Patent · US Active

Gas turbine rotor cover

US10443433B2 · kind B2 · utility

0Cited by
22References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 8, 2016
Grant dateOct 15, 2019
Priority date
Expiry dateSep 24, 2037

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2260/231
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A gas turbine rotor cover includes a body, the body having an inner side facing towards a central axis and an outer side facing away from the central axis, wherein the gas turbine rotor cover is configured and arranged to extend in an axial direction and a circumferential direction relative to the central axis. An inner layer of insulation is attached to the inner side of the body and extends along at least part of the length of the body in the axial direction and/or an outer layer of insulation is attached to the outer side of the body, and extends along at least part of the length of the body in the axial direction. A gas turbine containing the gas turbine rotor cover is also disclosed.

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