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High-efficiency mixed-flow turbine

A turbine, mixed flow technology, applied in the direction of gas turbine installations, blade support elements, engine elements, etc.

Inactive Publication Date: 2011-04-13
大同北方天力增压技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] The invention provides a high-efficiency mixed-flow turbine, which is used to solve the existing problem of improving the efficiency of the turbine, starting from reducing the gas incident loss, turning loss, and residual speed loss, under the premise of reasonable blade curve and ensuring blade strength Reasonable blade thickness distribution law, and the problem of determining the hub and hub line according to the gas flow field distribution

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Embodiment Construction

[0049] A high-efficiency mixed flow turbine, comprising a turbine blade 1, a hub 2, and a disc 3; the hub 2 is arranged in the axial direction of the hub 3, and the turbine blade 1 is arranged radially of the hub 2; the disc is a semi-open disc ;The shape parameter of the hub is: radius R of the bottom arc of the turbine hub 2 =92mm, turbine inlet hub inclination angle α 2 =32°, turbine outlet hub inclination angle α 3 =6.11°, turbine outlet hub diameter D 0 =φ58mm, turbine inlet hub diameter D b =φ145mm, turbine blade axial height Z m =76.5mm. The number of turbine blades is twelve, and the blade profile curve adopts a double equation model, namely:

[0050] Coordinate Z along the turbine axis direction = 0 ~ 21.65 [mm],

[0051] θ = C 1 { 1 - [ 1 - ( 21.65 ...

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Abstract

The invention discloses a high-efficiency mixed-flow turbine which comprises turbine blades (1), a hub (2) and a turbine disk (3), wherein the center of the turbine disk is axially provided with the hub (2); the hub (2) is provided with the turbine blades (1) in the radial direction; and each turbine blade (1) is composed of a convex surface (4) and a concave surface (5). The shape parameters of the hub is as follows: the turbine hub bottom arc radius R2 is 92mm, the turbine inlet hub inclination angle alpha 2 is 30 degrees, the turbine outlet hub inclination angle alpha 3 is 6.11 degrees, the turbine outlet hub diameter Do is phi 58mm, the turbine inlet hub diameter Db is phi 145mm, and the turbine blade axial height Zm is 76.5mm. The number of the turbine blades is twelve, and the profile curve of the blades is in a double-equation mode. By using the reasonable hub and hub hood wire, the efficiency of the turbocharger is enhanced, the oil consumption is lowered, the use cost is saved, and the high-efficiency mixed-flow turbine can be completely used as a substitute for imported goods.

Description

Technical field: [0001] The invention belongs to the technical field of turbochargers for diesel engines, in particular to a high-efficiency mixed flow turbine Background technique [0002] The turbine is a key part of the turbocharger that rotates at high temperature at high speed. Its function is to convert the exhaust gas energy of the internal combustion engine into mechanical work that drives the compressor to rotate at high speed coaxially. Common turbines have three types: axial flow, radial flow, and mixed flow. As far as the working method is concerned, the mixed flow type is a mixed mode between the axial flow type and the radial flow type. The turbocharger is more effective, but the disadvantage is that the design is difficult and prohibitive. Invention content: [0003] The invention provides a high-efficiency mixed-flow turbine, which is used to improve the efficiency of the existing turbine, starting from reducing the gas incident loss, turning loss, and res...

Claims

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Application Information

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IPC IPC(8): F01D5/30F01D5/14F02C6/12F02B37/00
CPCY02T10/144Y02T10/12
Inventor 董复兴韩国强朱爱国张晋东刘文奇王彦斌
Owner 大同北方天力增压技术有限公司