Effect of Flow in the Rotor on the Performance of a Sirocco Fan
Effect of Flow in the Rotor on the Performance of a Sirocco Fan
批准号:
09650211
负责人:
ADACHI Tsutomu
金额:
$1.34万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (C)
财政年份:
1997
资助国家:
日本
项目状态:
已结题
起止时间:
1997 至 1999
中文摘要
Effects of blade shape on the performance of a Sirocco fan was measured using9runner blades with different blade shape in the same casing.These9different runner blades have inner diameter of 130 mm,outer diameter of 160 mm,and 46 mm in width.Considering from the velocity triangles at the blade inlet,the blade inlet angles are to be taken 10至15°。For the runner blades with these values the efficiency was good,but large discharge couldn‘t be obtained。Inlet angle must be taken in the range of 75-90°。The outlet angle is desired to be 150~160°。For these runner blades flow flows along the blade surface,though it once separates at the leading edge and reattaches at the trailing edge.The flow velocity takes large value at the pressure surface and smaller values at the suction surface at the center of the blade width.Deviation angle,i.e.,the difference of blade outlet angle and flow outlet angle,takes zero value,if proper design is conducted。The ratio of wake width to the blade pitch becomes larger,if the blade thickness is larger。If the blade outlet angle is larger than 160°,the outlet flow circulate。Inlet vortex arise because of the sudden flow turning at the blade inlet。The extent of inlet vortex is influenced by the inclination angle of blade。The inclination ratio,i.e.,the ratio of blade inclination angleθand the inlet angleβ-I D21--D2is important。The maximum values of pressure and discharge can be obtained at(θ/βI D21 ii D2)=0.35。Considering the above affairs,the valuesβI D 21 I D 2)=75~90°,(θ/βI D 21 I D 2)=0.35 andβI D 22 I D 2=150~160°are suitable for the blade design.The blade thickness must be thinner as possible.
英文摘要
Effects of blade shape on the performance of a Sirocco fan was measured using 9 runner blades with different blade shape in the same casing. These 9 different runner blades have inner diameter of 130 mm, outer diameter of 160 mm, and 46 mm in width. Considering from the velocity triangles at the blade inlet, the blade inlet angles are to be taken 10〜15°. For the runner blades with these values the efficiency was good, but large discharge couldn't be obtained. Inlet angle must be taken in the range of 75〜90°. The outlet angle is desired to be 150〜160°. For these runner blades flow flows along the blade surface, though it once separates at the leading edge and reattaches at the trailing edge. The flow velocity takes large value at the pressure surface and smaller values at the suction surface at the center of the blade width. Deviation angle, i.e., the difference of blade outlet angle and flow outlet angle, takes zero value, if proper design is conducted. The ratio of wake width to the blade pitch becomes larger, if the blade thickness is larger. If the blade outlet angle is larger than 160°, the outlet flow circulate. Inlet vortex arise because of the sudden flow turning at the blade inlet. The extent of inlet vortex is influenced by the inclination angle of blade. The inclination ratio,i.e., the ratio of blade inclination angle θand the inlet angle βィイD21ィエD2 is important. The maximum values of pressure and discharge can be obtained at (θ/βィイD21ィエD2) =0.35. Considering the above affairs, the values βィイD21ィエD2)=75〜90°, (θ/βィイD21ィエD2) =0.35 and βィイD22ィエD2=150〜160°are suitable for the blade design. The blade thickness must be thinner as possible.
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安達勤,杉田尚弘他: "シロッコファンの性能と内部流れ" 日本機械学会関西学生会卒業研究発表講演会. (1999)
Tsutomu Adachi、Naohiro Sugita 等:“多叶片风扇的性能和内部流动”日本机械工程学会关西学生会毕业研究报告讲座(1999 年)。
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安達 勤、杉田 尚弘: "シロッコファンの性能と内部流れ"日本機械学会関西支部卒業研究発表講演会. 96 (1999)
Tsutomu Adachi、Naohiro Sugita:“西洛克风扇的性能和内部流动”日本机械工程师学会关西分会毕业研究报告96(1999)。
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安達 勤、杉田 尚弘: "シロッコファンの性能と内部流れ"日本機械学会関西支部卒業研究発表会講演会. 96 (1999)
足立勉、杉田直宏:《西洛克风扇的性能与内部流动》日本机械工程学会关西分会毕业研究报告讲座96(1999)。
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Tsutomu Adachi, Naohiro Sugita: "Flow and its Performance of a Sirocco Fan"Preprint of the 42th Turbomachinery Society of Japan. (in Japanese). 37-42 (1999)
Tsutomu Adachi、Naohiro Sugita:“多叶片风扇的流动及其性能”第 42 届日本涡轮机械学会预印本。
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安達勤: "Turbomachinery Fluid Dynamics and Heat Transfer" Marcel Deber Inc, 349-365(440) (1997)
Tsutomu Adachi:“涡轮机械流体动力学和传热”Marcel Deber Inc,349-365(440) (1997)
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