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公开(公告)号:USD920892S1
公开(公告)日:2021-06-01
申请号:US29695051
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:US10414480B2
公开(公告)日:2019-09-17
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:US20160069122A1
公开(公告)日:2016-03-10
申请号:US14942966
申请日:2015-11-16
Applicant: The Boeing Company
Inventor: Gregory A. Tubbs
CPC classification number: E06B3/5072 , B64D11/02 , E04B2/7407 , E05D15/26 , E06B3/34 , E06B3/48 , E06B3/481 , E06B3/486 , E06B3/5054 , E06B7/28 , E06B2003/343
Abstract: The present disclosure is generally directed to a method of operation for a convertible door system including a door accessible compartment having a moveable dividing wall that substantially divides the compartment into a first and a second sub-compartment. A first door assembly, configured to allow access to the first sub-compartment, is disposed between a first of two opposing sidewalls and the moveable dividing wall. A second door assembly, configured to allow access to the second sub-compartment, is disposed between a second of the two opposing sidewalls and the moveable dividing wall. A first and a second hinge assembly are adapted to rotationally join the first and second door assembly to respective opposing sidewalls. A third hinge assembly is adapted to rotationally join the moveable dividing wall to either the first door assembly or the second door assembly.
Abstract translation: 本公开总体上涉及一种用于可转换门系统的操作方法,该可转换门系统包括具有可移动分隔壁的门可接近室,其基本上将隔室分成第一和第二子隔室。 构造成允许进入第一子隔间的第一门组件设置在两个相对侧壁中的第一侧壁和可移动分隔壁之间。 构造成允许进入第二子隔间的第二门组件设置在两个相对的侧壁中的第二侧壁和可移动分隔壁之间。 第一和第二铰链组件适于将第一和第二门组件旋转地连接到相应的相对侧壁。 第三铰链组件适于将可移动分隔壁旋转地连接到第一门组件或第二门组件。
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公开(公告)号:US08752339B1
公开(公告)日:2014-06-17
申请号:US13666286
申请日:2012-11-01
Applicant: The Boeing Company
Inventor: Gregory A. Tubbs
IPC: E04B1/346
CPC classification number: E06B3/5072 , B64D11/02 , E04B2/7407 , E05D15/26 , E06B3/34 , E06B3/48 , E06B3/481 , E06B3/486 , E06B3/5054 , E06B7/28 , E06B2003/343
Abstract: The present disclosure is generally directed to a system and method of operation for a convertible door system including a door accessible compartment having a moveable dividing wall that substantially divides the compartment into a first and a second sub-compartment. A first door assembly, configured to allow access to the first sub-compartment, is disposed between a first of two opposing sidewalls and the moveable dividing wall. A second door assembly, configured to allow access to the second sub-compartment, is disposed between a second of the two opposing sidewalls and the moveable dividing wall. A first and a second hinge assembly are adapted to rotationally join the first and second door assembly to respective opposing sidewalls. A third hinge assembly is adapted to rotationally join the moveable dividing wall to either the first door assembly or the second door assembly.
Abstract translation: 本公开总体上涉及一种用于可转换门系统的系统和操作方法,该系统和方法包括具有可移动分隔壁的门可接近室,其基本上将隔室分成第一和第二子隔室。 构造成允许进入第一子隔间的第一门组件设置在两个相对侧壁中的第一侧壁和可移动分隔壁之间。 构造成允许进入第二子隔间的第二门组件设置在两个相对的侧壁中的第二侧壁和可移动分隔壁之间。 第一和第二铰链组件适于将第一和第二门组件旋转地连接到相应的相对侧壁。 第三铰链组件适于将可移动分隔壁旋转地连接到第一门组件或第二门组件。
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公开(公告)号:USD1012815S1
公开(公告)日:2024-01-30
申请号:US29694695
申请日:2019-06-12
Applicant: The Boeing Company
Designer: Gregory A. Tubbs , Phillip E. Pacini
Abstract: FIG. 1 is a front perspective view of an air grille panel showing our new design in an aircraft sidewall panel assembly environment;
FIG. 2 is a back perspective view of the air grille panel of FIG. 1 in the aircraft sidewall panel assembly environment;
FIG. 3 is a front elevational view of the air grille panel of FIG. 1;
FIG. 4 is a back elevational view of the air grille panel of FIG. 3;
FIG. 5 is a left side elevational view of the air grille panel of FIG. 3; and,
FIG. 6 is a right side elevational view of the air grille panel of FIG. 3.
