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1. 发明公开

EP4311762A1 AN AIRCRAFT DOOR WITH AN ANTI-VIBRATION DEVICE 审中-实审
公开(公告)号：EP4311762A1
公开(公告)日：2024-01-31
申请号：EP22400007.5
申请日：2022-07-29
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH , AIRBUS HELICOPTERS
发明人： Vayssiere, Aurélien , Arnoult, Pierre , Fruitet, Pierre , Facompre, Alexandre
IPC分类号： B64C1/14 , E05B77/36 , E05B83/42 , B64C27/00 , F16F7/104
摘要： The invention relates to an aircraft door (7) with an inner door space (7d); a door opening system (8) arranged at least partly in the inner door space, comprising: at least one locking device (8c) for locking the aircraft door in a locked state, actuation kinematics (8b) for actuating the at least one locking device, and at least one transmission rod (8d) coupling the actuation kinematics with the at least one locking device; wherein the at least one transmission rod is displaceable in the inner door space by means of the actuation kinematics for actuating the at least one locking device; and an anti-vibration device (9) mounted in the inner door space to the at least one transmission rod for absorbing vibrations of the at least one transmission rod, wherein the anti-vibration device is displaceable in the inner door space together with the at least one transmission rod.

2. 发明公开

EP3095590A1 A CARBON FIBER REINFORCED POLYMER PANEL ARRANGEMENT 有权
标题翻译： KOHLENSTOFFFASERVERSTÄRKTEPOLYMERPLATTENANORDNUNG
公开(公告)号：EP3095590A1
公开(公告)日：2016-11-23
申请号：EP15400019.4
申请日：2015-05-18
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Vayssiere, Aurélien , Joussellin, Fabrice , Bittmann, Konrad
IPC分类号： B29C65/56 , B29C65/76 , B29C70/72 , B64C1/14 , B29K63/00 , B29K105/08 , B29K307/04
CPC分类号： B29C65/56 , B29C65/76 , B29C66/1142 , B29C66/2276 , B29C66/43 , B29C66/543 , B29C66/71 , B29C66/7212 , B29C66/73941 , B29C70/78 , B29K2105/0809 , B29L2005/00 , B29L2031/3082 , B29L2031/3088 , B64C1/1446 , B64C1/32 , Y02T50/43 , B29K2307/04 , B29K2063/00
摘要： The invention relates to a carbon fiber reinforced polymer panel arrangement (9) comprising at least one carbon fiber reinforced polymer panel (9b) that is provided with interlocking elements (12a, 12b) associated with a zip fastener (8a, 8b), said interlocking elements (12a, 12b) being rigidly attached to an associated interlocking element tape (14a, 14b), said associated interlocking element tape (14a, 14b) being sewed to said at least one carbon fiber reinforced polymer panel (9b). The invention relates further to a vehicle comprising such a carbon fiber reinforced polymer panel arrangement and to a method of manufacturing such a carbon fiber reinforced polymer panel arrangement.
摘要翻译：本发明涉及一种碳纤维增强聚合物面板装置（9），其包括至少一个碳纤维增强聚合物面板（9b），其具有与拉链（8a，8b）相关联的互锁元件（12a，12b），所述互锁元件（12a，12b）刚性地连接到相关联的互锁元件带（14a，14b）上，所述相关联的互锁元件带（14a，14b）被缝合到所述至少一个碳纤维增强聚合物面板（9b）上。本发明进一步涉及包含这种碳纤维增强聚合物面板装置的车辆和制造这种碳纤维增强聚合物面板装置的方法。

3. 发明公开

EP4071046A1 A ROTARY WING AIRCRAFT WITH A FIREWALL ARRANGEMENT 有权
公开(公告)号：EP4071046A1
公开(公告)日：2022-10-12
申请号：EP21400008.5
申请日：2021-04-09
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Vayssiere, Aurélien , Neukirch, Hubert , Kammerer, Markus , Rein, Bernhard
IPC分类号： B64C1/10 , B64C27/04 , B64D29/04 , B64C1/40 , F16J3/04
摘要： The invention relates to a rotary wing aircraft with a fuselage that forms an aircraft interior region, the fuselage comprising an upper primary skin that separates the aircraft interior region from an aircraft upper deck arranged above the fuselage, wherein the aircraft upper deck comprises an engine accommodating region with a firewall arrangement 10, the engine accommodating region accommodating at least one aircraft engine 11 within the firewall arrangement 10, wherein the firewall arrangement 10 comprises at least one gasket 10g for tightening pass-through of a torque tube 15 that connects the at least one aircraft engine 11 to a main gear box 17 of the rotary wing aircraft, and wherein the at least one gasket 10g comprises at least two fire proof shells 12b and a ringshaped flexible fire proof bellows 13.

