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公开(公告)号：US20210031922A1
公开(公告)日：2021-02-04
申请号：US16527733
申请日：2019-07-31
Applicant: THE BOEING COMPANY
Inventor： Kevin Cassou , Gregory A. Tubbs
Abstract: A vehicle includes an interior cabin, a primary structure within the interior cabin, a plurality of securing mounts having first ends directly coupled to the primary structure, and second ends, and an overhead support platform system directly coupled to the second ends of the plurality of securing mounts. The overhead support platform system includes at least one adapter rail having a plurality of commodity mounts. At least one commodity is directly coupled to the overhead support platform system. The commodity is adaptively secured to one or more of the plurality of commodity mounts.
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公开(公告)号：US20190071162A1
公开(公告)日：2019-03-07
申请号：US16177006
申请日：2018-10-31
Applicant: The Boeing Company
Inventor： Cory M. Hitchcock , Thomas S. Perkins , Erik Ivar Wiman , Gregory A. Tubbs
Abstract: Systems and methods are provided for securing aircraft sidewall. One embodiment comprises a hanger for supporting sections of sidewall for an aircraft. The hanger includes an elongated vertical member that attaches to a frame of the aircraft, and sets of keyholes that are each arranged in a vertical pattern along the member and that are each configured to support a corresponding section of sidewall of the aircraft. Each keyhole includes a receptacle dimensioned to receive a fitting from a section of sidewall, and a slot dimensioned to slidably accept the fitting via the receptacle to secure the fitting in place. The slot size of keyholes in each set varies from one end of the vertical pattern to another end of the vertical pattern.
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公开(公告)号：US10137975B2
公开(公告)日：2018-11-27
申请号：US15091962
申请日：2016-04-06
Applicant: The Boeing Company
Inventor： Cory M. Hitchcock , Thomas S. Perkins , Erik Ivar Wiman , Gregory A. Tubbs
Abstract: Systems and methods are provided for securing aircraft sidewall. One embodiment comprises a hanger for supporting sections of sidewall for an aircraft. The hanger includes an elongated vertical member that attaches to a frame of the aircraft, and sets of keyholes that are each arranged in a vertical pattern along the member and that are each configured to support a corresponding section of sidewall of the aircraft. Each keyhole includes a receptacle dimensioned to receive a fitting from a section of sidewall, and a slot dimensioned to slidably accept the fitting via the receptacle to secure the fitting in place. The slot size of keyholes in each set varies from one end of the vertical pattern to another end of the vertical pattern.
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公开(公告)号：US11548613B2
公开(公告)日：2023-01-10
申请号：US16455724
申请日：2019-06-27
Applicant: The Boeing Company
Inventor： Gregory A. Tubbs , Phillip E. Pacini
Abstract: There is provided an air grille panel assembly for a vehicle. The assembly includes an air grille panel having air grille openings, a top end, and a bottom end. The top end is configured for coupling to a sidewall panel in a cabin of the vehicle. The bottom end is configured for coupling to a raceway assembly on a floor in the cabin. The assembly further includes a frame member disposed around a perimeter of each of the air grille openings, to define each of the air grille openings, an air grille coupled to the frame member and covering each of the air grille openings, and a cover member releasably attached to the air grille. The assembly is configured for coupling to the sidewall panel, via a float attachment, that allows for a vertical adjustment, to accommodate different installed positions of the assembly in the cabin of the vehicle.
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公开(公告)号：US11034429B2
公开(公告)日：2021-06-15
申请号：US16112068
申请日：2018-08-24
Applicant: The Boeing Company
Inventor： Gregory A. Tubbs , Paul J. Wilcynski
Abstract: Disclosed herein is an example ceiling header system for an aircraft cabin that includes a ceiling between a first storage bin and a second storage bin. The ceiling header system includes a ceiling header that includes a top surface that conforms to the ceiling and a bottom surface that is opposite the top surface. The ceiling header system also includes a curtain track. The top surface is configured to be held against the ceiling via the curtain track being placed against the bottom surface, the curtain track being (i) attachable at a first end of the curtain track to a first rail of the first storage bin and (ii) attachable at a second end of the curtain track to a second rail of the second storage bin.
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Patent Agency Ranking
公开(公告)号：USD920891S1
公开(公告)日：2021-06-01
申请号：US29695043
申请日：2019-06-14
Applicant: The Boeing Company
Designer： Gregory A. Tubbs , Kevin Cassou , David A. Young , Trevis Kurz , Franco M. Cagnina , Gary E. Liljebeck , Adam Boroughs
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公开(公告)号：USD920890S1
公开(公告)日：2021-06-01
申请号：US29695042
申请日：2019-06-14
Applicant: The Boeing Company
Designer： Gregory A. Tubbs , Kevin Cassou , David A. Young , Trevis Kurz , Franco M. Cagnina , Gary E. Liljebeck , Adam Boroughs
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公开(公告)号：US20200062370A1
公开(公告)日：2020-02-27
申请号：US16112068
申请日：2018-08-24
Applicant: The Boeing Company
Inventor： Gregory A. Tubbs , Paul J. Wilcynski
Abstract: Disclosed herein is an example ceiling header system for an aircraft cabin that includes a ceiling between a first storage bin and a second storage bin. The ceiling header system includes a ceiling header that includes a top surface that conforms to the ceiling and a bottom surface that is opposite the top surface. The ceiling header system also includes a curtain track. The top surface is configured to be held against the ceiling via the curtain track being placed against the bottom surface, the curtain track being (i) attachable at a first end of the curtain track to a first rail of the first storage bin and (ii) attachable at a second end of the curtain track to a second rail of the second storage bin.
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公开(公告)号：US10220931B2
公开(公告)日：2019-03-05
申请号：US14935788
申请日：2015-11-09
Applicant: THE BOEING COMPANY
Inventor： Thomas Seth Perkins , Cory Michael Hitchcock , John Erik West , Adam R. Weston , Gregory A. Tubbs
Abstract: A return air bridge for use in an aircraft assembly includes an inboard portion configured to couple to a sidewall assembly at a bottom edge of the sidewall assembly and an outboard portion configured to couple to a structural member. The return air bridge also includes at least one support coupling the inboard portion to the outboard portion such that a return air flow path is defined between the inboard portion and the outboard portion. The outboard portion comprises a plate configured to direct an air flow along the return air flow path upwardly with respect to the bottom edge of the sidewall assembly.
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公开(公告)号：US20170291676A1
公开(公告)日：2017-10-12
申请号：US15091962
申请日：2016-04-06
Applicant: The Boeing Company
Inventor： Cory M. Hitchcock , Thomas S. Perkins , Erik Ivar Wiman , Gregory A. Tubbs
IPC: B64C1/06
Abstract: Systems and methods are provided for securing aircraft sidewall. One embodiment comprises a hanger for supporting sections of sidewall for an aircraft. The hanger includes an elongated vertical member that attaches to a frame of the aircraft, and sets of keyholes that are each arranged in a vertical pattern along the member and that are each configured to support a corresponding section of sidewall of the aircraft. Each keyhole includes a receptacle dimensioned to receive a fitting from a section of sidewall, and a slot dimensioned to slidably accept the fitting via the receptacle to secure the fitting in place. The slot size of keyholes in each set varies from one end of the vertical pattern to another end of the vertical pattern.
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