-
公开(公告)号：US20210245859A1
公开(公告)日：2021-08-12
申请号：US16787129
申请日：2020-02-11
Applicant: THE BOEING COMPANY
Inventor： Thomas Seth Perkins , Xiaoxi Wang
Abstract: A panel assembly (such as for an internal cabin of an aircraft) includes at least one liquid flow path formed on at least one surface through surface treatment. The at least one liquid flow path is formed in relation to at least one bank on the at least one surface. The at least one liquid flow path is configured to divert liquid to a desired location.
-
公开(公告)号：USD908054S1
公开(公告)日：2021-01-19
申请号：US29674060
申请日：2018-12-19
Applicant: The Boeing Company
Designer： Thomas Seth Perkins , Adam R. Weston
-
公开(公告)号：US20170129581A1
公开(公告)日：2017-05-11
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
CPC classification number: B64C1/066 , B64C1/40 , B64C2001/009 , Y02T50/46
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.
-
公开(公告)号：US12269574B2
公开(公告)日：2025-04-08
申请号：US16787115
申请日：2020-02-11
Applicant: THE BOEING COMPANY
Inventor： Xiaoxi Wang , Thomas Seth Perkins
Abstract: A method includes providing a structure having a surface, treating a portion of the surface to modify a wettability of the portion of the structure, and forming at least one liquid flow path on the surface through said treating.
-
公开(公告)号：US20210245858A1
公开(公告)日：2021-08-12
申请号：US16787115
申请日：2020-02-11
Applicant: THE BOEING COMPANY
Inventor： Xiaoxi Wang , Thomas Seth Perkins
Abstract: A method includes providing a structure having a surface, treating a portion of the surface to modify a wettability of the portion of the structure, and forming at least one liquid flow path on the surface through said treating.
-
Patent Agency Ranking
公开(公告)号：US10926860B2
公开(公告)日：2021-02-23
申请号：US16225208
申请日：2018-12-19
Applicant: The Boeing Company
Inventor： Thomas Seth Perkins , Adam R. Weston
Abstract: A decompression panel assembly for use in an aircraft includes a body panel having an opening defined therein and a cover panel positioned within the opening and spaced from the body panel. The decompression panel assembly also includes an annular spacer panel positioned outboard from the cover panel and the body panel. The spacer panel is spaced from the cover panel to define a first annular flow path between the cover panel and the spacer panel, and the spacer panel is spaced from the body panel to define a second annular flow path between the body panel and the spacer panel.
-
公开(公告)号：US12275520B2
公开(公告)日：2025-04-15
申请号：US16787129
申请日：2020-02-11
Applicant: THE BOEING COMPANY
Inventor： Thomas Seth Perkins , Xiaoxi Wang
Abstract: A panel assembly (such as for an internal cabin of an aircraft) includes at least one liquid flow path formed on at least one surface through surface treatment. The at least one liquid flow path is formed in relation to at least one bank on the at least one surface. The at least one liquid flow path is configured to divert liquid to a desired location.
-
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.
-
9.发明授权公开(公告)号：US09440744B2
公开(公告)日：2016-09-13
申请号：US14228554
申请日：2014-03-28
Applicant: THE BOEING COMPANY
Inventor： Thomas Seth Perkins , Allan A. Loken , Robert J. Christian , James Pease , Sara Beth Cromyak
CPC classification number: B64D13/00 , B64C1/18 , B64C2001/009
Abstract: Decompression panel assemblies and methods of equalizing air pressure differential are provided. The decompression panel assembly includes a panel comprising an opening defined therein, a vent cover coupled across the opening, and a latching mechanism. The vent cover is configured to move between a first position and a second position. The latching mechanism is configured to maintain the vent cover in the first position when a pressure differential across the panel is below a predetermined value and facilitate the vent cover moving to the second position when the pressure differential across the panel exceeds the predetermined value.
Abstract translation: 提供减压板组件和均压气压差的方法。 减压面板组件包括包括限定在其中的开口的面板，跨过开口连接的通气盖以及闭锁机构。 通气盖构造成在第一位置和第二位置之间移动。 闭锁机构构造成当跨越面板的压差低于预定值时将通气盖保持在第一位置，并且当跨越面板的压力差超过预定值时，便于通气盖运动到第二位置。
-
10.发明申请公开(公告)号：US20150108274A1
公开(公告)日：2015-04-23
申请号：US14228554
申请日：2014-03-28
Applicant: THE BOEING COMPANY
Inventor： Thomas Seth Perkins , Allan A. Loken , Robert J. Christian , James Pease , Sara Beth Cromyak
IPC: B64D13/00
CPC classification number: B64D13/00 , B64C1/18 , B64C2001/009
Abstract: Decompression panel assemblies and methods of equalizing air pressure differential are provided. The decompression panel assembly includes a panel comprising an opening defined therein, a vent cover coupled across the opening, and a latching mechanism. The vent cover is configured to move between a first position and a second position. The latching mechanism is configured to maintain the vent cover in the first position when a pressure differential across the panel is below a predetermined value and facilitate the vent cover moving to the second position when the pressure differential across the panel exceeds the predetermined value.
Abstract translation: 提供减压板组件和均压气压差的方法。 减压面板组件包括包括限定在其中的开口的面板，跨过开口连接的通气盖以及闭锁机构。 通气盖构造成在第一位置和第二位置之间移动。 闭锁机构构造成当跨越面板的压差低于预定值时将通气盖保持在第一位置，并且当跨越面板的压力差超过预定值时，便于通气盖运动到第二位置。
-
-
-
-
-
-
-
-
-
Search Results
15
records
(took 0.014 seconds)
