公开(公告)号：US11753166B2

公开(公告)日：2023-09-12

申请号：US17527394

申请日：2021-11-16

Applicant: The Boeing Company

Inventor： Joe Files ,  Steven Ellis Rhynard ,  Daniel Paul Warren ,  John Charles Rand

IPC: B64D11/00

CPC classification number: B64D11/003 ,  B64D11/0015

Abstract: An assembly for an interior of a vehicle with the assembly having a monument wall configured to mount to the interior of the vehicle. A panel is configured to mount to an overhead support structure adjacent to the monument wall. The panel includes a front side configured to face into the interior of the vehicle and an opposing back side. One or more latch assemblies are configured to connect the panel to the overhead support structure adjacent to the monument wall. The latch assemblies include a latch mounted to the back side of the panel, a track with one or more rails, a follower with an arm and a head with the head sized to engage with the track, and a pull mechanism to unlock the latch.

公开(公告)号：US20230150672A1

公开(公告)日：2023-05-18

申请号：US17527394

申请日：2021-11-16

Applicant: The Boeing Company

Inventor： Joe Files ,  Steven Ellis Rhynard ,  Daniel Paul Warren ,  John Charles Rand

IPC: B64D11/00

CPC classification number: B64D11/003 ,  B64D11/0015

Abstract: An assembly for an interior of a vehicle with the assembly having a monument wall configured to mount to the interior of the vehicle. A panel is configured to mount to an overhead support structure adjacent to the monument wall. The panel includes a front side configured to face into the interior of the vehicle and an opposing back side. One or more latch assemblies are configured to connect the panel to the overhead support structure adjacent to the monument wall. The latch assemblies include a latch mounted to the back side of the panel, a track with one or more rails, a follower with an arm and a head with the head sized to engage with the track, and a pull mechanism to unlock the latch.

公开(公告)号：US20210237902A1

公开(公告)日：2021-08-05

申请号：US16778712

申请日：2020-01-31

Applicant: The Boeing Company

Inventor： Joe Files ,  Jeffrey Allen Cartwright ,  Adam Arthur Logue ,  Robert B. Fowler

IPC: B64F5/10

Abstract: An assembly to connect a panel to a support member. The assembly may include a saddle fitting configured to connect to the support member and including first and second plates. A back fitting may be positioned between the second plate of the saddle fitting and a second face of the panel. An index fitting includes a flange that may be positioned between the first plate of the saddle fitting and a first face of the panel, and a boss that extends outward from the flange and through the opening in the panel. The index fitting is wider than the panel and sized to fit within the gap of the saddle fitting with a first end of the index fitting contacting against the first plate and a second end of the index fitting contacting against the second plate. One or more fasteners may connect the saddle fitting to the index fitting.

公开(公告)号：US10239617B2

公开(公告)日：2019-03-26

申请号：US14851188

申请日：2015-09-11

Applicant: The Boeing Company

Inventor： Joe Files ,  Adam Arthur Logue ,  Meiling Chi ,  Steven Ellis Rhynard ,  Lance Smithson

IPC: B64D11/00 ,  A62B25/00 ,  A62B18/02

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.

公开(公告)号：US12300407B2

公开(公告)日：2025-05-13

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 ,  F21W107/30

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.

公开(公告)号：US11987342B2

公开(公告)日：2024-05-21

申请号：US17517917

申请日：2021-11-03

Applicant: The Boeing Company

Inventor： Steven Ellis Rhynard ,  Joe Files ,  Randall Vincent Fraker ,  Andrew P. Keleher ,  Thomas Leonard LeBlanc

IPC: B64D11/00 ,  B64C1/14

CPC classification number: B64C1/1407 ,  B64D11/00

Abstract: Crew egress pathways and crew egress pathway exits in aircraft, with the crew egress pathway exits comprising apparatuses, systems, and methods for reliable deployment and stowage of support straps within crew egress pathway exit hatches positioned, with crew egress pathway exit hatches configured to deploy within aircraft passenger compartments in aircraft.

公开(公告)号：US20240076027A1

公开(公告)日：2024-03-07

申请号：US17929088

申请日：2022-09-01

Applicant: The Boeing Company

Inventor： Joe Files ,  Adam A. Logue ,  Robert B. Fowler ,  Steven E. Rhynard ,  Jeffrey A. Cartwright

IPC: B64C1/06 ,  B60Q3/43 ,  B64D13/06

CPC classification number: B64C1/068 ,  B60Q3/43 ,  B64C1/061 ,  B64D13/06 ,  B64D2013/0603

Abstract: A support box apparatus includes longitudinal members that span forward to aft and transverse members that span inboard to outboard between the longitudinal members. The longitudinal members and the transverse members are formed of composite honeycomb sandwich panels. The support box apparatus also includes attachment components configured to couple the longitudinal members or the transverse members to structural components of an aircraft, electrical wiring attached to the longitudinal members or the transverse members, environmental control system (ECS) ducting attached to the longitudinal members or the transverse members, and life support lines attached to the longitudinal members or the transverse members.

公开(公告)号：US11851185B2

公开(公告)日：2023-12-26

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.

公开(公告)号：US20230391440A1

公开(公告)日：2023-12-07

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 ,  B64D11/00 ,  B64F5/10

CPC classification number: B64C1/061 ,  B64D11/00 ,  B64F5/10

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.

公开(公告)号：US20230140351A1

公开(公告)日：2023-05-04

申请号：US17517917

申请日：2021-11-03

Applicant: The Boeing Company

Inventor： Steven Ellis Rhynard ,  Joe Files ,  Randall Vincent Fraker ,  Andrew P. Keleher ,  Thomas Leonard LeBlanc

IPC: B64C1/14 ,  B64D11/00

Abstract: Crew egress pathways and crew egress pathway exits in aircraft, with the crew egress pathway exits comprising apparatuses, systems, and methods for reliable deployment and stowage of support straps within crew egress pathway exit hatches positioned, with crew egress pathway exit hatches configured to deploy within aircraft passenger compartments in aircraft.