Apparatus for Increasing Augmentor.
Abstract
The patent application relates to an apparatus for increasing the flameholder capability in the thrust augmentor of a fanjet engine, having two rows of circumferentially spaced holes in the outer stator casing. Flow diverter vanes extend into the holds and intercept a portion of the hot gas from the last turbine rotor and direct the flow into the fan air channel leading to the augmentor. The holes in the two rows have different sizes to provide for different penetration into the cold fan air flow in the channel adjacent the outer stator casing.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 29, 1975
- Accession Number
- ADD001625
Entities
People
- George D. Lewis
Organizations
- United States Department of the Air Force