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Design method for low-rotary-inertia turbine

A technology of moment of inertia and design method, applied in calculation, special data processing applications, instruments, etc., can solve problems such as optimization, inability to effectively improve the low-speed response of the turbocharger, and inability to effectively reduce the moment of inertia of the turbine. The effect of reducing and reducing the probability of solidification defects and improving mechanical efficiency and reliability

Active Publication Date: 2017-05-31
HUNAN TYEN MACHINERY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the existing technology, the optimization of the turbine blades is mainly carried out, and the heavy turbine wheel back is not optimized, and the turbine wheel back occupies a large part of the turbine's own weight, so the existing technology cannot effectively reduce the moment of inertia of the turbine, so that The low-speed response of the supercharger cannot be effectively improved

Method used

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  • Design method for low-rotary-inertia turbine
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  • Design method for low-rotary-inertia turbine

Examples

Experimental program
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Effect test

Embodiment 1

[0042] Such as figure 2 As shown, it is a wheel back structure diagram of a low moment of inertia turbine provided by Embodiment 1 of the present invention. The blank part in the right figure is the part removed compared with the existing turbine, and the shaded part is the retained wheel back and ribs. A structure in which 5 center-radiating reinforcing ribs are evenly arranged is adopted, the cross-section of the reinforcing ribs is rectangular, and the width and thickness of each section of each of the reinforcing ribs are equal.

[0043] Compared with the existing turbine, the low moment of inertia turbine provided by Embodiment 1 of the present invention is 9% lighter in weight and 7% lower in moment of inertia. Compared with the center of mass of the rotating system composed of corresponding components, the existing turbine rotating system is biased towards the floating bearing at the compressor end. The displacement is 2.2mm, which effectively improves the low-speed re...

Embodiment 2

[0045] Such as image 3 As shown, it is a wheel back structure diagram of a low moment of inertia turbine provided by Embodiment 2 of the present invention. The low moment of inertia turbine adopts a structure with 8 centrally emanating ribs evenly arranged, and the cross section of the ribs is circular , the diameter of each reinforcing rib gradually decreases from the center to the outside.

[0046] Compared with the existing turbine, the low moment of inertia turbine provided by Embodiment 2 of the present invention is 12% lighter in weight and 9% lower in moment of inertia. The shift is 2.5mm, which effectively improves the low-speed response and mechanical efficiency of the supercharger.

Embodiment 3

[0048] Such as Figure 4 As shown, it is a wheel back structure diagram of a low moment of inertia turbine provided by Embodiment 3 of the present invention. The low moment of inertia turbine adopts a structure with 8 centrally emanating ribs evenly arranged, and the cross section of the ribs is rectangular. The width of each reinforcing rib gradually decreases from the center to the outside, and the thickness remains constant.

[0049] Compared with the existing turbine, the low moment of inertia turbine provided by Embodiment 3 of the present invention is 8% lighter in weight and 6% lower in moment of inertia. The displacement is 2.1mm, which effectively improves the low-speed response and mechanical efficiency of the supercharger.

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Abstract

The invention discloses a design method for a low-rotary-inertia turbine. The design method comprises the steps that a primary scheme for the low-rotary-inertia turbine is set, and a digital model of an existing turbine and a digital model of the primary scheme of the low-rotary-inertia turbine are built; stress analysis is conducted on the exiting turbine and the primary scheme of the low-rotary-inertia turbine; stress analysis results are processed. According to the low-rotary-inertia turbine obtained through the design method for the low-rotary-inertia turbine, the high mechanical strength and the long life are achieved, the mass and the rotary inertia of the turbine are decreased, the low-speed responsiveness of a pressurizing system and the mechanical efficiency and reliability of a bearing system can be effectively improved, and then the pressurizer efficiency is improved; meanwhile, due to the fact that compared with the existing turbine, part of materials on the turbine back of the low-rotary-inertia turbine are removed, the integral uniformity of the turbine is improved.

Description

technical field [0001] The invention relates to the field of turbochargers, in particular to a low moment of inertia turbine design method. Background technique [0002] Since the beginning of this century, governments at home and abroad have successively raised the fuel consumption and exhaust emission standards of road vehicles and non-road vehicles in order to cope with global warming and oil crisis. The depletion of oil resources and the increasing emission standards have led many countries to guide the development of engines in the direction of small displacement and high power. With the development of low fuel consumption rate, turbocharging technology can improve vehicle engine power, reduce energy consumption and reduce emissions. This technology is currently one of the most effective means to achieve the goal of energy saving and emission reduction in the automotive industry and to improve engine efficiency. [0003] The turbine is one of the core components of the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
CPCG06F30/17
Inventor 陈少林刘朝峰靳鹏龙鑫吴葱史亚东朱茂蒙刘艳东张涛
Owner HUNAN TYEN MACHINERY
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