Accession Number:

ADA261296

Title:

Advanced Bristle Seals for Gas Turbine Engines

Descriptive Note:

Final rept, May-Nov 1992

Corporate Author:

ENGINEERED DESIGNS INC CINCINNATI OH

Personal Author(s):

Report Date:

1993-01-28

Pagination or Media Count:

49.0

Abstract:

A seven month proof-of-concept program was conducted for an advanced bristle seal, called a bush seal, for use in gas turbine engines. This program was performed as a Small Business Innovation Research SBIR Phase I project. Bush seal specimen and a full ring bush seal were designed, evaluated, and manufactured for testing. An analytical study of the potential of the bush seal relative to a labyrinth seal was conducted. Static and dynamic testing of the bush seal was performed to determine the behavior of the bristles under pressurization and during contact with a rotating labyrinth tooth. Stable behavior of the bristle elements was observed during static pressurization of a full ring bush seal. The dynamic testing of various configurations of bush seal against a rotating labyrinth tooth showed minimal wear of the bristles relative to a conventional labyrinth seal. the development and application of the bush seal concept to gas turbine engines has the potential of improving the engines performance while decreasing the degradation of the seal performance over time.

Subject Categories:

  • Adhesives, Seals and Binders
  • Mechanics
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE