| 摘要 |
A nacelle inlet for an aircraft engine of a type having an engine fan case with a forward flange includes an acoustic inner barrel (202) having a forward edge and an aft edge, an outer shell (204) having a nose lip portion (223) with a trailing inner edge (221), and an outer barrel portion (225) having an aft portion. The nacelle inlet also includes an aft attachment flange (250) configured to attach the inlet to the forward flange of the engine fan case, and an aft bulkhead (227) having an aft end and connecting the outer barrel portion (225) of the outer shell (204) to the aft attachment flange (250). The forward edge of the acoustic inner barrel (202) is connected to the trailing inner edge (221) of the nose lip portion (223), and the aft portion (218) of the inner barrel (202) is attached to the aft attachment flange (250). |
