Patent · US Active

Turbomachine component displacement apparatus and method of use

US9429041B2 · kind B2 · utility

3Cited by
63References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 14, 2014
Grant dateAug 30, 2016
Priority date
Expiry dateSep 4, 2034

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/5383
  • WIPO fieldMachine tools
  • WIPO sectorMechanical engineering

Abstract

Various embodiments include apparatuses adapted to displace components from a location within a turbomachine. In some embodiments an apparatus for displacing a component of a gas turbine from a first slot in a spacer disk includes a body including a mounting member configured to affixedly attach to a second slot of the spacer disk, a linear actuator coupled to the body and a displacement arm coupled to the linear actuator, the displacement arm actuatable in a first axial direction by the linear actuator to contact the component and displace the component relative to the first slot.

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