Patent · US Active

Wall panel assembly for a gas turbine engine

US10386067B2 · kind B2 · utility

0Cited by
10References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 15, 2016
Grant dateAug 20, 2019
Priority date
Expiry dateJun 13, 2037

Classification

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

Abstract

A wall panel assembly includes a first liner panel and a coating. The first liner panel has an inner first liner panel surface and a first liner panel outer surface each axially extending between a first liner panel first end and a first liner panel second end. The coating is disposed on at least one of the first liner panel inner surface and the first liner panel outer surface. The coating has an overall thickness that varies axially between the first liner panel first end and the first liner panel second end.

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