Bleed system driven in simplified manner for a turbojet or turboprop engine
作者： Michel Gilbert Brault , Pascal Noël Brossier
DOI:
关键词: Electrical conduit 、 Casing 、 Flow (psychology) 、 Manifold (fluid mechanics) 、 Bleed 、 Gas compressor 、 Turboprop 、 Mechanical engineering 、 Turbojet 、 Engineering
摘要: A bypass gas turbine engine having an intermediate structural casing positioned between a primary flow path and path, configured low pressure compressor high compressor. The further bleed device arranged to deflect portion of from the toward path. includes annular cavity defining manifold situated upstream opening along outer wall plurality conduits casing, tubes around connecting at least one regulating valve disposed interior each tubes.
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