BRUSH SEAL LEAKAGE PERFORMANCE WITH GASEOUS WORKING FLUIDS AT STATIC AND LOW ROTOR SPEED CONDITIONS
- Author(s):
- Carlile, Julie A. ( National Aeronautics and Space Administration Lewis Research Center )
- Hendricks, Robert C.
- Yoder, Dennis A.
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1992
- Issue:
- NASA-TM-105400
- No.:
- G3/34 0068745
- Pt.:
- NAS 1.15:105400
- Paper no.:
- N92-16265
- Page(from):
- 1
- Page(to):
- 9
- Pages:
- 9
- Pub. info.:
- National Aeronautics and Space Adminstration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
National Aeronautics and Space Adminstration |
National Aeronautics and Space Adminstration |
National Aeronautics and Space Adminstration |
8
Technical Paper
Relative performance comparison between baseline labyrinth and dual brush compressor discharge seals in a T-700 engine test
The American Society of Mechanical Engineers |
3
Technical Paper
Some Peliminary Results of Brush Seal/Rotor Interference Effects on Leakage at Zero and Low RPM Using a Tapered-Plug Rotor
National Aeronautics and Space Adminstration |
National Aeronautics and Space Administration |
National Aeronautics and Space Adminstration |
National Aeronautics and Space Adminstration |
National Aeronautics and Space Adminstration |
The American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
12
Technical Paper
Metallographic Analysis of Brush Bristle and Integrity Testing of Brush Seal in Shroud Ring of T-700 Engine
National Aeronautics and Space Adminstration |