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:
Sep. 02, 2014
Filed:
Jun. 18, 2011
Applicants:
Kaushik Rajashekara, Carmel, IN (US);
George A. Pontones, Indianapolis, IN (US);
Inventors:
Kaushik Rajashekara, Carmel, IN (US);
George A. Pontones, Indianapolis, IN (US);
Assignee:
Other;
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 41/00 (2006.01); H02J 9/06 (2006.01); H02J 1/10 (2006.01); H02J 3/38 (2006.01);
U.S. Cl.
CPC ...
B64D 41/00 (2013.01); H01M 2250/20 (2013.01); H02J 1/10 (2013.01); B64D 2041/005 (2013.01); Y02T 90/36 (2013.01); B64D 2221/00 (2013.01); H02J 9/066 (2013.01); H02J 3/387 (2013.01); Y02T 50/54 (2013.01); Y02T 90/32 (2013.01);
Abstract
One embodiment of the present application is directed to a unique method for powering one or more critical loads in an aircraft. Another embodiment is a unique apparatus for powering one or more critical loads upon failure of one or more engines. Other embodiments include unique methods, systems, devices, and apparatus' for powering power loads in an aircraft. Further embodiments, forms, features, aspects, benefits, and advantages of the present application shall become apparent from the description and figures provided herewith.