Patent · US Active

Method for setting a radial gap of an axial-throughflow turbomachine and compressor

US7766611B2 · kind B2 · utility

4Cited by
5References
4Claims
0Family size

Assignee

Inventors

Key dates

Filing dateApr 28, 2006
Grant dateAug 3, 2010
Priority date
Expiry dateJun 4, 2028

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF01D19/02
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

The invention relates a method for improving the hot-starting behavior of a turbomachine. By virtue of the setting of a radial gap formed between a brushing edge of a blade profile and a guide face lying opposite this, in which setting a guide ring forming the guide face can be acted upon with a coolant, the hot-starting behavior can be improved, in that the guide ring is cooled before the start of the machine.

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