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.:
Date of Patent:
Jul. 16, 2019
Filed:
Jul. 30, 2014
Applicant:
The Boeing Company, Huntington Beach, CA (US);
Inventors:
Alan E. Landmann, Woodinville, WA (US);
Mark A. Negley, Kirkland, WA (US);
Jaffar S. Iqbal, Seattle, WA (US);
Bret A. Voss, Seattle, WA (US);
Mark M. Gmerek, Clinton, WA (US);
Giacomo Licciardi, Seattle, WA (US);
Assignee:
The Boeing Company, Chicago, IL (US);
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B32B 27/12 (2006.01); B32B 5/02 (2006.01); B32B 37/18 (2006.01); B32B 27/40 (2006.01); B64D 13/00 (2006.01); F16F 9/30 (2006.01);
U.S. Cl.
CPC ...
B32B 27/12 (2013.01); B32B 5/02 (2013.01); B32B 27/40 (2013.01); B32B 37/18 (2013.01); F16F 9/306 (2013.01); B32B 2307/51 (2013.01); B32B 2307/56 (2013.01); B32B 2315/085 (2013.01); B32B 2605/18 (2013.01); B64D 13/00 (2013.01);
Abstract
A panel includes a structural substrate and a damping element including a viscoelastic material (VEM) layer coupleable to the structural substrate of the aircraft, and a constraining layer coupled to the VEM layer. The VEM layer is configured to dampen a vibration of the structural substrate. The constraining layer is configured to apply a shear force to the VEM layer.