| 摘要 |
A turbine engine nozzle assembly (50) includes an outer band (54) including a leading edge (70), a trailing edge (74), and a body (78) extending therebetween; an inner band (56) including a leading edge (72), a trailing edge (76), and a body (78) extending therebetween; and at least one vane (52) extending between the outer and inn er bands including a first sidewall (60) and a second sidewall (62) connected togethe r at a leading edge (64) and a trailing edge (66), the at least one vane leading ed ge (64) being positioned downstream from the inner and outer band leading edges. The turbine engine nozzle assembly (50) further includes a retention system to couple the nozzle to an engine combustor that includes a first annular ring (290) coupl ed between the outer band and the combustor, and a second annular ring (291) coupled between the inner band and the combustor.
|
