CN103016398A - Centrifugal impeller flow passage design method for controlling curvature distribution - Google Patents
Centrifugal impeller flow passage design method for controlling curvature distribution Download PDFInfo
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Abstract
Description
技术领域 technical field
本发明属于流体机械设计造型方法,具体涉及一种控制曲率分布的离心叶轮流道设计方法。The invention belongs to a fluid machine design modeling method, in particular to a centrifugal impeller flow path design method for controlling curvature distribution.
背景技术 Background technique
离心式叶轮机械是喷气式航空发动机的一个核心部件,并广泛应用于各种流体压缩、或流体膨胀的功能转换领域。离心式叶轮机械的子午流道的设计对离心式叶轮机械性能影响很大。但子午流道设计一直没有明确的设计准则,一般依赖设计人员经验,设计主观随意性较大。目前常规的轮盖线、轮毂线设计方法,一般通过圆弧加直线方法连接而成。这种设计方式很容易引起流动损失,降低离心式叶轮机械的做功效率。Centrifugal impeller machinery is a core component of jet aeroengines, and is widely used in the field of functional conversion of various fluid compressions or fluid expansions. The design of the meridian channel of the centrifugal impeller machinery has a great influence on the performance of the centrifugal impeller machinery. However, there is no clear design criterion for the design of the meridian flow channel, which generally depends on the experience of the designer, and the design is relatively subjective and arbitrary. At present, the conventional design method of the wheel cover line and the wheel hub line is generally formed by connecting arcs and straight lines. This design method is easy to cause flow loss and reduce the work efficiency of centrifugal impeller machinery.
发明内容 Contents of the invention
本发明的目的是提供一种控制曲率分布的离心叶轮流道设计方法,具有良好的流动性能,能够提高离心式叶轮机械的功能做功效率。The purpose of the present invention is to provide a centrifugal impeller channel design method that controls the curvature distribution, has good flow performance, and can improve the functional work efficiency of centrifugal impeller machinery.
本发明采用的技术方案为:The technical scheme adopted in the present invention is:
该离心叶轮的子午流道由轮盖线、轮毂线、进口线、出口线包络而成,设计步骤为:The meridian channel of the centrifugal impeller is enveloped by the wheel cover line, hub line, inlet line, and outlet line. The design steps are:
(1)通过控制轮盖线、轮毂线曲率在轴向上的分布,来参数化形成;轮盖线和轮毂线的曲率分布规律,采用如下公式确定:,(1) Parametrically formed by controlling the curvature distribution of the wheel cover line and the hub line in the axial direction; the curvature distribution law of the wheel cover line and the hub line is determined by the following formula: ,
其中,C(m)为轮盖线或轮毂线的曲率,m是轮盖线或轮毂线的无量纲长度;μ是最大曲率所在流向无量纲位置,μ的优选值为0.4~0.6;A是轮盖线或轮毂线曲率的无量纲幅值,且,其中R2是离心叶轮的出口半径;Among them, C(m) is the curvature of the wheel cover line or the hub line, m is the dimensionless length of the wheel cover line or the wheel hub line; μ is the dimensionless position of the maximum curvature, and the optimal value of μ is 0.4~0.6; A is the dimensionless magnitude of the curvature of the crown line or hub line, and , where R 2 is the outlet radius of the centrifugal impeller;
确定轮盖线和轮毂线的具体步骤为:The specific steps to determine the wheel cover line and hub line are:
(101)根据一维流动计算方法分别确定轮盖线和轮毂线的4个端点位置;(101) According to the one-dimensional flow calculation method, respectively determine the positions of the four endpoints of the wheel cover line and the hub line;
(102)将轮盖线均分为n(50≤n≤200)段,确定除两端点外的n-1个点的轴向坐标,根据第一个点的曲率k以及该点的坐标(Z1,R1),确定第二点的坐标(Z2,R2);然后以第二个点的曲率k以及该点坐标,确定第三个点的坐标(Z3,R3);以此类推,得到轮盖线所有点的坐标;(102) Divide the wheel cover line into n (50≤n≤200) segments, determine the axial coordinates of n-1 points except the two ends, according to the curvature k of the first point and the coordinates of the point ( Z 1 , R 1 ), determine the coordinates of the second point (Z 2 , R 2 ); then use the curvature k of the second point and the coordinates of this point to determine the coordinates of the third point (Z 3 , R 3 ); By analogy, the coordinates of all points of the wheel cover line are obtained;
(103)将得到的轮盖线上n+1个点用光滑曲线拟合,就可以得到光滑的轮盖曲线;(103) Fit n+1 points on the obtained wheel cover line with a smooth curve to obtain a smooth wheel cover curve;
(104)采用步骤(102)和(103)的方法,得到轮毂曲线;(104) Obtain the hub curve by adopting the methods of steps (102) and (103);
(2)由步骤(1)得到的轮盖曲线、轮毂曲线绕旋转轴转动360°,得到轮盖面和轮毂面。(2) The wheel cover curve and hub curve obtained in step (1) are rotated 360° around the rotation axis to obtain the wheel cover surface and hub surface.
所述轮毂线最大曲率半径幅值A为轮盖线最大曲率的0.3~0.8倍。The maximum curvature radius amplitude A of the hub line is 0.3-0.8 times of the maximum curvature of the wheel cover line.
