某型三叶螺旋桨的设计及性能试验

项松; 佟刚; 吴江; 赵为平; 杨康; 王吉

doi:10.13224/j.cnki.jasp.2016.08.001

某型三叶螺旋桨的设计及性能试验

doi: 10.13224/j.cnki.jasp.2016.08.001

项松^1,2,
佟刚^1,2,
吴江^1,2,
赵为平¹,
杨康^1,2,
王吉^1,2

1. 沈阳航空航天大学辽宁省通用航空重点实验室, 沈阳 110136;
2. 辽宁通用航空研究院科研管理办公室, 沈阳 110136

基金项目:

辽宁省“百千万人才工程”项目（2014921048）；辽宁省科学技术计划面上项目（2015020167）；沈阳市科学技术计划项目（F16-205-1-07）

详细信息

作者简介:
项松(1978-),男,辽宁辽阳人,高级工程师,硕士,主要从事高效率螺旋桨设计技术研究.

中图分类号: V211.44
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- 文章访问数: 1114
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- 被引次数: 0
出版历程
- 收稿日期: 2016-02-04
- 刊出日期: 2016-08-28

Design and performance test of a kind of three-blade propeller

1. Liaoning Key Laboratory of General Aviation, Shenyang Aerospace University, Shenyang 110136, China;
2. Management Office of Science and Research, Liaoning General Aviation Academy, Shenyang 110136, China

摘要

摘要: 根据飞行速度、需用拉力、螺旋桨转速等参数，设计了某型飞机的三叶螺旋桨，获得了弦长和桨叶角沿着径向的分布.制造了三叶复合材料螺旋桨（直径为1.75m），在螺旋桨试验台上测试了不同转速下螺旋桨的拉力.为了获得螺旋桨的动态性能，制造了螺旋桨的缩比模型（直径为0.96m），在西北工业大学NF-3风洞的三元试验段测试了螺旋桨的气动性能数据，包括：拉力、扭矩、功率、效率.结果表明：螺旋桨最大效率为85.63%，所设计的三叶复合材料螺旋桨适用于螺旋桨需用功率为70kW左右的发动机（比如Rotax912），提出的螺旋桨设计方法具有较好的应用价值.
- 三叶螺旋桨 /
- 气动性能 /
- 风洞试验 /
- 效率 /
- 通用航空
Abstract: According to the flight velocity, the required thrust and rotation speed of propeller, the three-blade propeller of an aircraft was designed, and the chord length and pitch angle distribution along the radial direction of propeller were obtained. The three-blade composite propeller (diameter of 1.75m) was manufactured based on the designed results, and the thrust of this propeller under various rotation speeds was measured using a propeller test rig. In order to obtain the dynamic performance of propeller, the scaled propeller(diameter of 0.96m) was manufactured, while the aerodynamic performance data of thrust, torque, power and efficiency were measured at the three-dimension test section of Northwestern Polytechnical University NF-3 wind tunnel. Results show that the maximum efficiency of propeller is 85.63%, this three-blade propeller is suitable for the 70kW engine (for example: Rotax 912), so this designed method of propeller has good applicable value.
- three-blade propeller /
- aerodynamic performance /
- wind tunnel test /
- efficiency /
- general aviation

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参考文献(18)

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