Combined guide vane and mixer for a gas turbine engine
Patent
·
OSTI ID:5282731
The multi-lobed mixer downstream of the turbine of a gas turbine engine is constructed to include the exit guide vanes for the turbine carried on the inner diameter of the mixer so as to prevent diffusing with a consequential reduction of pressure losses and engine weight.
- Assignee:
- United Technologies Corp.
- Patent Number(s):
- US 4045957
- OSTI ID:
- 5282731
- Country of Publication:
- United States
- Language:
- English
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