[go: up one dir, main page]

CN102996504B - Centrifugal impeller flow passage design method for controlling slope distribution - Google Patents

Centrifugal impeller flow passage design method for controlling slope distribution Download PDF

Info

Publication number
CN102996504B
CN102996504B CN201210545524.XA CN201210545524A CN102996504B CN 102996504 B CN102996504 B CN 102996504B CN 201210545524 A CN201210545524 A CN 201210545524A CN 102996504 B CN102996504 B CN 102996504B
Authority
CN
China
Prior art keywords
line
wheel cover
centrifugal impeller
hub
curve
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201210545524.XA
Other languages
Chinese (zh)
Other versions
CN102996504A (en
Inventor
徐全勇
黄旭东
周明
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tsinghua University
Original Assignee
Tsinghua University
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Tsinghua University filed Critical Tsinghua University
Priority to CN201210545524.XA priority Critical patent/CN102996504B/en
Publication of CN102996504A publication Critical patent/CN102996504A/en
Application granted granted Critical
Publication of CN102996504B publication Critical patent/CN102996504B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention belongs to fluid mechanical design modeling methods and in particular relates to a centrifugal impeller flow passage design method for controlling slope distribution. Meridional flow passage design steps of a centrifugal impeller comprise the following steps: carrying out parameterized formation by controlling distribution of slopes of a wheel cap line and a wheel hub line in the axial direction; and then rotating an obtained wheel cap curve and a wheel hub curve with 360 degrees around a rotation shaft to obtain a wheel cap face and a wheel hub face. Appropriate slope distribution regularity can be flexibly selected to control distribution of flow load of the centrifugal impeller in the axial direction according to flow acting situations of the centrifugal impeller by controlling the slopes of the flow passage curves, and the acting efficiency and the stable work boundary of the centrifugal impeller are improved. The centrifugal impeller flow passage design method can be widely applied to flow design of various centrifugal and diagonal flow turbomachinery.

Description

一种控制斜率分布的离心叶轮流道设计方法A Centrifugal Impeller Flow Path Design Method Controlling the Slope Distribution

技术领域 technical field

本发明属于流体机械设计造型方法,具体涉及一种控制斜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 slope 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。目前常规的子午流道型线设计方法,一般通过圆弧加直线连接而成。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. Generally, it depends on the experience of the designer, and the design is relatively subjective. At present, the conventional design method of meridian runner profile 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

本发明提出了一种控制斜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 invention proposes a centrifugal impeller channel design method for controlling slope distribution, which 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、轮毂线斜率在轴向上的分布,来参数化形成;轮盖线和轮毂线的斜率分布规律,采用三次多项式S(x)=Ax3+Bx2+Cx+D来确定,其中S为曲线斜率,x为无量纲流向长度,A、B、C、D为无量纲系数,具体值如下表所示:(1) Parametrically formed by controlling the distribution of the slope of the wheel cover line and the hub line in the axial direction; the slope distribution of the wheel cover line and the hub line adopts the cubic polynomial S(x)=Ax 3 +Bx 2 +Cx +D to determine, where S is the slope of the curve, x is the length of the dimensionless flow direction, and A, B, C, and D are dimensionless coefficients. The specific values are shown in the following table:

A A B B C C D D. 轮盖线 wheel cover line 3e-4 3e-4 4.0e-2 4.0e-2 0.42e-1 0.42e-1 4.76 4.76 轮毂线 hub line 3e-4 3e-4 5.1e-2 5.1e-2 1.46 1.46 6.37 6.37

;

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,根据第一个点的斜率k以及该点的坐标(Z1,R1),确定第二点的坐标(Z2,R2);然后以第二个点的斜率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 slope 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 slope 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.

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斜率,可以根据离心叶轮的流动做功情况,灵活选择合适的斜率分布规律,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 slope of the flow channel curve, the appropriate slope 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斜率分布图。Figure 3 is a graph of a typical slope 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斜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 path design method for controlling slope distribution. The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

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 wheel cover line 1, the hub line 2, the inlet line 3 and the outlet line 4, as shown in Fig. 1 and Fig. 2 .

该子午流道的设计步骤为:The design steps of the meridian flow channel are:

(1) 轮盖线和轮毂线的斜率分布规律,采用三次多项式S(x)=Ax3+Bx2+Cx+D来确定,其中S为曲线斜率,x为无量纲流向长度,A、B、C、D为无量纲系数,具体值如下表所示:(1) The slope distribution of the wheel cover line and the hub line is determined by the cubic polynomial S(x)=Ax 3 +Bx 2 +Cx+D, where S is the slope of the curve, x is the dimensionless flow length, A, B , C, and D are dimensionless coefficients, and the specific values are shown in the following table:

