Rotor blade assembly tool for gas turbine engine
US9328621B2 · kind B2 · utility
3Cited by
11References
6Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jan 21, 2014 |
| Grant date | May 3, 2016 |
| Priority date | — |
| Expiry date | Aug 8, 2035 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10T29/53983
- WIPO fieldMachine tools
- WIPO sectorMechanical engineering
Abstract
A rotor blade assembly tool for coupling a plurality of circumferentially spaced rotor blades to a rotor disc of a turbine rotor assembly, includes a base ring with an array of circumferentially spaced resilient fingers axially extending from the base ring. The resilient fingers are configured each to radially abut a blade seal, damper or other engine component against radially inner facing surfaces of platforms of the respective blades when the blades are being seated onto the disc during an assembly procedure.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.