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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.

Patent No.:

US 9862175 B1

PDFFull Text
Date of Patent:
Jan. 09, 2018

Filed:

Jul. 09, 2015

Molybdenum composite hybrid laminates and methods

Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Marc R. Matsen, Seattle, WA (US);

Mark A. Negley, Bellevue, WA (US);

Marc J. Piehl, Renton, WA (US);

Kay Y. Blohowiak, Issaquah, WA (US);

Alan E. Landmann, Woodinville, WA (US);

Richard H. Bossi, Renton, WA (US);

Robert L. Carlsen, Kent, WA (US);

Gregory Alan Foltz, Seattle, WA (US);

Geoffrey A. Butler, Seattle, WA (US);

Liam S. Cavanaugh Pingree, Seattle, WA (US);

Stephen G. Moore, Renton, WA (US);

John Mark Gardner, Newcastle, WA (US);

Robert A. Anderson, Federal Way, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:

John Goff

Int. Cl.
CPC ...
B32B 37/00 (2006.01); B32B 37/14 (2006.01); B32B 7/12 (2006.01); B32B 15/00 (2006.01); B32B 15/08 (2006.01); B32B 19/02 (2006.01); B32B 27/00 (2006.01); B32B 3/06 (2006.01); B29C 73/10 (2006.01);
U.S. Cl.
CPC ...
B32B 37/144 (2013.01); B32B 3/06 (2013.01); B32B 7/12 (2013.01); B32B 15/00 (2013.01); B32B 15/08 (2013.01); B32B 19/02 (2013.01); B32B 27/00 (2013.01); B29C 73/10 (2013.01); B32B 2250/42 (2013.01); B32B 2260/021 (2013.01); B32B 2305/08 (2013.01); B32B 2307/202 (2013.01); B32B 2307/204 (2013.01); B32B 2307/54 (2013.01); B32B 2307/558 (2013.01); B32B 2311/00 (2013.01); B32B 2398/00 (2013.01); B32B 2405/00 (2013.01); B32B 2605/18 (2013.01); Y10T 29/49208 (2015.01); Y10T 29/49885 (2015.01); Y10T 156/10 (2015.01); Y10T 428/24752 (2015.01); Y10T 428/31678 (2015.04);
Abstract

A method of forming a molybdenum composite hybrid laminate is disclosed. The method includes treating a surface of each of a plurality of molybdenum foil layers. The method further includes interweaving the surface treated molybdenum foil layers with a plurality of composite material layers. The method further includes bonding with an adhesive layer each of the surface treated molybdenum foil layers to adjacent composite material layers to form a molybdenum composite hybrid laminate having improved yield strength.

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