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Double-channel turbine bypass bleeding device

A bleed device and double-channel technology, which is applied to gas turbine devices, machines/engines, internal combustion piston engines, etc., can solve the problem of increased mechanical wear of actuators and transmission mechanisms, instability of turbine inlet pressure and waste gas bypass, and impact on turbines. Supercharger engine working stability and other issues to achieve the effect of improving working stability, avoiding constant changes in valve opening, and avoiding abnormal wear and tear

Active Publication Date: 2011-02-16
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

The swing of the valve cover leads to unstable turbine inlet pressure and waste gas bypass flow, which affects the working stability of the turbocharger and even the engine;
[0008] 3. The continuous swing of the valve cover also leads to increased mechanical wear of the actuator and the transmission mechanism, shortens the service life, and causes abnormal noise

Method used

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  • Double-channel turbine bypass bleeding device
  • Double-channel turbine bypass bleeding device
  • Double-channel turbine bypass bleeding device

Examples

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Embodiment Construction

[0032] Examples, as attached figure 2 As shown, a double-channel turbine bypass air-bleed device for a double-channel turbocharger whose valve opening and bypass air-bleed volume can be precisely controlled includes a turbine volute 2, and the turbine volute 2 is provided with The first air intake channel 3a of the volute and the second air intake channel 3b of the volute, the first air intake channel 3a of the volute is communicated with the first air release channel 1a, and the second air intake channel 3b of the volute is communicated with the second air discharge channel 3b. Air channel 1b, the outlet of the first air release channel 1a and the second air release channel 1b is provided with a concave valve seat 4, and a common valve cover 6 is provided on the concave valve seat 4, and the valve cover 6 It is slidingly connected with the concave valve seat 4, and the valve cover 6 is in transmission connection with the power drive device.

[0033] The concave valve seat 4...

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PUM

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Abstract

The invention discloses a double-channel turbine bypass bleeding device which comprises a turbine volute, wherein the turbine volute is provided with two inlet channels, the two inlet channels are respectively communicated with a bleeding channel, the outlets of the two bleeding channels are provided with concave valve bases, the concave valve bases are provided with a shared valve cover, and the valve cover and the concave valve base form a slip connection, so that the characteristic curve of the flow of valves and the flow area of the valves almost changes linearly. By using rack-and-pinion transmission, the accurate control on the opening and the flow area of the valves can be realized. Thus, the invention can accurately control the amount of bypass waste gas, thereby realizing the optimum matching of a pressure booster and an engine.

Description

technical field [0001] The invention relates to a waste gas bypass device of a turbocharger, in particular to a double-channel turbine bypass exhaust device for dual-channel simultaneous discharge of a dual-channel turbine. Background technique [0002] For vehicle engines, in order to solve the performance problem of low working conditions, the high working condition bleed configuration is mostly used. At this time, the design of the turbocharger is to make the engine performance below the middle speed to obtain the maximum torque, that is, the supercharger and the diesel engine are matched according to the maximum torque condition. When the engine rotates at a high speed, in order to limit the boost pressure, the maximum explosion pressure and the speed of the supercharger within the allowable range, part of the exhaust or part of the supercharged air of the engine is discharged through the purge valve, so that the supercharger A section of the operating line of the compr...

Claims

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Application Information

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IPC IPC(8): F02C6/12F02B37/16
CPCY02T10/144Y02T10/12
Inventor 朱智富袁道军王航李永泰杨金玉刘功利张建国宋丽华
Owner 康跃科技(山东)有限公司
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