Preliminary experimental results for a cryogenic brush seal configuration
Abstract
Preliminary fluid nitrogen flow data are reported for a five-brush, ceramic-coated-rub-runner brush seal system, where the brushes and the rub runner were placed at each end of a centrally pressurized multifunction tester ('back-to-back' set of brushes) and tested at rotor speeds of 0, 10, 18, and 22.5 krpm. After testing, both the brushes and the ceramic-coated rub runner appeared pristine. The coating withstood both the thermomechanical and dynamic loadings with minor wear track scarring. The bristle tips showed some indication of material shearing (smearing) wear. The Ergun porous flow equation was applied to the brush seal data. The Ergun relation, which required heuristic information to characterize the coefficients, fit the gaseous data but was in poor agreement with the fluid results. The brush seal exit conditions were two phase. Two-phase, choked-flow design charts were applied but required one data point at each rotor speed to define the (C(sub f)A x Constant) flow and area coefficients. Reasonable agreement between prediction and data was found, as expected, but such methods are not to be construed as two-phase-flow brush seal analyses.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- June 1993
- Bibcode:
- 1993STIN...9328627C
- Keywords:
-
- Brush Seals;
- Choked Flow;
- Cryogenic Equipment;
- Flow Equations;
- Nitrogen;
- Shearing;
- Wear;
- Ceramic Coatings;
- Dynamic Loads;
- Rotor Speed;
- Thermodynamics;
- Fluid Mechanics and Heat Transfer