Experimental burner for testing materials for gas turbine blades.

摘要

Experimental burner for testing materials for gas turbine blades designed to work at temperatures of up to 1300 degrees centigrade in atmospheres identical to those in the burner of combined cycle gas turbines. It consists of a furnace fitted with a multigas burner, a preheated secondary air supply and a specimen holder which can cool them internally with compressed air. This unit permits the development of materials for working at very high temperatures and aggressive oxidizing environments, such as those that act on gas turbine blades.