A A B B C C D D. 轮盖线 wheel cover line 3e-4 3e-4 4.0e-2 4.0e-2 0.42e-1 0.42e-1 4.76 4.76 轮毂线 hub line 3e-4 3e-4 5.1e-2 5.1e-2 1.46 1.46 6.37 6.37

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);(101) According to the one-dimensional flow calculation, 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);

(102)将轮盖线均分为100段,根据步骤(1)的公式确定共计101个离散点的曲率分布规律如下表所示:(102) Divide the wheel cover line into 100 segments, and determine the curvature distribution law of a total of 101 discrete points according to the formula in step (1), as shown in the following table:

m% m% S S 0 0 2.32822752 2.32822752 1.081193125 1.081193125 2.684830529 2.684830529 2.158423216 2.158423216 3.052522752 3.052522752 3.231690273 3.231690273 3.431304189 3.431304189 4.302531701 4.302531701 3.821744421 3.821744421 5.370643162 5.370643162 4.223781636 4.223781636 6.434353142 6.434353142 4.637521399 4.637521399 7.493103413 7.493103413 5.064098509 5.064098509 8.548594601 8.548594601 5.504275681 5.504275681 9.598761667 9.598761667 5.957385241 5.957385241

10.64259234 10.64259234 6.424558357 6.424558357 11.68162113 11.68162113 6.90694199 6.90694199 12.7149665 12.7149665 7.404196413 7.404196413 13.74096037 13.74096037 7.916498385 7.916498385 14.75987996 14.75987996 8.445282513 8.445282513 15.7750857 15.7750857 8.992472579 8.992472579 16.78168811 16.78168811 9.555828644 9.555828644 17.77826145 17.77826145 10.13622719 10.13622719 18.77284031 18.77284031 10.73894675 10.73894675 19.75956937 19.75956937 11.36083407 11.36083407 20.73470078 20.73470078 12.00065915 12.00065915 21.70652987 21.70652987 12.66517963 12.66517963 22.68583208 22.68583208 13.3630336 13.3630336 23.65146125 23.65146125 14.08025866 14.08025866 24.6019665 24.6019665 14.81672705 14.81672705 25.53737196 25.53737196 15.57258196 15.57258196 26.45749724 26.45749724 16.3476886 16.3476886 27.36147888 27.36147888 17.14132595 17.14132595 28.25352674 28.25352674 17.9574741 17.9574741 29.13529651 29.13529651 18.79829935 18.79829935 29.99991337 29.99991337 19.65719931 19.65719931 30.84714997 30.84714997 20.53264277 20.53264277 31.6970085 31.6970085 21.44647939 21.44647939 32.52933638 32.52933638 22.37828312 22.37828312 33.34397638 33.34397638 23.32532585 23.32532585 34.1556733 34.1556733 24.30460663 24.30460663 34.96250196 34.96250196 25.31572893 25.31572893 35.75124714 35.75124714 26.3412808 26.3412808 36.52547077 36.52547077 27.38215321 27.38215321 37.31243403 37.31243403 28.4771139 28.4771139 38.08141862 38.08141862 29.58511401 29.58511401 38.83476969 38.83476969 30.7036116 30.7036116 39.59375993 39.59375993 31.86377058 31.86377058 40.34926271 40.34926271 33.05391233 33.05391233 41.09005012 41.09005012 34.25336808 34.25336808 41.82388345 41.82388345 35.46919189 35.46919189 42.57060858 42.57060858 36.7360406 36.7360406 43.30440203 43.30440203 38.01054488 38.01054488 44.02879026 44.02879026 39.29034799 39.29034799 44.76325115 44.76325115 40.60891827 40.60891827 45.4956161 45.4956161 41.94554822 41.94554822 46.22123034 46.22123034 43.2858758 43.2858758 46.94775593 46.94775593 44.63791383 44.63791383 47.68331216 47.68331216 46.01715949 46.01715949 48.41532489 48.41532489 47.39829165 47.39829165

