Invention Grant
- Patent Title: Mixer assembly group for a turbofan engine
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Application No.: US15696619Application Date: 2017-09-06
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Publication No.: US10995698B2Publication Date: 2021-05-04
- Inventor: Predrag Todorovic , Thomas Kubisch
- Applicant: Rolls-Royce Deutschland Ltd & Co KG
- Applicant Address: DE Blankenfelde-Mahlow
- Assignee: Rolls-Royce Deutschland Ltd & Co KG
- Current Assignee: Rolls-Royce Deutschland Ltd & Co KG
- Current Assignee Address: DE Blankenfelde-Mahlow
- Agency: Shuttleworth & Ingersoll, PLC
- Agent Timothy Klima
- Priority: DE102016217033.3 20160907
- Main IPC: F02K1/00
- IPC: F02K1/00 ; F02K1/38 ; F02K1/48 ; F02K1/80 ; F02K3/06

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.
Public/Granted literature
- US20180066605A1 MIXER ASSEMBLY GROUP FOR A TURBOFAN ENGINE Public/Granted day:2018-03-08
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