本发明具有以下的有益效果:The present invention has following beneficial effect:
通过控制流道曲线的曲率,可以根据离心叶轮的流动做功情况,灵活选择合适的曲率分布规律,控制离心叶轮流动负荷在轴向的分布,提高了做功效率和离心叶轮的稳定工作边界,可广泛应用于各种离心式、斜流式叶轮机械的流动设计。By controlling the curvature of the flow path curve, the appropriate curvature distribution law can be flexibly selected according to the flow and work of the centrifugal impeller, and the distribution of the flow load of the centrifugal impeller in the axial direction can be controlled, which improves the work efficiency and the stable working boundary of the centrifugal impeller, and can be widely used It is applied to the flow design of various centrifugal and oblique flow impeller machines.
附图说明 Description of drawings
图1是本发明的结构原理简图。Fig. 1 is a schematic diagram of the structure principle of the present invention.
图2是图1中子午流道的示意图。Fig. 2 is a schematic diagram of the meridian flow channel in Fig. 1 .
图3是本发明实施的典型的曲率分布图。Figure 3 is a graph of a typical curvature profile for an implementation of the present invention.
图中标号:Labels in the figure:
1-轮盖线;2-轮毂线;3-进口线;4-出口线。1-Wheel cover line; 2-Hub line; 3-Inlet line; 4-Exit line.
具体实施方式 Detailed ways
本发明提供了一种控制曲率分布的离心叶轮流道设计方法,下面结合附图和具体实施方式对本发明做进一步说明。The present invention provides a centrifugal impeller flow channel design method for controlling curvature distribution. The present invention will be further described below in conjunction with the accompanying drawings and specific implementation methods.
离心式叶轮机械的轴向纵切面,一般称之为子午流道。该子午流道由轮盖线1、轮毂线2、进口线3和出口线4包络而成,如图1和图2所示。The axial longitudinal section of centrifugal impeller machinery is generally called meridian flow channel. The meridian flow channel is enveloped by the
该子午流道的设计步骤为:The design steps of the meridian flow channel are:
(1)根据公式确定轮盖线曲率分布曲线,取μ=0.5,A=0.03,m在区间[0,1]内,e为自然常数2.718,因此获得C的分布曲线如图3中轮盖曲率所示。(1) According to the formula To determine the curvature distribution curve of the wheel cover line, take μ=0.5, A=0.03, m is in the interval [0,1], and e is the natural constant 2.718, so the distribution curve of C obtained is shown in Figure 3 as shown in the wheel cover curvature.
(101)在曲率分布线上取n=100个点,作为下一步确定曲线点所需的曲率值,如下表所示。(101) Take n=100 points on the curvature distribution line as the curvature value required for determining the curve points in the next step, as shown in the table below.
(102)根据一维流动计算方法分别确定轮盖线首尾端点坐标为(-75,78.5)(-8.4,118),轮毂线的首尾端点坐标为(-75,30)(0,118);(102) According to the one-dimensional flow calculation method, determine the coordinates of the first and last endpoints of the wheel cover line as (-75,78.5) (-8.4,118), and the coordinates of the first and last endpoints of the hub line as (-75,30) (0,118);
(103)将轮盖线均分为100段,确定除两端点外的99个点的轴向坐标,根据第一个点的曲率C以及该点的坐标(Z1,R1),确定第二点的坐标(Z2,R2);然后以第二个点的曲率C以及该点坐标,确定第三个点的坐标(Z3,R3);以此类推,得到轮盖线所有点的坐标;(103) Divide the wheel cover line into 100 segments, determine the axial coordinates of 99 points except the two ends, and determine the first point according to the curvature C of the first point and the coordinates of this point (Z 1 , R 1 ). The coordinates of the second point (Z 2 , R 2 ); then use the curvature C of the second point and the coordinates of this point to determine the coordinates of the third point (Z 3 , R 3 ); and so on, to get all the wheel cover lines the coordinates of the point;
(104)将上表的轮盖线上101个点用光滑曲线拟合,就可以得到光滑的轮盖曲线,如图2所示;(104) Fit the 101 points on the wheel cover line in the above table with a smooth curve to obtain a smooth wheel cover curve, as shown in Figure 2;
(105)采用步骤(102)-(104)的方法,得到轮毂曲线,如图2所示;(105) Adopt the method of steps (102)-(104) to obtain the hub curve, as shown in Figure 2;
(2)由步骤(1)得到的轮盖曲线、轮毂曲线绕旋转轴转动360°,得到轮盖面和轮毂面。(2) The wheel cover curve and hub curve obtained in step (1) are rotated 360° around the rotation axis to obtain the wheel cover surface and hub surface.
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Cited By (3)
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CN106593943A (en) * | 2016-12-06 | 2017-04-26 | 大连理工大学 | Nuclear main pump runner forming method based on intermediate line control |
CN110374900A (en) * | 2019-08-09 | 2019-10-25 | 西安交通大学 | A kind of flow-mixing blower fan with sinusoidal pattern meridional channel |
CN111120400A (en) * | 2019-12-24 | 2020-05-08 | 哈尔滨工程大学 | A centrifugal compressor for micro gas turbine |
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Publication number | Priority date | Publication date | Assignee | Title |
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CN106593943A (en) * | 2016-12-06 | 2017-04-26 | 大连理工大学 | Nuclear main pump runner forming method based on intermediate line control |
CN106593943B (en) * | 2016-12-06 | 2019-01-04 | 大连理工大学 | A kind of core main pump runner forming method based on intermediate line traffic control |
CN110374900A (en) * | 2019-08-09 | 2019-10-25 | 西安交通大学 | A kind of flow-mixing blower fan with sinusoidal pattern meridional channel |
CN111120400A (en) * | 2019-12-24 | 2020-05-08 | 哈尔滨工程大学 | A centrifugal compressor for micro gas turbine |
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