COMBUSTOR, GAS TURBINE ENGINE AND ASSEMBLING METHOD FOR COMBUSTOR

摘要

PROBLEM TO BE SOLVED: To provide a deflector flared cone assembly 75 of a single part for a gas turbine engine combustor 16 to enhance lengthening of a service life of the combustor with high cost-effectiveness and in a reliable form. SOLUTION: This combustor includes an air swirl generating device 90. The assembly of the single part includes a deflector part 76 and a flared cone part 78. The deflector part 76 includes an integral opening part 168 extending in a peripheral direction through the deflector part 76 to receive cooling fluid. Since rope for brazing and tape for brazing loaded in advance are received by the deflector flared cone assembly 75, the deflector flared cone assembly 75 is fixed to the air swirl generating device 90 within the combustor in a single brazing work.