Patent · US Active

Method and apparatus for gas turbine engine temperature management

US8517663B2 · kind B2 · utility

0Cited by
6References
10Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 30, 2008
Grant dateAug 27, 2013
Priority date
Expiry dateJun 27, 2032

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF02C9/18
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A cooling system for a turbine engine, as well as a methodology for controlling the cooling system, is described. A valve member is disposed between a cooling fluid passage and a wheel space of the turbine engine and operates to admit cooling fluid to the wheel space for cooling thereof. The valve assembly is responsive to a condition in the wheel space and varies the flow of additional cooling fluid to the wheel space based on that condition.

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