Patent · US Active

Gas turbine and mounting method

US10018051B2 · kind B2 · utility

0Cited by
13References
8Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 29, 2014
Grant dateJul 10, 2018
Priority date
Expiry dateJun 18, 2035

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2260/83
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

An insert element fastens to an annular segment body of a turbine of a gas turbine. The annular segment body has a recess on a hot-gas side. The insert element is designed to cover the recess and has a concave front side and a rear side having at least one shaped portion for positioning on the annular segment body. An annular segment has the insert element, a gas turbine has the insert element, and a mounting method mounts the insert element.

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