公开(公告)号：US12122524B2

公开(公告)日：2024-10-22

申请号：US18354549

申请日：2023-07-18

申请人： GOODRICH CORPORATION

发明人： Timothy C Haynes ,  Drew Hartman

IPC分类号： B64D25/14 ,  B64D47/02 ,  G08B5/36 ,  H05B45/22 ,  H05B45/30

CPC分类号： B64D25/14 ,  G08B5/36 ,  H05B45/22 ,  H05B45/30

摘要： A light system for an evacuation slide may include a readiness indicator light assembly. The readiness indicator light assembly may comprise a first light emitting diode configured to emit a first color and a second light emitting diode configured to emit a second color. The light system may be configured to power the first light emitting diode after initial deployment of the evacuation slide and to power the second light emitting diode after the internal pressure of the evacuation slide is greater than a minimum pressure threshold.

公开(公告)号：US12091151B2

公开(公告)日：2024-09-17

申请号：US17756667

申请日：2020-11-30

申请人： LATECOERE

发明人： Emmanuel Rouzade

IPC分类号： B64C1/14 ,  B64D25/14

CPC分类号： B64C1/1423 ,  B64D25/14

摘要： An aircraft door including a retaining device for a deployable evacuation device, the retaining device having at least: a beam; a first retention member fixed on a second end of the beam by a detachable clip, the first retention member being connected to the deployable evacuation device; a second retention member, which can be coupled to the first retention member, mounted on the door frame; retraction devices that moves between: an activated position, in which the second retention member is on the trajectory of the first retention member, and a deactivated position, in which the second retention member is outside the trajectory of the first retention member.

公开(公告)号：US12077305B2

公开(公告)日：2024-09-03

申请号：US16711638

申请日：2019-12-12

申请人： GOODRICH CORPORATION

发明人： Ivan Kruts ,  Steven Evans

IPC分类号： F16B2/16 ,  B64D25/14 ,  F16B21/16

CPC分类号： B64D25/14 ,  F16B2/16 ,  F16B21/165 ,  Y10T24/45461 ,  Y10T403/592

摘要： A releasable restraint may comprise a base and a socket coupled to the base. The socket may include a head and a shaft extending from the head, wherein the shaft defines a base channel configured to receive the base. A sleeve may be configured to translate relative to the shaft of the socket. A plurality of balls may be located in a plurality of frustoconical ball openings formed through the shaft of the socket. A plug may be received by a plug channel defined by the socket.

公开(公告)号：US20240286748A1

公开(公告)日：2024-08-29

申请号：US18655389

申请日：2024-05-06

申请人： THE BOEING COMPANY

发明人： Angela Noelani Cruz ,  Mark Edward King ,  Steven Philip McDonald

IPC分类号： B64D25/18 ,  B64C1/14 ,  B64D25/14

CPC分类号： B64D25/18 ,  B64D25/14 ,  B64C1/1407

摘要： An emergency evacuation system includes a first floatation device, an inflator operably coupled to the first floatation device, and a second floatation device coupled to the first floatation device. The inflator is configured to inflate the first floatation device to deploy the emergency evacuation system outside of a compartment, such as proximate to a door of a vehicle.

公开(公告)号：US12049324B2

公开(公告)日：2024-07-30

申请号：US17018852

申请日：2020-09-11

申请人： UNITED AIRLINES, INC.

发明人： William J. Rushin ,  Edison Herrera

IPC分类号： B64D25/14 ,  B65D6/00 ,  B65D25/20 ,  A62B1/20

CPC分类号： B64D25/14 ,  B65D11/10 ,  B65D25/20 ,  A62B1/20 ,  Y10T29/49716

摘要： An emergency escape slide container includes a first portion having a first end wall and a first side wall, the first side wall and the first end wall defining a first storage space that is sized and shaped to receive an emergency escape slide. The first side wall also includes a first rolling mechanism. The emergency escape slide container also includes a second portion having a second end wall and a second side wall, the second side wall and the second end wall defining a second storage space sized and shaped to receive the emergency escape slide. The second side wall also includes a second rolling mechanism. The first portion and the second portion cooperate to define a third storage space therebetween, the third storage space being equal to a combination of the first storage space and the second storage space.

公开(公告)号：US20240247529A1

公开(公告)日：2024-07-25

申请号：US18416970

申请日：2024-01-19

申请人： Rohr, Inc.

发明人： Damien Buchet

IPC分类号： E05F15/00 ,  B64C1/14 ,  B64D25/14

CPC分类号： E05F15/00 ,  B64C1/1407 ,  B64D25/14 ,  E05Y2900/502

摘要： An interlock assembly for an aircraft door includes a shaft, an interlock first portion, and an auto-disarm second portion. The shaft is rotatable about the second rotational axis between an armed position and a disarmed position. The shaft includes an interlock cam and an auto-disarming cam. In a first interlock position, the interlock first portion permits rotation of the shaft between the armed position and the disarmed position. In a second interlock position, the interlock first portion prevents rotation of the shaft from the disarmed position to the armed position. In a first auto-disarm position, the auto-disarm second portion permits rotation of the shaft between the armed position and the disarmed position. In a second auto-disarm position, the auto-disarm second portion prevents rotation of the shaft from the disarmed position to the armed position.

