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Sidewall panel assembly

A panel assembly, panel technology, applied in the direction of connecting members, fuselage bulkheads, thin plate connections, etc., can solve the problems of insufficient panel alignment, difficult panel installation and disassembly, etc., to achieve less maintenance problems, easy installation, and simple installation and the effect of the disassembly function

Active Publication Date: 2019-11-19
SAFRAN CABIN INC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Most aircraft sidewall panel seams have issues with insufficient panel alignment
Panels can also be difficult to install and remove and direct noise and cold air to passengers sitting in the cabin

Method used

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  • Sidewall panel assembly
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Examples

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Embodiment Construction

[0022] The following description and drawings are illustrative and should not be construed as limiting. Numerous specific details are described in order to provide a thorough understanding of the present disclosure. However, in certain instances, well known or conventional details are not described in order to avoid obscuring the description. References in this disclosure to "one embodiment" or "an embodiment" may, but do not necessarily, refer to the same embodiment; and, such references refer to at least one of the embodiments.

[0023] Reference in this specification to "one embodiment" or "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one embodiment of the present disclosure. The appearances of the phrase "in one embodiment" in various places in the specification do not necessarily all refer to the same embodiment, nor do they necessarily refer to separate or alternative emb...

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PUM

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Abstract

A panel assembly that is configured to be secured to a frame that includes a panel having a top and a bottom, a first bracket assembly and a second bracket assembly is disclosed. The first bracket assembly includes a first pivot member and a first bracket. One of the first bracket and first pivot member is secured to the panel and the other is configured to be secured to the frame. The first bracket includes a slot defined therein that includes a throat and a pivot opening. The throat is defined between first and second throat surfaces and the throat is narrower than the pivot opening. The second bracket assembly includes a second pivot member and a second bracket. One of the second bracket and second pivot member is secured to the panel and the other is configured to be secured to the frame. The second bracket includes a pivot opening.

Description

[0001] Cross References to Related Applications [0002] This application claims the benefit of U.S. Provisional Application No. 62 / 479,128, filed March 30, 2017, which is hereby incorporated by reference in its entirety. technical field [0003] This application relates generally to sidewall panel assemblies for use in aircraft. Background technique [0004] Most aircraft sidewall panel seams suffer from insufficient panel alignment. The panels can also be difficult to install and remove and direct noise and cold air to passengers sitting in the cabin. Contents of the invention [0005] According to a first aspect of the present invention there is provided a panel assembly configured to be secured to a frame. The panel assembly includes a panel, a first bracket assembly and a second bracket assembly, the panel having a top and a bottom. The first bracket assembly includes a first pivot member and a first bracket. One of the first bracket and the first pivot member is ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/06B64C1/12
CPCB64C1/066B64C1/12F16B5/07F16B5/126F16B5/123F16B5/0088F16B21/09F16B21/04F16B21/02F16B19/1081
Inventor T·史密森J·T·佩恩T·D·梅里尔S·M·希尔斯C·布鲁克斯M·班格特M·D·里奇斯
Owner SAFRAN CABIN INC