Wing type blade combination welding positioning tool

By designing the combined welding positioning tooling of airfoil blades, the problem of inaccurate positioning of blades in the prior art is solved, accurate positioning of blades and efficient welding is achieved, and impeller performance is improved.

CN222957856UActive Publication Date: 2025-06-10ZHEJIANG YILIDA TECH CO LTD
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Patent Information

Application Number
CN202422116395.3
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-08-30
Publication Date
2025-06-10
Estimated Expiration
2034-08-30

AI Technical Summary

Technical Problem

The prior art cannot accurately locate and adjust the combined welding of airfoil blades, resulting in inconsistent molding effects after welding and affecting the performance of the impeller.

Method used

A combined welding positioning tool for airfoil blades is designed, including positioning main body, side baffle, side positioning plate and limiting parts. Through the cooperation of these components, accurate positioning of windward panels, leeward panels, reinforcement ribs and round steel is achieved.

Benefits of technology

The blade design profile curve is achieved completely restored, and the fitting surfaces of different sections can be adjusted as needed, which improves welding accuracy and production efficiency, and reduces the occurrence of defective products.

✦ Generated by Eureka AI based on patent content.

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Abstract

A wing type blade combination welding positioning tool comprises a positioning body, the positioning body is formed by fixedly connecting a first positioning plate, a second positioning plate and a plurality of connecting pieces, a first notch is formed in the upper portion of the first positioning plate, and a second notch is formed in the upper portion of the second positioning plate; the positioning main body limits the movement of the leeward panel, the windward panel and the round steel to be welded along the inside and outside direction through the first notch and the second notch, and the reinforcing rib is arranged between the leeward panel and the windward panel; the side baffle is arranged on one side of the first positioning plate, so that one side of the leeward panel to be welded and one side of the windward panel to be welded abut to be flush with each other; the side baffles and / or the first positioning plate are / is provided with limiting pieces used for limiting the position of the round steel. The side positioning plate is arranged on the side, away from the first positioning plate, of the second positioning plate through an adjusting piece, a third notch is formed in the upper portion of the side positioning plate, and the distance between the side positioning plate and the second positioning plate is adjustable, so that the third notch positions the side of the leeward panel.
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Description

Technical Field

[0001] The utility model relates to a combined welding positioning tool for wing-shaped blades. Background Art

[0002] Figure 1 、 Figure 2 As shown in the schematic diagram of the wing-shaped blade involved in this patent application, which is formed by welding a windward panel, a leeward panel, two stiffeners and a round steel. The existing combined welding of blades all adopts measurement and scribing, and a manual positioning and clamping tooling. This method can neither meet the precise requirements of dimensions, nor has design margins, and cannot be adjusted conveniently and observably.

[0003] Due to the complex shape design of the wing-shaped blade and the need for multiple parts to be combined and paired for welding, there is no special welding positioning tooling in the workshop at present, which cannot guarantee the forming effect after welding and the consistency of each wing-shaped blade, resulting in uncontrollable factors in the performance of the impeller composed of multiple wing-shaped blades. Summary of the Invention

[0004] In view of the deficiencies in the above problems, the utility model provides a combined welding positioning tool for wing-shaped blades.

[0005] To achieve the above object, the utility model provides a combined welding positioning tool for wing-shaped blades, including:

[0006] A positioning main body, which is fixedly connected by a first positioning plate, a second positioning plate and a plurality of connecting pieces. A first notch is opened at the upper part of the first positioning plate, and a second notch is opened at the upper part of the second positioning plate. The positioning main body restricts the movement of the leeward panel, the windward panel and the round steel to be welded in the inner and outer directions through the first notch and the second notch, and the stiffeners are arranged between the leeward panel and the windward panel;

[0007] A side baffle, which is arranged on one side of the first positioning plate to make one side of the leeward panel and the windward panel to be welded abut flush; a limiting member for restricting the position of the round steel is arranged on the side baffle and / or the first positioning plate;

[0008] A side positioning plate, which is arranged on the side of the second positioning plate away from the first positioning plate through an adjusting member. A third notch is opened at the upper part of the side positioning plate, and the distance between the side positioning plate and the second positioning plate is adjustable, so that the third notch positions the side part of the leeward panel.

