公开(公告)号：US20230166852A1

公开(公告)日：2023-06-01

申请号：US17590454

申请日：2022-02-01

申请人： GOODRICH CORPORATION

发明人： BHAVIK MUGERAYA ,  POLY PUTHUR JOHN ,  SRIJITH PURUSHOTHAMAN

IPC分类号： B64D25/14 ,  G05D16/20

CPC分类号： B64D25/14 ,  G05D16/2013

摘要： An inflation control system for an inflatable device may comprise: a compressed fluid source; a solenoid valve connected to the compressed fluid source and configured to control a flow of gas to the inflatable device; and a control circuit comprising a power source, a pressure switch, and an electrical switch, the control circuit configured to energize, via the power source, the solenoid valve in response to both the pressure switch and the electrical switch being in a closed state, the pressure switch configured to open and de-energize the solenoid valve in response to being exposed to a pressure at or exceeding a pressure threshold.

公开(公告)号：US20190233173A1

公开(公告)日：2019-08-01

申请号：US15883964

申请日：2018-01-30

申请人： GOODRICH CORPORATION

发明人： Timothy C. Haynes ,  Drew Hartman

IPC分类号： B65D35/44 ,  B64D25/14 ,  B64D25/18 ,  B63C9/04 ,  B65D47/06

CPC分类号： B65D35/44 ,  B63C9/04 ,  B63C2009/042 ,  B64D25/14 ,  B64D25/18 ,  B65D47/06

摘要： Systems and methods are disclosed herein for an inflation pouch. The inflation pouch may include a border on a first end and a nozzle on a second end, wherein the border defines an interior volume of the inflation pouch, and the interior volume is in fluid communication with the nozzle. The border further comprises a zipping fastener or a hook and loop fastener. The nozzle may couple with an inflation valve of an inflatable structure. The interior volume of the inflation pouch is in fluid communication with an interior volume of the inflatable structure.

公开(公告)号：US20190017519A1

公开(公告)日：2019-01-17

申请号：US15647771

申请日：2017-07-12

申请人： GOODRICH CORPORATION

发明人： ERIC MCFARLAND

IPC分类号： F04F5/46 ,  B60C29/00

CPC分类号： F04F5/463 ,  B63C9/24 ,  B64D25/14 ,  F04F5/16 ,  F04F5/42 ,  F04F5/466

摘要： An aspirator assembly for an inflatable device includes an outer housing disposed about an axis, an inner housing disposed about the axis, and a manifold coupled through the outer housing to an annulus located between the inner housing and the outer housing, the manifold providing pressurized gas to said annulus via a plurality of gas ejector nozzles. The annulus may be divided into a plurality of annulus segments by a plurality of vanes protruding radially from the inner housing

公开(公告)号：US20180273191A1

公开(公告)日：2018-09-27

申请号：US15466550

申请日：2017-03-22

申请人： GOODRICH CORPORATION

发明人： TIMOTHY C. HAYNES ,  RYAN SCHMIDT

IPC分类号： B64D25/14

CPC分类号： B64D25/14

摘要： An evacuation assembly of an aircraft includes an evacuation slide and a sheet coupled to the evacuation slide. The sheet may be deployable in a wind curtain configuration and a canopy configuration. In the wind curtain configuration, the sheet may extend, as a substantially vertical panel, longitudinally along opposing lateral sides of the evacuation slide. In the canopy configuration the sheet may extend over at least a portion of a top side of the evacuation slide. In the canopy configuration, the sheet may include a first portion that is the substantially vertical panel that extends longitudinally along the opposing lateral sides of the evacuation slide and a second portion that extends over the top side of the evacuation slide. The second portion of the curtain may in a furled, collapsed form in the wind curtain configuration and may be configured to unfurl in the canopy configuration.

