AN APPARATUS FOR SOLDERING GAS TURBINE BLADES.
Abstract
The apparatus for soldering gas turbine blades with cooling channels formed between the blade body and a thin-walled shell and with the use of heat-resistant solders in a reductive gas medium or a vacuum differs in that, to uniformly compress the shell to the blade body in the process of soldering, the blade is placed in a container with a pocket formed by thin walls which are adjacent to the blade surface and compressed by excess pressure outside the pocket or a vacuum within it.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 26, 1964
- Accession Number
- AD0601562
Entities
People
- I. K. Sklyarov
- Yu. I. Bereznidov
Organizations
- National Air and Space Intelligence Center