[0009] Further, there are three connecting pieces and they are arranged in parallel.

[0010] Further, the limiting member includes a welding nut fixedly connected to the first positioning plate and a limiting rod screwed to the welding nut.

[0011] Further, the limiting member further includes a locking nut screwed onto the limiting rod.

[0012] Further, there are two side positioning plates, and the adjusting member includes an adjusting screw rod and a plurality of adjusting nuts screwed onto the adjusting screw rod.

[0013] The beneficial effects of the present utility model compared with the prior art are as follows:

[0014] 1. The outer contour curve of the blade during design can be completely restored, the fitting curved surface of different cross-sections can be adjusted as needed, and the position of the cross-section can also be continuously adjusted manually and steplessly.

[0015] 2. It is highly integrated, can simultaneously satisfy the positioning of four or five parts together, omits the scribing positioning operation, and greatly improves the production efficiency.

[0016] 3. It reduces the difficulty of positioning scribing during manual welding. This set of positioning tooling is designed to not only meet the positioning of each component, improve accuracy, but also reduce the difficulty of scribing operation, improve production efficiency, and reduce defective products. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 is a schematic diagram of the airfoil blade involved;

[0018] Figure 2 is an exploded view of the airfoil blade involved;

[0019] Figure 3 is a schematic diagram of a combined welding positioning tooling for an airfoil blade involved Figure 1 ;

[0020] Figure 4 is a schematic diagram of a combined welding positioning tooling for an airfoil blade involved Figure 2 ;

[0021] Figure 5 is a schematic diagram of the airfoil blade placed in the combined welding positioning tooling for the airfoil blade Figure 1 ;

[0022] Figure 6 is a schematic diagram of the airfoil blade placed in the combined welding positioning tooling for the airfoil blade Figure 2 ;

[0023] Figure 7 is Figure 6 a schematic diagram after hiding the side baffle.

[0024] In the figure: 1. Windward panel; 2. Leeward panel; 3. Reinforcing rib; 4. Round steel; 10. Positioning main body; 101. First positioning plate; 1011. First notch; 102. Connecting piece; 103. Second positioning plate; 1031. Second notch; 20. Side baffle; 30. Limiting piece; 301. Welding nut; 302. Limiting rod; 303. Locking nut; 40. Side positioning plate; 401. Third notch; 50. Adjusting piece; 501. Adjusting screw rod; 502. Adjusting nut. Specific embodiments

[0025] As Figures 1 to 7 Shown in the figure, a wing-shaped blade combined welding positioning tooling according to an embodiment of the present invention includes a positioning main body 10, which is fixedly connected and formed by a first positioning plate 101, a second positioning plate 103 and a plurality of connecting pieces 102. A first notch 1011 is provided in the upper part of the first positioning plate 101, and a second notch 1031 is provided in the upper part of the second positioning plate 103. The positioning main body 10 restricts the movement of the leeward panel 2, the windward panel 1 and the round steel 4 to be welded in the inner and outer directions through the first notch 1011 and the second notch 1031. The reinforcing rib 3 is arranged between the leeward panel 2 and the windward panel 1; the side baffle 20 is arranged on one side of the first positioning plate 101 to make one side of the leeward panel 2 and the windward panel 1 to be welded abut flush; a limiting piece 30 for restricting the position of the round steel 4 is arranged on the side baffle 20 and / or the first positioning plate 101; the side positioning plate 40 is arranged on the side of the second positioning plate 103 away from the first positioning plate 101 through the adjusting piece 50. A third notch 401 is provided in the upper part of the side positioning plate 40. The distance between the side positioning plate 40 and the second positioning plate 103 is adjustable, so that the third notch 401 positions the side part of the leeward panel 2; there are three connecting pieces 102 and they are arranged in parallel; the limiting piece 30 includes a welding nut 301 fixed on the first positioning plate 101 and a limiting rod 302 screwed with the welding nut 301; the limiting piece 30 further includes a locking nut 303 screwed on the limiting rod 302; there are two side positioning plates 40, and the adjusting piece 50 includes an adjusting screw rod 501 and a plurality of adjusting nuts 502 screwed on the adjusting screw rod 501.

