Patent · US Active

Non-linearly deflecting brush seal land

US9957825B2 · kind B2 · utility

0Cited by
17References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 4, 2016
Grant dateMay 1, 2018
Priority date
Expiry dateOct 1, 2036

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A brush seal land is disclosed. The brush seal land may comprise a first portion configured to be coupled to a turbine disc of an aircraft engine and a second portion having a contact surface. The brush seal land may comprise a concave annular structure. The second portion may deflect through a clearance area in response to contact with a brush. The second portion may not deflect in response to contact with a brush after the second portion has deflected through a clearance area in response to contact with the brush. The contact surface comprises tungsten carbide. The brush seal land may comprise INCONEL. The brush seal land may be configured to be coupled to an annular member extending from the turbine disc. The brush seal land may reduce abrasion to an annular member extending from the turbine disc by a brush.

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