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. 29, 2025

Filed:

Jul. 25, 2022
Applicant:

Battelle Memorial Institute, Columbus, OH (US);

Inventors:

Steven M. Risser, Reynoldsburg, OH (US);

Amy Marie Heintz, Pacific Grove, CA (US);

Rachel M. Thurston, Columbus, OH (US);

John Bartholomew, Hilliard, OH (US);

Erica Howard, Columbus, OH (US);

Richard G. Rateick, Jr., South Bend, IN (US);

Ian Haggerty, Powell, OH (US);

Assignee:

Battelle Memorial Institute, Columbus, OH (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/14 (2006.01); B32B 7/027 (2019.01); B32B 7/12 (2006.01); B32B 9/00 (2006.01); B32B 9/04 (2006.01); B32B 15/02 (2006.01); B32B 17/06 (2006.01); B32B 18/00 (2006.01); F41G 7/22 (2006.01); H05B 3/86 (2006.01); H05B 3/84 (2006.01);
U.S. Cl.
CPC ...
B32B 17/061 (2013.01); B32B 7/027 (2019.01); B32B 7/12 (2013.01); B32B 9/002 (2013.01); B32B 9/007 (2013.01); B32B 9/04 (2013.01); B32B 9/041 (2013.01); B32B 15/02 (2013.01); B32B 18/00 (2013.01); F41G 7/2293 (2013.01); H05B 3/86 (2013.01); B32B 2255/205 (2013.01); B32B 2307/30 (2013.01); B32B 2307/302 (2013.01); B32B 2307/412 (2013.01); B32B 2605/18 (2013.01); F41G 7/2253 (2013.01); H05B 3/84 (2013.01);
Abstract

An approach to seeker windows for aircraft comprises a window layer comprising an IR transparent material, the window layer comprising a first side and a second side substantially opposite the first side; and a heating layer on the first side or the second side of the window layer, the heating layer configured to apply a heating profile to the window layer to reduce thermal shock imparted to the window layer when the seeker window is exposed to hypersonic flight conditions.


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