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:
Apr. 18, 2017
Filed:
Jun. 24, 2014
Applicant:
Eads Deutschland Gmbh, Ottobrunn, DE;
Inventors:
Juergen Steinwandel, Uhldingen-Muehlhofen, DE;
Johannes Stuhlberger, Munich, DE;
Assignee:
Airbus Defence and Space GmbH, Ottobrunn, DE;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 1/00 (2006.01); F23C 99/00 (2006.01); F23N 5/00 (2006.01); F23R 3/28 (2006.01); F02C 7/00 (2006.01);
U.S. Cl.
CPC ...
F23C 99/001 (2013.01); F02C 7/00 (2013.01); F23N 5/006 (2013.01); F23R 3/28 (2013.01); F23N 2041/20 (2013.01); F23R 2900/00009 (2013.01); Y02T 50/677 (2013.01);
Abstract
A gas turbine includes a combustion chamber and a microwave source to produce microwave radiation. The gas turbine is arranged to guide the microwave radiation into a cavity of the combustion chamber. Due to the microwave radiation, in the cavity of the combustion chamber, combustion in the cavity may be supported and thus lean operation of the gas turbine is made possible.
Steinwandel, Juergen. (2017). High frequency-stabilized combustion in aircraft gas turbines (U.S. Patent No. 9625145). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9625145
Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile