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.

Date of Patent:
May. 04, 2021

Filed:

Sep. 06, 2017
Applicant:

Rolls-royce Deutschland Ltd & CO KG, Blankenfelde-Mahlow, DE;

Inventors:

Predrag Todorovic, Berlin, DE;

Thomas Kubisch, Koenigs-Wusterhausen, DE;

Assignee:

Rolls-Royce Deutschland Ltd & Co KG, Blankenfelde-Mahlow, DE;

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 1/00 (2006.01); F02K 1/38 (2006.01); F02K 1/48 (2006.01); F02K 1/80 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02K 1/386 (2013.01); F02K 1/48 (2013.01); F02K 1/80 (2013.01); F02K 3/06 (2013.01); F05D 2220/32 (2013.01); F05D 2230/642 (2013.01); F05D 2250/61 (2013.01); F05D 2250/75 (2013.01); F05D 2260/30 (2013.01); F05D 2260/964 (2013.01); F05D 2300/501 (2013.01); F05D 2300/6033 (2013.01); Y02T 50/60 (2013.01);
Abstract

A mixer assembly group for a turbofan engine, having a primary flow channel extending along a central axis of the turbofan engine and a secondary flow channel. The mixer assembly group includes a mixer for guiding a first fluid flow from the primary flow channel and a second fluid flow from the secondary flow channel in the direction of an exhaust of the turbofan engine, as well as for intermixing the first and second fluid flows, and a connection appliance, which has at least one connection component that is fixated at the mixer and by means of which the mixer assembly group is to be fixated at two different first and second engine components of the turbofan engine, with are subject to operating temperatures of different heights during operation of the turbofan engine.


Find Patent Forward Citations

Loading…