The broken lines in the drawings depict portions of the air grille panel that form no part of the claimed design. The dash-dot lines shown in FIGS. 1-6 depict the bounds of the claimed design and neither the dash-dot lines, nor the surface within or between the dash-dot boundary form part of the claimed design. The additional elements shown in broken lines in FIGS. 1-2 depict environmental subject matter only and form no part thereof.-
公开(公告)号:USD921570S1
公开(公告)日:2021-06-08
申请号:US29695041
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:US09187950B1
公开(公告)日:2015-11-17
申请号:US14274107
申请日:2014-05-09
Applicant: The Boeing Company
Inventor: Gregory A. Tubbs
CPC classification number: E06B3/5072 , B64D11/02 , E04B2/7407 , E05D15/26 , E06B3/34 , E06B3/48 , E06B3/481 , E06B3/486 , E06B3/5054 , E06B7/28 , E06B2003/343
Abstract: The present disclosure is generally directed to a system and method of operation for a convertible door system including a door accessible compartment having a moveable dividing wall that substantially divides the compartment into a first and a second sub-compartment. A first door assembly, configured to allow access to the first sub-compartment, is disposed between a first of two opposing sidewalls and the moveable dividing wall. A second door assembly, configured to allow access to the second sub-compartment, is disposed between a second of the two opposing sidewalls and the moveable dividing wall. A first and a second hinge assembly are adapted to rotationally join the first and second door assembly to respective opposing sidewalls. A third hinge assembly is adapted to rotationally join the moveable dividing wall to either the first door assembly or the second door assembly.
Abstract translation: 本公开总体上涉及一种用于可转换门系统的系统和操作方法,该系统和方法包括具有可移动分隔壁的门可接近室,其基本上将隔室分成第一和第二子隔室。 构造成允许进入第一子隔间的第一门组件设置在两个相对侧壁中的第一侧壁和可移动分隔壁之间。 构造成允许进入第二子隔间的第二门组件设置在两个相对的侧壁中的第二侧壁和可移动分隔壁之间。 第一和第二铰链组件适于将第一和第二门组件旋转地连接到相应的相对侧壁。 第三铰链组件适于将可移动分隔壁旋转地连接到第一门组件或第二门组件。
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公开(公告)号:US20230166826A1
公开(公告)日:2023-06-01
申请号:US17818056
申请日:2022-08-08
Applicant: THE BOEING COMPANY
Inventor: Russell W. Keck , Gregory A. Tubbs
Abstract: An assembly for use in a vehicle cabin includes a floor coupling structure and a sidewall coupling structure. The floor coupling structure includes a floor interface portion and a sidewall interface portion that extends transversely relative to the floor interface portion. The floor interface portion is configured to attach the floor coupling structure to a floor assembly of an internal cabin of a vehicle. The sidewall coupling structure has at least one friction-fit portion and a sidewall attachment section. The sidewall attachment section is configured to couple the sidewall coupling structure to a sidewall assembly of the internal cabin. The at least one friction-fit portion is configured to couple to the sidewall interface portion of the floor coupling structure.
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公开(公告)号:US11362494B2
公开(公告)日:2022-06-14
申请号:US16459531
申请日:2019-07-01
Applicant: The Boeing Company
Inventor: Colin R. Kreiger , Alexander J. Matsuoka , Derrick B. Pruitt , Michael E. Frick , Gregory A. Tubbs
Abstract: There is provided a raceway cover assembly for installing conductive element(s) in an aircraft. The raceway cover assembly includes a raceway cover for removable coupling to a raceway. The raceway is configured for attachment to a sidewall assembly for use in a cabin of the aircraft. The raceway cover includes a first cover side, a second cover side, and retaining element(s) disposed on the first cover side. The raceway cover assembly further includes the conductive element(s) coupled and retained to the first cover side, with the retaining element(s), to form the raceway cover assembly. The conductive element(s) and the raceway cover are assembled together at a location off of the aircraft, prior to installing the raceway cover assembly with the one or more conductive elements in the aircraft, which allows for routing of the one or more conductive elements in the raceway cover at the location off of the aircraft.
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公开(公告)号:USD921569S1
公开(公告)日:2021-06-08
申请号:US29695040
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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