Patent · US Active

Passage wall section for an annular flow passage of an axial turbomachine with radial gap adjustment

US8721270B2 · kind B2 · utility

5Cited by
5References
15Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 10, 2011
Grant dateMay 13, 2014
Priority date
Expiry dateJul 23, 2032

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF01D11/22
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A passage wall section of an annular flow passage of an axial turbomachine is provided. A guide ring has a first toothing arrangement which is in contact with a second toothing arrangement arranged on a sidewall of a circumferential groove which accommodates the guide ring, wherein for axial displacement of the displaceable guide ring, the guide ring is rotatable in a circumferential direction.

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