COMBUSTOR COMPRISING PANELS WITH SKEWED SIDE WALLS
摘要:
A combustor of a gas turbine engine including a first forward liner panel (72A-1, 74A-1). The forward liner panel including a liner panel forward edge (130), a liner panel aft edge (132) opposite of the liner panel forward edge, and a first liner panel side edge (134) between the liner panel aft edge and the liner panel forward edge. The first liner panel side edge is non-perpendicular to the liner panel forward edge and oriented at an angle about perpendicular to a swirl flow (I, O) in the combustor.
信息查询
0/0