公开(公告)号：US10733858B2

公开(公告)日：2020-08-04

申请号：US15521958

申请日：2015-10-22

申请人： LATECOERE

发明人： Boucourt Gerard

IPC分类号： B64D45/00 ,  G08B13/196 ,  H04N5/232 ,  H04N5/33 ,  H04N5/77 ,  H04N7/18 ,  H04N21/214 ,  H04N21/218 ,  H04N21/414

摘要： The monitoring and security of at least one enclosure, allowing a constant and complete view of the enclosure, and a modulated assessment of the state of security of same. The invention proposes to transmit images of the enclosure wirelessly to a mobile medium for helping the flight crew assess the situation and the measures to take in case of a sensitive security situation.

公开(公告)号：US10240383B2

公开(公告)日：2019-03-26

申请号：US15728888

申请日：2017-10-10

申请人： LATECOERE

发明人： Cyrille Bessettes ,  Damien Buchet ,  Nicolas Lutzi ,  Renaud Othomene

IPC分类号： E05F15/70 ,  B64C1/14 ,  E05F15/40 ,  E05F15/60 ,  E05F11/54

摘要： An aircraft electric door including a locking system for actuating a safety catch for locking the door, a system for moving the door between open and closed positions, and a single electric motor for actuating both the locking system and the system for moving the door.

公开(公告)号：US20180273156A1

公开(公告)日：2018-09-27

申请号：US15764065

申请日：2016-09-29

申请人： LATECOERE

发明人： Patrick VERGNOT ,  Christian ROMEC

IPC分类号： B64C1/14

CPC分类号： B64C1/143 ,  B64C1/1461 ,  E05Y2201/62 ,  E05Y2201/626

摘要： The invention proposes a simple system, with small space requirement, without hinge arms or sealing skirt, while providing secure and effective opening. To achieve this, the invention provides a door opening by a lateral guidance defining an integrated doubling-back kinematics, towards the interior then the exterior of the fuselage. An opening system of an emergency door (1) is positioned in an aircraft fuselage (2), the door and the fuselage comprising respective frameworks (11, 21) extending opposite each other. According to the invention, the system comprises a control handle (5) for rotating, combined with a bolt/latch pair, and an opening mechanism (30) equipped, in the upper corner areas (Zs) of the door (1), with a pivoting lever (6) hinged on an upper edge of the fuselage (2) and provided with guide tracks interacting with the bulk/latch pair and with a door attachment fitting (12), upper and lower rollers mounted in the lateral framework of the door (11c) in connection with the guide tracks (20s, 20i) mounted in the opposing fuselage framework (21c), the upper guide tracks (20s) being inclined rising towards the interior of the cabin (I) and the lower guide tracks (20i) being curved.

公开(公告)号：US20180044969A1

公开(公告)日：2018-02-15

申请号：US15728888

申请日：2017-10-10

申请人： LATECOERE

发明人： Cyrille BESSETTES ,  Damien BUCHET ,  Nicolas LUTZI ,  Renaud OTHOMENE

IPC分类号： E05F15/70 ,  E05F15/60 ,  E05F15/40 ,  E05F11/54 ,  B64C1/14

CPC分类号： E05F15/70 ,  B64C1/1407 ,  B64C1/1423 ,  B64C1/1446 ,  E05F11/54 ,  E05F15/40 ,  E05F15/60 ,  E05Y2900/502

摘要： The invention aims to integrate the activation of the opening/closing phases around a single electric motor, including the treatment of the external window that may be present. An airplane electric door according to the invention has a locking system provided with means for locking a safety catch and a system (200) for coordinating door movements having a single actuating electric motor (2), a cylindrical support (501) having a vertical rotation axis (Z′Z), said support (501) being intended to be rotated by the motor (2), and a fixed guide (91). The support (501) has at least one guideway (511) connected to the arm (6), this guideway (511) being at least partially helical along the vertical axis (Z′Z) of the support (501); The fixed guide (9), which is likewise cylindrical with a vertical axis (Z′Z), possesses at least one double, vertical (91v) and horizontal (91h), camway for guiding the arm (6) successively in these two directions in a manner connected to the arm (6) in order to prevent it from lifting vertically and then to pivot it.

