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端壁狭缝射流对舰用燃气轮机压气机性能的影响

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为了探索端壁狭缝射流对舰用燃气轮机压气机叶栅性能的影响,本文采用带转捩的SST κ-ω湍流模型对压气机叶栅气动性能进行数值模拟,探究了端壁狭缝射流的射流角度和组合方式对压气机叶栅流动分离的影响规律.结果发现,端壁狭缝射流具有显著抑制叶栅角区分离、降低流动损失的作用,其中组合射流具有更好的流动控制效果.在射流流量仅为0.435%主流流量的情况下,30°组合射流可使损失降低27.63%,静压系数提高9.2%.端壁狭缝射流主要通过抑制端区二次流动、促进低能流体与主流的掺混和控制通道涡、集中脱落涡及诱导涡的发展来降低叶栅损失,改善叶栅性能.
Effects on end-wall slot jet among the performance of compressor of marine gas turbine
In order to explore the effect of end-wall slot jet on the performance of compressor cascades in marine gas turbines,the SST κ-ω turbulence model with transition was adopted to numerically simulate the aerodynamic performance of compressor cascades.And the influence of the jet angle and combination method of the end-wall slot jet on the flow separa-tion of compressor cascades was explored.It can be found that the end-wall slot jet significantly inhibited the corner separa-tion and reduced flow loss,among which the combined jet has better flow control effect.When the jet flow rate is only 0.435%of the mainstream flow rate,30°combined jet can reduce the loss by 27.63%and increase the static pressure coefficient by 9.2%.The end-wall slot jet mainly reduces the flow loss and improves the performance of the cascade by suppressing the secondary flow in the endwall region,promoting the mixing of low-energy fluid with mainstream,and controlling the devel-opment of passage vortex,concentrated shed vortices,and induced vortices.

marine gas turbine cascadeend-wall slot jetflow controlangular separation

左财宝、李臣、袁均福

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江苏海事职业技术学院,江苏南京 211170

江苏船舶节能减排工程技术研究中心,江苏南京 211170

舰用燃气轮机叶栅 端壁狭缝射流 流动控制 角区分离

2024

舰船科学技术
中国舰船研究院,中国船舶信息中心

舰船科学技术

CSTPCD北大核心
影响因子:0.373
ISSN:1672-7649
年,卷(期):2024.46(24)