PatentDe  


Dokumentenidentifikation EP1312808 13.12.2007
EP-Veröffentlichungsnummer 0001312808
Titel Rotorschaufel für Kreiselverdichter
Anmelder Nuovo Pignone Holding S.p.A., Florence, IT
Erfinder Rossi, Eugenio, 55049 Viareggio Lucca, IT;
Rocchi, Gianluca, 50135 Florence, IT
Vertreter derzeit kein Vertreter bestellt
DE-Aktenzeichen 60223223
Vertragsstaaten CH, DE, FR, GB, LI, SE
Sprache des Dokument EN
EP-Anmeldetag 14.11.2002
EP-Aktenzeichen 022578678
EP-Offenlegungsdatum 21.05.2003
EP date of grant 31.10.2007
Veröffentlichungstag im Patentblatt 13.12.2007
IPC-Hauptklasse F04D 29/30(2006.01)A, F, I, 20051017, B, H, EP
IPC-Nebenklasse F04D 29/28(2006.01)A, L, I, 20051017, B, H, EP   

Beschreibung[en]

The present invention relates to a rotor blade for a centrifugal compressor with a medium flow coefficient.

More precisely, the invention relates to a cylindrical blade for a centrifugal rotor of a multi-stage compressor.

In the field of centrifugal compressors, the flow coefficient is defined as &PHgr; = (4*q)/(&pgr;*d2*u") in which:

  • q is the volume flow rate;
  • d is the outer diameter of the rotor;
  • u" is the peripheral velocity of the rotor.

This dimensionless coefficient can be used to define the operating characteristic of the compressor, and can be used to classify the different types of compressor at the design stage.

Compressors are therefore made to handle different flow rates, in other words to operate with different values of the flow coefficient, according to the applications for which they are intended.

For example, we may mention compressors with a medium flow coefficient, in which &PHgr; has values in the vicinity of 0.04, and compressors with a medium-high flow coefficient, for which &PHgr; is approximately 0.06.

However, one of the main requirements common to all compressors relates to the high aerodynamic efficiency which must be attained in most of the stages.

The geometric configuration of the rotor blading significantly affects the aerodynamic efficiency (see for example GB 1144445 which propose a calculation foor the vane angles in order to increase the aerodynamic efficiency), due to the fact that the geometric characteristics of the blade determine the distribution of the relative velocities of the fluid along the rotor, thus affecting the distribution of the boundary layers along the walls and, in the final analysis, the friction losses.

The aerodynamic efficiency is particularly critical for rotors made with stages having two-dimensional blades, in other words purely radial rotors in which the blades are flat or cylindrical with generatrices parallel to the axis of rotation of the rotor.

Conventionally, for reasons of economy in manufacture, the blades used in this type of rotor have a relatively simple geometry in which the median line of the section consists of an arc of a circumference and the thickness is constant along the blade, except in the region of the leading edge, which is formed by a semicircular fillet or, in particular cases, by a tapering of the thickness.

Although two-dimensional blades are made by relatively simple machining processes and are therefore very widely used, their geometry does not enable a high aerodynamic efficiency of the rotor to be achieved.

The present invention therefore seeks to provide a blade which, by means of a suitable configuration, enables a high aerodynamic efficiency to be achieved.

The present invention also seeks to provide a blade which can be manufactured economically on a large scale by automated processes.

According to the invention, there is provided a cylindrical blade for a rotor of the purely radial type of a centrifugal compressor with a medium flow coefficient, the said blade comprising a first surface of the pressure side and a second surface of the suction side having equal curvature, both having generatrices parallel to the axis (Z) of rotation of the rotor, characterized in that the intersection of each of the said surfaces on a plane (Y, X) of a right-hand Cartesian reference system (Y, X, Z), having an axis of ordinates (X) and an axis of abscissae (Y), and an axis (Z) coinciding with the axis of rotation of the rotor, is a curved line defined by a discrete set of points belonging to the said curve whose coordinates (y) on the axis of abscissae and (x) on the axis of ordinates are expressed as a function of the outer radius (R) of the rotor as the ratios y/R and x/R respectively between the values of the coordinate of each point and the value of the said radius (R) of the rotor, the coordinates (y, x) of the said points being variable within a range of ± 0.600 mm on both the abscissa and the ordinate:

