| 摘要 |
PROBLEM TO BE SOLVED: To provide a gas turbine engine which is highly productive and manufactured at a low cost.SOLUTION: A gas turbine engine 100 comprises: a compressor 1 which compresses air through rotation thereof; a combustor 2 which burns fuel with a supply of compressed air sent from the compressor 1; and a turbine 3 which rotates by receiving combustion gas sent out from the combustor 2. The gas turbine engine also has an axial diffuser 52 (152) which converts velocity energy of the compressed air sent out from the compressor 1 into pressure energy and guides the same to the combustor 2 after directing a compressed air flow. The axial diffuser 52 (152) has irregularities formed by bending a plate material as guide passages 52p of the compressed air. |
