-
公开(公告)号:US12122523B2
公开(公告)日:2024-10-22
申请号:US17856563
申请日:2022-07-01
申请人: Goodrich Corporation
IPC分类号: B64D25/14 , B64F5/10 , D06M15/564
CPC分类号: B64D25/14 , B64F5/10 , D06M15/564 , D06M2200/25
摘要: An aircraft evacuation slide assembly may be comprised of a plurality of composite textiles. Each composite textile may comprise a fabric substrate, an inner polyurethane coating, and an outer heat reflective coating. The outer heat reflective coating may comprise nanofillers that improve polymer properties, such as mechanical, barrier, thermal, flame retardancy, and electrical properties. Moreover, the outer heat reflective coating may comprise nanofillers that enable hot air welding and radio frequency welding of the plurality composite textiles to form the aircraft evacuation slide assembly.
-
公开(公告)号:US20240300655A1
公开(公告)日:2024-09-12
申请号:US18667092
申请日:2024-05-17
申请人: GOODRICH CORPORATION
发明人: Ivan Kruts , Kamil Czechowski
CPC分类号: B64D25/14 , B64F5/10 , F16K3/32 , F16K31/002
摘要: A regulator arrangement for an inflatable includes a regulator housing comprising a bore, the bore comprising a longitudinal axis, a piston disposed in the bore and configured to translate, with respect to the regulator housing, along the longitudinal axis, an adjuster plug disposed in the bore and axially adjacent the piston, an adjuster plug stop disposed at least partially within the bore, and a spring member disposed between the adjuster plug and the piston. The adjuster plug comprises a tapered head and a shaft portion extending from the tapered head. The adjuster plug stop comprises a tapered surface configured to contact the tapered head.
-
公开(公告)号:US12071968B2
公开(公告)日:2024-08-27
申请号:US16983130
申请日:2020-08-03
申请人: Goodrich Corporation
摘要: A releasable restraint may comprise a bracket and a puller removably coupled to the bracket. A first tube portion and a second tube portion may be rotatably coupled to the puller. A torsion spring may be configured to bias the first tube portion in a first circumferential direction and the second tube portion in a second, opposite circumferential direction.
-
公开(公告)号:US12066847B2
公开(公告)日:2024-08-20
申请号:US17836376
申请日:2022-06-09
申请人: Goodrich Corporation
IPC分类号: G05D7/01 , B64D25/14 , F16K17/164 , F16K31/06 , F16K31/42
CPC分类号: G05D7/0126 , B64D25/14 , F16K17/164 , F16K31/06 , F16K31/42
摘要: A regulator valve assembly for a compressed fluid source may comprise a valve housing defining a main fluid channel, a secondary fluid channel, a primary outlet, a primary inlet, and a secondary inlet. A poppet may be located in the main fluid channel, The poppet may define a poppet channel and a poppet outlet. The poppet channel may be fluidly connected to the secondary inlet. A rod may be configured to translate in and out the poppet outlet. A pin may be biased toward the secondary fluid channel. The pin may be configured to translate into a translation path of the rod. A solenoid valve may be configured to control a flow of fluid into the secondary fluid channel.
-
公开(公告)号:US12018702B2
公开(公告)日:2024-06-25
申请号:US18110025
申请日:2023-02-15
申请人: Altevac, LLC
发明人: Blair White
摘要: An aspirator assembly for inflating an emergency slide. The aspirator assembly includes a bell housing, a mixing chamber, and a nozzle assembly. The bell housing includes a ring defining an inlet port at which a check valve is located and into which ambient air can flow. The mixing chamber has an outlet port, The nozzle assembly is located in the mixing chamber and includes plural passageway sections defining concentric rings and cross bars. The passageway sections include internal passageways in communication with plural nozzle jets through which a compressed air is introduced into the mixing chamber to mix with the ambient air. The passageway sections are of an airfoil shape cross-section having a rounded leading end directed towards the inlet port and a trailing end is directed toward the outlet port to reduce air turbulence within the mixing chamber.
-
公开(公告)号:US11905023B2
公开(公告)日:2024-02-20
申请号:US18180215
申请日:2023-03-08
申请人: The Boeing Company
发明人: Robert J. Lenaburg , Paul J. Wilcynski , Rodney M. Burgin , Steven P. McDonald , Bruce E. Wallace
摘要: An evacuation slide to provide an egress path from an exit of an aircraft. The evacuation slide includes one or more slide lanes. One or more jump targets and indicators are positioned along each of the slide lanes to visually inform persons how to enter a ramp of the slide. Lights illuminate one or more sections of the slide to further provide visual guidance on how to enter the ramp.
