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公开(公告)号：US12275519B2
公开(公告)日：2025-04-15
申请号：US17804861
申请日：2022-06-01
Applicant: The Boeing Company
Inventor： Steven Ellis Rhynard , Joe Files , Jason Empleo , Kenneth M. Reynolds
IPC: B64C1/06
Abstract: A vertical intercostal for an aircraft vehicle having a vehicle cabin and an over-monument fairing arranged in a non-flex zone area of the vehicle cabin. The intercostal includes a frame member that includes an upper frame attachment region, a lower frame attachment region, and an intermediate frame attachment region to provide lateral structural support for the over-monument fairing to the airframe of the aircraft.
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2.发明公开公开(公告)号：US20230242257A1
公开(公告)日：2023-08-03
申请号：US17586882
申请日：2022-01-28
Applicant: THE BOEING COMPANY
Inventor： Steven Ellis Rhynard , Joe Files , Adam Arthur Logue , Long Hoang Duong , Kenneth Merkley Reynolds , Jason W. Mullins
IPC: B64D11/00
CPC classification number: B64D11/003 , B64D2011/0038 , B64D2011/0046
Abstract: A stowage bin lighting assembly for mounting to an internal cabin of a vehicle includes a chassis having a plate extending longitudinally between ends. The chassis supports light mount pedestals, wire standoffs, and at least one valance support above the upper surface. The stowage bin lighting assembly includes a light mounted to the light mount pedestals positioned above the plate by the light mount pedestals for providing lighting from the stowage bin assembly to the internal cabin of the vehicle. The stowage bin lighting assembly includes a wire electrically connected to the light to supply power to the light and coupled to at least one of the wire standoffs to control a position of the wire relative to the plate. The stowage bin lighting assembly includes a valance coupled to the valance mount pedestals configured to be coupled to the stowage bin assembly by the valance support.
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公开(公告)号：US11643848B2
公开(公告)日：2023-05-09
申请号：US16412603
申请日：2019-05-15
Applicant: The Boeing Company
Inventor： Joe Files , Adam A. Logue
CPC classification number: E05B63/22 , B64C1/066 , E05F1/1008 , E05F3/20 , E05Y2900/502
Abstract: An aircraft panel system including a first panel, having a hinged coupling configured to couple the first panel to an aircraft structure, a second panel disposed adjacent to the first panel such that the first panel and the second panel together form cabin surface of an aircraft, and a latch mechanism configured to releasably couple the second panel to the aircraft structure, where the first panel is configured to pivot about the hinged coupling from a latched position to an actuation position to actuate the latch mechanism and cause a release of the second panel from the latch mechanism.
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公开(公告)号：US12187406B2
公开(公告)日：2025-01-07
申请号：US17582478
申请日：2022-01-24
Applicant: The Boeing Company
Inventor： Steven Ellis Rhynard , Joe Files
Abstract: A bulkhead assembly for an aircraft passenger cabin having a floor and a secondary support member includes upper and lower bulkhead panels and a bulkhead coupling member. The upper bulkhead panel defines an elongated tower portion that protrudes through a slot opening in an overhead closeout panel, and directly or indirectly connects to the secondary support member. The lower bulkhead panel connects to the upper bulkhead panel and to the floor via the bulkhead coupling member. A method for installing the bulkhead assembly in the passenger cabin includes connecting the lower bulkhead panel to the floor, joining the lower bulkhead panel to the base of the upper bulkhead panel using a bulkhead coupling member, inserting the terminal end through the slot opening, and connecting the terminal end to the secondary support member behind the overhead closeout panel.
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公开(公告)号：US20230234695A1
公开(公告)日：2023-07-27
申请号：US17582478
申请日：2022-01-24
Applicant: The Boeing Company
Inventor： Steven Ellis Rhynard , Joe Files
CPC classification number: B64C1/10 , B64D11/0023
Abstract: A bulkhead assembly for an aircraft passenger cabin having a floor and a secondary support member includes upper and lower bulkhead panels and a bulkhead coupling member. The upper bulkhead panel defines an elongated tower portion that protrudes through a slot opening in an overhead closeout panel, and directly or indirectly connects to the secondary support member. The lower bulkhead panel connects to the upper bulkhead panel and to the floor via the bulkhead coupling member. A method for installing the bulkhead assembly in the passenger cabin includes connecting the lower bulkhead panel to the floor, joining the lower bulkhead panel to the base of the upper bulkhead panel using a bulkhead coupling member, inserting the terminal end through the slot opening, and connecting the terminal end to the secondary support member behind the overhead closeout panel.
