Patent · US Active

Gas turbine engine rapid response clearance control system with air seal segment interface

US10370999B2 · kind B2 · utility

6Cited by
6References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 6, 2014
Grant dateAug 6, 2019
Priority date—
Expiry dateJun 4, 2036

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF04D29/526
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

An active clearance control system of a gas turbine engine includes an air seal segment with a bridge hook having a lugged aperture.

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