公开(公告)号：US20240208190A1

公开(公告)日：2024-06-27

申请号：US18086947

申请日：2022-12-22

申请人： Air Cruisers Company, LLC

发明人： Christian Thomson

IPC分类号： B32B27/12 ,  B32B5/02 ,  B32B7/027 ,  B32B15/04 ,  B32B15/18 ,  B32B15/20 ,  B32B27/08 ,  B32B27/32 ,  B32B27/34 ,  B32B27/36 ,  B63C9/04 ,  B63C9/125 ,  B64D25/14

CPC分类号： B32B27/12 ,  B32B5/02 ,  B32B7/027 ,  B32B15/04 ,  B32B15/18 ,  B32B15/20 ,  B32B27/08 ,  B32B27/32 ,  B32B27/34 ,  B32B27/36 ,  B63C9/04 ,  B63C9/1255 ,  B64D25/14 ,  B32B2307/306 ,  B32B2307/54 ,  B32B2307/718 ,  B32B2437/00 ,  B32B2439/00 ,  B32B2607/00 ,  B63C2009/042

摘要： Described is a fabric or flexible composite material for an inflatable safety product. The fabric or flexible composite material includes a substrate and a film covering a surface of the substrate. In certain embodiments, the substrate and the film have a same base polymer. The film may be fused to the substrate without an adhesive. A method of forming an inflatable safety product includes forming a fabric or flexible composite material by fusing a film to a substrate without an adhesive.

公开(公告)号：US20240083587A1

公开(公告)日：2024-03-14

申请号：US17985391

申请日：2022-11-11

申请人： GOODRICH CORPORATION

发明人： Vasantha Kumara Jnanegowda ,  Sunil Deshapande

IPC分类号： B64D25/14 ,  B64D25/18

CPC分类号： B64D25/14 ,  B64D25/18

摘要： A system for releasing a blowout panel and softcover release of an evacuation slide in an aircraft is provided. The system includes a first actuator, a second actuator; and a controller. The controller is configured to receive an indication that an evacuation event has begun; and, responsive to receiving the indication of the evacuation event beginning: send a first signal to the first actuator that magnetizes a first magnetostriction material within the first actuator, thereby releasing the blowout panel of a packboard compartment in which the evacuation slide is present; and send a second signal to the second actuator that magnetizes a second magnetostriction material within the second actuator, thereby releasing a key-loop of lacing associated with the softcover in which the evacuation slide is present in the packboard compartment.

公开(公告)号：US20230406504A1

公开(公告)日：2023-12-21

申请号：US18144601

申请日：2023-05-08

申请人： JETZERO, INC.

发明人： Jennifer Whitlock ,  Brendan Kennelly ,  Mark Allan Page

IPC分类号： B64D11/00 ,  B64C39/00 ,  B64C1/22 ,  B64C1/14 ,  B64D25/14 ,  B64C39/10 ,  B64C1/10

CPC分类号： B64D11/00 ,  B64C39/00 ,  B64C1/22 ,  B64C2039/105 ,  B64D25/14 ,  B64C39/10 ,  B64C1/10 ,  B64C1/1423

摘要： Technologies for providing emergency egress routes for a blended wing body aircraft are described herein. In some examples, the emergency egress routes are through a side cabin bulkhead and aft one or more cargo holds. In some examples, the blended wing body aircraft has wings that are high geometry wings. In these examples, the emergency egress routes do not penetrate an aft spar, reducing weight and increasing the integrity of the aircraft.

公开(公告)号：US20230349479A1

公开(公告)日：2023-11-02

申请号：US17871589

申请日：2022-07-22

申请人： GOODRICH CORPORATION

发明人： POLY JOHN ,  VASANTHA KUMARA JNANEGOWDA

IPC分类号： F16K17/16 ,  B64D25/14 ,  F16K31/06 ,  F16K31/40

CPC分类号： F16K17/16 ,  B64D25/14 ,  F16K31/0655 ,  F16K31/406 ,  B33Y80/00

摘要： A regulator valve assembly may comprise: a housing defining an actuator cavity and a piston head cavity; a piston rod comprising a piston head disposed within the piston head cavity and a rod end disposed within the actuator cavity; and a disc retainer within the housing. The actuator cavity can have a top region of the actuator cavity and a bottom region of the actuator cavity. The piston head cavity can comprise a regulator inlet and an inlet port. The disc retainer can be coupled to a proximate seating surface of the inlet port, wherein a first face of a membrane disc is coupled to a lateral seating surface of the inlet port disposed between the piston head cavity and the disc retainer. Also disclosed are methods of using and manufacturing regulator valve assemblies.