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公开(公告)号：US11767096B2
公开(公告)日：2023-09-26
申请号：US17530607
申请日：2021-11-19
申请人： THE BOEING COMPANY
发明人： Matthew W. Walter
CPC分类号： B64C1/32 , B64C1/1476
摘要： A system for initiating a canopy release signal for a canopy of an aircraft includes a first striker secured to the canopy, and a first initiator assembly secured to a fuselage of the aircraft. The first initiator assembly has a protrusion. The first striker is configured to be rotated against the protrusion of the first initiator assembly. The canopy release signal is output in response to the first striker rotating against the protrusion of the first initiator assembly.
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公开(公告)号：US20220126975A1
公开(公告)日：2022-04-28
申请号：US17429082
申请日：2020-02-04
申请人： VISION SYSTEMS
发明人： Philippe BENENTENDI , Mathieu SIMON
摘要： Ejection system for a vehicle emergency exit ejection system for a vehicle emergency exit, the emergency exit extending along a base surface and being designed to cooperate in a mounted position with a receiving frame of the vehicle, the ejection system including a retaining element and a locking mechanism designed to cooperate with the retaining element in a locking configuration in which a movable part of the locking mechanism prevents a relative movement of the retaining element and the locking mechanism in a direction of ejection of the emergency exit which is transversal to the base surface, the movable part being configured to be moved in a closing plane that extends transversally to the base surface and an ejection configuration in which the locking mechanism is capable of moving in the direction of ejection relative to the retaining element.
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公开(公告)号：US11235852B2
公开(公告)日：2022-02-01
申请号：US16127088
申请日：2018-09-10
发明人： Nicolas Behr , Daniel N. Moe , David Barrett
摘要： A bi-directional egress hatch for a passenger aircraft may allow passengers to rapidly and safely exit an overhead cabin of the aircraft onto the main deck, while allowing cabin crew to safely ascend into the overhead cabin if need be. Hatch panels may blend in with overhead bin doors and ceiling panels of the main cabin; the inner portions of the hatch panels (facing the overhead cabin) may include anti-skid portions and graspable handles for descending passengers. The hatch may be easily activated by a passenger with a single motion (or remotely activated, or autodeployed). Once activated, the hatch panels may swing open and a telescoping ladder may deploy from the inner portion to the main deck, remaining rigid once reaching the floor. Similarly, any barriers protecting the ladder from passengers in the overhead cabin may be released, granting access to the telescoping ladder.
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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：US20210171183A1
公开(公告)日：2021-06-10
申请号：US16768755
申请日：2018-12-19
申请人： LEONARDO S.P.A.
发明人： Mimmo Di Castri , Federico Campera
摘要： An emergency exit for a helicopter is described that comprises: a wall defining an opening; a removable part engaging the opening in a removable manner; and a seal interposed between the wall and the removable part. The seal is transformable between: a first configuration, in which it prevents removal of the removable part from the wall following application of a predetermined load on the removable part; and a second configuration, in which it allows removal of the removable part from the wall following application of the predetermined load on the removable part. The emergency exit comprises an insert interposed between the seal and the wall; at least one of the insert and the seal comprise at least one tooth engaging a recess with a shape corresponding to the tooth and defined by the other of the insert and said seal, when the seal keeps, in use, the removable part constrained to wall.
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公开(公告)号：US10711515B2
公开(公告)日：2020-07-14
申请号：US16002861
申请日：2018-06-07
申请人： Goodrich Corporation
发明人： Jerry A. Lambert
摘要： A pyrotechnic egress system may comprise a case defining an opening, a gas generator disposed within the case, the gas generator configured to generate a gas flame in response to being ignited, and an ignition line disposed at the opening and configured to ignite the gas generator, wherein the case directs the gas flame through the opening for deflagrating a window.
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7.发明申请公开(公告)号：US20190210708A1
公开(公告)日：2019-07-11
申请号：US16327201
申请日：2017-09-07
申请人： LEONARDO S.P.A.
CPC分类号： B64C1/32 , B64C1/1484 , B64C1/1492 , B64C27/04
摘要： A window with an emergency exit function for a helicopter is described that comprises: a frame shaped as a framework that can be coupled to a door of said helicopter provided with an opening; and a transparent element designed to engage the opening and held in position by the frame; the frame comprises a first side arranged abutting against the transparent element when a first force below a threshold value is exerted on the latter in a direction transversal to a first plane of a main portion of the transparent element, and which can be elastically moved away from the transparent element when the first force exerted on the latter exceeds the threshold value; and a second side having greater flexural rigidity than the first side in a second plane transversal to first plane and arranged abutting against the transparent element even when the force is greater than said threshold value.
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公开(公告)号：US20180170558A1
公开(公告)日：2018-06-21
申请号：US15837139
申请日：2017-12-11
申请人： Goodrich Corporation
CPC分类号： B64D25/12 , B64C1/32 , B64D25/08 , B64D45/00 , B64D2045/0085
摘要： The present disclosure relates to an aircraft comprising a passenger module, and also a method of protecting a passenger on an aircraft. The passenger module is configured to be ejected through a skin of the aircraft in response to an ejection command. The ejection command may be given in response to a fatal condition to the aircraft being detected or manually indicated.
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公开(公告)号：US09688379B2
公开(公告)日：2017-06-27
申请号：US13630287
申请日：2012-09-28
发明人： Maik Koch , Matthias Breuer
CPC分类号： B64C1/1469 , B64C1/14 , B64C1/18 , B64C1/32
摘要： An actuation device for opening an emergency exit flap of a cockpit door is provided. The actuation device comprises a support structure, at least two securing elements, an actuation element and a deflection mechanism. The support structure is configured so as to be fastened to the emergency exit flap. The securing elements are integrated into the support structure and are configured so as to fasten the actuation device, and thus the emergency exit flap, to the cockpit door. The actuation element is connected to the support structure. Therein, the deflection mechanism connects the securing elements to the actuation element in such a way that a force which is exerted on the actuation element is diverted in such a way that the securing elements are released from the cockpit door.
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公开(公告)号：US08826597B2
公开(公告)日：2014-09-09
申请号：US13431078
申请日：2012-03-27
申请人： Nicolas Raspic
发明人： Nicolas Raspic
CPC分类号： B64C1/1492 , B60J10/365 , B60J10/70 , B61D19/023 , B64C1/14 , B64C1/32 , B64C27/04 , Y02T30/30
摘要： A weatherproof surround, for a jettisonable panel (5) of a vehicle (1) such as a helicopter, possesses four confinement flanges (17-20) integrally formed with a projecting ridge for spring-clipping a corresponding locking strip. Longitudinal foldable shoulders connect the confinement flanges (17-20) to a central trunk (13). Each confinement flange (17-20) can be folded back through pivot angle (31) of at least 90°.
摘要翻译： 用于诸如直升机的车辆（1）的可抛弃面板（5）的防风雨环绕罩具有与突出脊一体形成的四个限制凸缘（17-20），用于弹簧夹持相应的锁定条。 纵向折叠肩部将限制法兰（17-20）连接到中央主干（13）。 每个约束法兰（17-20）可以通过至少90°的枢转角（31）折回。
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