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:
May. 30, 2017
Filed:
Jun. 09, 2014
Applicant:
Mtu Aero Engines Ag, Munich, DE;
Inventors:
Hermann Klingels, Dachau, DE;
Stephan Klaen, Berlin, DE;
Christian Scherer, Roehrmoos, DE;
Uwe Vogel, Munich, DE;
Assignee:
MTU Aero Engines AG, Munich, DE;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 33/04 (2006.01); F02K 1/00 (2006.01); F02K 1/12 (2006.01); F02K 1/80 (2006.01);
U.S. Cl.
CPC ...
F02K 1/008 (2013.01); B64D 33/04 (2013.01); F02K 1/006 (2013.01); F02K 1/1207 (2013.01); F02K 1/80 (2013.01); F05D 2250/42 (2013.01); F05D 2260/50 (2013.01); F05D 2260/56 (2013.01); F05D 2260/57 (2013.01);
Abstract
A thrust deflecting device for deflecting a thrust stream is disclosed, which includes a flap system having a plurality of deflecting flaps, each of which is pivotable around its yaw axis, the flap system being situated between parallel control surfaces such as baffle plates which, together with the flap system, form a box structure, which is pivotable around a pivot axis running in the direction of the transverse axis for the purpose of deflecting the thrust stream in the pitch direction, an aircraft engine also being disclosed.