4. 发明公开

EP4269254A1 A GROUND SUPPORT EQUIPMENT SYSTEM FOR USE ON AN AIRCRAFT 审中-实审
公开(公告)号：EP4269254A1
公开(公告)日：2023-11-01
申请号：EP22400002.6
申请日：2022-04-28
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH , Airbus Helicopters
发明人： Vayssiere, Aurélien , Schneele, Tobias , Fruitet, Pierre , Untiedt, Martin , Goettling, Susanne , Schindler, Armin , Vazquez-Gonzalez, Ainhoa
IPC分类号： B64D45/00 , B64F1/00
摘要： The present embodiments relate to a ground support equipment system (150) for use on an aircraft (100), comprising: a plurality of ground support equipment modules (192, 194) mountable to associated aircraft components (193, 195) of an aircraft (100) parked on ground (105) for protecting the associated aircraft components (193, 195) from environmental conditions, in particular rain, wind, snow, frost, sand, and/or salt conditions; and a plurality of connecting means (200) adapted to connect the plurality of ground support equipment modules (192, 194) to at least one common interconnection device (212) for rendering mounting of the plurality of ground support equipment modules (192, 194) to the associated aircraft components (193, 195) discernible for a pilot of the aircraft (100).

5. 发明公开

EP3854679A1 A VEHICLE WITH AT LEAST ONE EMERGENCY EXIT SYSTEM 有权
公开(公告)号：EP3854679A1
公开(公告)日：2021-07-28
申请号：EP20315009.9
申请日：2020-01-24
申请人： AIRBUS HELICOPTERS , AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Vayssiere, Aurélien , Rein, Bernhard , Lässig, Sven , Neukirch, Hubert , Fruitet, Pierre
IPC分类号： B64C1/14 , B64C1/32 , B64C27/04 , B64D25/08
摘要： The invention relates to a vehicle with at least one emergency exit system 5c, the at least one emergency exit system 5c comprising a jettisonable component 2i that is accommodated and locked in an associated frame structure 2l of the vehicle in normal operation mode and releasable from the associated frame structure 2l for being jettisoned from the vehicle in an emergency mode; and further comprising an emergency evacuation assistance device 9 that is adapted to assist in an emergency evacuation of the vehicle via the associated frame structure 2l in the emergency mode; wherein the emergency evacuation assistance device 9 is attached to the jettisonable component 2i such that the emergency evacuation assistance device 9 is deployed by means of the jettisonable component 2i when the jettisonable component 2i is jettisoned from the vehicle in the emergency mode.

6. 发明授权

EP3061685B1 A SLIDING CLOSING ELEMENT, IN PARTICULAR A SLIDING DOOR OR A SLIDING WINDOW, FOR A SLIDING CLOSING ELEMENT ARRANGEMENT OF A VEHICLE, IN PARTICULAR OF AN AIRCRAFT 有权
标题翻译：滑盖元素，特别是滑动滑动WINDOWS下，车辆的滑动闭锁元件组件，尤其是飞机
公开(公告)号：EP3061685B1
公开(公告)日：2017-01-04
申请号：EP15400009.5
申请日：2015-02-24
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Joussellin, Fabrice , Vayssiere, Aurélien
IPC分类号： B64C1/14
CPC分类号： E05D15/0621 , B64C1/1438 , E05D13/006 , E05D15/0643 , E05D15/0678 , E05D15/1047 , E05D15/28 , E05D2015/1057 , E05Y2201/64 , E05Y2900/502 , E06B3/46
摘要： The invention relates to a sliding closing element (5) for a sliding closing element arrangement of a vehicle, said sliding closing element arrangement comprising at least one rail (2a) that is adapted for slidably supporting said sliding closing element (5), said sliding closing element (5) comprising at least one fail safe sliding arm assembly (6) with at least one bogie support arm (7) and at least one safety arm (8), said at least one bogie support arm (7) comprising at least one bogie assembly (9) with at least one guide roller that is adapted for rolling along said at least one rail (2a) in operation, and said at least one safety arm (8) being adapted for retaining said at least one fail safe sliding arm assembly (6) on said at least one rail (2a) in case of a failure of said at least one bogie support arm (7).
摘要翻译：本发明涉及的滑动关闭元件（5）一种用于车辆的滑动关闭元件布置，所述滑动闭元件布置包括至少一个轨道（2a）中并是angepasst用于可滑动地支承所述滑动封闭元件（5），所述滑动闭合元件（5）包括至少一个故障安全与至少一个转向架支撑臂（7）和至少一个安全臂（8），所述至少一个转向架支撑臂（7）至少包括：滑动臂组件（6）一个转向架组件（9）具有至少一个导向辊没被angepasst用于在外科手术中沿着所述至少一个轨（2a）的滚动，且所述至少一个安全臂（8）的angepasst用于保持所述至少一个故障安全滑动臂组件（6）上的至少一个所述导轨（2a）中在至少一个转向架的故障的情况下臂所述支承件（7）。

