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公开(公告)号：US12049294B2
公开(公告)日：2024-07-30
申请号：US17291444
申请日：2019-11-06
申请人： LATECOERE
发明人： Nicolas Capron
CPC分类号： B64C1/1423 , E05F1/10 , E05Y2201/474 , E05Y2800/252 , E05Y2900/502
摘要： An emergency opening device (1) for an aircraft door having: a tubular operating member (2); elastic compression device (3). The operating member (2) includes a first end element (10) and a second end element (11) that can move in translation with respect to one another. The first end element (10) having a cylindrical retractable rotary stop (20), that can move between a first angular position of transmission and a second angular position of release.
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公开(公告)号：US12043366B2
公开(公告)日：2024-07-23
申请号：US17619009
申请日：2020-06-12
申请人： LATECOERE
CPC分类号： B64C1/143 , B64C1/1461 , E05D3/06 , E05D15/34 , E05D2007/0484 , E05Y2900/502
摘要： The invention relates to an aircraft door having a support arm (6) connected to a support forearm (9) by a first pivot connection (7) about a first pivot axis (8), the support forearm (9) being connected to the leaf (5) by a second pivot connection (10) about a second pivot axis (11) parallel to the first pivot axis (8). The support arm (6) is connected to the door frame (4) by two hinges (13, 14) each having a pivot (26, 27) for rotating the support arm (6) about a third pivot axis (12) which is parallel to the first pivot axis (8) and to the second pivot axis (11), this pivot (26, 27) being connected to the door frame (4) by an attachment (22, 23) that is translatably adjustable in two directions (35, 37, 43, 47) orthogonal to one another and orthogonal to the third pivot axis (12).
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公开(公告)号：US11920386B2
公开(公告)日：2024-03-05
申请号：US17618994
申请日：2020-06-12
申请人： LATECOERE
发明人： Gregory Dubosc
CPC分类号： E05B83/36 , B64C1/1423 , B64C1/1461
摘要： Aircraft door including a support arm (10) connecting a door leaf (5) and a door frame (13), the locking/unlocking mechanism of which includes: a control shaft (17) extending along a substantially vertical axis; a guide track (29); an actuating finger (32) attached to the support arm (10); the locking/unlocking mechanism having: an actuating configuration in which the actuating finger (32) is inserted into the guide track (29), the rotation of the control shaft (17) causing the actuating finger (32) to move along the guide track (29); a release configuration in which the actuating finger (32) is outside the guide track (29).
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公开(公告)号：US20240025530A1
公开(公告)日：2024-01-25
申请号：US18255884
申请日：2021-11-26
申请人： LATECOERE
发明人： Sebastien Devillez
CPC分类号： B64C1/1423 , B64D25/14
摘要： An aircraft door architecture having: a door (1); an ejector (3); an inflatable evacuation device (4); an emergency energy source (6) connected to the ejector (3) and to the inflatable evacuation device (4); a control unit (9) having the two following operating states: a nominal operating state in which the inflatable evacuation device (4) is kept in its retracted position and the emergency energy source is deactivated; an emergency operating state in which the emergency energy source (6) activates the actuation device of the ejector (3) in an emergency opening mode of the door (1), and activates the inflation device of the inflatable evacuation device (4) in an emergency inflation mode.
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公开(公告)号：US11878804B2
公开(公告)日：2024-01-23
申请号：US17625120
申请日：2020-07-06
申请人： LATECOERE
发明人： Sabastien Devillez
CPC分类号： B64D25/08 , B64C1/1407 , E05F1/105 , E05Y2800/252 , E05Y2900/502
摘要： An emergency opening device of an aircraft door including a tubular actuating member (2); a resilient compression device; a retaining member for retaining the tubular actuating member (2), having a retaining wire (12) which, when the tubular actuating member (2) is in the retracted position, is held taut between a first attachment (14, 17) and a second attachment (16, 18); a release device which includes a cutting member (22) for transversely cutting the retaining wire (12).
