The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jul. 10, 2018

Filed:

Apr. 01, 2015
Applicant:

B/e Aerospace, Inc., Wellington, FL (US);

Inventors:

Peter John Leslie Burd, Carmarthenshire, GB;

Venkata Prasanth Suman Neti, Stevenage, GB;

Assignee:

B/E Aerospace, Inc., Wellington, FL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16B 5/02 (2006.01); F16B 5/01 (2006.01); F16B 37/04 (2006.01); F16B 33/00 (2006.01); F16B 11/00 (2006.01);
U.S. Cl.
CPC ...
F16B 5/02 (2013.01); F16B 5/01 (2013.01); F16B 33/00 (2013.01); F16B 37/048 (2013.01); F16B 11/006 (2013.01); Y10T 29/4981 (2015.01); Y10T 29/49622 (2015.01); Y10T 29/49948 (2015.01);
Abstract

In an illustrative embodiment, an insert apparatus for creating an attachment point in an aircraft panel includes a flange insert configured for bonding against an inner surface of a skin of the aircraft panel such that a portion of a load from a component mounted to the attachment point is distributed through the skin. The flange insert may include a wide flange, a bore, and a central opening through the wide flange and the bore, and a nut including an enlarged end and a shaft, where the nut is disposed in the central opening of the flange such that the enlarged end is proximate the wide flange and the shaft extends along the bore. Upon bonding to the aircraft panel, the bore may extend from an underside of the wide flange to proximate an outer surface of the skin of the aircraft panel.


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