  • x/R = 0.450; y/R = -0.397
  • x/R = 0.455; y/R = -0.391
  • x/R = 0.461; y/R = -0.387
  • x/R = 0.468; y/R = -0.384
  • x/R = 0.474; y/R = -0.381
  • x/R = 0.480; y/R = -0.377
  • x/R = 0.486; y/R = -0.374
  • x/R = 0.493; y/R = -0.371
  • x/R = 0.499; y/R = -0.368
  • x/R = 0.505; y/R = -0.365
  • x/R = 0.512; y/R = -0.362
  • x/R = 0.518; y/R = -0.359
  • x/R = 0.524; y/R = -0.356
  • x/R = 0.531; y/R = -0.353
  • x/R = 0.537; y/R = -0.350
  • x/R = 0.543; y/R = -0.347
  • x/R = 0.550; y/R = -0.344
  • x/R = 0.556; y/R = -0.341
  • x/R = 0.562; y/R = -0.337
  • x/R = 0.568; y/R = -0.334
  • x/R = 0.575; y/R = -0.331
  • x/R = 0.581; y/R = -0.328
  • x/R = 0.587; y/R = -0.321
  • x/R = 0.593; y/R = -0.321
  • x/R = 0.599; y/R = -0.318
  • x/R = 0.605; y/R = -0.314
  • x/R = 0.612; y/R = -0.311
  • x/R = 0.618; y/R = -0.307
  • x/R = 0.624; y/R = -0.303
  • x/R = 0.630; y/R = -0.300
  • x/R = 0.650; y/R = -0.287
  • x/R = 0.670; y/R = -0.275
  • x/R = 0.690; y/R = -0.261
  • x/R = 0.709; y/R = -0.248
  • x/R = 0.729; y/R = -0.234
  • x/R = 0.748; y/R = -0.220
  • x/R = 0.767; y/R = -0.205
  • x/R = 0.785; y/R = -0.190
  • x/R = 0.804; y/R = -0.175
  • x/R = 0.822; y/R = -0.160
  • x/R = 0.844; y/R = -0.140
  • x/R = 0.866; y/R = -0.120
  • x/R = 0.888; y/R = -0.100
  • x/R = 0.910; y/R = -0.079
  • x/R = 0.931; y/R = -0.058
  • x/R = 0.952; y/R = -0.037
  • x/R = 0.972; y/R = -0.015
  • x/R = 0.993; y/R = 0.007

The invention will now be described in greater detail, by way of example, with reference to the drawings, in which:-

  • Figure 1 is a front view, in partial section, of a rotor having blades according to the invention;
  • Figure 2 is a view, in partial section, of the rotor, taken through the line II-II in Figure 1;
  • Figure 3 is a schematic axonometric view of a blade according to the invention;
  • Figure 4 shows the profile of the blade of Figure 3 at the position of its geometric intersection with the hub of the rotor.

With reference to Figures 1 and 2, a rotor 10 of the purely radial type with an outer radius R belonging to a centrifugal compressor with a medium flow coefficient comprises a plurality of cylindrical blades 1.

Each blade 1 comprises a first surface 3 of the pressure side facing forwards with respect to the direction of rotation of the rotor, indicated by the arrow F, and a second surface 5 of the suction side, opposite the first surface.

The surfaces 3 and 5 are substantially cylindrical, have equal curvature, and are made with generatrices parallel to the axis Z of rotation of the rotor 10.

The two surfaces 3 and 5 are joined together at one end by a known method; for example, a tapering of the thicknesses, or alternatively a semicircular fillet (not illustrated) is provided at the leading edge 4.

With reference to Figures 3 and 4, the projection of each of the said surfaces 3 and 5 on a plane Y, X of a right-handed Cartesian system Y, X, Z, having an axis of ordinates X, an axis of abscissae Y, and an axis Z coinciding with the axis of rotation of the rotor 10, is a curved line 7 defined by a discrete set of points 9 belonging to the said curve 7, whose coordinates y, on the axis of abscissae, and x, on the axis of ordinates, are conveniently expressed as a function of the outer radius R of the rotor.

As a result of this definition of the curve 7, the surfaces 3 and 5, and substantially the blade 1, can be conveniently formed by means of automatic machines, for example those of the numerically controlled type, or the like.

According to the operating conditions for which they are intended, the rotor 10 and correspondingly the blades 1 can also be made in various sizes.

According to the known law of similarity, the characteristics of a rotor are in fact, within certain limits, substantially dependent on the curvature of the blades, and are therefore, as a first approximation, equal for similar rotors.

By applying the law of similarity, it is possible to disregard the absolute dimensions of the blade and define its geometry, for example by means of the ratios x/R and y/R of the coordinates of the points 9 to the value of the outer radius R of the rotor.

It has also been found that the efficiency varies only slightly with the variation of the curvatures of the surfaces 3 and 5, and therefore of the curve 7 when this is kept within a range of variation of the coordinates y, x of the points 9 equal to ± 0.600 mm.

The curve 7 of the blade 1 according to the invention, expressed as a function of the outer radius R of the rotor, in the form, respectively, of the ratios y/R and x/R between the values of the coordinates of each point and the value of the said radius R, is defined by the following values:

  • x/R = 0.450; y/R = -0.397
  • x/R = 0.455; y/R = -0.391
  • x/R = 0.461; y/R = -0.387
  • x/R = 0.468; y/R = -0.384
  • x/R = 0.474; y/R = -0.381
  • x/R = 0.480; y/R = -0.377
  • sir = 0.486; y/R = -0.374
  • x/R = 0.493; y/R = -0.371
  • x/R = 0.499; y/R = -0.368
  • x/R = 0.505; y/R = -0.365
  • x/R = 0.512; y/R = -0.362
  • x/R = 0.518; y/R = -0.359
  • x/R = 0.524; y/R = -0.356
  • x/R = 0.531; y/R = -0.353
  • x/R = 0.537; y/R = -0.350
  • x/R = 0.543; y/R = -0.347
  • x/R = 0.550; y/R = -0.344
  • x/R = 0.556; y/R = -0.341
  • x/R = 0.562; y/R = -0.337
  • x/R = 0.568; y/R = -0.334
  • x/R = 0.575; y/R = -0.331
  • x/R = 0.581; y/R = -0.328
  • x/R = 0.587; y/R = -0.321
  • x/R = 0.593; y/R = -0.321
  • x/R = 0.599; y/R = -0.318
  • x/R = 0.605; y/R = -0.314
  • x/R = 0.612; y/R = -0.311
  • x/R = 0.618; y/R = -0.307
  • x/R = 0.624; y/R = -0.303
  • x/R = 0.630; y/R = -0.300
  • x/R = 0.650; y/R = -0.287
  • x/R = 0.670; y/R = -0.275
  • x/R = 0.690; y/R = -0.261
  • x/R = 0.709; y/R = -0.248
  • x/R = 0.729; y/R = -0.234
  • x/R = 0.748; y/R = -0.220
  • x/R = 0.767; y/R = -0.205
  • x/R = 0.785; y/R = -0.190
  • x/R = 0.804; y/R = -0.175
  • x/R = 0.822; y/R = -0.160
  • x/R = 0.844; y/R = -0.140
  • x/R = 0.866; y/R = -0.120
  • x/R = 0.888; y/R = -0.100
  • x/R = 0.910; y/R = -0.079
  • x/R = 0.931; y/R = -0.058
  • x/R = 0.952; y/R = -0.037
  • x/R = 0.972; y/R = -0.015
  • x/R = 0.993; y/R = 0.007.

Example of embodiment

A rotor 10 was made with an outer radius of 200 mm and with 17 cylindrical blades 1 having surfaces 3 of the pressure sides and surfaces 5 of the suction sides with equal curvature, defined by the following coordinates y, x of a discrete set of points 9 of the curve 7 of the intersection of one of the surfaces 3 and 5 with the plane Y, X of a right-hand system of Cartesian axes Y, X, Z where Y is the axis of abscissae and X is the axis of ordinates:

  • x = 89.957; y = -79.420;
  • x = 91.036; y = -78.247;
  • x = 92.261; y = -77.492;
  • x = 93.504; y = -76.790;
  • x = 94.753; y = -76.115;
  • x = 96:007; y = -75.462;
  • x = 97.264; y = -74.820;
  • x = 98.524; y = -74.190;
  • x = 99.788; y = -73.573;
  • x = 101.064; y = -72.962;
  • x = 102.321; y = -72.354;
  • x = 103.592; y = -71.758;
  • x = 104.867; y = -71.171;
  • x = 106.139; y = -70.576;
  • x = 107.407; y = -69.973;
  • x = 108.673; y = -69.363;
  • x = 109.934; y = -68.745;
  • x = 111.191; y = -68.119;
  • x = 112.449; y = -67.483;
  • x = 113.692; y = -66.840;
  • x = 114.937; y = -66.188;
  • x = 116.177; y = -65.529;
  • x = 117.414; y = -64.261;
  • x = 118.646; y = -64.185;
  • x = 119.874; y = -63.502;
  • x = 121.098; y = -62.811;
  • x = 122.317; y = -62.112;
  • x = 123.533; y = -61.406;
  • x = 124.744; y = -60.693;
  • x = 125.951; y = -59.972;
  • x = 130.003; y = -57.480;
  • x = 134.008; y = -54.910;
  • x = 137.965; y = -52.265;
  • x = 141.875; y = -49.548;
  • x = 145.737; y = -46.763;
  • x = 149.553; y = -43.913;
  • x = 153.323; y = -41.000;
  • x = 157.048; y = -38.028;
  • x = 160.728; y = -35.000;
  • x = 164.365; y = -31.918;
  • x = 168.848; y = -27.992;
  • x = 173.262; y = -23.989;
  • x = 177.613; y = -19.912;
  • x = 181.903; y = -15.768;
  • x = 186.137; y = -11.563;
  • x = 190.317; y = -7.303;
  • x = 194.448; y = -2.994;
  • x = 198.537; y = 1.364.

When this rotor was subjected to fluid-dynamic testing, its polytropic stage efficiency was found to be considerably higher than that of prior art rotors.


Anspruch[de]
Zylindrische Laufschaufel für einen Rotor der rein radialen Bauart eines Kreiselverdichters mit einem mittleren Strömungskoeffizienten, wobei die Schaufel (1) eine erste Fläche (3) der Druckseite und eine zweite Fläche (5) der Saugseite aufweist, die gleiche Krümmung aufweisen, wobei beide zu der Drehachse (Z) des Rotors parallele Erzeugende aufweisen, dadurch gekennzeichnet, dass die Schnittlinie jeder der Flächen (3, 5) auf einer Ebene (Y, X) eines rechtshändigen kartesischen Referenzsystems (Y, X, Z), das eine Ordinatenachse (X) und eine Abszissenachse (Y) sowie eine Achse (Z) aufweist, die mit der Drehachse des Rotors zusammenfällt, eine gekrümmte Linie (7) bildet, die durch eine diskrete Menge von zu der Kurve (7) gehörenden Punkten bildet, deren Koordinaten (y) auf der Abszissenachse und (x) auf der Ordinatenachse in Abhängigkeit von dem Außenradius (R) des Rotors als Verhältnisse y/R bzw. x/R zwischen den Werten der Koordinate jedes Punktes und dem Wert des Radius (R) des Rotors angegeben sind, wobei die Koordinaten (y, x) der Punkte innerhalb eines Bereichs von ±0,600 mm sowohl auf der Abszisse als auch auf der Ordinate variabel sind: x/R = 0.450; y/R = -0.397 x/R = 0.455; y/R = -0.391 x/R = 0.461 ; y/R = -0.387 x/R = 0.468; y/R = -0.384 x/R = 0.474; y/R = -0.381 x/R = 0.480; y/R = -0.377 x/R = 0.436; y/R = -0.374 x/R = 0.493; y/R = -0.371 x/R = 0.499; y/R = -0.368 x/R = 0.505; y/R = -0.365 x/R = 0.512; y/R = -0.362 x/R = 0.518; y/R = -0.359 x/R = 0.524; y/R = -0.356 x/R = 0.531; y/R = -0.353 x/R = 0.537; y/R = -0.350 x/R = 0.543; y/R = -0.347 x/R = 0.550; y/R = -0.344 x/R = 0.556; y/R = -0.341 x/R = 0.562; y/R = -0.337 x/R = 0.568; y/R = 0.334 x/R = 0.575; y/R = -0.331 x/R = 0.581; y/R = -0.328 x/R = 0.587; y/R = -0.321 x/R = 0.593; y/R = -0.321 x/R = 0.599; y/R = -0.318 x/R = 0.605; y/R = -0.314 x/R = 0.612; y/R = -0.311 x/R = 0.618; y/R = -0.307 x/R = 0.624; y/R = -0.303 x/R = 0.630; y/R = -0.300 x/R = 0.650; y/R = -0.287 x/R = 0.670; y/R = -0.275 x/R = 0.690; y/R = -0.261 x/R = 0.709; y/R = -0.248 x/R = 0.729; y/R = -0.234 x/R = 0.748; y/R = -0.220 x/R = 0.767; y/R = -0.205 x/R = 0.785; y/R = -0.190 x/R = 0.804; y/R = -0.175 x/R = 0.822; y/R = -0.160 x/R = 0.844; y/R = -0.140 x/R = 0.866; y/R = -0.120 x/R = 0.888; y/R = -0.1 a0 x/R = 0.910; y/R = -0.079 x/R = 0.931; y/R = -0.058 x/R = 0.952; y/R = -0.037 x/R = 0.972; y/R = -0.015 x/R = 0.993; y/R = 0.007 Zylindrische Laufschaufel nach Anspruch 1, bei der die gekrümmte Linie (7) durch die folgenden Koordinaten (y, x) einer diskreten Menge von zu der Kurve (7) gehörenden Punkten definiert ist und bei der der Rotor einen Außenradius (R) von 200 mm aufweist : x = 89.957; y = -79.420; x = 91.036; y = -78.247; x = 92.261; y = -77.492; x = 93.504; y = -76.790; x = 94.753; y = -76.115; x = 96.007; y = -75.462; x = 97.264; y = -74.820; x = 98.524; y = -74.190; x = 99.788; y = -73.573; x = 101.064; y = -72.962; x = 102.321; y = -72.354; x = 103.592; y = -71.758; x = 104.867; y = -71.171; x = 106.139; y = -70.576; x = 107.407; y = -69.973; x = 108.673; y = -69.363; x = 109.934; y = -68.745; x = 111.191; y = -68.119; x = 112.449; y = -67.483; x = 113.692; y = -66.840; x = 114.937; y = -66.188; x = 116.177; y = -65.529; x = 117.414; y = -64.261; x = 118.646; y = -64.185; x = 119.874; y = -63.502; x = 121.098; y = -62.811; x = 122.317; y = -62.112; x = 123.533; y = -61.406; x = 124.744; y = -60.693; x = 125.951; y = -59.972; x = 130.003; y = -57.480; x = 134.008; y = -54.910; x = 137.965; y = -52.265; x = 141.875; y = -49.548; x = 145.737; y = -46.763; x = 149.553; y = -43.913; x = 153,323; y = -41.000; x = 157.048; y = -38.028; x = 160.728; y = -35.000; x = 164.365; y = -31.918; x = 168.848; y = -27.992; x = 173.262; y = -23.989; x = 177.613; y = -13.912; x = 181.903; y = -15.768; x = 186.137; y = -11.563; x = 190.317; y = -7.303; x = 194.448; y = -2.994; x = 198.537; y = 1.364. Rotor der rein radialen Bauart eines Kreiselverdichters mit einem mittleren Strömungskoeffizienten, dadurch gekennzeichnet, dass er mehrere zylindrische Laufschaufeln (1) gemäß einem beliebigen der vorhergehenden Ansprüche enthält. Rotor nach Anspruch 3, dadurch gekennzeichnet, dass er einen Außenradius von 200 mm aufweist und dass er 17 Laufschaufeln (1) enthält.
Anspruch[en]
Cylindrical blade for a rotor of the purely radial type of a centrifugal compressor with a medium flow coefficient, the said blade (1) comprising a first surface (3) of the pressure side and a second surface (5) of the suction side having equal curvature, both having generatrices parallel to the axis (Z) of rotation of the rotor, characterized in that the intersection of each of the said surfaces (3, 5) on a plane (Y, X) of a right-hand Cartesian reference system (Y, X, Z), having an axis of ordinates (X) and an axis of abscissae (Y), and an axis (Z) coinciding with the axis of rotation of the rotor, is a curved line (7) defined by a discrete set of points belonging to the said curve (7) whose coordinates (y) on the axis of abscissae and (x) on the axis of ordinates are expressed as a function of the outer radius (R) of the rotor as the ratios y/R and x/R respectively between the values of the coordinate of each point and the value of the said radius (R) of the rotor, the coordinates (y, x) of the said points being variable within a range of ± 0.600 mm on both the abscissa and the ordinate: x/R = 0.450; y/R = -0.397 x/R = 0.455; y/R = -0.391 x/R = 0.461; y/R = -0.387 x/R = 0.468; y/R = -0.384 x/R = 0.474; y/R = -0.381 x/R = 0.480; y/R = -0.377 x/R = 0.486; y/R = -0.374 x/R = 0.493; y/R = -0.371 x/R = 0.499; y/R = -0.368 x/R = 0.505; y/R = -0.365 x/R = 0.512; y/R = -0.362 x/R = 0.518; y/R = -0.359 x/R = 0.524; y/R = -0.356 x/R = 0.531; y/R = -0.353 x/R = 0.537; y/R = -0.350 x/R = 0.543; y/R = -0.347 x/R = 0.550; y/R = -0.344 x/R = 0.556; y/R = -0.341 x/R = 0.562; y/R = -0.337 x/R = 0.568; y/R = -0.334 x/R = 0.575; y/R = -0.331 x/R = 0.575; y/R = -0.331 x/R = 0.581; y/R = -0.328 x/R = 0.587; y/R = -0.321 x/R = 0.593; y/R = -0.321 x/R = 0.599; y/R = -0.318 x/R = 0.605; y/R = -0.314 x/R = 0.612; y/R = -0.311 x/R = 0.618; y/R = -0.307 x/R = 0.624; y/R = -0.303 x/R = 0.630; y/R = -0.300 x/R = 0.650; y/R = -0.287 x/R = 0.670; y/R = -0.275 x/R = 0.690; y/R = -0.261 x/R = 0.709; y/R = -0.248 x/R = 0.729; y/R = -0.234 x/R = 0.748; y/R = -0.220 x/R = 0.767; y/R = -0.205 x/R = 0.785; y/R = -0.190 x/R = 0.804; y/R = -0.175 x/R = 0.822; y/R = -0.160 x/R = 0.844; y/R = -0.140 x/R = 0.866; y/R = -0.120 x/R = 0.888; y/R = -0.100 x/R = 0.910; y/R = -0.079 