Annular-nozzle straight-line-arc-line blade profile line design method

A technology of annular nozzle and blade profile, which is applied in the field of annular nozzle blade profile design, can solve the problems that are not conducive to blade profile processing and manufacturing, numerical simulation and optimal design, the process of modifying profile is cumbersome and complicated, and it is difficult to ensure the straight line and Problems such as smooth transition of arc segments

Active Publication Date: 2018-03-30
CHONGQING UNIV
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Problems solved by technology

This geometric modeling method mainly has the following two disadvantages: first, it is difficult to ensure a smooth transition between the straight line and the arc when designing the arc segment through the empirical parameter method, which will inevitably cause more flow loss; The ratio of the straight l...

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  • Annular-nozzle straight-line-arc-line blade profile line design method
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  • Annular-nozzle straight-line-arc-line blade profile line design method

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Embodiment Construction

[0079] Below in conjunction with embodiment the present invention will be further described, but should not be interpreted as the above-mentioned scope of the present invention is limited to following embodiment. Without departing from the above-mentioned technical idea of ​​the present invention, various replacements and changes can be made according to common technical knowledge and customary means in this field, and all should be included in the protection scope of the present invention.

[0080] This embodiment takes a turboexpander supporting a certain low-pressure air separation process as an example. The design parameters of the turboexpander and the main structural dimensions of the impeller are shown in Table 1, and the gas is discharged in the axial direction.

[0081] Table 1 Turboexpander design parameters and main structural dimensions of the impeller

[0082]

[0083] Design according to the following steps (in the parameters, use "1" to indicate the inlet, "2...

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Abstract

The invention discloses a method used for annular-nozzle straight-line-arc-line blade profile line design of a radial-axial-flow-type turboexpander. The method includes: dividing a blade into two parts of a suction surface and a pressure surface, also dividing a blade profile line of each part into a straight-line segment and an arc-line segment, and utilizing mathematical expressions to carry outcoordinate solving on the straight-line segment and the arc-line segment through programming. According to the method, a Bezier curve is adopted for solving for arc-line segment coordinates to realize smooth transition of the straight-line segment and the arc-line segment, thus geometric curvature continuity of the nozzle blade profile line can be well guaranteed, and more flow losses can be avoided; and in addition, the blade profile line is divided into the straight-line segment and the arc-line segment through programming, the mathematical expressions are respectively used for representation, a design process is simpler, more convenient and faster, and subsequent work processes of machining manufacturing, numerical simulation, optimization design and the like on the nozzle blade profile line are facilitated.

Description

technical field [0001] The invention relates to a method for designing the profile of an annular nozzle blade, in particular to a method for designing the profile of a linear-arc blade of an annular nozzle of a radial-axial turboexpander. Background technique [0002] The turboexpander is the main source of cooling capacity in the cryogenic system, and it is also the core component of the modern air separation plant and cryogenic liquefaction system. Its performance is of great significance to the economy and safety of the entire plant. The main flow part of the turboexpander includes an annular nozzle, a radial-axial flow impeller and a diffuser, wherein the annular nozzle is one of the main flow channels for the turboexpander to generate energy, and the design of the blade profile of the annular nozzle is Turboexpander performance has a significant impact. Straight-arc blades are a type of circular nozzle blades. The blades are simple straight lines and arcs, and have the...

Claims

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Application Information

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IPC IPC(8): G06F17/50
CPCG06F30/17G06F30/20
Inventor 孙皖侯予陈双涛步珊珊马在勇潘良明
Owner CHONGQING UNIV
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