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公开(公告)号：US11565814B2
公开(公告)日：2023-01-31
申请号：US17485884
申请日：2021-09-27
Applicant: B/E Aerospace, Inc.
Inventor： Travis J. Vaninetti , Jefferey M. McKee , Justin C. Christenson , Shawn A. Claflin
Abstract: A slim aircraft monument is installable in an aircraft cabin adjacent to an aisle and has an upper portion, a lower portion, and a middle portion between the upper and lower portions. The monument includes a storage compartment accessible from a first side and a door on an adjacent side, the door deployable into the adjacent aisle or cabin space to reveal folding interconnected panels also deployable into the cabin space. The interconnected panels unfold into a horizontal workspace and, beneath the workspace, a series of vertically stacked storage bays capable of accommodating storage drawers and a cart bay configured for temporary accommodation of a half-size galley cart.
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公开(公告)号：US10422169B2
公开(公告)日：2019-09-24
申请号：US15943765
申请日：2018-04-03
Applicant: B/E Aerospace, Inc.
Inventor： Justin C. Christenson , Charles F. Forster
Abstract: A flexible hinge assembly for aircraft interior components and the like, including: a first structural component, wherein the first structural component includes a core material and one or more skin layers coupled to the core material; a second structural component, wherein the second structural component includes a core material and one or more skin layers coupled to the core material; wherein the one or more skin layers of the first structural component and the one or more skin layers of the second structural component are one or more of coupled together and integrally formed; and a flexure disposed between the first structural component and the second structural component, wherein the flexure is formed by the coupled together and/or integrally formed skin layers.
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公开(公告)号：US20160009357A1
公开(公告)日：2016-01-14
申请号：US14754620
申请日：2015-06-29
Applicant: B/E Aerospace, Inc.
Inventor： Justin C. Christenson , Graydon E. Loar
CPC classification number: B64C1/1423 , B64C1/1407 , B64D11/02 , E05D15/58 , E05F17/00 , E05Y2800/122 , E06B3/5009
Abstract: A telescoping aircraft door is disclosed having first and second panels that slide relative to one another to extend and retract as the door closes and opens, respectively. The first panel is hinged to the door frame in a traditional manner, and the second panel is fixed to the door frame by a linkage that limits the arc of the second panel. By selecting the location and length of the linkage, the relative movement of the two panels can be predictably controlled to reduce the depth of the door when closed and the length of the door when opened.
Abstract translation: 公开了一种伸缩式飞机门，其具有分别相对于彼此滑动的第一和第二面板，以在门关闭和打开时分别延伸和缩回。 第一面板以传统的方式铰接到门框，并且第二面板通过限制第二面板的弧的连杆固定到门框。 通过选择连杆的位置和长度，可以可预测地控制两个面板的相对运动，以在关闭时减小门的深度，并且在打开时减小门的长度。
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公开(公告)号：US11130575B2
公开(公告)日：2021-09-28
申请号：US16408935
申请日：2019-05-10
Applicant: B/E Aerospace, Inc.
Inventor： Travis J. Vaninetti , Jefferey M. McKee , Justin C. Christenson , Shawn A. Claflin
Abstract: A slim aircraft monument includes a structure installable in an aircraft passenger cabin adjacent to a cabin space (e.g., in front of an otherwise unused exit door). The slim monument has an overall width of not more than four to six inches. The slim monument includes a side door with an external handle, the door deployable into the cabin space to reveal a group of nested interconnected panels within. The nested panels are similarly deployable into the cabin space to form a substantially horizontal work surface and, underneath the work surface, vertically stacked bays providing temporary storage for storage drawers and a cart space adjacent to the storage drawers, the cart space capable of accommodating a half-size galley cart.
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公开(公告)号：US10907400B2
公开(公告)日：2021-02-02
申请号：US15978705
申请日：2018-05-14
Applicant: B/E Aerospace, Inc.
Inventor： Justin C. Christenson
Abstract: In a preferred embodiment, a telescoping panel door for an aircraft compartment includes a first panel configured for hinged connection to a surface of a door frame, a second panel, and a linkage fixing a distance that the second panel can extend from the door frame, where the second panel is configured for connection to the door frame via the linkage. The door operates such that, in a closed position, the second panel is extended from an interior of the first panel, the first and second panels cooperate to completely cover an opening defined by the door frame, and the linkage is generally parallel to the plane defined by the door frame. In an open position, the second panel is retracted into the interior of the first panel by operation of the linkage and the first and second panels are nested to reduce a distanced spanned by the panels.
