Throat area control device and method in turbine guide vane electric welding process
A turbine guide vane and control device technology, applied in auxiliary devices, manufacturing tools, welding equipment, etc., can solve the problems of unqualified throat area of turbine blades, welding quality restricted by casting wool, scrapping, etc., and achieve advanced design concepts, The effect of precise device design and low experience requirements
Active Publication Date: 2018-03-16
AECC AVIATION POWER CO LTD
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Problems solved by technology
[0003] The object of the present invention is to provide a throat area control device and method in the spot welding process of turbine guide vanes, which solves the problem that the existing welding process does not control the throat area of the turbine that affects the important performance of the aeroengine, and the welding quality is restricted. Because of the casting wool, the turbine blade throat area caused by welding is unqualified and scrapped
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[0045] The present invention will be further described in detail below in conjunction with the drawings.
[0046] Such as figure 1 As shown, the present invention provides a throat area control device during spot welding of turbine guide blades, which includes a double-blade positioning fixture, a pre-welding measuring tool, and a welding fixture. Among them, the double-blade positioning fixture serves for quick clamping and The function of disassembling the double blade body; the pre-welding measuring tool is used to fine-tune the blade throat area by matching with the double blade body positioning fixture; the welding fixture is used to weld the adjusted blade body and the edge plate to complete the qualified throat area Turbine blades.
[0047] The double blade positioning fixture includes a compression screw 1, a rotary compression beam 2, a first compression block 3, an area adjustment block 4, a blade positioning and matching base 5, a circular permanent magnet ring 6 and a p...
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The invention provides a throat area control device and method in turbine guide vane electric welding process. Before a vane, firstly, the turbine guide vane is fixed through a dual-vane-body positioning clamp; then, the throat area on the welded turbine vane is calculated through a measuring tool for measuring before welding; and finally, by means of an area adjusting block, fine adjustment is performed on an angular direction positioning point of the vane body, and the throat area is adjusted qualified. An inductor external controller adopted by the device and method can display the area ofthe corresponding state in real time and transiently, and according to the corresponding changing, the area is controlled within a qualified range before welding and then is fixed. Due to the fact that the device is accurate in design, the requirement on experience of an operator is low. The device is successfully applied in actual welding, an original outdated welding method is replaced, and because the design concept is advanced, the device is easily popularized in turbine guide vane welding.
Description
Technical field [0001] The invention is applied to the combined welding of high-vortex guide blades, and is particularly suitable for a throat area control device and method during spot welding of turbine guide blades. Background technique [0002] In the field of aero-engines, the domestic welding of relatively complex high-pressure turbine guide blades adopts integrated fixed clamping welding. The welding process does not control the area of the turbine throat that affects the important performance of aero-engines. The welding quality is restricted by the casting material, which causes the welding As a result, the turbine blade throat area is unqualified and scrapped. This technology has been solidified and applied for more than ten years and has a huge impact on the production of aero engines. In order to solve the shortcomings of the technology in practical application, it is urgent to innovate in technology and invent a method and control device to solve this problem. Sum...
Claims
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Login to View More IPC IPC(8): B23K37/04B23K37/00B23K11/36B23K11/11
CPCB23K11/11B23K11/36B23K37/00B23K37/04B23K37/0443
Inventor 温学兵王冬齐永超杨嘉肖红冯永龙崔保卫王瑞科
Owner AECC AVIATION POWER CO LTD