Patent · US Active

Blade outer air seal surface

US10702964B2 · kind B2 · utility

0Cited by
11References
13Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 4, 2017
Grant dateJul 7, 2020
Priority date
Expiry dateFeb 28, 2038

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49982
  • WIPO fieldMachine tools
  • WIPO sectorMechanical engineering

Abstract

A blade outer air seal for a gas turbine engine having a surface that is eccentric with respect to the engine rotation centerline, and a method for creating same, are disclosed. Also, a method for grinding a work piece having nominal curvature defined by a work piece curvature centerline is disclosed, comprising the steps of: a) determining a desired surface profile for the work piece; b) providing a rotating grinding surface having a grinding rotation centerline; c) offsetting the grinding rotation centerline from the work piece curvature centerline; and d) applying the rotating grinding surface to the work piece while rotating the rotating grinding surface about the grinding rotation centerline to create the desired surface profile.

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