公开(公告)号：US20180283065A1

公开(公告)日：2018-10-04

申请号：US15943765

申请日：2018-04-03

Applicant: B/E Aerospace, Inc.

Inventor： Justin C. CHRISTENSON ,  Charles F. FORSTER

IPC: E05D1/02 ,  B32B3/30 ,  B32B3/12

CPC classification number: E05D1/02 ,  A47D5/006 ,  B32B3/12 ,  B32B3/30 ,  B32B2250/44 ,  B32B2605/003 ,  B32B2605/18 ,  B64D11/00 ,  E05Y2800/43 ,  E05Y2800/68 ,  E05Y2900/502 ,  E05Y2900/538

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.

公开(公告)号：US20170130518A1

公开(公告)日：2017-05-11

申请号：US15406690

申请日：2017-01-14

Applicant: B/E AEROSPACE, INC.

Inventor： Justin C. CHRISTENSON ,  Graydon E. LOAR

IPC: E06B3/50 ,  B64C1/14 ,  E06B5/00

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.

公开(公告)号：US20180284818A1

公开(公告)日：2018-10-04

申请号：US15942799

申请日：2018-04-02

Applicant: B/E Aerospace, Inc.

Inventor： Justin C. CHRISTENSON

IPC: G05D23/185 ,  F16K11/07

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.

公开(公告)号：US20170001704A1

公开(公告)日：2017-01-05

申请号：US15234684

申请日：2016-08-11

Applicant: B/E Aerospace, Inc.

Inventor： Justin C. CHRISTENSON ,  Graydon E. Loar

IPC: B64C1/14

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。