METHOD AND DEVICE FOR MANUFACTURING GAS TURBINE ENGINE COMBUSTOR

摘要

PROBLEM TO BE SOLVED: To provide a gas turbine engine combustor 16. SOLUTION: This engine combustor includes a Venturi 36 and a secondary swirler 34 extending around the Venturi in the circumferential direction. The secondary swirler has a gap 120 between a part of the secondary swirler and the Venturi. A primary swirler 32 connected to the Venturi 36 is arranged so that the Venturi is between the secondary swirler 34 and the primary swirler 34. COPYRIGHT: (C)2006,JPO&NCIPI