公开(公告)号：US20180273189A1

公开(公告)日：2018-09-27

申请号：US15466217

申请日：2017-03-22

申请人： GOODRICH CORPORATION

发明人： Timothy C. Haynes ,  Daniel Bahena

IPC分类号： B64D25/14

CPC分类号： B64D25/14 ,  B65D63/10 ,  B65D63/1027

摘要： An evacuation system may comprise an evacuation slide configured to be deployed from an aircraft, a first strap coupled to the evacuation slide, a second strap coupled to the evacuation slide, and a releasable restraint extending through the first strap and the second strap. The releasable restraint may comprise a first stem connected to a first bead and a second stem connected to a second bead, wherein a diameter of the second stem may be different from a diameter of the first stem.

公开(公告)号：US10054265B2

公开(公告)日：2018-08-21

申请号：US15363997

申请日：2016-11-29

申请人： GOODRICH CORPORATION

发明人： Eric McFarland

IPC分类号： B67D7/00 ,  F17C7/00 ,  F17C1/00

CPC分类号： F17C7/00 ,  B64D25/14 ,  F15B2211/218 ,  F17C1/005 ,  F17C2227/0332

摘要： Systems and methods for a heated gas cylinder assembly are disclosed. The heated gas cylinder assembly may comprise a cylinder shell and a heat exchanger disposed within the cylinder shell. The heat exchanger and the cylinder shell may define an interior chamber configured to hold a gas mixture. The heat exchanger may comprise an inner bore configured to receive a pyrotechnic composition. In response to igniting the pyrotechnic composition, the heat exchanger may provide thermal conduction to the gas mixture. The gas mixture may be simultaneously heated and released, or the gas mixture may be preheated before release.

公开(公告)号：US20180141669A1

公开(公告)日：2018-05-24

申请号：US15356822

申请日：2016-11-21

申请人： Goodrich Corporation

发明人： Nick Ruegsegger ,  Steven Evans

IPC分类号： B64D25/14

CPC分类号： B64D25/14 ,  B63C9/24 ,  F04F5/16

摘要： An aspirator assembly for an inflatable device may have an inner housing disposed about an axis with an outlet formed through the inner housing. An outer housing may also be disposed about the axis with a surface of the outer housing covering the outlet. The outer housing may be translatable relative to the inner housing to expose the outlet in response to a gas pressure within the aspirator assembly being above a threshold.

公开(公告)号：US20180127082A1

公开(公告)日：2018-05-10

申请号：US15863776

申请日：2018-01-05

申请人： The Boeing Company

发明人： Sergey Barmichev ,  Mithra Sankrithi ,  David Eckert

IPC分类号： B64C1/24 ,  B64D25/18 ,  B64D25/14 ,  B64D25/08

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.

公开(公告)号：US09957054B2

公开(公告)日：2018-05-01

申请号：US14814309

申请日：2015-07-30

申请人： GOODRICH CORPORATION

发明人： Jaro S. Volny ,  Drew Hartman

IPC分类号： B64D25/14 ,  A62B1/20

CPC分类号： B64D25/14 ,  A62B1/20

摘要： Disclosed is an emergency slide system comprising a slide having a telescoping structural support, and a slide surface. The emergency slide system further comprises a gas deployment device comprising a gas generator, compressed gas cylinder, or both. The gas deployment device may further include an aspirator, according to various embodiments. The telescoping structural support provides a more compact and quickly deployable system.

公开(公告)号：US09932128B1

公开(公告)日：2018-04-03

申请号：US15350817

申请日：2016-11-14

申请人： Goodrich Corporation

发明人： Jaro S Volny ,  Drew Hartman

IPC分类号： B64D47/02 ,  B64F1/20 ,  F21V1/20 ,  F21V21/00 ,  B64D25/14 ,  F21V23/06 ,  F21V17/02 ,  F21V7/00 ,  F21V23/02 ,  F21S9/02

CPC分类号： B64D47/02 ,  B64D25/14 ,  B64D2203/00 ,  F21S9/02 ,  F21V7/00 ,  F21V17/02 ,  F21V23/02 ,  F21V23/06 ,  F21W2107/30

摘要： A light assembly for an aircraft evacuation system may comprise a first casing including a weighted portion. A light source may be disposed within the first casing. A second casing may be coupled to the first casing by a bearing. The first casing may be configured to rotate with respect to the second casing about an axis. A center of mass of the first casing may be offset from the axis.