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1. 发明授权

EP2112065B1 Verfahren zur Rettung eines bemannten oder unbemannten Fluggeräts, insbesondere einer Drohne 有权转让
标题翻译：一种用于载人或无人飞机的救援过程中，尤其是无人驾驶飞机
公开(公告)号：EP2112065B1
公开(公告)日：2014-06-18
申请号：EP09001353.3
申请日：2009-01-30
申请人： Cassidian Airborne Solutions GmbH
发明人： Martinkat, Norbert
IPC分类号： B64C39/02 , B64D25/12 , B64D45/04 , B64D17/80 , B64D25/00
CPC分类号： B64C39/024 , B64C2201/141 , B64C2201/185 , B64D17/80 , B64D25/00 , G05D1/0055

2. 发明公开

EP2305560A2 Device for opening a passenger door in case of emergency 有权转让
标题翻译： Vorrichtung zumÖffneneinerPassagiertürim Notfall
公开(公告)号：EP2305560A2
公开(公告)日：2011-04-06
申请号：EP11000043.7
申请日：2009-03-02
申请人： Eurocopter Deutschland GmbH
发明人： Andres, Stefan , Bartosch, Hans , Buchs, Wolfgang , Held, Manfred , Hertle, Rainer
IPC分类号： B64C1/14 , B64C1/32 , B64D25/00 , B64D25/12 , E05B51/02 , F42B3/00
CPC分类号： B64C1/1407 , E05F15/53 , E05F15/54 , E05F15/63 , E05F15/72 , E05Y2201/422 , E05Y2201/434 , E05Y2201/72 , E05Y2800/252 , E05Y2800/67 , E05Y2900/502 , E05Y2900/531 , F42B3/006 , F42B3/04
摘要： The invention relates to a device for opening a passenger door (1) of an aircraft in case of emergency, which is fastened so it is manually pivotable on the fuselage (3) of the aircraft via a hinge and/or support arm configuration (2), an auxiliary-energy-operated emergency opening drive (4) being provided between the fuselage (3) and the passenger door (1), which automatically opens the passenger door (1) in accordance with an emergency control unit (5), the auxiliary energy for the emergency opening drive (4) being pyrotechnic energy, whose gas expanding inside an expansion chamber (6) after triggering by the emergency control unit (5) impinges the emergency opening drive (4) with pressure medium to open the passenger door (1). The emergency opening drive (4") comprises a turbine (13) for generating a rotational movement from the pyrotechnic energy, which works together with a downstream reduction gear (14) to open the passenger door (1).
摘要翻译：本发明涉及一种用于在紧急情况下打开飞机的乘客门（1）的装置，其被紧固，使得其可以通过铰链和/或支撑臂构造（2）手动地枢转在飞行器的机身（3）上），在机身（3）和乘客门（1）之间设置有辅助能量操作的应急开启驱动器（4），其根据应急控制单元（5）自动打开乘客门（1）用于紧急打开驱动器（4）的辅助能量是烟火能量，其在由应急控制单元（5）触发之后在膨胀室（6）内膨胀的气体用压力介质撞击紧急打开驱动器（4）以打开乘客门（1）。紧急打开驱动器（4“）包括用于从烟火能量产生旋转运动的涡轮机（13），其与下游减速齿轮（14）一起工作以打开乘客门（1）。

3. 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。

4. 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

5. 发明授权

EP3263445B1 AIRCRAFT WITH SELECTIVELY ATTACHABLE PASSENGER POD ASSEMBLY 有权
公开(公告)号：EP3263445B1
公开(公告)日：2018-10-17
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.

6. 发明公开

EP2570348A1 Support unit to connect a ballistic parachute to a helicopter 审中-公开
标题翻译： Befestigungfüreinen ballistischen Rettungsfallschirm a einem Helikopter
公开(公告)号：EP2570348A1
公开(公告)日：2013-03-20
申请号：EP11425237.2
申请日：2011-09-19
申请人： Marega Piergiovanni
发明人： Marega Piergiovanni
IPC分类号： B64D25/12 , B64C27/00
CPC分类号： B64D25/12 , B64C27/006 , B64C27/04
摘要： A ballistic parachute (11) is carried by a support unit (12), which has a tube (13) with an intermediate portion (19) arranged coaxially inside the rotor shaft of a helicopter (2); the tube (13) is secured at its lower end to a fixed structure (15) of the helicopter (1) and, at its upper end (25), supports a plate defining a lower base for the parachute (11); the parachute (11) is enclosed above by a dome (28), which can be removed by activating an ejection system via a control cable (45) that passes axially through the tube (13); the cables of the parachute (11) are connected to a fastening body (35), which is fitted on the upper end (25) of the tube (13), is arranged above the plate (27) and can axially rotate with respect to the tube (13).
摘要翻译：弹道降落伞（11）由支撑单元（12）承载，该支撑单元具有在直升机（2）的转子轴内同轴布置的中间部分（19）的管（13）; 管（13）的下端固定在直升机（1）的固定结构（15）上，并且在其上端（25）处支撑限定用于降落伞（11）的下基座的板; 降落伞（11）由圆顶（28）封闭，其可以通过轴向穿过管（13）的控制缆索（45）启动排出系统而被移除。降落伞（11）的电缆连接到安装在管（13）的上端（25）上的紧固体（35），布置在板（27）的上方，并可相对于管（13）。

