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:
Oct. 22, 2019
Filed:
May. 31, 2016
Applicant:
Rolls-royce Deutschland Ltd & CO KG, Blankenfelde-Mahlow, DE;
Inventor:
Dimitrie Negulescu, Berlin, DE;
Assignee:
ROLLS-ROYCE DEUTSCHLAND LTD & CO KG, Blankenfelde-Mahlow, DE;
Primary Examiner:
Int. Cl.
CPC ...
F02K 3/075 (2006.01); F02K 3/077 (2006.01); B64C 30/00 (2006.01); B64D 27/16 (2006.01); F02K 1/15 (2006.01); F02K 3/06 (2006.01); F01D 15/12 (2006.01); F01D 17/16 (2006.01); F02C 9/18 (2006.01); F02C 9/22 (2006.01);
U.S. Cl.
CPC ...
B64D 27/16 (2013.01); B64C 30/00 (2013.01); F01D 15/12 (2013.01); F01D 17/162 (2013.01); F02C 9/18 (2013.01); F02C 9/22 (2013.01); F02K 1/15 (2013.01); F02K 3/06 (2013.01); F02K 3/077 (2013.01); F05D 2220/323 (2013.01); F05D 2240/128 (2013.01); F05D 2240/30 (2013.01); F05D 2270/20 (2013.01);
Abstract
An adaptive aircraft engine including a first, inner bypass duct inside a core engine of the aircraft engine and a second, outer bypass duct at least partially surrounding the first bypass duct, and adaption means, in particular adjustable nozzles for altering a flowed-through cross-section of the core engine with the first bypass duct and for altering the flowed-through cross-section of the second bypass duct depending on the flying speed. An aircraft having at least one adaptive aircraft engine is also provided.