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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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2.发明公开公开(公告)号：US20240208634A1
公开(公告)日：2024-06-27
申请号：US18145439
申请日：2022-12-22
申请人： The Boeing Company
发明人： Leanne Campbell
CPC分类号： B64C1/143 , B64D13/02 , E05C17/02 , E05Y2900/502 , E05Y2900/531
摘要： Systems, apparatuses and methods provides for technology that moves a locking vent door from an opening position to a locking position, where in the opening position, the locking vent door opens a locking vent, and in the locking position, the locking vent door closes the locking vent. When the locking vent door is in the locking position, the technology prohibits movement of a handle from an engaged position to a disengaged position. When the locking vent door is in the opening position the technology moves the handle from the engaged position to the disengaged position, moves a lock from a locking position to an unlocking position, and moves a pressurization vent door from the pressurization position to the depressurization position based on the lock being moved from the locking position to the unlocking position.
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3.发明申请公开(公告)号：US20180170579A1
公开(公告)日：2018-06-21
申请号：US15383267
申请日：2016-12-19
申请人： EMBRAER S.A.
发明人： Rogério Scafutto SCOTTON , Natália Vianna CORREIA , Luiz Fernando DOS SANTOS , Thomas WARING , Richard WARING
CPC分类号： B64C1/1407 , B05B12/32 , B05B13/041 , B05B13/0431 , B05B13/06 , B05B13/0618 , B05B13/069 , B05B15/60 , B05D1/02 , B05D7/22 , B25J5/005 , B25J11/0075 , B64C1/143 , B64C1/1438 , B64C1/1461 , B64C1/18 , B64C1/22 , B64C1/34 , B64F5/10 , Y10S901/01 , Y10S901/27
摘要： Systems and methods are provided by which a treatment fluid (e.g., a liquid corrosion inhibitor) may be applied onto the interior surfaces of an aircraft fuselage which employ an automated guided vehicle (AGV) comprising a carriage assembly and a robotic spray system carried by the carriage assembly supported by a support platform positioned laterally of an aircraft fuselage in alignment with the cabin door opening thereof. The AGV may thus be deployable through the cabin door opening of the fuselage to a deployed position within the interior of the fuselage so as to be moveable along a longitudinal axis of the fuselage to allow the robotic spray assembly to spray the treatment fluid onto interior surfaces of the fuselage. A sealing door assembly located rearwardly of the AGV which is moveable relative to a door opening in the fuselage may also be provided so as to sealingly close the door opening of the fuselage when the AGV is deployed within the interior of the fuselage.
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4.发明申请公开(公告)号：US20170247100A1
公开(公告)日：2017-08-31
申请号：US15441510
申请日：2017-02-24
CPC分类号： B64C1/1423 , B64C1/143 , B64C1/24 , B64C39/10 , B64C2039/105 , B64D27/14 , Y02T50/12
摘要： An aircraft of flying wing or blended wing body type comprising, for access to a pressurized housing, a non-pressurized door in the trailing edge of the aircraft and a pressurized door on the pressurized housing. The distance between the center of the pressurized door and a plane of symmetry of the aircraft is less than or equal to the distance between the center of the non-pressurized door and the plane of symmetry, and the pressurized door is outside a rear wall of the pressurized housing or upstream of a rear extremum point of the housing in the absence of any such rear wall. This aircraft has optimum aerodynamic performance and the circulation of passengers between the pressurized housing and the exterior of the aircraft may be fluid.
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公开(公告)号：US20170183078A1
公开(公告)日：2017-06-29
申请号：US15388836
申请日：2016-12-22
IPC分类号： B64C1/14
CPC分类号： B64C1/1461 , B64C1/06 , B64C1/1415 , B64C1/1423 , B64C1/143 , B64C1/22 , B64C39/10 , B64C2039/105 , Y02T50/12
摘要： A flying wing or blended body aircraft comprising at least one door installed in the leading edge of the aircraft. The lateral edges of the door extend each in a plane parallel to the plane of symmetry of the aircraft, when the door is closed. It reduces the aerodynamic penalties of a door installed in the leading edge of such an aircraft. It also reduces noise related to airflow at the door, and improves the robustness of the aircraft with respect to impacts.
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公开(公告)号：US20170166292A1
公开(公告)日：2017-06-15
申请号：US15444762
申请日：2017-02-28
CPC分类号： B64C1/1423 , B60N2/4279 , B60N2/797 , B64C1/143 , B64D11/064 , B64D11/0644 , E05C19/02 , E05F15/40 , E06B7/00 , E06B7/28
摘要： Systems and methods for securing an emergency exit door on an armrest of a seat are provided. A system includes a latch connected to an armrest of a seat of a vehicle. The latch is moveable relative to the armrest between a stowed position and a deployed position. The latch is structured and arranged to engage an edge of a door that is associated with an exit of the vehicle to hold the door on the armrest.
