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1. 发明授权

EP3740426B1 SHOCK ABSORBER CONFIGURED WITH A DEFORMABLE ENERGY ABSORBING MEMBER 有权
公开(公告)号：EP3740426B1
公开(公告)日：2024-08-07
申请号：EP19741293.5
申请日：2019-01-17
IPC分类号： B64C1/14 , F16F7/12 , F16F9/00 , F16F9/16 , F16F9/48 , F16F9/58 , E05F3/00
CPC分类号： E05F5/10 , E05Y2900/50220130101 , E05Y2201/21220130101 , E05Y2900/53120130101 , E05B77/54 , B64C1/1469 , B64D45/00 , B64C2001/00920130101 , F16F9/48 , F16F9/19 , F16F9/0218

2. 发明公开

EP4406829A1 AIRCRAFT SECTION AND AIRCRAFT HAVING A MONUMENT WITH TWO LAVATORIES 审中-公开
公开(公告)号：EP4406829A1
公开(公告)日：2024-07-31
申请号：EP24154440.2
申请日：2024-01-29
申请人： Airbus Operations GmbH
发明人： Meyer, Michael , Canton, Thomas
IPC分类号： B64C1/14 , B64D11/02 , B64D45/00
CPC分类号： B64D11/02 , B64C1/1469 , B64D45/0026
摘要： The present disclosure relates to an aircraft section (100) arranged between a cockpit (5) and a cabin area (2) of an aircraft (1). The aircraft section comprises a cockpit aisle (120) configured to allow access to the cockpit (5) from the cabin area (2), and a monument extending in a longitudinal direction and a transverse direction of the aircraft (1). The monument includes a first lavatory (110), a second lavatory (150) arranged adjacent to the first lavatory (110) in the transverse direction and comprising the cockpit aisle (120), a first separation wall (132) separating the first lavatory (110) from the second lavatory (150), a first boundary wall (133) delimiting the first lavatory (110) and a first portion of a rear wall of the cockpit (5), and a second boundary wall (142) delimiting the second lavatory (150) and a second portion of a rear wall of the cockpit (5). The second boundary wall (142) is parallel to the first boundary wall (133) what forms a continuous wall with the first boundary wall (133). The monument further includes an outer door (161) movable between an open position, where the cockpit aisle (120) is accessible from the cabin area (2), and a closed position, where the cockpit aisle (120) is blocked with respect to the cabin area (2).

3. 发明授权

EP3133013B1 FLIGHT DECK DOOR ASSEMBLY 失效
公开(公告)号：EP3133013B1
公开(公告)日：2018-06-06
申请号：EP15181845.7
申请日：2015-08-20
申请人： Airbus Operations GmbH
发明人： Bredemeier, Kai , Koch, Maik
IPC分类号： B64C1/14
CPC分类号： B64C1/1469 , B64D11/02
摘要： A flight deck door assembly (10) for an aircraft includes a flight deck bulkhead (9a, 9b) defining an access opening from a passenger deck area (PD) to a flight deck area (FD) of the aircraft, a lavatory bulkhead (9c) spaced apart from the flight deck bulkhead (9a, 9b) and defining a lavatory monument (2), a first lock containment (4a) arranged in a first portion (9a) of the flight deck bulkhead opposite to a door jamb (6) formed by a second portion of the flight deck bulkhead, a second lock containment (4b) arranged in the lavatory bulkhead (9c), and a flight deck door (5) having a door blade (5c) hingedly coupled to the door jamb (6). The flight deck door (5) is configured to latch to the first lock containment (4a) in a first closing position (C1) and to latch to the second lock containment (4b) in a second closing position (C2).

4. 发明公开

EP3130533A1 FLIGHT DECK DOOR SURVEILLANCE AND LOCK CONTROL 有权
标题翻译：飞行甲板门监控和锁定控制
公开(公告)号：EP3130533A1
公开(公告)日：2017-02-15
申请号：EP16183763.8
申请日：2016-08-11
申请人： Rosemount Aerospace Inc.
发明人： FLECK, Travis W. , LEPPERT, Adam
IPC分类号： B64C1/14 , B64D45/00 , G07C9/00
CPC分类号： B64D45/0015 , B64C1/1469 , B64D2045/0035 , G07C9/00563
摘要： In one example, a method includes capturing, by a camera system including at least one camera device positioned within an aircraft, image data of an interior of the aircraft. The method further includes determining, by a processing device positioned within the aircraft, that one or more alert criteria are satisfied, and outputting, in response to determining that the one or more alert criteria are satisfied, at least a portion of the captured image for transmission to a ground-based computing device via a wireless communications network. The method further includes receiving, from the ground-based computing device, a lock override command configured to cause the processing device to unlock an electronically-controlled door lock of a flight deck door of the aircraft, and responsively unlocking the electronically-controlled door lock of the flight deck door.
摘要翻译：在一个示例中，一种方法包括通过包括位于飞机内的至少一个相机装置的相机系统捕捉飞机内部的图像数据。该方法还包括由位于飞机内的处理设备确定满足一个或多个警报标准，并且响应于确定满足一个或多个警报标准，输出至少一部分捕获图像用于通过无线通信网络传输到地面计算设备。该方法还包括从地面计算设备接收锁定超控命令，该锁定超控命令被配置为使处理设备解锁飞机的驾驶舱门的电子控制门锁，并且响应地解锁电子控制门锁的飞行甲板门。