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公开(公告)号：US11878474B2
公开(公告)日：2024-01-23
申请号：US16959192
申请日：2018-12-26
申请人： LATECOERE
IPC分类号： B29C65/62 , B29C65/56 , B29C65/20 , B29C65/60 , B29C65/00 , F16B5/04 , F16B17/00 , B29L31/30
CPC分类号： B29C65/564 , B29C65/20 , B29C65/605 , B29C65/62 , B29C66/0242 , B29C66/02242 , B29C66/0326 , B29C66/03241 , B29C66/1122 , B29C66/21 , B29C66/43 , B29C66/71 , B29C66/7212 , B29C66/72141 , B29C66/73921 , F16B5/04 , F16B17/008 , B29L2031/3082 , B29L2031/3085 , B29L2031/3097
摘要： This invention relates to an assembly of regions (10a, 10b) of composite parts (2a, 2b) with thermoplastic matrix, including a plurality of riveting points along regions (10a, 10) of the parts that overlap through the superposition of two faces (12a, 12b) of these regions (10a, 10b) which are positioned facing one another, each region (10a, 10b) having another, opposite, face (11a, 11b) which remains visible with the part (2a, 2b). The riveting is performed using assembly ties (6) made of thermoplastic resin-based composite material compatible with the material of the parts (2a, 2b). These ties (6), which are made up at least in part of a stitch of backstitch produced using a filament of a material selected from a fiber coated with aramid resin, a carbon fiber and a glass fiber, are embedded in said regions (10a, 10b) and passing right through the same with an orientation comprised between 30° and 90° with respect to their faces (11a, 11b; 12a, 12b).
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公开(公告)号：US11511845B2
公开(公告)日：2022-11-29
申请号：US15733974
申请日：2019-05-28
申请人： LATECOERE
发明人： Fabien Louvel
IPC分类号： B64C1/14
摘要： An emergency exit door (2) for an aircraft cabin, the door includes an opening-assist mechanism and an opening/closing device having a control lever (7), which can selectively be actuated to either unlock the door (2) and permit the action of the door (2) opening assist mechanism or to lock the door (2). The control lever (7) includes an adaptation mechanism (10) for adjusting the lever arm, the adaptation mechanism (10) being moveable between at least two positions: an opening-action position and a closing-action position, the lever arm (LO) of the control lever (7) in the opening-action position being shorter than the lever arm (LF1, LF2) of the control lever (7) in the closing-action position.
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公开(公告)号：US20220153401A1
公开(公告)日：2022-05-19
申请号：US17435829
申请日：2020-03-03
申请人： LATECOERE
发明人： Sabastien DEVILLEZ
IPC分类号： B64C1/14
摘要： An aircraft pressurized cabin door (1) having a fuselage panel (2) and a door structure (3) that includes: two circumferential beams (4) arranged on the lateral edges of the door (1); a plurality of longitudinal beams (5). Each longitudinal beam (5) is an open profile having an outer face to which the fuselage panel (2) is fixed and an inner face, the door structure (3) further including an internal force-absorbing frame (12) fixed to the inner face of each longitudinal beam (5), this internal force-absorbing frame (12) having a plurality of uprights (13) each extending opposite a circumferential beam (4), each upright (13) being fixed to several longitudinal beams (5).
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公开(公告)号：US20210214065A1
公开(公告)日：2021-07-15
申请号：US15733979
申请日：2019-05-28
申请人： LATECOERE
发明人： Sabastien DEVILLEZ
摘要： Aircraft pressurized cabin door (1) including an outer panel (2) and a door structure (3). The door structure (3) includes two circumferential beams (4) fastened to the lateral edges of the door (1); a plurality of longitudinal beams (5) arranged substantially perpendicularly between the circumferential beams (4) and fastened to the outer panel (2), each longitudinal beam (5) extending from one circumferential beam (4) to the other. Each longitudinal beam (5) is an open profile of which the opening (18) is directed toward the outer panel (2), this opening (18) being closed by the internal face of the outer panel (2) to which the longitudinal beam (5) is fastened. Each beam includes a structural redundancy element.
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10.发明申请公开(公告)号：US20200346768A1
公开(公告)日：2020-11-05
申请号：US16957414
申请日：2018-12-23
申请人： LATECOERE
发明人： Christian ROMEC
摘要： An assembly for arming/disarming a slide of an airplane door according to the invention comprises a system with two releasable connection mechanisms (2) linked with the door (1) and a cabin floor of the airplane, each mechanism (2) comprising a releasable connector (21b) secured to the door (1), extending at right angles to the floor on each side of a door bottom, and an anchor fitting (22b) fixed to the cabin floor. Each connector (21b) is equipped with an elastic centering element (70) and a locking/unlocking grab (25b) on the corresponding anchor fitting (22b), the connectors (21b) being linked by a girt bar (5). Each grab (25b) being rotationally mobile, one of the grabs (25b) is driven by a single command (5; 25b) which drives the other grab in rotation via the girt bar (5).
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