Wing sectional material combination type turbine centrifugal impeller

A combined and centrifugal technology, applied in the direction of non-variable pumps, supporting elements of blades, components of pumping devices for elastic fluids, etc., can solve problems such as high production costs, poor versatility, and complex molds

Inactive Publication Date: 2015-05-13
张凤荣
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The performance of turbomachinery largely depends on the structure and shape of the turbine impeller blades. The existing centrifugal airfoil impeller technology often adopts precision milling and manual shaping methods for processing, which is difficult to process and expensive to produce. High, it is difficult to form large-scale production
Although injection molding is used for small centrifugal impellers, the cost of molds remains high and the production cycle is long, which is far from meeting the dynamic needs of the increasingly competitive market
Centrifugal impellers with a slightly larger machine size are usually limited in tonnage by injection molding, and when the blades are airfoil-shaped, the mold is complicated and it is difficult to pull the core out of the mold
Most of the existing centrifugal fans are in the form of single-plate blades, which have low efficiency and high noise; although some impellers adopt a single-plate space-distorted blade structure to reduce noise, they still do not achieve the purpose of improving efficiency. In order to obtain High-efficiency centrifugal impellers are usually realized by precision casting, injection molding, die-casting and other methods, which makes the manufacturing cost of the fan high, the mold making cycle is long, and the versatility between different machine numbers is poor; the centrifugal impeller mostly uses single-plate blades, although simplified Manufacturing process, but at the same time generally lead to the consequences of low operating efficiency, narrow range of working conditions, and high noise
Although some impellers use airfoil blades, most of them are limited to manual patchwork welding, the accuracy of the airfoil is poor, the production cost is high, and it is not suitable for large-scale and large-scale production

Method used

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  • Wing sectional material combination type turbine centrifugal impeller
  • Wing sectional material combination type turbine centrifugal impeller
  • Wing sectional material combination type turbine centrifugal impeller

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0064] Embodiment 1: the making of centrifugal airfoil profile

[0065] Centrifugal airfoil blade profile of the present invention is made into following two big classes:

[0066] 1. Aviation aerodynamic standard airfoil structure profiles

[0067] The document "Method for Manufacturing High-efficiency Energy-saving Fan Impeller Using Airfoil Structure Sections" discloses the cross-sectional structure of standard airfoil structure sections of aviation aerodynamics, including asymmetric airfoils (as attached Figure 6 ), symmetrical airfoil (if attached Figure 7 ), and the airfoil derived from the symmetrical airfoil based on the center arc is also included here (as shown in the attached Figure 8 ), the middle arc can be a single arc or a combination of multiple arcs, it can also be a part of an elliptic curve, or it can be a part of other function curves and their combination;

[0068] 2. Composite airfoil structure profile generated based on aerodynamic standard airfoil ...

Embodiment 2

[0075] Embodiment 2: Select the type of airfoil structure profile, and determine the section form

[0076] (1) Determine the airfoil profile line of the airfoil according to the engineering calculation flow pattern;

[0077] (2) The airfoil section size is not large, or the airfoil solid structure can be selected when the blade wear resistance, strength, stiffness and other conditions are considered;

[0078] (3) When the size of the airfoil section is large, different forms of hollow section structures can be selected under the conditions of blade strength and stiffness;

[0079] (4) When the size of the airfoil section is large, the combined blade section structure can also be used: it can be a joint structure, such as an attached Figure 15 ; It can also be a mortise and tenon structure, such as attached Figure 16 .

Embodiment 3

[0080] Example 3: blade profile material

[0081] According to the different media (occasions) applicable to the impeller blades, different materials are selected. Blade material can be metal material, non-metal material, composite material;

[0082] The airfoil blade profile is manufactured by extruding, extruding and drawing.

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Abstract

The invention provides a wing sectional material combination type turbine centrifugal impeller and belongs to the field of turbine mechanical vane machining. Aviation aerodynamic force standard wing type structure sectional materials and composite wing type structure sectional materials generated on the basis of a standard wing type are used, the structure sectional materials are used as vane blank materials, and a centrifugal impeller vane is manufactured. A wing type structure vane with the uniform section or the non-uniform section is used, according to the difference of calculating flow patterns and using places (media), the space warping structure of the vane is determined, and the front edge and the back edge of the vane can be decorated according to situations. The front disc space curve face and the back disc space curve face are matched through the methods of cutting, stamping and forming milling, and the vane, a front disc and a back disc are integrally connected to form the impeller. The method is suitable for large-batch, large-scale and module production of centrifugal impellers, universality is high, the centrifugal impeller is especially suitable for centrifugal fan and centrifugal water pump industries, and great promotional value is achieved.

Description

Technical field [0001] The present invention involves the field of fan technology. Specifically, it is a combination of a combination of wing profile. Background technique [0002] The performance of transparent machinery to a large extent depends on the structure and shape of the diaphragm impeller blades. The existing centrifugal wing -type leaf wheel technology often uses precision milling and manual plastic surgery.High, it is difficult to form large -scale production.Although the small centrifugal leaf wheels are used in injection molding, the cost of molds is high, and the production cycle is long, which is far from meeting the increasingly competitive dynamic needs of the market.The centrifugal leaf wheel with a slightly large machine number is often limited by the tonnage of injection molding, and when the leaves are wing type, the mold is complex and the mold is difficult to draw core.Most of the existing centrifugal fans are used in the form of single -board blades. The...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F04D29/28F01D5/14
Inventor 张凤荣韩军王雪鹏
Owner 张凤荣
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