The aft rotors (28c, 28d) are reversibly tiltable between a vertical lift orientation, wherein the aft rotors (28c, 28d) are below the tip booms (16a, 16b), and a forward thrust orientation, wherein the aft rotors (28c, 28d) are aft of the tip booms (16a, 16b). One of a plurality of payload modules (12) is interchangeable coupled to the airframe (24), wherein each payload module (12) has a respective function.

7. 发明公开

EP3377406A2 DETACHABLE PILOTABLE CAPSULES AND AIRCRAFTS INCLUDING DETACHABLE PILOTABLE CAPSULES 审中-公开
公开(公告)号：EP3377406A2
公开(公告)日：2018-09-26
申请号：EP16865851.6
申请日：2016-11-15
申请人： A.L.D. Advanced Logistics Development Ltd.
发明人： BLUVBAND, Zigmund , KUSHNIR, Emanuel , ASNIN, Gleb
IPC分类号： B64D25/12 , B64D5/00 , B64C3/46 , B64C13/18 , B64C29/00 , B64C39/06 , B64D27/16
CPC分类号： B64D5/00 , B64C3/46 , B64C13/18 , B64C29/0075 , B64C30/00 , B64C39/062 , B64C2201/206 , B64D25/12 , B64D27/16
摘要： The present invention includes pilotable capsules, detachable from an aircraft and aircrafts including such capsules. According to some embodiments, there may be provided one or more capsules capable of flight and designed to detachably connect to an aircraft. According to some embodiments, detachable capsules may be designed to carry cargo and/or passengers. According to some embodiments, detachable capsules may, after detachment, be piloted by pilots or by automated systems (unmanned) or a combination of the two.

8. 发明公开

EP3263445A1 AIRCRAFT WITH SELECTIVELY ATTACHABLE PASSENGER POD ASSEMBLY 有权
标题翻译：具有可选的客运POD组件的飞机
公开(公告)号：EP3263445A1
公开(公告)日：2018-01-03
申请号：EP16185727.1
申请日：2016-08-25
申请人： Bell Helicopter Textron Inc.
发明人： McCULLOUGH, John Richard , OLDROYD, Paul K.
IPC分类号： B64C1/28 , B64C17/02 , B64C29/02 , B64C39/02 , B64C27/26 , B64C27/28 , B64D25/12 , B64C1/32 , B64C27/30 , B64D17/80
CPC分类号： B64C29/0033 , B64C1/28 , B64C1/32 , B64C11/28 , B64C17/02 , B64C27/26 , B64C27/28 , B64C27/30 , B64C29/02 , B64C39/024 , B64C39/08 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/128 , B64C2201/185 , B64C2211/00 , B64D17/80 , B64D25/12 , G08G5/0065 , G08G5/0069 , G08G5/025
摘要： In some embodiments, an aircraft (10) includes a flying frame (12) having an airframe (26), a propulsion system (34) attached to the airframe (26) and a flight control system (68) operably associated with the propulsion system (34) wherein, the flying frame (12) has a vertical takeoff and landing mode and a forward flight mode. A pod assembly (70) is selectively attachable to the flying frame (12) such that the flying frame (12) is rotatable about the pod assembly (70) wherein, the pod assembly (70) remains in a generally horizontal attitude during vertical takeoff and landing, forward flight and transitions therebetween.
摘要翻译：在一些实施例中，飞行器（10）包括具有机身（26）的飞行框架（12），连接到机身（26）的推进系统（34）和可操作地与推进系统（34），其中，所述飞行框架（12）具有垂直起飞和着陆模式以及前进飞行模式。荚组件（70）可选择性地连接到飞行框架（12），使得飞行框架（12）可围绕荚组件（70）旋转，其中荚组件（70）在垂直起飞期间保持大致水平的姿态和着陆，向前飞行和其间的过渡。

9. 发明公开

EP1928733A4 AIRCRAFT SAFETY SYSTEM 审中-公开
标题翻译：飞机的安全系统
公开(公告)号：EP1928733A4
公开(公告)日：2012-09-12
申请号：EP06774876
申请日：2006-08-28
申请人： GLOBAL WELL CORP LTD
发明人： BERTANI ROMOLO LORENZO
IPC分类号： B64C1/32 , B64C3/10 , B64D25/12
CPC分类号： B64D25/12 , B64C3/10 , Y02T50/12

10. 发明公开

EP2147861A1 RECOVERY AND RESCUE SYSTEM FOR AIRCRAFT 审中-公开
标题翻译： BERGUNGS- UND RETTUNGSSYSTEMFÜRFLUGZEUGE
公开(公告)号：EP2147861A1
公开(公告)日：2010-01-27
申请号：EP07866344.0
申请日：2007-12-05
申请人： Garcia Barrientos, Francisco Javier
发明人： Garcia Barrientos, Francisco Javier
IPC分类号： B64D17/72 , B64D17/76 , B64D17/80
CPC分类号： B64D17/72 , B64D17/76 , B64D17/80 , B64D25/00 , B64D25/12
摘要： The recovery and rescue system includes a sail (5) with rigging (10) fitted around a spreader conduit (4), with an intake and outlet nozzle, wherein a starting system (6) is provided, including mechanical (12-13) and electromechanical (17-18) opening mechanisms, in the first case operated by a manual lever (16) and in the second case operated by a button (19). Air driven through the intake of the spreading conduit (4) activates the starting system (6) in order to spread the sail (5) and by parachute means retain or brake the aircraft wherein the said system assembly is fitted. Said system can be housed inside the aircraft in a container provided for the purpose.
摘要翻译：回收和救援系统包括具有安装在吊具导管（4）周围的索具（10）的帆（5），具有进出口喷嘴，其中提供起动系统（6），其包括机械（12-13）和机电（17-18）打开机构，在第一种情况下由手动杆（16）操作，第二种情况由按钮（19）操作。通过吸入扩散管道（4）驱动的空气激活启动系统（6）以扩展帆（5），并且降落伞装置保持或制动其中安装有所述系统组件的飞行器。所述系统可以被安装在飞机内设置的容器中。

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