发明授权
US4086022A Gas turbine engine with improved compressor casing for permitting higher air flow and pressure ratios before surge 失效
具有改进的压缩机壳体的燃气涡轮发动机,用于在喘振之前允许更高的气流和压力比

Gas turbine engine with improved compressor casing for permitting higher
air flow and pressure ratios before surge
摘要:
A plurality of skewed slots of a particular shape are provided within a compressor casing adjacent at least one stage of compressor blade tips, the slots having an axial length greater than that of the adjacent blade tips. The slots are provided such that upon occurrence of compressor surge or stall, the stagnating air occurring about the blade row may be directed by the slots downstream of the compressor blade row back into the main stream of fluid passing through the compressor. By such an arrangement, the slots provide a compressor in which the air flow and pressure ratio may be increased before reaching compressor stall or surge.
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