Patent · US Active

Active turbine tip clearance control system

US9316111B2 · kind B2 · utility

13Cited by
16References
13Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 15, 2011
Grant dateApr 19, 2016
Priority date
Expiry dateNov 30, 2033

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF01D11/24
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

An active tip clearance control (ATCC) system of a gas turbine engine includes an ejector to selectively drive an air flow passing through the ATCC system. A high pressure air flow as a motive flow of the ejector is controlled by a valve according to engine operation requirements.

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