5. 发明授权

EP2574551B1 Poste de pilotage d'un aéronef comportant un strapontin 有权
标题翻译：飞机驾驶舱有隆隆的座位
公开(公告)号：EP2574551B1
公开(公告)日：2016-08-31
申请号：EP12186328.6
申请日：2012-09-27
申请人： Airbus Operations
发明人： Guering, Bernard
IPC分类号： B64D11/06 , B64D45/00
CPC分类号： B64D11/0689 , B64C1/1469 , B64D11/06 , B64D11/0606 , B64D11/064 , B64D11/0691 , B64D45/0015

6. 发明授权

EP2668093B1 DOOR ASSEMBLY WITH TWO DOOR LEAVES 有权
标题翻译：带双门翼门体
公开(公告)号：EP2668093B1
公开(公告)日：2016-06-29
申请号：EP12700278.0
申请日：2012-01-11
申请人： Airbus Operations GmbH
发明人： KOCH, Maik , BREUER, Matthias
IPC分类号： B64C1/14
CPC分类号： B64C1/1469 , B64C2001/009 , E04G5/003 , E05B65/1026 , E05C7/02 , E05F1/10 , E05F15/611 , E05F15/72 , E05F17/002 , E05G5/003 , E05Y2900/502 , E06B3/2605

7. 发明公开

EP2668093A1 DOOR ASSEMBLY WITH TWO DOOR LEAVES 有权
标题翻译：带双门翼门体
公开(公告)号：EP2668093A1
公开(公告)日：2013-12-04
申请号：EP12700278.0
申请日：2012-01-11
申请人： Airbus Operations GmbH
发明人： KOCH, Maik , BREUER, Matthias
IPC分类号： B64C1/14 , B64D45/00 , E06B9/04 , E06B3/36
CPC分类号： B64C1/1469 , B64C2001/009 , E04G5/003 , E05B65/1026 , E05C7/02 , E05F1/10 , E05F15/611 , E05F15/72 , E05F17/002 , E05G5/003 , E05Y2900/502 , E06B3/2605
摘要： A door assembly for a vehicle with two door leaves is stated. In each case the door leaves can be opened in such a manner that the maximum angle of opening between them can be limited. After a door leaf has been opened, the door leaves can thus only be pivoted together so that opening the first door leaf results in closing the second door leaf. As a result of this, access to a space in a vehicle may be controlled.

8. 发明授权

EP1921006B1 Latch device for cockpit door of an aircraft 有权
标题翻译：用于舱门到飞行器的驾驶舱的锁定装置
公开(公告)号：EP1921006B1
公开(公告)日：2013-07-17
申请号：EP07405290.3
申请日：2007-09-28
申请人： JAMCO CORPORATION
发明人： Saku, Fumiaki c/o Jamco Corp. , Watanabe, Tadashi c/o Jamco Corp. , Sekikawa, Yasuo c/o Jamco Corp.
IPC分类号： B64C1/14 , B64D45/00 , E05B51/02
CPC分类号： B64C1/1469 , B64C2001/009 , B64D45/0015 , E05B51/023

9. 发明公开

EP2496476A2 PARTIE AVANT D'UN AERONEF COMPORTANT UN SAS D'ACCES AU COCKPIT. 有权
标题翻译：带安全锁驾驶舱飞机座舱
公开(公告)号：EP2496476A2
公开(公告)日：2012-09-12
申请号：EP10795423.2
申请日：2010-11-05
申请人： Airbus
发明人： PUJOL, Olivier , LALANDE, Sébastien
IPC分类号： B64D45/00 , B64C1/14
CPC分类号： B64D45/0015 , B64C1/1469 , B64D2045/002
摘要： The invention relates to a front section (1) of the fuselage of an aircraft comprising secure access between the cockpit (2) and the passenger cabin (3) while being compact. For this purpose, the front section (1) comprises a separation means (9) including at least one mobile element (10) suitable for being slid between an extended closing position in which said separation means (9) defines, together with the door of the cockpit (5), a transition area (7) between the cockpit (2) and the passenger cabin (3), preventing persons from crossing between the passenger cabin (3) and said transition area (7); and a retracted open position in which said separation means (9) allows persons to cross between the passenger cabin (3) and said transition area (7).

10. 发明公开

EP1921006A3 Latch device of cockpit door of an aircraft 有权
标题翻译：锁定设备舱门到飞机的驾驶舱
公开(公告)号：EP1921006A3
公开(公告)日：2012-03-07
申请号：EP07405290.3
申请日：2007-09-28
申请人： JAMCO CORPORATION
发明人： Saku, Fumiaki c/o Jamco Corp. , Watanabe, Tadashi c/o Jamco Corp. , Sekikawa, Yasuo c/o Jamco Corp.
IPC分类号： B64C1/14 , B64D45/00 , E05B51/02
CPC分类号： B64C1/1469 , B64C2001/009 , B64D45/0015 , E05B51/023
摘要： A latch device for detecting pressure reduction of a cockpit in an aircraft and releasing a bolt and a stopper device are provided so as to prevent a cockpit door from unexpectedly opening by an impact. A main latch device 100 of the cockpit door has a frame 112 fixed to a door panel, and a latch base 120 is mounted to the frame 112 capable of pivotal rotation with a pin 122 as a fulcrum. A bolt 132 is inserted into a catch in conjunction with a door handle 130. A holding/releasing portion 150 holds the latch base 120. When a pressure difference occurs between a cockpit 4 and a cabin 5, a pressure-sensing piston 160 is pushed in, a trigger 170 and a flapper 180 are rotated and the latch base 120 is released. A stopper device 190 regulates movement of the trigger 170 by movement of an inertial piston 192 when an impact force is applied from the cabin 5 side.

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