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Synergistic turbocharger with gradual change air flue

An air passage and turbine technology, which is applied in the field of exhaust turbochargers, can solve the problems of unreasonable structure, inability to increase the intake pressure at the intake end of the turbine shell, and affecting the output power of the turbine.

Inactive Publication Date: 2013-01-02
江苏索特动力工程有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In the existing exhaust-type turbocharger, the structure of the turbine shell 1 in the turbine and the pressure shell 8 in the compressor is unreasonable. In the gradual change air passage of the turbine shell 1, the air outlet gap directly leading to the turbine is designed This structure can neither increase the intake pressure at the intake end of the turbine shell nor reduce the exhaust pressure of the turbine. The pressure difference between the intake end and the exhaust end of the turbine has not been maximized. Under these conditions, the further improvement of the output power of the turbine is affected, and the structure design of the air outlet gap directly affects the output power of the turbine
Similarly, the fit gap structure between the booster impeller and the pressure shell in the compressor also directly affects the output compressed air density of the compressor, thereby affecting the improvement of the turbocharger's supercharging effect

Method used

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  • Synergistic turbocharger with gradual change air flue
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  • Synergistic turbocharger with gradual change air flue

Examples

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Embodiment 1

[0015] Example 1: A gradual airway synergistic turbocharger, such as figure 2 As shown, it includes a turbine shell 1, a turbine 2, a turbine shaft 3, a sliding bearing 4, an intermediate body 5, a diffuser plate 6, a supercharged impeller 7 and a compressor shell 8. The turbine 2 and the supercharged impeller 7 are respectively mounted on the turbine shaft 3 At both ends, the turbine 2 is located in the turbine shell 1, the supercharged impeller 7 is located in the compressor shell 8, the turbine shaft 3 is installed on the intermediate body 5 through two sliding bearings 4, and the turbine shell 1 is fixedly installed on the left side of the intermediate body 5. A heat shield 9 is provided between the two. The left side of the diffuser plate 6 is hermetically connected with the intermediate body 5, and the right side of the diffuser plate 6 is sealed and connected with the pressure shell 8 into one body. The lubricating oil path on the intermediate body 5 Connected with two s...

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Abstract

The invention discloses a synergistic turbocharger with a gradual change air flue. A lower gradual change air flue is divided into a left intake gap and a right intake gap by a lower air flue partition board in a turbine shell, an upper gradual change air flue is divided into a left exhaust gap and a right exhaust gap by an upper air flue partition board, and the width of the left exhaust gap is greater than the width of the left intake gap; the width of the right exhaust gap is greater than the width of the right intake gap; in a gas compressor, the width of an upper air outlet is equal to the width of a lower air inlet. Owing to redesign of the intake gap and the exhaust gap of the upper gradual change air flue of the turbine shell to the turbine, the intake gap at the starting end is smaller than the exhaust gap of a terminal, the push pressure of the intake starting end of the turbine shell is increased, the exhaust pressure of the terminal is reduced, and the output power of the turbine is improved. Through changing the sizes of the intake gap of the gradual change air flue on a pressing shell and the exhaust gap of the terminal, the intake gap of the starting end is greater than the exhaust gap of the terminal, the oxygen density in the output compressed air is improved, and supercharge and oxygenation performances of the turbocharger are improved.

Description

【Technical Field】 [0001] The invention relates to a turbocharger, in particular to an exhaust-type turbocharger. 【Background technique】 [0002] Exhaust turbocharger uses high-temperature and high-temperature exhaust gas discharged from an internal combustion engine as a power source. The high-temperature and pressure exhaust gas discharged from the internal combustion engine is introduced into the turbine in the turbocharger, and the energy contained in the exhaust gas is used to drive the turbine in the turbine to rotate, thereby driving the turbine Rotation, while driving the coaxial compressor impeller to rotate, the compressor will compress and boost the intake air to the intake system of the diesel engine, filling the internal combustion engine cylinder with high-density air, which can increase the fuel injection volume per time , It can not only increase the output power of the same type internal combustion engine, but also significantly improve the economy of the internal...

Claims

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Application Information

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IPC IPC(8): F02B37/00F01D25/24F04D29/40
CPCY02T10/144Y02T10/12
Inventor 汤俊韩青曹红艳胡兵陆仁杰
Owner 江苏索特动力工程有限公司
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