-
公开(公告)号:US20230375103A1
公开(公告)日:2023-11-23
申请号:US17888881
申请日:2022-08-16
申请人: Goodrich Corporation
发明人: VASANTHA KUMARA JNANEGOWDA , POLY JOHN , GUANGQING SHEN , KAMIL KRZYSZTOF CZECHOWSKI , PIOTR JÓZEF ZAJAC
CPC分类号: F16K31/406 , F16K17/403 , B64D25/14
摘要: A valve arrangement for inflating an inflatable device includes a valve body comprising an inlet, an outlet, a main fluid channel, a first ball detent, and a second ball detent. A lifter and a sleeve are located in the main fluid channel. A locking ball is disposed at least partially within a locking ball aperture disposed in the sleeve. A piston is coupled to the lifter and fluidly coupled to a command pressure cavity of the valve body. A spring biases the lifter toward a ball locking position whereby the lifter urges the locking ball at least partially into the first ball detent. A valve operation initiator controls a flow of pressurized gas into the command pressure cavity to urge the lifter to a ball releasing position to free the sleeve, as to the locking ball, to translate to an open position to fluidly couple the inlet with the outlet.
-
公开(公告)号:US11802629B1
公开(公告)日:2023-10-31
申请号:US17888881
申请日:2022-08-16
申请人: Goodrich Corporation
发明人: Vasantha Kumara Jnanegowda , Poly John , Guangqing Shen , Kamil Krzysztof Czechowski , Piotr Józef Zajac
CPC分类号: F16K31/406 , F16K17/403 , B64D25/14
摘要: A valve arrangement for inflating an inflatable device includes a valve body comprising an inlet, an outlet, a main fluid channel, a first ball detent, and a second ball detent. A lifter and a sleeve are located in the main fluid channel. A locking ball is disposed at least partially within a locking ball aperture disposed in the sleeve. A piston is coupled to the lifter and fluidly coupled to a command pressure cavity of the valve body. A spring biases the lifter toward a ball locking position whereby the lifter urges the locking ball at least partially into the first ball detent. A valve operation initiator controls a flow of pressurized gas into the command pressure cavity to urge the lifter to a ball releasing position to free the sleeve, as to the locking ball, to translate to an open position to fluidly couple the inlet with the outlet.
-
公开(公告)号:US20230339618A1
公开(公告)日:2023-10-26
申请号:US17889299
申请日:2022-08-16
申请人: B/E AEROSPACE, INC.
发明人: NAKUL GUPTA , PRIYANK ANAVADIYA , SINDHU THOMAS , VINAY CHULLIYIL NARAYANAN NAIR , YASWANTH KUMAR MADDALI
CPC分类号: B64D25/14 , B64D45/00 , B64D2045/007
摘要: An evacuation guidance system may comprise a plurality of floor guidance lights, a plurality of seat guidance lights, a plurality of exit signs, and a controller in communication with the plurality of floor guidance lights, the plurality of seat guidance lights, and the plurality of exit signs. The plurality of floor guidance lights may include a plurality of fore-aft floor lights and a plurality of port-starboard floor lights. The controller may be configured to determine a closest exit door to each floor guidance light, each seat guidance light, and each exit sign. The controller may command each floor guidance light, each seat guidance light, and each exit sign to indicate a direction of the closest exit door.
-
公开(公告)号:US20230312114A1
公开(公告)日:2023-10-05
申请号:US17856563
申请日:2022-07-01
申请人: Goodrich Corporation
IPC分类号: B64D25/14 , B64F5/10 , D06M15/564
CPC分类号: B64D25/14 , B64F5/10 , D06M15/564 , D06M2200/25
摘要: An aircraft evacuation slide assembly may be comprised of a plurality of composite textiles. Each composite textile may comprise a fabric substrate, an inner polyurethane coating, and an outer heat reflective coating. The outer heat reflective coating may comprise nanofillers that improve polymer properties, such as mechanical, barrier, thermal, flame retardancy, and electrical properties. Moreover, the outer heat reflective coating may comprise nanofillers that enable hot air welding and radio frequency welding of the plurality composite textiles to form the aircraft evacuation slide assembly.
-
-
-
-
-
-
-
-
-