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Bypass duct with guide vane ring in a turbofan engine
Bypass duct with guide vane ring in a turbofan engine
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机译:涡轮风扇发动机中带有导向叶片环的旁路管道
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摘要
The bypass duct has support struts, which are formed as guide vanes-support struts (3) with bigger thickness and chord length than the guide vanes (2) in an aligned aerodynamic form. A flow channel (4) existing between a suction side (7) of the guide vane-support strut and a guide vane (2.1) adjacent to the suction side is extended by a guide vane modifying in the geometry against other guide vanes depending on the respective formation of the guide vane-support strut for reducing the peak pressures of a circumferential pressure field.
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