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Patent Agency Ranking
公开(公告)号：US20230150673A1
公开(公告)日：2023-05-18
申请号：US17527493
申请日：2021-11-16
Applicant: The Boeing Company
Inventor： Steven Ellis Rhynard , Joe Files
CPC classification number: B64D11/003 , B64C7/00
Abstract: An assembly configured to be mounted within an interior of a vehicle. The assembly includes a monument wall configured to be mounted in the interior of the vehicle. A panel is configured to attach to a support structure above the monument wall with the panel having a first edge and a second edge. A latch configured to be mounted to the panel between the first edge and the second edge. A pull member is attached to the panel and comprises an elongated member attached to the latch and a handle. A translating hinge is configured to be mounted to the second edge of the panel to provide for translating and pivoting movement of the panel within an access area between the monument wall and the support structure to connect and disconnect the panel from the support structure.
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公开(公告)号：US20230150644A1
公开(公告)日：2023-05-18
申请号：US17527633
申请日：2021-11-16
Applicant: The Boeing Company
Inventor： Adam Arthur Logue , Jeffrey Allen Cartwright , Steven Ellis Rhynard , Joe Files
IPC: B64C1/06
CPC classification number: B64C1/066
Abstract: A panel assembly for an overhead support structure of a vehicle. The panel assembly includes a panel movable relative to the overhead support structure between a stowed position and an open position. One or more actuators release the panel from the stowed position. The actuators include first and second bodies arranged together and configured to move relative to each other and with the first body movable relative to the overhead support structure between first and second positions. The first position orients the second body at a first angular position relative to the overhead support structure that engages a catch on the second body with a latch pin. The second position orients the second body at a different second angular position relative to the overhead support structure to release the catch from the latch pin and thereby release the panel from the stowed position.
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8.发明申请OXYGEN BOX FOR A LIMITED MAINTENANCE ACCESS AREA ABOVE A CEILING PANEL OF AN AIRCRAFT CABIN 审中-公开氧气盒有限维护接触区上方飞机舱的天花板公开(公告)号：US20170073072A1
公开(公告)日：2017-03-16
申请号：US14851188
申请日：2015-09-11
Applicant: The Boeing Company
Inventor： Joe Files , Adam Arthur Logue , Meiling Chi , Steven Ellis Phynard , Lance Smithson
CPC classification number: B64D11/00 , A62B18/02 , A62B25/005 , B64D2231/025
Abstract: An oxygen box is secured in an oxygen box hole through a panel of an aircraft cabin by fasteners that are positioned in an interior volume of the oxygen box and are inserted through holes in a back wall of the oxygen box that are aligned with fastener openings in an exterior bracket positioned behind the panel and behind the oxygen box opening where the fasteners are received by the fastener openings in the exterior bracket and the fasteners removably attach the oxygen box to the exterior bracket.
Abstract translation: 氧气箱通过位于氧气箱的内部容积中的紧固件通过飞机机舱的面板固定在氧气箱孔中，并且通过与氧气箱的后壁中的孔对准地插入，该孔与紧固件开口对准 位于面板后面的氧气箱开口后面的外部支架，其中紧固件由外部支架中的紧固件开口接收，并且紧固件将氧气盒可拆卸地附接到外部支架。
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公开(公告)号：US20240212883A1
公开(公告)日：2024-06-27
申请号：US18087106
申请日：2022-12-22
Applicant: The Boeing Company
Inventor： Joe Files , Jeffrey Cartwright , Steven Ellis Rhynard
IPC: H01B7/40 , F21V23/00 , H02G15/007
CPC classification number: H01B7/40 , F21V23/001 , H02G15/007 , B64D2221/00 , F21W2107/30
Abstract: A connector to support wiring and space the wiring away from a housing. The connector includes a saddle that receives the wiring. A clip is attached to the saddle and attaches to the housing. The saddle and the clip are sized to secure the wiring to the housing. The size of the saddle and the clip spaces the wiring away from the housing to prevent the wiring from contacting the housing and potentially being damaged.
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公开(公告)号：US11780584B2
公开(公告)日：2023-10-10
申请号：US17527493
申请日：2021-11-16
Applicant: The Boeing Company
Inventor： Steven Ellis Rhynard , Joe Files
CPC classification number: B64D11/003 , B64C7/00
Abstract: An assembly configured to be mounted within an interior of a vehicle. The assembly includes a monument wall configured to be mounted in the interior of the vehicle. A panel is configured to attach to a support structure above the monument wall with the panel having a first edge and a second edge. A latch configured to be mounted to the panel between the first edge and the second edge. A pull member is attached to the panel and comprises an elongated member attached to the latch and a handle. A translating hinge is configured to be mounted to the second edge of the panel to provide for translating and pivoting movement of the panel within an access area between the monument wall and the support structure to connect and disconnect the panel from the support structure.
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