Double-layer volute structure of turbocharger compressor

A turbocharger and compressor technology, applied in the field of power machinery, can solve the problems of narrowing the flow rate and increasing the pressure ratio, and achieve the effects of reducing the compression loss, improving the flow capacity, and reducing the complexity of the processing process

Inactive Publication Date: 2011-05-25
CHINA NORTH IND GRP NO 70 RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The invention provides a double-layer volute structure of a turbocharger compressor, which meets the gas collection requirements of a back-to-back two-stage compressor, and solves the problem that the pressure ratio increases and the flow rate narrows after the turbocharger adopts dual compressors

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  • Double-layer volute structure of turbocharger compressor
  • Double-layer volute structure of turbocharger compressor
  • Double-layer volute structure of turbocharger compressor

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Embodiment Construction

[0009] Such as figure 1 As shown, a double-layer volute of a turbocharger compressor includes an intake housing 1 and a volute 2 . The intake housing 1 is connected with the volute 2 with a pressing plate and screws. The intake shell 1 adopts an intake bypass recirculation structure, the slotting position is in the middle of the long and short blades of the first stage compressor impeller, and the slot width is 7% to 9% of the radius of the guide section of the intake shell. %. The gas flow path of the volute 2 is divided into two stages, the first stage adopts an annular flow path, and the second stage adopts a conventional snail-shaped flow path. The design features of the annular flow channel are: from the outlet of the diffuser to the largest radius of the flow channel, etc., it is designed according to the width, which belongs to the diffuser section in the annular flow channel; from the largest radius of the flow channel to the outlet of the flow channel, it is designe...

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Abstract

The invention discloses a double-layer volute structure of a turbocharger compressor. The double-layer volute structure comprises an air intake shell (1) and a volute (2), wherein the air intake shell (1) is connected with the volute (2) through a pressing plate and screws; the air intake shell (1) has an intake air bypass recycling structure; and an air flow passage of the volute (2) is divided into two stages of which the first stage is an annular flow passage and the second stage is the conventional snail-shaped flow passage. In terms of design features, the annular flow passage is designed according to equivalent width from a diffuser outlet to a part with the maximum radius of the flow passage and is designed according to a constant section from the part with the maximum radius of the flow passage to a flow passage outlet. By using the double-layer volute structure of the turbocharger compressor, the complexity of processing technology is reduced, the supercharging pressure and the capacity of doing work are improved, the loss of the compressed air in the annular flow passage is reduced, and the circulating capacity of the annular flow passage is improved.

Description

Technical field: [0001] The invention belongs to the technical field of power machinery, and in particular relates to a turbocharger compressor double-layer volute structure. Background technique [0002] As the power density of the engine increases, the technical indicators of the turbocharger need to be continuously strengthened, which requires a turbocharger with higher performance. Therefore, the development of a turbocharger with a high pressure ratio, high efficiency, high reliability, and a wide range of available flow rates is a necessary condition for increasing engine power and improving engine dynamic performance, but this is beyond the single-compressor turbocharger. The pressure ratio, flow range and efficiency level that the compressor can achieve. Many engine applications are forced to adopt a two-stage turbocharging system. From a performance point of view, a two-stage turbocharging system has many advantages, but it also has the following disadvantages comp...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F04D29/42
Inventor 邓春龙王振彪王林起
Owner CHINA NORTH IND GRP NO 70 RES INST
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