Three-dimensional nozzle ring vane of variable geometry turbocharger and design method thereof
A technology of turbocharger and nozzle ring, applied in mechanical equipment, machine/engine, gas turbine installation, etc., to achieve the effect of high success rate, widening flow range and improving turbine efficiency
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[0034] The present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.
[0035] The variable geometry turbocharger nozzle ring three-dimensional vanes of the present invention include but are not limited to variable geometry turbochargers (VGT). For convenience of expression, VGT is used as an example for description in this specification.
[0036] The present invention is designed on the basis of NASA's axial flow compressor cascade tests between 1940 and 1960, according to aerodynamic principles. The design of the nozzle ring vanes is mainly formed by stacking several sections of the vanes in the radial direction according to a certain law. attached figure 1 The geometric parameters and flow parameters used in the blade forming are indicated: the leading edge construction angle β q , the trailing edge structural angle β h , intake angle β 1 , outlet angle β 2 , attack angle i, trailing edge bending angle δ,...
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