49.14793261 49.14793261 48.77911285 48.77911285 49.88908244 49.88908244 50.17321563 50.17321563 50.6329808 50.6329808 51.56957463 51.56957463 51.38159653 51.38159653 52.96339465 52.96339465 52.13671281 52.13671281 54.35230083 54.35230083 52.89793139 52.89793139 55.73561284 55.73561284 53.66755874 53.66755874 57.11429406 57.11429406 54.45013836 54.45013836 58.48557459 58.48557459 55.23483435 55.23483435 59.83023415 59.83023415 56.03177849 56.03177849 61.16597678 61.16597678 56.84604016 56.84604016 62.49105911 62.49105911 57.669658 57.669658 63.78852295 63.78852295 58.50122558 58.50122558 65.05770015 65.05770015 59.35293003 59.35293003 66.3136157 66.3136157 60.22802514 60.22802514 67.55102947 67.55102947 61.10222131 61.10222131 68.73739341 68.73739341 61.99970614 61.99970614 69.90696689 69.90696689 62.92383305 62.92383305 71.0549536 71.0549536 63.86078224 63.86078224 72.16253241 72.16253241 64.81380023 64.81380023 73.23572679 73.23572679 65.79407145 65.79407145 74.2843528 74.2843528 66.80078791 66.80078791 75.30176227 75.30176227 67.82096445 67.82096445 76.27619754 76.27619754 68.86896438 68.86896438 77.22216587 77.22216587 69.9442864 69.9442864 78.13549514 78.13549514 71.04565632 71.04565632 79.0143245 79.0143245 72.17364204 72.17364204 79.85923184 79.85923184 73.32709666 73.32709666 80.66920419 80.66920419 74.50916573 74.50916573 81.44580417 81.44580417 75.73116451 75.73116451 82.1950839 82.1950839 76.97682679 76.97682679 82.90654766 82.90654766 78.24197995 78.24197995 83.58050177 83.58050177 79.56403717 79.56403717 84.23515278 84.23515278 80.91612755 80.91612755 84.85454996 84.85454996 82.28494047 82.28494047 85.43584244 85.43584244 83.69361042 83.69361042 85.9904904 85.9904904 85.16644159 85.16644159 86.5245884 86.5245884 86.65374539 86.65374539 87.01940575 87.01940575 88.15135633 88.15135633 87.47946666 87.47946666 89.74955535 89.74955535 87.92964662 87.92964662 91.36933979 91.36933979 88.34395631 88.34395631 92.99704241 92.99704241 88.7245832 88.7245832 94.68622279 94.68622279 89.08560158 89.08560158 96.45034258 96.45034258 89.42611574 89.42611574 98.22160165 98.22160165 89.73091521 89.73091521 100 100 90 90

(103)将轮盖线均分为100段,确定除两端点外的中间99个点的轴向坐标,根据第一个点的斜率k以及该点的坐标(Z1,R1),确定第二点的坐标(Z2,R2);然后以第二个点的斜率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;下表列出前15个点坐标,余点以此类推获得。(103) Divide the wheel cover line into 100 segments, determine the axial coordinates of the middle 99 points except the two ends, and determine according to the slope k 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 slope k 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 the wheel cover line The coordinates of all points; the following table lists the coordinates of the first 15 points, and the remaining points are obtained by analogy.

Z Z R R -75.0 -75.0 78 78 -72.0408 -72.0408 77.9949 77.9949 -69.0817 -69.0817 77.9924 77.9924 -66.1225 -66.1225 77.9898 77.9898 -63.1633 -63.1633 77.9873 77.9873 -60.2042 -60.2042 77.9847 77.9847 -57.245 -57.245 77.9821 77.9821 -54.2858 -54.2858 77.9796 77.9796 -51.3266 -51.3266 77.977 77.977 -48.3675 -48.3675 77.9745 77.9745 -45.4083 -45.4083 77.9719 77.9719 -42.45 -42.45 78.0193 78.0193 -39.5072 -39.5072 78.3191 78.3191 -36.6048 -36.6048 78.8906 78.8906 -33.7679 -33.7679 79.7287 79.7287

(104)将得到的轮盖线上101个点用光滑曲线拟合,就可以得到光滑的轮盖曲线;(104) Fit 101 points on the obtained wheel cover line with a smooth curve to obtain a smooth wheel cover curve;

(105)采用步骤(102)-(104)的方法,得到轮毂曲线;(105) Obtain the hub curve by adopting the method of steps (102)-(104);

(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.

Claims (1)

1.一种控制斜率分布的离心叶轮流道设计方法,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,其特征在于,设计步骤为:1. A centrifugal impeller flow path design method for controlling the slope distribution, the meridional flow path of this centrifugal impeller is enveloped by wheel cover line, hub line, inlet line, and outlet line, and it is characterized in that the design steps are: (1)通过控制轮盖线、轮毂线斜率在轴向上的分布,来参数化形成;轮盖线和轮毂线的斜率分布规律,采用三次多项式S(m)=Ax3+Bx2+Cx+D来确定,其中S为曲线斜率,x为无量纲流向长度,A、B、C、D为无量纲系数,具体值如下:(1) Parametrically formed by controlling the distribution of the slope of the wheel cover line and the hub line in the axial direction; the slope distribution of the wheel cover line and the hub line adopts the cubic polynomial S(m)=Ax 3 +Bx 2 +Cx +D to determine, where S is the slope of the curve, x is the length of the dimensionless flow direction, A, B, C, and D are dimensionless coefficients, and the specific values are as follows: A A B B C C D D. 轮盖线 wheel cover line 3e-4 3e-4 4.0e-2 4.0e-2 0.42e-1 0.42e-1 4.76 4.76 轮毂线 hub line 3e-4 3e-4 5.1e-2 5.1e-2 1.46 1.46 6.37 6.37
; 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,根据第一个点的斜率k以及该点的坐标(Z1,R1),确定第二点的坐标(Z2,R2);然后以第二个点的斜率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 slope 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 slope 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.
CN201210545524.XA 2012-12-14 2012-12-14 Centrifugal impeller flow passage design method for controlling slope distribution Active CN102996504B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210545524.XA CN102996504B (en) 2012-12-14 2012-12-14 Centrifugal impeller flow passage design method for controlling slope distribution