x/R = 0.931; y/R = -0.058 x/R = 0.952; y/R = -0.037 x/R = 0.972; y/R = -0.015 x/R = 0.993; y/R = 0.007 Cylindrical blade according to Claim 1, in which the said curved line (7) is defined by the following coordinates (y, x) of a discrete set of points belonging to the said curve (7) and in which the said rotor has an outer radius (R) of 200 mm: x = 89.957; y = -79.420; x = 91.036; y = -78.247; x = 92.261; y = -77.492; x = 93.504; y = -76.790; x = 94.753; y = -76.115; x = 96:007; y = -75.462; x = 97.264; y = -74.820; x = 98.524; y = -74.190; x = 99.788; y = -73.573; x = 101.064; y = -72.962; x = 102.321; y = -72.354; x = 103.592; y = -71.758; x = 104.867; y = -71.171; x = 106.139; y = -70.576; x = 107.407; y = -69.973; x = 108.673; y = -69.363; x = 109.934; y = -68.745; x = 111.191; y = -68.119; x = 112.449; y = -67.483; x = 113.692; y = -66.840; x = 114.937; y = -66.188; x = 116.177; y = -65.529; x = 117.414; y = -64.261; x = 118.646; y = -64.185; x = 119.874; y = -63.502; x = 121.098; y = -62.811; x = 122.317; y = -62.112; x = 123.533; y = -61.406; x = 124.744; y = -60.693; x = 125.951; y = -59.972; x = 130.003; y = -57.480; x = 134.008; y = -54.910; x = 137.965; y = -52.265; x = 141.875; y = -49.548; x = 145.737; y = -46.763; x = 149.553; y = -43.913; x = 153.323; y = -41.000; x = 157.048; y = -38.028; x = 160.728; y = -35.000; x = 164.365; y = -31.918; x = 168.848; y = -27.992; x = 173.262; y = -23.989; x = 177.613; y = -19.912; x = 181.903; y = -15.768; x = 186.137; y = -11.563; x = 190.317; y = -7.303; x = 194.448; y = -2.994; x = 198.537; y = 1.364. Rotor of the purely radial type of a centrifugal compressor with a medium flow coefficient, characterized in that it incorporates a plurality of cylindrical blades (1) according to any one of the preceding claims. Rotor according to Claim 3, characterized in that it has an outer radius of 200 mm and in that it incorporates 17 blades (1).
Anspruch[fr]
Pale cylindrique pour un rotor du type purement radial d'un compresseur centrifuge avec un coefficient de débit moyen, ladite pale (1) comprenant une première surface (3) de l'intrados et une deuxième surface (5) de l'extrados ayant une courbure identique, les deux ayant des génératrices parallèles à l'axe (Z) de rotation du rotor, caractérisée en ce que l'intersection de chacune desdites surfaces (3, 5) sur un plan (Y, X) d'un système (Y, X, Z) de référence cartésien de droite, ayant un axe des ordonnées (X) et un axe des abscisses (Y), et un axe (Z) coïncidant avec l'axe de rotation du rotor, est une ligne courbe (7) définie par un ensemble discret de points appartenant à ladite courbe (7) dont les coordonnées (y) sur l'axe des abscisses et (x) sur l'axe des ordonnées sont exprimées en fonction du rayon extérieur (R) du rotor en tant que rapports y/R et x/R respectivement entre les valeurs des coordonnées de chaque point et la valeur dudit rayon (R) du rotor, les coordonnées (x, y) desdits points pouvant varier dans la limite d'un écart de ± 0,600 mm sur à la fois l'abscisse et l'ordonnée : x/R = 0,450 ; y/R = -0,397 x/R = 0,455 ; y/R = -0,391 x/R = 0,461 ; y/R = -0,387 x/R = 0,468 ; y/R = -0,384 x/R = 0,474 ; y/R = -0,381 x/R = 0,480 ; y/R = -0,377 x/R = 0,486 ; y/R = -0,374 x/R = 0,493 ; y/R = -0,371 x/R = 0,499 ; y/R = -0,368 x/R = 0,505 ; y/R = -0,365 x/R = 0,512 ; y/R = -0,362 x/R = 0,518 ; y/R = -0,359 x/R = 0,524 ; y/R = -0,356 x/R = 0,531 ; y/R = -0,353 x/R = 0,537 ; y/R = -0,350 x/R = 0,543 ; y/R = -0,347 x/R = 0,550 ; y/R = -0,344 x/R = 0,556 ; y/R = -0,341 x/R = 0,562 ; y/R = -0,337 x/R = 0,568 ; y/R = -0,334 x/R = 0,575 ; y/R = -0,331 x/R = 0,581 ; y/R = -0,328 x/R = 0,587 ; y/R = -0,321 x/R = 0,593 ; y/R = -0,321 x/R = 0,599 ; y/R = -0,318 x/R = 0,605 ; y/R = -0,314 x/R = 0,612 ; y/R = -0,311 x/R = 0,618 ; y/R = -0,307 x/R = 0,624 ; y/R = -0,303 x/R = 0,630 ; y/R = -0,300 x/R = 0,650 ; y/R = -0,287 x/R = 0,670 ; y/R = -0,275 x/R = 0,690 ; y/R = -0,261 x/R = 0,709 ; y/R = -0,248 x/R = 0,729 ; y/R = -0,234 x/R = 0,748 ; y/R = -0,220 x/R = 0,767 ; y/R = -0,205 x/R = 0,785 ; y/R = -0,190 x/R = 0,804 ; y/R = -0,175 x/R = 0,822 ; y/R = -0,160 x/R = 0,844 ; y/R = -0,140 x/R = 0,866 ; y/R = -0,120 x/R = 0,888 ; y/R = -0,100 x/R = 0,910 ; y/R = -0,079 x/R = 0,931 ; y/R = -0,058 x/R = 0,952 ; y/R = -0,037 x/R = 0,972 ; y/R = -0,015 x/R = 0,993 ; y/R = 0,007 Pale cylindrique selon la revendication 1, dans laquelle ladite ligne courbe (7) est définie par les coordonnées (y, x) suivantes d'un ensemble discret de points appartenant à ladite courbe (7) et dans laquelle ledit rotor a un rayon extérieur (R) de 200 mm : x = 89,957 ; y = -79,420 ; x = 91,036 ; y = -78,247 ; x = 92,261 ; y = -77,492 ; x = 93,504 ; y = -76,790 ; x = 94,753 ; y = -76,115 ; x = 96,007 ; y = -75,462 ; x = 97,264 ; y = -74,820 ; x = 98,524 ; y = -74,190 ; x = 99,788 ; y = -73,573 ; x = 101,064 ; y = -72,962 ; x = 102,321 ; y = -72,354 ; x = 103,592 ; y = -71,758 ; x = 104,867 ; y = -71,171 ; x = 106,139 ; y = -70,576 ; x = 107,407 ; y = -69,973 ; x = 108,673 ; y = -69,363 ; x = 109,934 ; y = -68,745 ; x = 111,191 ; y = -68,119; x = 112,449 ; y = -67,483 ; x = 113,692 ; y = -66,840 ; x = 114,937 ; y = -66,188 ; x = 116,177 ; y = -65,529 ; x = 117,414 ; y = -64,261 ; x = 118,646 ; y = -64,185 ; x = 119,874 ; y = -63,502 ; x = 121,098 ; y = -62,811 ; x = 122,317 ; y = -62,112 ; x = 123,533 ; y = -61,406 ; x = 124,744 ; y = -60,693 ; x = 125,951 ; y = -59,972 ; x = 130,003 ; y = -57,480 ; x = 134,008 ; y = -54,910 ; x = 137,965 ; y = -52,265 ; x = 141,875 ; y = -49,548 ; x = 145,737 ; y = -46,763 ; x = 149,553 ; y = -43,913 ; x = 153,323 ; y = -41,000 ; x = 157,048 ; y = -38,028 ; x = 160,728 ; y = -35,000 ; x = 164,365 ; y = -31,918 ; x = 168,848 ; y = -27,992 ; x = 173,262 ; y = -23,989 ; x = 177,613 ; y = -19,912 ; x = 181,903 ; y = -15,768 ; x = 186,137 ; y = -11, 563 ; x = 190,317 ; y = -7,303 ; x = 194,448 ; y = -2,994 ; x = 198,537 ; y = 1,364 ; Rotor du type purement radial d'un compresseur centrifuge avec un coefficient de débit moyen, caractérisé en ce qu'il intègre une pluralité de pales cylindriques (1) selon l'une quelconque des revendications précédentes. Rotor selon la revendication 3, caractérisé en ce qu'il comporte un rayon extérieur de 200 mm et en ce qu'il intègre 17 pales (1).






IPC
A Täglicher Lebensbedarf
B Arbeitsverfahren; Transportieren
C Chemie; Hüttenwesen
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F Maschinenbau; Beleuchtung; Heizung; Waffen; Sprengen
G Physik
H Elektrotechnik

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