Patent · US Active

Method and device for setting a predetermined radial gap width for rotor blades of a turbomachine

US9969055B2 · kind B2 · utility

1Cited by
7References
7Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 7, 2013
Grant dateMay 15, 2018
Priority date
Expiry dateFeb 16, 2035

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF01D25/26
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A method and device for setting a predetermined radial gap width for rotor blades arranged in a housing of a turbomachine is provided. The method includes removing a housing part and at least partially exposing the rotor blades which are to be machined, arranging a grinding device in the region of a rotor blade which is to be machined such that the tip of the rotor blade is machined using a grinding disk of the grinding device, screening off the machining region by arranging a screening device which is formed so as to counter a release of grinding dust from the screen off machining region, providing a suction extraction such that it extracts grinding dust from the screened-off machining region and grinding the tip of the rotor blade in situ producing the radial gap width.

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