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Patent Agency Ranking
公开(公告)号：US10900577B2
公开(公告)日：2021-01-26
申请号：US15942799
申请日：2018-04-02
Applicant: B/E Aerospace, Inc.
Inventor： Justin C. Christenson
Abstract: A valve assembly for mixing water from hot and cold water sources to obtain water at a resulting intermediate temperature that is suitable for hand washing or the like, including: a housing defining an internal fluid flow channel in fluid communication with a hot water inlet port that selectively supplies a hot water flow to the internal fluid flow channel and a cold water inlet port that selectively supplies a cold water flow to the internal fluid flow channel; and a valve member disposed within the internal fluid flow channel operable for simultaneously partially or wholly obstructing the hot water flow from the hot water inlet port to the internal fluid flow channel and the cold water flow from the cold water inlet port to the internal fluid flow channel such that each contributes a predetermined proportional water flow to the internal fluid flow channel.
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公开(公告)号：US20220009634A1
公开(公告)日：2022-01-13
申请号：US17485884
申请日：2021-09-27
Applicant: B/E Aerospace, Inc.
Inventor： Travis J. Vaninetti , Jefferey M. McKee , Justin C. Christenson , Shawn A. Claflin
Abstract: A slim aircraft monument is installable in an aircraft cabin adjacent to an aisle and has an upper portion, a lower portion, and a middle portion between the upper and lower portions. The monument includes a storage compartment accessible from a first side and a door on an adjacent side, the door deployable into the adjacent aisle or cabin space to reveal folding interconnected panels also deployable into the cabin space. The interconnected panels unfold into a horizontal workspace and, beneath the workspace, a series of vertically stacked storage bays capable of accommodating storage drawers and a cart bay configured for temporary accommodation of a half-size galley cart.
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公开(公告)号：US20180258686A1
公开(公告)日：2018-09-13
申请号：US15978705
申请日：2018-05-14
Applicant: B/E Aerospace, Inc.
Inventor： Justin C. Christenson
CPC classification number: E06B3/5009 , B64C1/1423 , B64D11/00 , E05D15/58 , E05F17/00 , E05Y2800/122 , E06B3/5045 , E06B3/921 , E06B5/00
Abstract: In a preferred embodiment, a telescoping panel door for an aircraft compartment includes a first panel configured for hinged connection to a surface of a door frame, a second panel, and a linkage fixing a distance that the second panel can extend from the door frame, where the second panel is configured for connection to the door frame via the linkage. The door operates such that, in a closed position, the second panel is extended from an interior of the first panel, the first and second panels cooperate to completely cover an opening defined by the door frame, and the linkage is generally parallel to the plane defined by the door frame. In an open position, the second panel is retracted into the interior of the first panel by operation of the linkage and the first and second panels are nested to reduce a distanced spanned by the panels.
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公开(公告)号：US10099768B2
公开(公告)日：2018-10-16
申请号：US15234684
申请日：2016-08-11
Applicant: B/E Aerospace, Inc.
Inventor： Justin C. Christenson , Graydon E. Loar
Abstract: A telescoping aircraft door is disclosed having first and second panels that slide relative to one another to extend and retract as the door closes and opens, respectively. The first panel is hinged to the door frame in a traditional manner, and the second panel is fixed to the door frame by a linkage that limits the arc of the second panel. By selecting the location and length of the linkage, the relative movement of the two panels can be predictably controlled to reduce the depth of the door when closed and the length of the door when opened.
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公开(公告)号：US09976336B2
公开(公告)日：2018-05-22
申请号：US15406690
申请日：2017-01-14
Applicant: B/E AEROSPACE, INC.
Inventor： Justin C. Christenson
CPC classification number: E06B3/5009 , B64C1/1423 , B64D11/00 , E05D15/58 , E05F17/00 , E05Y2800/122 , E06B3/5045 , E06B3/921
Abstract: In a preferred embodiment, a telescoping panel door for an aircraft compartment includes a first panel configured for hinged connection to a surface of a door frame, a second panel, and a linkage fixing a distance that the second panel can extend from the door frame, where the second panel is configured for connection to the door frame via the linkage. The door operates such that, in a closed position, the second panel is extended from an interior of the first panel, the first and second panels cooperate to completely cover an opening defined by the door frame, and the linkage is generally parallel to the plane defined by the door frame. In an open position, the second panel is retracted into the interior of the first panel by operation of the linkage and the first and second panels are nested to reduce a distanced spanned by the panels.
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