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公开(公告)号：US11505324B2
公开(公告)日：2022-11-22
申请号：US16863751
申请日：2020-04-30
发明人： Luis Melendez
摘要： Disclosed are methods, systems, and non-transitory computer-readable medium for supersonic flight entry/exit management. For instance, the method may include determining whether a transition between supersonic and subsonic flight is approaching; and in response to determining the transition between subsonic and supersonic flight is approaching, performing a supersonic flight entry/exit process. The supersonic flight entry/exit process may include: obtaining center of gravity (CG) information for the vehicle, drag information for the vehicle, and a planned trajectory of the vehicle (trajectory data); performing an analysis of the trajectory data to determine whether the planned trajectory is safe and consistent; based on a result of the analysis, adjusting the planned trajectory or confirming the planned trajectory of the vehicle; and based on the adjusted planned trajectory or the confirmed planned trajectory of the vehicle, generating actuator instructions to execute the adjusted planned trajectory or the confirmed planned trajectory.
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公开(公告)号：US20220324547A1
公开(公告)日：2022-10-13
申请号：US17615998
申请日：2020-06-03
申请人： LATECOERE
发明人： Emmanuel Rouzade
摘要： The invention concerns an aircraft door having a lever (3) for emergency opening from outside, disposed in a lever window. The lever (3) for emergency opening from outside includes: a main arm (7) having a first aerodynamic surface (9); a profiled cowling (8) with a second aerodynamic surface (10); a driving stop (18) capable of rotating the profiled cowling (8) from its concealing position to its separated position when the main arm (7) passes from its retracted position to its deployed position.
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公开(公告)号：US11148817B2
公开(公告)日：2021-10-19
申请号：US16422473
申请日：2019-05-24
申请人： GOODRICH CORPORATION
发明人： Cyle Teal , Neil Cross
摘要： An arm restraint assembly configured to pierce a canopy in response to expulsion of an ejection seat from a cockpit may comprise a primary arm configured to pivot relative to the ejection seat. A canopy piercer may be coupled to the primary arm. The primary arm may be configured to rotate to a fully-deployed position while located within the cockpit. An apex of the canopy piercer may be oriented toward the canopy, when the primary arm is in the fully-deployed position.
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公开(公告)号：US20210246706A1
公开(公告)日：2021-08-12
申请号：US17166136
申请日：2021-02-03
申请人： Ratier-Figeac SAS
发明人： Emmanuel HOURADOU , Raphael PLATA
摘要： An emergency actuation device for opening a door, the emergency actuation device includes: at least one pressurised gas supply; an actuator including: an actuator chamber, an actuator piston moveable between a retracted position and a fully extended position to open the door, a vent for venting the actuator chamber when the actuator piston is in its extended position. The emergency actuation device further includes a percussion device including a percussion piston moveable on activation of the percussion device between: a storage position in which the pressurised gas supply is isolated from the actuator and an activated position in which the pressurised gas supply is coupled to the actuator. The actuator is coupled to the percussion device; and the actuator is configured such that movement of the actuator piston towards its activated position resets the percussion piston.
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公开(公告)号：US20200070987A1
公开(公告)日：2020-03-05
申请号：US16556479
申请日：2019-08-30
发明人： Michael RÖDER
摘要： A passenger door arrangement for an aircraft segment, which arrangement comprises a passenger door, which is configured to assume a raised state and a lowered state, and a “girt bar,” for arming and disarming an escape slide, the girt bar not altering its position relative to the passenger door in the transition from disarming to arming, when the passenger door is in the lowered state. Additionally an aircraft segment, which comprises the passenger door portion and a fuselage portion, an external engagement arrangement being fixed to the fuselage portion.
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公开(公告)号：US20180251224A1
公开(公告)日：2018-09-06
申请号：US15448404
申请日：2017-03-02
申请人： GOODRICH CORPORATION
发明人： Daniel Bahena , Timothy C. Haynes
摘要： An inflatable flotation device includes a main body having a distal end and a proximal end configured to be positioned nearer to the aircraft than the distal end, the main body configured to inflate to provide an evacuation route. The inflatable flotation device further includes an extendable portion coupled to the proximal end of the main body and having a plurality of segments coupled together. The inflatable flotation device further includes a weighted object coupled to the extendable portion and configured to cause the extendable portion to extend in response to a distance from the proximal end of the main body being equal to or greater than a threshold distance.
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公开(公告)号：US20180202466A1
公开(公告)日：2018-07-19
申请号：US15405797
申请日：2017-01-13
申请人： Goodrich Corporation
发明人： Timothy C Haynes , Daniel Bahena
摘要： An aspirator may comprise an aspirator body defining an air channel. An aspirator barrel may have a first aspirator barrel segment coupled to the aspirator body and may have a second aspirator barrel segment. The second aspirator barrel segment configured to fit at least partially within the first aspirator barrel segment when the aspirator barrel is in a stowed state and configured to interlock with the first aspirator barrel segment in an extended position when the aspirator barrel is in a deployed state.
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公开(公告)号：US09902485B2
公开(公告)日：2018-02-27
申请号：US14311105
申请日：2014-06-20
申请人： THE BOEING COMPANY
发明人： Sergey Barmichev , Mithra Sankrithi , David Eckert
CPC分类号： B64C1/24 , B64D25/08 , B64D25/14 , B64D25/18 , Y10S244/905
摘要： Systems, methods, and apparatus for permitting evacuation of an aircraft following a water landing are disclosed. In one or more embodiments, the disclosed method involves deploying, an evacuation unit, from inside a storage housing located proximate a door of the aircraft. In one or more embodiments, the evacuation unit comprises at least one step and a wave fence. In at least one embodiment, when the evacuation unit is fully deployed, at least a portion of the wave fence is in water-tight contact with at least a portion of a frame of the door such that water flow into the aircraft is prevented and/or inhibited.
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9.发明授权公开(公告)号：US09469401B2
公开(公告)日：2016-10-18
申请号：US14132982
申请日：2013-12-18
发明人： Yves Durand , Bernard Guering
摘要： A toilet area for an aircraft cabin comprising an access door and housing a toilet bowl. The toilet area also comprises an evacuation exit, the access door occupying a closed position in the toilet area in a toilet configuration and a folded position in the toilet area in an evacuation configuration. Usage in particular in a flying wing aircraft is provided.
摘要翻译： 一种用于飞机机舱的卫生间区域，其包括通道门和容纳马桶。 厕所区域还包括撤离出口，进入门在马桶构造中占据马桶区域中的关闭位置，并且在抽空构造中在厕所区域中的折叠位置。 特别提供飞翼飞机的使用。
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公开(公告)号：US6003813A
公开(公告)日：1999-12-21
申请号：US144406
申请日：1998-08-31
申请人： Mark E. Wentland , Gregory J. Oakes
发明人： Mark E. Wentland , Gregory J. Oakes
CPC分类号： B64D11/00 , B64D25/08 , B64D2011/0046
摘要： An overhead rest area is provided in the crown of an aircraft above the ceiling for the main passenger cabin. A permanent access stairway is provided at one end of the overhead rest area, and an emergency escape apparatus is provided at another location of the rest area. The emergency escape apparatus can include a slide swingable between a closed position in which its underside forms a smooth continuation of the ceiling of the passenger cabin and a downward swung open position providing an escape route from the overhead rest area to the passenger cabin.
摘要翻译： 在主客舱的天花板上方的飞机的顶部设置有头顶休息区域。 在顶棚休息区的一端设有永久通道楼梯，在其余区域的另一位置设有紧急逃生装置。 紧急逃生装置可以包括一个可在其下侧形成乘客舱顶部的平滑延续的关闭位置和向下摆动的打开位置之间摆动的滑动件，该向下摆动的打开位置提供从顶部支架区域到客舱的逃生路线。
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