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:
Feb. 19, 2013

Filed:

Dec. 08, 2006
Applicants:

Akif O. Bolukbasi, Phoenix, AZ (US);

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

Tuan A. Nguyen, Mukllteo, WA (US);

Mostafa Rassaian, Bellevue, WA (US);

Kevin R. Davis, Covington, WA (US);

William J. Koch, Bellevue, WA (US);

Lee C. Firth, Renton, WA (US);

Inventors:

Akif O. Bolukbasi, Phoenix, AZ (US);

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

Tuan A. Nguyen, Mukllteo, WA (US);

Mostafa Rassaian, Bellevue, WA (US);

Kevin R. Davis, Covington, WA (US);

William J. Koch, Bellevue, WA (US);

Lee C. Firth, Renton, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

Energy absorbing structure disposed beneath the cargo area of an aircraft provides maximum energy absorption and structural strength using carbon fiber reinforced epoxy composites. The energy absorbing structure uses laminated stanchions having ply drop-offs to produce stable, progressive crushing of the stanchions during a wheels-up crash landing. Integrally formed flanges on the stanchions allow direct mounting of the stanchions on the structural members of the aircraft, without the need for specialized fittings.


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