Clip attachment system connecting aircraft structures to each other

US9463535B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9463535-B2
Application numberUS-201314088410-A
CountryUS
Kind codeB2
Filing dateNov 24, 2013
Priority dateJun 21, 2011
Publication dateOct 11, 2016
Grant dateOct 11, 2016

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

In one advantageous embodiment of the present disclosure, an apparatus and method for supporting a load is provided. The apparatus comprises a structure having an inner surface with a shape configured to substantially conform to an outer surface of a stringer. A number of pins extends from the inner surface of the structure such that the number of pins are configured to engage holes in the outer surface of the stringer when the structure is placed over the outer surface of the stringer. The pins support the structure with respect to the stringer when a load is applied to the structure. A number of members extends from the outer surface of the structure such that the number of members is configured to connect to a part.

First claim

Opening claim text (preview).

What is claimed is: 1. A method for supporting a part, the method comprising: engaging a clip with a stringer via: connecting a first member of the clip to a second member of the clip via a center portion; flexing the center portion into a flexed position; while flexing the center portion, aligning a pin extending away from a contact section of the first member, with a hole in a first side of an outer surface of the stringer, and aligning a pin extending away from a contact s…

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What does patent US9463535B2 cover?
In one advantageous embodiment of the present disclosure, an apparatus and method for supporting a load is provided. The apparatus comprises a structure having an inner surface with a shape configured to substantially conform to an outer surface of a stringer. A number of pins extends from the inner surface of the structure such that the number of pins are configured to engage holes in the oute…
Who is the assignee on this patent?
Boeing Co
What technology area does this patent fall under?
Primary CPC classification B64C1/403. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Oct 11 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).