Internal combustion engine variable geometry turbine supercharger nozzle ring components
A technology of turbocharger and internal combustion engine, applied to internal combustion piston engines, engine components, combustion engines, etc., can solve the problem of small changes in intake passages, low boost regulation performance, and blade material performance that cannot better meet the requirements of use, etc. problems, to achieve the effects of small losses, reduced fuel consumption, and improved economical use
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[0020] In Figures 1 and 2,
[0021] The nozzle ring assembly of the present invention is a series of products, suitable for turbochargers with a turbine diameter of 30-150mm, and suitable for use with an engine power of 50-1000KW. It includes a fork 1, a mounting plate 2 and blades 3. The mounting plate 2 is in the shape of a ring, and three groups of blades 3 are evenly spaced and arranged in the same direction on the same circumference of the side of the mounting plate 2, and each group is composed of three blades 3. Each group of blades is separated from each other. According to the size of the turbocharger, it can also be grouped into four or five groups. According to the size of the turbocharger, each group can also be composed of four or five pieces. Each group of blades 3 can be opened and stacked with each other at the same time. On the mounting plate 2, there are three connection holes 4 between the positions of each group of blades. On the other side of the mounting...
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