Method of manufacturing a hollow blade for a turboshaft engine
US5253419A · kind A · utility
Assignee
Inventors
Key dates
| Filing date | Jan 4, 1993 |
| Grant date | Oct 19, 1993 |
| Priority date | — |
| Expiry date | Jan 4, 2013 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10T29/49339
- WIPO fieldMachine tools
- WIPO sectorMechanical engineering
Abstract
A hollow blade for a turboshaft engine, such as a fan rotor blade of large chord, is manufactured by a method in which primary components including two outer metal sheets and at least one intermediate sheet are hot formed so that the components are curved and twisted to a desired shape, diffusion barriers are formed at selected positions on the intermediate sheet, the shaped components are assembled and located on suitable process tooling, the assembled components are diffusion welded together, the welded assembly is internally pressurized by gas to inflate and superplastically deform selected areas to form a hollow in said assembly, and performing finishing operations on the hollow assembly to obtain the hollow blade.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.