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:
Sep. 12, 2017

Filed:

Aug. 31, 2015
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Timothy Todd King, Freeland, WA (US);

Douglas R. Ackerman, Langley, WA (US);

Gil-Antonio Lora, Seattle, WA (US);

Kenneth G. Davis, Brier, WA (US);

Mark J. Nadvornick, Lynnwood, WA (US);

Brett N. Altmyer, Everett, WA (US);

Jason W. Mullins, Edmonds, WA (US);

Christopher J. Steele, Kirkland, WA (US);

Matthew R. Thomas, Marysville, WA (US);

Cynthia T. Parrish, Bellevue, WA (US);

James R. McCune, Stanwood, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 1/06 (2006.01); B64D 11/00 (2006.01); B64F 5/00 (2017.01);
U.S. Cl.
CPC ...
B64C 1/066 (2013.01); B64D 11/00 (2013.01); B64F 5/0009 (2013.01);
Abstract

A support system for a crown area of an aircraft and a corresponding method is disclosed. The support system includes a crown integration panel (CIP). The CIP is configured to provide a mounting surface for a plurality of aircraft equipment and to provide an electrical ground for at least one of the aircraft equipment of the plurality of aircraft equipment. The system further includes a first attachment and a second attachment attached to the CIP. The first attachment and the second attachment are configured to attach to an airframe of the aircraft. The system further includes a crown raceway support (CRS) having a first end and a second end, where the first end is attached to a first end of the CIP and the second end is configured to attach to an outboard rail of the aircraft.


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