ROTOR BLADE OF AN AXIAL TURBO-COMPRESSOR

• 1. 将叶片连接在轴流式涡轮压缩机的鼓形转子上 [P] . 中国专利： CN103671251B . 2018.02.09
• 2. 将叶片连接在轴流式涡轮压缩机的鼓形转子上 [P] . 中国专利： CN103671251A . 2014-03-26
• 3. ROTOR BLADE FOR AXIAL TURBO-COMPRESSOR [P] . CS8902619A1 . 1990-10-12

  机译： 轴向涡轮压缩机转子叶片

• 4. Axial-flow turbo-compressor stator blade - has profile angle to peripheral vector smaller at blade tip and root than at blade centre [P] . 法国专利： FR2334853A1 . 1977-07-08

  机译： 轴流式涡轮压缩机定子叶片-叶片顶部和根部的周向矢量轮廓角小于叶片中心

• 5. Axial-flow turbo-compressor stator blade - has profile angle to peripheral vector smaller at blade tip and root than at blade centre [P] . 德国专利： DE2552073A1 . 1977-05-26

  机译： 轴流式涡轮压缩机定子叶片-叶片顶部和根部的周向矢量轮廓角小于叶片中心

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• 7. Effect of Upstream Rotor Vortical Disturbances on the Time-Average Performance of Axial Compressor Stators: Part 2 — Rotor Tip Vortex/Streamwise Vortex-Stator Blade Interactions [O] . T. V. Valkov, C. S. Tan 1998
• 8. EFFECT OF BLADE-THICKNESS TAPER ON AXIAL-VELOCITY DISTRIBUTION AT THE LEADING EDGE OF AN ENTRANCE ROTOR-BLADE ROW WITH AXIAL INLET, AND THE INFLUENCE OF THIS DISTRIBUTION ON ALINEMENT OF THE ROTOR BLADE FOR ZERO ANGLE OF ATTACK [R] . John D Stanits 1953

• 1. Experimental Investigation of Unsteady Pressure on an Axial Compressor Rotor Blade Surface [J] . Qingwei Wang ,Bo Liu ,Xiaorong Xiang . 能源与动力工程（英文） . 2010,第2期
• 2. Nonlinear Pre⁃deformation Method for Compressor Rotor Blade [J] . Yongliang Wang ,Shihao Li ,Longkai Zheng . 哈尔滨工业大学学报:英文版 . 2021,第4期
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