7. 发明公开

EP3100947A1 A JETTISONABLE EMERGENCY EXIT FOR A VEHICLE 有权
标题翻译：阿布扎比诺富特FÜREIN FAHRZEUG
公开(公告)号：EP3100947A1
公开(公告)日：2016-12-07
申请号：EP15400023.6
申请日：2015-06-05
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH , Airbus Helicopters
发明人： Joussellin, Fabrice , Vayssiere, Aurélien , Fruitet, Pierre , Mathieu, Laure-Anne , Heboub, Hassène , Benentendi, Philippe
IPC分类号： B64C1/14
CPC分类号： B64C27/04 , B64C1/1492
摘要： The invention relates.to a jettisonable emergency exit (5c) for a vehicle, comprising an outer peripheral edge (2n) that is adapted to be accommodated in an associated frame provided in a vehicle, wherein at least one emergency exit retention means (9) and at least one emergency exit locking device (10, 11) are integrated into said outer peripheral edge (2n), said at least one emergency exit retention means (9) comprising at least one non-retractable pivot finger around which said jettisonable emergency exit (5c) is rotatable in an emergency mode, and said at least one emergency exit locking device (10, 11) comprising at least one locking hook that is adapted for locking said jettisonable emergency exit (5c) in an associated locking position in normal operation mode and for releasing said jettisonable emergency exit (5c) in an associated retracted position in said emergency mode.
摘要翻译：本发明涉及一种用于车辆的可抛弃紧急出口（5c），包括适于容纳在设置在车辆中的相关联的框架中的外周缘（2n），其中至少一个紧急出口保持装置（9）并且至少一个紧急出口锁定装置（10,11）集成到所述外周边缘（2n）中，所述至少一个紧急出口保持装置（9）包括至少一个不可伸缩的枢轴指，所述可坠毁的紧急出口（5c）可在紧急模式下旋转，并且所述至少一个紧急出口锁定装置（10,11）包括至少一个锁定钩，其适于在正常操作中将所述可坠毁的紧急出口（5c）锁定在相关联的锁定位置并且用于在所述紧急模式下将所述可坠毁的紧急出口（5c）释放在相关联的缩回位置。

8. 发明公开

EP4299436A1 A DOOR LOCKING ASSEMBLY FOR AN AIRCRAFT 审中-实审
公开(公告)号：EP4299436A1
公开(公告)日：2024-01-03
申请号：EP22400005.9
申请日：2022-06-30
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH , Airbus Helicopters
发明人： Vayssiere, Aurélien , Renard, Aurélien , Fruitet, Pierre , Rein, Bernhard
IPC分类号： B64C1/14
摘要： The invention relates to a door locking assembly (6) for locking a door (4) of an aircraft, comprising a locking hook (6a) adapted for blocking in a locking position a lockable arm (4e) of a door (4) of an aircraft; a release lever (6i) connected to the locking hook (6a) for moving the locking hook (6a) from a releasing position into the locking position in response to being actuated by a lockable arm (4e) of a door (4) of an aircraft; an operating handle (6d) connected at least to the release lever (6i) and rotatable for moving the locking hook (6a) from the locking position to the releasing position; and a locking indicator (6b) connected to the locking hook (6a) for indicating positioning of the locking hook (6a) in one of the locking position or the releasing position.

9. 发明授权

EP3095590B1 A CARBON FIBER REINFORCED POLYMER PANEL ARRANGEMENT AND METHOD 有权
公开(公告)号：EP3095590B1
公开(公告)日：2019-10-02
申请号：EP15400019.4
申请日：2015-05-18
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Vayssiere, Aurélien , Joussellin, Fabrice , Bittmann, Konrad
IPC分类号： B29C65/56 , B29C65/76 , B29C70/72 , B64C1/14 , B29K63/00 , B29K105/08 , B29K307/04

10. 发明公开

EP3061685A1 A sliding closing element, in particular a sliding door or a sliding window, for a sliding closing element arrangement of a vehicle, in particular of an aircraft 有权
标题翻译：滑盖元素，特别是滑动滑动WINDOWS下，车辆的滑动闭锁元件组件，尤其是飞机
公开(公告)号：EP3061685A1
公开(公告)日：2016-08-31
申请号：EP15400009.5
申请日：2015-02-24
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH
发明人： Joussellin, Fabrice , Vayssiere, Aurélien
IPC分类号： B64C1/14
CPC分类号： E05D15/0621 , B64C1/1438 , E05D13/006 , E05D15/0643 , E05D15/0678 , E05D15/1047 , E05D15/28 , E05D2015/1057 , E05Y2201/64 , E05Y2900/502 , E06B3/46
摘要： The invention relates to a sliding closing element (5) for a sliding closing element arrangement of a vehicle, said sliding closing element arrangement comprising at least one rail (2a) that is adapted for slidably supporting said sliding closing element (5), said sliding closing element (5) comprising at least one fail safe sliding arm assembly (6) with at least one bogie support arm (7) and at least one safety arm (8), said at least one bogie support arm (7) comprising at least one bogie assembly (9) with at least one guide roller that is adapted for rolling along said at least one rail (2a) in operation, and said at least one safety arm (8) being adapted for retaining said at least one fail safe sliding arm assembly (6) on said at least one rail (2a) in case of a failure of said at least one bogie support arm (7).

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