7. 发明授权

EP2252505B1 DEVICE FOR OPENING A PASSENGER DOOR IN CASE OF EMERGENCY 失效转让
标题翻译：用于开启乘客门紧急情况下
公开(公告)号：EP2252505B1
公开(公告)日：2012-12-05
申请号：EP09721985.1
申请日：2009-03-02
申请人： Eurocopter Deutschland GmbH
发明人： ANDRES, Stefan , BARTOSCH, Hans , BUCHS, Wolfgang , HELD, Manfred , HERTIE, Rainer
IPC分类号： B64C1/14 , B64C1/32 , B64D25/00 , B64D25/12 , E05B51/02 , F42B3/00
CPC分类号： B64C1/1407 , E05F15/53 , E05F15/54 , E05F15/63 , E05F15/72 , E05Y2201/422 , E05Y2201/434 , E05Y2201/72 , E05Y2800/252 , E05Y2800/67 , E05Y2900/502 , E05Y2900/531 , F42B3/006 , F42B3/04

8. 发明公开

EP1747990A3 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：EP1747990A3
公开(公告)日：2007-11-21
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
摘要： Fluggerät mit einem Rettungslandesystem, welches einen Gleitschirm für die Rettungslandephase des Fluggeräts (20) umfasst und einen Fluglagepositionierungsschirm (6) zum Abbremsen und nachfolgenden Verschwenken (Schwenkrichtung 8) des Fluggeräts bezogen auf die Flugrichtung, so dass die Hochachse (H) im wesentlichen der Zugrichtung des Fluglagepositionierungsschirmes (6) entspricht.

9. 发明授权

EP1280699B1 AN AIRCRAFT WITH A DETACHABLE PASSENGER ESCAPE CABIN AND AN AIRCRAFT WITH AIRBAGS 有权
标题翻译：与乘客释放地固定救生舱里的平面和安全气囊某型飞机
公开(公告)号：EP1280699B1
公开(公告)日：2003-11-05
申请号：EP00976197.4
申请日：2000-11-23
申请人： Giannakopoulos, Pavlos
发明人： Giannakopoulos, Pavlos
IPC分类号： B64C1/32 , B64D25/12 , B64D17/80
CPC分类号： B64D25/12 , B64D17/80 , B64D2201/00 , Y10S70/06 , Y10T70/7051
摘要： An aircraft with a detachable cabin (1) that serves to rescue its passengers as a result of the aircraft's sudden fall either due to its malfunction or fire. The cabin escapes either smoothly or by means of fast ejection and descends slowly to the Earth with the aid of a parachute (13; 14); during a crash on the ground or in the sea external airbags (38a-38f) with which it is equipped and which are located in its lower part are inflated thus absorbing the loads that are developed during the crash. In addition a conventional aircraft (70) of the type being already in use is also described and in which the parachute equipment (71) has already been applied; however, the proposed equipment of the airbag boxes (72a-72c) is adapted to it for the absorption of the energy produced due to its crash on Earth in case of its sudden fall.

10. 发明公开

EP1280699A1 AN AIRCRAFT WITH A DETACHABLE PASSENGER ESCAPE CABIN AND AN AIRCRAFT WITH AIRBAGS 有权
标题翻译：与乘客释放地固定救生舱里的平面和安全气囊某型飞机
公开(公告)号：EP1280699A1
公开(公告)日：2003-02-05
申请号：EP00976197.4
申请日：2000-11-23
申请人： Giannakopoulos, Pavlos
发明人： Giannakopoulos, Pavlos
IPC分类号： B64C1/32 , B64D25/12 , B64D17/80
CPC分类号： B64D25/12 , B64D17/80 , B64D2201/00 , Y10S70/06 , Y10T70/7051
摘要： An aircraft with a detachable cabin (1) that serves to rescue its passengers as a result of the aircraft's sudden fall either due to its malfunction or fire. The cabin escapes either smoothly or by means of fast ejection and descends slowly to the Earth with the aid of a parachute (13; 14); during a crash on the ground or in the sea external airbags (38a-38f) with which it is equipped and which are located in its lower part are inflated thus absorbing the loads that are developed during the crash. In addition a conventional aircraft (70) of the type being already in use is also described and in which the parachute equipment (71) has already been applied; however, the proposed equipment of the airbag boxes (72a-72c) is adapted to it for the absorption of the energy produced due to its crash on Earth in case of its sudden fall.

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