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公开(公告)号：US20170129585A1
公开(公告)日：2017-05-11
申请号：US15344724
申请日：2016-11-07
发明人： Johann Konrad Erben
CPC分类号： B64C1/1461 , B64C1/143 , E05B15/0086 , E05B17/2007 , E05B17/2034 , E05B79/10 , E05B83/42 , E05C3/02 , E05C3/12 , E05C9/00 , E05C19/12
摘要： A door assembly, particularly for doors of passenger aircraft, includes a door frame, a door having a door body hingedly installed in the door frame, at least one hooking pintle attached to the door frame or an edge of the door body extending along a pintle axis, and at least one door latch connected to an edge of the door body or the door frame, respectively, the door latch having a substantially C-shaped latch body configured to rotate around an axis parallel to the pintle axis of the hooking pintle. The door assembly further includes a bistable latch and hook mechanism configured to catch the door latch in hooking engagement with the hooking pintle and to retain the door latch in a direction perpendicular to the door body in an overcenter position.
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公开(公告)号：US20160214702A1
公开(公告)日：2016-07-28
申请号：US15007491
申请日：2016-01-27
发明人： Martin STUCKI
IPC分类号： B64C1/18
CPC分类号： B64C1/18 , B64C1/143 , B64C1/1461 , B64C1/1476 , B64C27/04
摘要： In a helicopter cabin that can be fastened to a fuselage structure of a helicopter, encompassing a cabin floor surface, which extends from a front area to a rear area of the helicopter cabin, with front seats and pilot cabin doors arranged in the front area, and the pilot cabin doors along with a front surface and additional walls include part of an outer hull of the helicopter cabin that envelops the cabin floor surface, the comfort is to be enhanced on the ground and during flight. This is accomplished by virtue of the fact that the cabin floor surface of the helicopter cabin exhibits a cutout with a cutout depth directed toward the longitudinal axis in the area of the front seats tapered in the direction of the longitudinal axis.
摘要翻译： 在可以被固定在直升机的机身结构上的直升机舱中，包括从前部区域延伸到直升机舱的后部区域的机舱地板表面，前排座椅和驾驶舱门安排在前部区域， 飞行员舱门以及前表面和附加墙壁包括直升机舱的外壳的一部分，其包围机舱地板表面，舒适性将在地面和飞行中得到增强。 这是通过直升机机舱的机舱地板表面具有切割深度的事实来实现的，切口深度指向在纵向轴线方向上渐缩的前座的区域中的纵向轴线。
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公开(公告)号：US20140103163A1
公开(公告)日：2014-04-17
申请号：US14119459
申请日：2012-05-29
申请人： LATECOERE
发明人： Patrick Lamat
IPC分类号： B64C1/14
CPC分类号： B64C1/1461 , B64C1/143
摘要： The invention relates to an aircraft including a cabin and a door panel (6) comprising, facing the lintel (5) of the opening (3), a sealing strip (13) having a heel piece (14) secured to the internal face of the door panel (6) and a flexible flap (15) that can deform elastically. In addition, the lintel (5) comprises a supporting face (21) for supporting the flexible flap (15), which face is set back from the profile of the fuselage (2) at the junction between the fuselage and the supporting face, such that, when the door panel (6) is in the closed position, the flexible flap (15) extends over the supporting face and matches the profile of the fuselage.
摘要翻译： 本发明涉及一种包括舱室和门板（6）的飞行器，其包括面向所述开口（3）的所述楣板（5），密封条（13），其具有固定到所述开口（3）的内表面 门板（6）和可弹性变形的柔性翼片（15）。 此外，楣板（5）包括用于支撑柔性挡板（15）的支撑面（21），该表面在机身和支撑面之间的接合处从机身（2）的轮廓放回， 当门板（6）处于关闭位置时，柔性挡板（15）在支撑面上延伸并与机身的轮廓相匹配。
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10.发明授权公开(公告)号：US08511610B2
公开(公告)日：2013-08-20
申请号：US12989205
申请日：2009-03-27
申请人： Alain Depeige
发明人： Alain Depeige
IPC分类号： B64C1/14
CPC分类号： B64C1/1407 , B64C1/14 , B64C1/143 , B64C1/1461
摘要： An aircraft door closing device, and an aircraft incorporating such a device. The door includes a leaf and, connected to the aircraft fuselage, a frame including an opening configured to take the leaf, the leaf adopting a closed position to block the opening and another position to reveal the opening. The device includes a bearing mechanism, some on the leaf and some on the frame, each formed by a crenelated structure, two crenelated structures being arranged such that the teeth of one pass through notches of the other as the leaf moves from one position to the other, and such that the teeth of the leaf structure bear, in the closed position, on the inside face of the corresponding teeth of the frame structure.
摘要翻译： 飞机关门装置，以及装有这种装置的飞机。 门包括叶片，并且连接到飞行器机身，框架包括构造成取叶的开口，叶片采取封闭位置以阻挡开口，另一位置露出开口。 该装置包括一个轴承机构，一些在叶片上，一些在框架上，每个都由一个楔形结构形成，两个楔形结构被布置成使得当叶片从一个位置移动到另一个位置时，一个齿通过另一个的齿 并且使得叶结构的齿在关闭位置处承载在框架结构的相应齿的内表面上。
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