Patent · US Active

Electric probe assembly, gas turbine engine having same and method of cooling same

US9551281B2 · kind B2 · utility

5Cited by
8References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 15, 2014
Grant dateJan 24, 2017
Priority date
Expiry dateMar 30, 2035

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2270/80
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A gas turbine engine comprises a hot section module which includes at least one electric probe assembly surrounded by an immediate environment having a local ambient temperature. The at least one electric probe assembly includes an electric probe having a probe body, and a conduit surrounding at least a portion of the probe body. In operation, the conduit carries a fluid flowing at a temperature lower than the local ambient temperature. The at least portion of the probe body is embedded in the fluid inside the conduit. The fluid thermally insulates the probe body from the local ambient temperature of the immediate environment around the at least one electric probe assembly.

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