Double-layer channel variable-section turbine control device

A technology of control device and variable cross-section, which is applied in the direction of gas turbine devices, mechanical equipment, engine components, etc., to achieve the effect of changing cross-sectional area, solving cost problems, and simply controlling valves

Active Publication Date: 2010-04-14
康跃科技(山东)有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The problem to be solved by the present invention is to provide a double-channel variable-section turbocharger control device for the limitations of traditional variable-section turbochargers, which can effectively solve the problem of traditional turbochargers with fixed-section turbochargers and waste gas bypass increases. At the same time reduce the complex adjustment structure of the rotary vane type and axially movable variable-section turbocharger, and realize the control function of the variable-section turbocharger

Method used

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  • Double-layer channel variable-section turbine control device

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0035] Example 1, such as figure 1 As shown, a double-layer channel variable cross-section turbine control device includes a single-inlet turbine shell 1, and the single-inlet turbine shell 1 is provided with an intake outer flow channel 2 and an intake inner flow channel 3, and the intake air flows out The channel 2 is located on the circumferential outside of the air intake inner flow channel 3, and a partition wall 21 is provided between the air intake outer flow channel 2 and the air intake inner flow channel 3. The air intake inner flow channel 3 has an air inlet 6 between which An outer runner air inlet 5 is provided near the air inlet 6 on the next wall, and an air inlet control device is arranged at the outer runner air inlet 5 .

[0036] The front end of the intake inner runner 3 is directly connected to the air inlet 6, and the high-temperature exhaust gas discharged from the engine directly enters the intake inner runner 3 along the inlet 6 and then provides power t...

Embodiment 2

[0044] Example 2, such as Figure 4 As shown, a double-layer channel variable cross-section turbine control device includes a double-inlet turbine housing 1, and the double-inlet turbine housing 1 is provided with an air inlet 6 located on the right side of the double-inlet volute, and the turbine housing 1 is equipped with There are intake outer flow channel 2 and intake inner flow channel 3 located on the right side of the double inlet volute, the intake outer flow channel 2 is located on the circumferential outer side of the intake inner flow channel 3, the front end of the intake inner flow channel 3 is connected to the air inlet 6 is directly connected, and the high-temperature exhaust gas discharged from the engine directly enters the intake inner flow channel 3 on the right side of the double-inlet volute along the air inlet 6, and then provides power to the turbine rotor, forming an internal flow on the right side of the double-inlet volute Road flow direction 4.

[0...

Embodiment 3

[0053] Example 3, such as Figure 7 As shown, in embodiment 2, the vent valves 12 respectively provided at the outer runner air inlet on the left side of the double-inlet volute and the outer runner air inlet on the right side of the double-inlet volute can also be provided by two sets of valves respectively. The air intake control device is controlled, wherein, the exhaust valve 12 at the inlet of the outer runner on the right side of the double inlet volute is controlled by the original inlet control device, and the air inlet valve 12 at the inlet of the outer runner on the left side of the double inlet volute is controlled by the original inlet control device. The air discharge valve 12 at the position is controlled by the left air intake control device, which includes a control actuator 17 arranged on the left side outside the volute, and the control actuator 17 controls the air discharge valve through the valve transmission pin 9 Exercise alone.

[0054] These two sets o...

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PUM

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Abstract

The invention discloses a double-layer channel variable-section turbine control device, belonging to the field of an internal combustion engine. The double-layer channel variable-section turbine control device comprises a turbine housing, wherein the turbine housing is internally provided with a gas inlet inner channel and a gas inlet outer channel; the gas inlet outer channel is positioned at the outer side of the circumferential direction of the gas inlet inner channel; and a partition wall is arranged between the gas inlet outer channel and the gas inlet inner channel. The double-layer channel variable-section turbine control device is characterized in that the gas inlet inner channel is provided with a gas inlet; the position on the partition wall, close to the gas inlet, is provided with an outer channel gas inlet which is provided with a gas inlet control device; the double-layer channel variable-section turbine control device can effectively guarantee that the double-layer channel variable-section turbine meets the supercharging needs of the all condition range of the engine, simultaneously has no existence of potential unreliability of rotary vane type and axial movement type variable-section turbine supercharger and has simple and reliable products.

Description

technical field [0001] The invention relates to a turbine control device for a variable-section exhaust gas turbocharger, in particular to a double-layer channel variable-section turbine control device, which belongs to the field of internal combustion engines. Background technique [0002] In China, with the implementation of the National III emission regulations, people's demand for engine turbochargers that can take into account both high and low speed performance of the engine is becoming stronger and stronger. Variable cross-section turbochargers have become the focus of research and development at home and abroad, and are currently widely used The structure of the rotating nozzle vane is added inside the turbine and the structure of the diffuser channel is changed axially to meet the requirement of variable cross section. Rotary vane and axially adjustable variable cross-section turbochargers change the flow channel of the turbine by changing the opening between the no...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F01D17/16F02B37/24F02C6/12
CPCY02T10/144Y02T10/12
Inventor 李延昭王航郭锡禄杨恒星郭伦海郭晓伟李永泰
Owner 康跃科技(山东)有限公司
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