[0026] The scheme can completely restore the outer contour curve of the blade design, can adjust the fitting curved surface of different cross-sections as needed, and the position of the cross-section can also be continuously adjusted manually and steplessly; highly integrated, it can simultaneously meet the positioning of four or five parts together, omitting the scribing positioning operation, greatly improving the production efficiency; reducing the difficulty of the positioning scribing work during manual welding. This positioning tooling is designed, which can not only meet the positioning of each component, improve the accuracy, but also reduce the difficulty of the scribing operation, improve the production efficiency and reduce the defective products.

[0027] During specific use, for the convenience of understanding the present invention, it is described in conjunction with the attached drawings;

[0028] See Figures 5 to 7 Before welding, the positioning body 10 formed by the first positioning plate 101, the second positioning plate 103, and the connecting member 102 plays a supporting role. The side baffle 20 keeps the windward panel 1 and the leeward panel 2 in abutting alignment on one side. The limiting member 30 restricts the position of one end of the round steel 4. The two side positioning plates 40 can restrict the position of the other side of the leeward panel 2 away from the side baffle 20. The reinforcing ribs are arranged between the leeward panel and the windward panel. In this way, the accurate positioning of the windward panel, the leeward panel, the two reinforcing ribs, and a round steel is achieved. After that, first, by means of manual spot welding, a plurality of parts are fixedly connected to form an integral wing-shaped blade. Then, the wing-shaped blade is removed from the positioning tooling for full welding.

[0029] The above are only the preferred embodiments of the present invention and are not intended to limit the present invention. For those skilled in the art, the present invention can have various changes and modifications. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included within the protection scope of the present invention.

Claims

1. A combined welding and positioning tool for airfoil blades, characterized in that: include A positioning body (10), the positioning body (10) being formed by a first positioning plate (101), a second positioning plate (103) and a plurality of connecting members (102) being fixedly connected, the first positioning plate (101) having a first notch (1011) formed on its upper portion, the second positioning plate (103) having a second notch (1031) formed on its upper portion, the positioning body (10) limiting the movement of the leeward panel (2), the windward panel (1) and the round steel (4) to be welded in the inward and outward directions through the first notch (1011) and the second notch (1031), and the reinforcing rib (3) being arranged between the leeward panel (2) and the windward panel (1); a side baffle (20), the side baffle (20) being arranged on one side of the first positioning plate (101) so as to abut against one side of the leeward panel (2) and the windward panel (1) to be welded until they are flush; a limiting member (30) for limiting the position of the round steel (4) is arranged on the side baffle (20) and / or the first positioning plate (101); A side positioning plate (40), the side positioning plate (40) being arranged on a side of the second positioning plate (103) away from the first positioning plate (101) through an adjusting member (50), a third notch (401) being provided on an upper portion of the side positioning plate (40), and an adjustable distance between the side positioning plate (40) and the second positioning plate (103), so that the third notch (401) forms a positioning for a side portion of the leeward panel (2).

2. The airfoil blade combined welding positioning tool according to claim 1, characterized in that: There are three connecting members (102) which are arranged in parallel.

3. The airfoil blade combined welding positioning tool according to claim 1, characterized in that: The limiting member (30) comprises a welding nut (301) fixedly connected to the first positioning plate (101) and a limiting rod (302) screwed to the welding nut (301).

4. The airfoil blade combined welding positioning tool according to claim 3, characterized in that: The limiting member (30) further comprises a locking nut (303) screwed onto the limiting rod (302).

5. The airfoil blade combined welding positioning tool according to claim 1, characterized in that: There are two side positioning plates (40), and the adjusting member (50) comprises an adjusting screw (501) and a plurality of adjusting nuts (502) screwed on the adjusting screw (501).