Patent ID: 11859515
Assignee: GENERAL ELECTRIC COMPANY
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F | IPC F

Claim 0:
1. A gas turbine engine comprising:
a casing defining at least a portion of a flow path;
at least one stator vane array of a low-pressure compressor disposed within the flow path, the at least one stator vane array having a first stator vane array and a second stator vane array, the first stator vane array being downstream from the second stator vane array, the first stator vane array and the second stator vane array being back-to-back in series, the first stator vane array having outlet vanes, and the outlet vanes each having an outlet vane trailing edge; and
at least one strut having a strut leading edge, the strut leading edge being upstream from the outlet vane trailing edges.