Patent · US Active

Ceramic regenerator for a gas turbine engine

US7861510B1 · kind B1 · utility

8Cited by
14References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 22, 2008
Grant dateJan 4, 2011
Priority date
Expiry dateMay 21, 2029

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2300/611
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A high temperature heat exchanger for use with a small gas turbine engine to produce a combined cycle power plant, where the heat exchanger includes ceramic heat exchange tubes of SiC that are tightly fitted to the heat exchanger so that no welds or brazing is used and prevent any thermal stresses between the tubes and the heat exchanger end plates or baffle plates. The heat exchanger includes an inner casing and an outer casing with the heat exchange tubes extending through the heat exchanger between the two casings, and the gas turbine engine operating in the space within the inner casing. The tubes are tightly fitted in holes within the end plates and baffle plates, and a molybdenum disulfide coating is used to form a seal.

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