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210545524.XA CN102996504B (en) 2012-12-14 2012-12-14 Centrifugal impeller flow passage design method for controlling slope distribution

Publications (2)

Publication Number Publication Date
CN102996504A CN102996504A (en) 2013-03-27
CN102996504B true CN102996504B (en) 2015-06-10

Family

ID=47925485

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210545524.XA Active CN102996504B (en) 2012-12-14 2012-12-14 Centrifugal impeller flow passage design method for controlling slope distribution

Country Status (1)

Country Link
CN (1) CN102996504B (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101149061A (en) * 2007-07-30 2008-03-26 北京航空航天大学 A kind of centrifugal impeller suitable for working under the condition of high rotating speed
CN201148995Y (en) * 2008-01-16 2008-11-12 天津内燃机研究所 Low noise cooling fan
CN201176959Y (en) * 2008-01-16 2009-01-07 天津内燃机研究所 Double-vane cooling fan
RU2354854C1 (en) * 2007-12-20 2009-05-10 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Axial blower or compressor high-rpm impeller

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2811348A1 (en) * 2010-08-12 2012-02-16 Nuovo Pignone S.P.A. Radial diffuser vane for centrifugal compressors

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101149061A (en) * 2007-07-30 2008-03-26 北京航空航天大学 A kind of centrifugal impeller suitable for working under the condition of high rotating speed
RU2354854C1 (en) * 2007-12-20 2009-05-10 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Axial blower or compressor high-rpm impeller
CN201148995Y (en) * 2008-01-16 2008-11-12 天津内燃机研究所 Low noise cooling fan
CN201176959Y (en) * 2008-01-16 2009-01-07 天津内燃机研究所 Double-vane cooling fan

Also Published As

Publication number Publication date
CN102996504A (en) 2013-03-27

Similar Documents

Publication Publication Date Title
CN104153820B (en) A kind of big meridian expansion variable geometry turbine with stepped ramp type sphere end wall
CN105971931B (en) A kind of design method of receded disk impeller splitterr vanes
CN104100305B (en) A kind of large meridian expansion variable geometry turbine with orthogonal type adjustable stator blade
CN113958519B (en) Automatic generation method for blades in different shapes of centrifugal impeller based on intermediate surface
CN105673558B (en) A kind of centrifugal fan blade based on the design of load method
CN105805043A (en) Design method for nonadjustable axial flow pump impeller with characteristic of long blades and short blades
CN114718659B (en) Turbine blade tip clearance flow control method coupling radial ribs and circumferential grooves
CN103671254A (en) Vane structure for weakening axial flow pump vane top leakage flow and leakage vortex
CN110657126A (en) Non-axisymmetrical hub structure for controlling flow of centrifugal impeller and centrifugal impeller
CN113221264A (en) Method for optimizing structural design of flow channel type guide vane of seawater desalination pump
CN103016398B (en) Centrifugal impeller flow passage design method for controlling curvature distribution
CN106089808B (en) A kind of blade diffuser and its formative method with trailing edge structures before swallow-tail form
CN104806571A (en) Efficient centrifugal air blower based on computational fluid dynamic simulation
CN105179322B (en) Blade root opens up the Profile For Compressor Stator leaf grating of wide straight-line groove
CN106382260B (en) A kind of tangential groove water conservancy diversion chip treated casing method and device of compressor
CN104500452B (en) A kind of vaneless diffuser structure and machining method with positive N prism side exit
CN104912604B (en) A kind of have the spin-ended anti-rotating plate structure pressing down and bestirring oneself
CN102996504B (en) Centrifugal impeller flow passage design method for controlling slope distribution
CN106567861A (en) Axial flow pump guide vane hydraulic design method and device
CN103628926A (en) The steam exhaust area is 3.0m2, and the final blade of the low pressure stage group of the variable speed industrial steam turbine
CN114186513A (en) Modeling design method for axial flow compressor blade with reverse S-shaped front edge
CN101749052A (en) The final stage moving blade of air-cooled feed pump steam turbine
CN202348525U (en) Axial-flow rotary propeller type water turbine
CN105864099B (en) A kind of design method of middle higher specific speed centrifugal pump impeller port of export edge folding blades structure
CN103806946A (en) The steam exhaust area is 2.1m2, and the final blade of the low-pressure stage group of the variable-speed industrial steam turbine

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant