Method of making cooled rocket combustion chamber construction
US5473817A · kind A · utility
12Cited by
6References
17Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Mar 14, 1994 |
| Grant date | Dec 12, 1995 |
| Priority date | — |
| Expiry date | Mar 14, 2014 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10T29/49348
- WIPO fieldMachine tools
- WIPO sectorMechanical engineering
Abstract
A method of producing a rocket combustion chamber/nozzle assembly in which a liner blank is deformed against the forming surface of a die to form a finished cooling liner, a structural jacket is electro-formed about the finished cooling liner, and fluid manifolds are secured to the finished cooling liner and structural jacket assembly.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.