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A New Design Method for Airfoil of Bidirectional Axial Flow Pump

A technology of airfoil design and design method, which is applied to parts, pumps, pump components, etc. of pumping devices used for elastic fluids, can solve problems such as cavitation, poor cavitation resistance, vibration, etc., and achieve low efficiency , easy operation, and simple design method

Active Publication Date: 2017-02-22
JIANGSU UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0005] Aiming at the common axial flow pump airfoil existing in the prior art, it can only achieve good results when it is running in the forward direction, and vibration, cavitation, noise, and symmetrical S-shaped airfoils have low efficiency and anti-steam during reverse operation. Corrosion performance is relatively poor and other problems; the invention provides a novel bidirectional axial flow pump airfoil design method, the axial flow pump impeller using the airfoil design method can achieve higher efficiency and comprehensive performance when operating in both directions

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  • A New Design Method for Airfoil of Bidirectional Axial Flow Pump
  • A New Design Method for Airfoil of Bidirectional Axial Flow Pump
  • A New Design Method for Airfoil of Bidirectional Axial Flow Pump

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Embodiment Construction

[0029] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments, but the protection scope of the present invention is not limited thereto.

[0030] A novel method for designing the airfoil of a bidirectional axial flow pump, including a common axial flow pump blade designed with NACA airfoil, the steps are as follows:

[0031] (1) Measure the airfoil coordinates of the common axial flow pump blade by a three-coordinate measuring instrument, thereby draw the corresponding airfoil on the xy coordinate axis, and obtain the original airfoil 1; as figure 1 As shown, the chord length of the original airfoil 1 is 100 mm, the relative camber is 2%, the relative thickness is 12%, and the maximum camber position is located at 2 / 5 of the chord length.

[0032] (2) On the xy coordinate axis, the bone line leading edge point A of the original airfoil 1 is placed at the origin (0,0), and the original airfoil is enlarged by ...

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Abstract

The invention provides a design method for a novel bi-directional axial flow pump airfoil profile. The method comprises the steps that airfoil profile coordinates of the different positions from the wheel hub to the wheel rim of a vane of a common axial flow pump are measured through a three coordinate measuring instrument, a corresponding airfoil profile is drawn on an xy coordinate axis, and an original airfoil profile is obtained; on the xy coordinate axis, the front edge point A of the bone line of the original airfoil profile is placed at the origin (0,0), and the original airfoil profile is enlarged to serve as a forward airfoil profile; the original airfoil profile is shrank, and an airfoil profile which is centrosymmetric to the shrank original airfoil profile about the origin serves as a reverse airfoil profile; translation is performed on the reverse airfoil profile to enable the front edge point B of the bone line of the reverse airfoil profile to be coincide with the back edge point C of the bone line of the forward airfoil profile, a chord line formed by connecting a back edge point E and a front edge point D passes though the origin and is parallel to an x axis, and the novel bi-directional axial flow pump airfoil profile can be obtained after arc lines near a back edge point B are processed. The design method for the novel bi-directional axial flow pump airfoil profile is simple and easy to operate; compared with an S-shaped symmetric airfoil profile, when the flow comes in the reverse direction, the novel bi-directional axial flow pump airfoil profile is more in accordance with the flow characteristics of hydromechanics, and the anti-cavitation property is relatively better.

Description

technical field [0001] The invention relates to the technical field of bidirectional axial flow pump airfoil design, in particular to a novel bidirectional axial flow pump airfoil design method based on ANSYS simulation design. Background technique [0002] In some pumping stations along rivers and lakes, coastal areas, and South-to-North Water Transfer Projects, it is often necessary to achieve water diversion and drainage through two-way pumping. At present, there are three commonly used ways to realize the two-way pumping function: to change the channel through the gate station to realize the two-way pumping, such as the Jiangdu pumping station; Wait for the pumping station; turn the blade of the one-way pump 180° and reverse the impeller to achieve it, such as the Qinhuai Xinhe pumping station. [0003] Ordinary axial flow pumps with unidirectional airfoils can also achieve reverse pumping when the impeller is reversed, but because the airfoil of the blade is in the rev...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F04D29/54F04D29/18
CPCF04D29/181
Inventor 魏洋洋马新华冯琦王伟蒋小平闫婧竹张琳
Owner JIANGSU UNIV
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