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:
Dec. 17, 2024
Filed:
Aug. 11, 2022
Applicant:
Rosemount Aerospace Inc., Burnsville, MN (US);
Inventors:
Joseph T. Pesik, Eagan, MN (US);
Jonathan Boer, Lakeville, MN (US);
Assignee:
Rosemount Aerospace Inc., Burnsville, MN (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G06T 7/13 (2017.01); B64D 45/00 (2006.01); B64D 47/08 (2006.01); G06T 7/181 (2017.01); G06T 7/246 (2017.01); G06T 7/70 (2017.01); G06T 7/73 (2017.01); G06V 10/22 (2022.01); G06V 10/75 (2022.01); G06V 10/82 (2022.01); G06V 20/10 (2022.01); G06V 20/17 (2022.01); G06V 20/52 (2022.01); G06V 20/56 (2022.01); G06V 20/64 (2022.01); G06V 40/10 (2022.01); G08G 5/06 (2006.01); H04N 7/18 (2006.01); B64C 1/14 (2006.01); B64C 25/36 (2006.01); B64D 25/14 (2006.01);
U.S. Cl.
CPC ...
G08G 5/065 (2013.01); B64D 45/00 (2013.01); B64D 45/0005 (2013.01); B64D 47/08 (2013.01); G06T 7/13 (2017.01); G06T 7/246 (2017.01); G06T 7/70 (2017.01); G06T 7/73 (2017.01); G06T 7/74 (2017.01); G06V 10/22 (2022.01); G06V 10/759 (2022.01); G06V 10/82 (2022.01); G06V 20/17 (2022.01); G06V 20/188 (2022.01); G06V 20/52 (2022.01); G06V 20/56 (2022.01); G06V 20/64 (2022.01); G06V 40/10 (2022.01); H04N 7/181 (2013.01); H04N 7/183 (2013.01); B64C 1/1423 (2013.01); B64C 25/36 (2013.01); B64D 25/14 (2013.01); B64D 2045/0085 (2013.01); G06T 2207/20076 (2013.01); G06T 2207/20081 (2013.01); G06T 2207/20084 (2013.01); G06T 2207/30196 (2013.01); G06T 2207/30241 (2013.01); G06T 2207/30248 (2013.01);
Abstract
A camera with a field of view toward an external environment of an aircraft is disposed within an aircraft door such that an engine inlet of an engine of the aircraft is within the field of view of the camera. A display device is disposed within an interior of the aircraft. A processor is operatively coupled to the camera and to the display device. The processor analyzes image data captured by the camera to determine whether persons or foreign objects are present near the engine inlet, or detect damage or deformation of the engine inlet.