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. 14, 2017

Filed:

Nov. 20, 2015
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Gregory J. Sweers, Chicago, IL (US);

Carol E. Anway, Chicago, IL (US);

Andrew M. Robb, Chicago, IL (US);

Jeong-Beom Ihn, Chicago, IL (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
G01B 7/00 (2006.01); B64D 45/00 (2006.01); B29C 65/48 (2006.01); B29C 65/50 (2006.01); B29C 65/82 (2006.01); B29C 65/00 (2006.01); B64C 3/20 (2006.01); G01N 27/02 (2006.01); G01N 27/20 (2006.01); G01M 5/00 (2006.01); B29L 31/30 (2006.01); B29K 105/20 (2006.01); F16B 11/00 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
B64D 45/00 (2013.01); B29C 65/483 (2013.01); B29C 65/5021 (2013.01); B29C 65/5028 (2013.01); B29C 65/5057 (2013.01); B29C 65/8276 (2013.01); B29C 65/8284 (2013.01); B29C 66/1122 (2013.01); B29C 66/45 (2013.01); B29C 66/721 (2013.01); B64C 3/20 (2013.01); G01M 5/0033 (2013.01); G01M 5/0083 (2013.01); G01M 5/0091 (2013.01); G01N 27/025 (2013.01); G01N 27/026 (2013.01); G01N 27/20 (2013.01); B29C 65/4835 (2013.01); B29C 65/8292 (2013.01); B29C 66/71 (2013.01); B29C 66/7212 (2013.01); B29C 66/72141 (2013.01); B29C 66/72143 (2013.01); B29C 66/7392 (2013.01); B29C 66/7394 (2013.01); B29C 66/73921 (2013.01); B29C 66/73941 (2013.01); B29K 2105/206 (2013.01); B29L 2031/3076 (2013.01); B29L 2031/3079 (2013.01); B29L 2031/3082 (2013.01); B29L 2031/3085 (2013.01); B64C 2001/0072 (2013.01); B64D 2045/0085 (2013.01); F16B 11/006 (2013.01); Y02T 50/433 (2013.01);
Abstract

Systems, methods, and apparatus for using aircraft bondline embedded current sensors to determine a lightning damage index are disclosed. A method of predicting lightning strike damage to at least one type of aircraft involves sensing, with at least one current sensor node embedded in at least one type of aircraft, induced current. The method further involves generating, with at least one current sensor node, at least one current signal representative of the induced current. Also, the method involves determining, electromagnetic density data associated with at least one region of at least one type of aircraft by using at least one current signal. Further, the method involves creating an index that provides a numeric representation for predicted lightning strike damage to at least one type of aircraft based on the electromagnetic density data, dimensions of at least one type of aircraft, and design features of at least one type of aircraft.


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