Patent · US Active

Brush seal assembly and method

US10844741B2 · kind B2 · utility

1Cited by
30References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 21, 2016
Grant dateNov 24, 2020
Priority date
Expiry dateFeb 10, 2038

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2260/96
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A brush seal assembly is adapted to be operatively mounted between a stator and a rotor of a gas turbine engine. The brush seal assembly comprises a housing and a seal operatively coupled to the housing. The seal comprises at least two annular brushes each having a plurality of bristles extending away from the housing. The at least two annular brushes and the housing defines a cavity therebetween. The housing defines at least one circumferential surface within the cavity. The housing comprises at least one discontinuity defined in the at least one circumferential surface. The at least one discontinuity disrupts a continuity of annularity of the circumferential surface.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.