公开(公告)号：US20170316664A1

公开(公告)日：2017-11-02

申请号：US15521958

申请日：2015-10-22

申请人： LATECOERE

发明人： Boucourt GERARD

IPC分类号： G08B13/196 ,  H04N5/232 ,  H04N5/33 ,  H04N5/77 ,  H04N7/18 ,  H04N21/414 ,  B64D45/00 ,  H04N21/214 ,  H04N21/218

摘要： The aim of the invention is to optimise the monitoring and security of at least one enclosure, allowing a constant and complete view of the enclosure, and a modulated assessment of the state of security of same. For this purpose, the invention proposes to transmit images of the enclosure wirelessly to a mobile medium for helping the flight crew assess the situation and the measures to take in case of a sensitive security situation. According to one embodiment, the optimised system for monitoring and securing an enclosure, a cockpit (3), a cabin (2) and/or a luggage hold (4) of an aircraft (1), comprises video cameras (21a to 23a, 21 b to 23b, 24 to 28) distributed so as to define a field of view inside or outside the enclosure (2 to 4), mobile (2T) or fixed (3A) display media dedicated to members of the crew of the enclosure capable, via suitable wireless transmission/reception means (20A), of receiving image streams transmitted by the video cameras (21a to 23a, 21b to 23b, 24 to 28) and of connecting to auxiliary data sources and to means for locking/unlocking (7 to 10, 41) the enclosure (2 to 4) arranged in areas sensitive with respect to security.

公开(公告)号：US20170233098A1

公开(公告)日：2017-08-17

申请号：US15497633

申请日：2017-04-26

申请人： LATECOERE

发明人： Boucourt GERARD

IPC分类号： B64D45/00 ,  G06K9/00 ,  H04N7/18

摘要： The aim of the invention is to optimise the monitoring and security of at least one enclosure, allowing a constant and complete view of the enclosure, and a modulated assessment of the state of security of same. For this purpose, the invention proposes to transmit images of the enclosure wirelessly to a mobile medium for helping the flight crew assess the situation and the measures to take in case of a sensitive security situation. According to one embodiment, the optimised system for monitoring and securing an enclosure, a cockpit (3), a cabin (2) and/or a luggage hold (4) of an aircraft (1), comprises video cameras (21a to 23a, 21b to 23b, 24 to 28) distributed so as to define a field of view inside or outside the enclosure (2 to 4), mobile (2T) or fixed (3A) display media dedicated to members of the crew of the enclosure capable, via suitable wireless transmission/reception means (20A), of receiving image streams transmitted by the video cameras (21a to 23a, 21b to 23b, 24 to 28) and of connecting to auxiliary data sources and to means for locking/unlocking (7 to 10, 41) the enclosure (2 to 4) arranged in areas sensitive with respect to security.

公开(公告)号：US20160107755A1

公开(公告)日：2016-04-21

申请号：US14897330

申请日：2014-06-13

申请人： LATECOERE

发明人： Cyrille BESSETTES ,  Damien BUCHET ,  Renaud OTHOMENE

IPC分类号： B64D25/14 ,  B64C1/14

CPC分类号： B64D25/14 ,  B64C1/1407

摘要： The objective of the invention is to replace the rope bar of the door evacuation slide with individual connections. According to a preferred embodiment, the mechanism for arming/disarming an aircraft door evacuation slide (1, 15, 16) includes two releasable connectors (21) disposed to either side of the base of the door and each includes two half connectors (21s, 21i), a so-called upper half connector (21s, 41, 4a, 42) rigidly connected to the door (1) and having an attachment device (33) for attachment to the slide, and a so-called lower half connector (21i) fixed to the cabin floor (6). Each upper half connector (21s) includes a movable inner part controlled by a ring (43) and housed in the corresponding lower half-connector (21i). The mechanism can also include an electric motor coupled to two rods (31), each rod (31) being capable of rotating the control ring (43) of each upper half connector (21s) between two angular positions: an armed position and a disarmed position.

摘要翻译： 本发明的目的是用单独的连接来更换门疏散滑块的绳条。 根据优选实施例，用于布置/撤防飞机门排气滑架（1,15,16）的机构包括两个可释放的连接器（21），其设置在门的基座的任一侧，并且每个包括两个半连接器（21s， 21i），刚性地连接到门（1）并且具有用于附接到滑块的附接装置（33）的所谓的上半部连接器（21s，41,4a，42）和所谓的下半连接器 21i）固定在机舱地板（6）上。 每个上半部连接器（21s）包括由环（43）控制并容纳在相应的下半连接器（21i）中的可移动内部部分。 该机构还可以包括耦合到两个杆（31）的电动马达，每个杆（31）能够使每个上半连接器（21s）的控制环（43）在两个角度位置之间旋转：武装位置和撤防 位置。

公开(公告)号：US20240336346A1

公开(公告)日：2024-10-10

申请号：US18574393

申请日：2022-06-16

申请人： LATECOERE

发明人： Sebastien DEVILLEZ

IPC分类号： B64C1/14

CPC分类号： B64C1/1461

摘要： An assembly of a vehicle door (3) and of a panel (1) surrounding the door in which an edge protector (4) extends along a skin (3a) of the vehicle door facing the skin (1a) of the panel and has a portion disposed between the skins (1a, 3a) following when in a nominal position the geometric alignment of their exterior faces. This edge protector (4) has in a median portion (4b) a profile that is adapted to evolve and is made of an elastic material so that it has sufficient flexibility in a direction parallel to the distance between the skins (1a, 3a) and a transverse stiffness in the internal-external direction and its contact with the skin (1a) of the panel does not block opening of the door or damage the skins (1a, 3a).

公开(公告)号：US12071215B2

公开(公告)日：2024-08-27

申请号：US17759655

申请日：2021-01-26

申请人： LATECOERE

发明人： Emmanuel Rouzade ,  Gregory Dubosc

IPC分类号： B64C1/14

CPC分类号： B64C1/1423

摘要： An aircraft door including an external opening/closing lever (7) and an internal opening/closing lever (9) which are coupled by an engaging mechanism (12) which includes: a stop (24) which entrains a counter-stop (23) when the internal opening/closing lever (9) is in its closed position and the external opening/closing lever (7) is pivoted from its closed position to its open position; a lug (22) that rotates as one with the internal opening/closing lever; an engaging pawl (15) which is spaced apart from the path of the lug (22) in a passive position, and disposed on the path of the lug (22) in an active position; a support base (16) designed to push the engaging pawl (15) back into its passive position when the external opening/closing lever (7) is in its closed position.

公开(公告)号：US20240149534A1

公开(公告)日：2024-05-09

申请号：US18549017

申请日：2022-03-09

申请人： LATECOERE

发明人： Jean Michel Borlot

IPC分类号： B29C65/36 ,  B29C65/72

CPC分类号： B29C65/3696 ,  B29C65/72 ,  B29K2101/12

摘要： An installation for welding a stack of parts made of thermoplastic composite materials (20) in a local welding plane (P), this installation including an electromagnetic induction head (8), pairs of elements for guiding and pressing the workpiece stack (20) in this local plane (P), and, on each side of the induction head (8), at least one pair of guide elements, each pair of guide elements having a lower guide element (14) and an upper guide element (10) that are superposed, receiving between one another the stack of parts (20) by guiding it in the direction perpendicular to the local welding plane (P).