Airfoil profile for a turbine nozzle

Information

  • Patent Grant
  • 11326460
  • Patent Number
    11,326,460
  • Date Filed
    Thursday, July 15, 2021
    2 years ago
  • Date Issued
    Tuesday, May 10, 2022
    2 years ago
Abstract
An airfoil profile for a turbine nozzle of a gas turbine is provided. The turbine nozzle may include an airfoil portion having an uncoated nominal profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1, wherein the X, Y, and Z coordinates are distances in inches measured in a Cartesian coordinate system, the corresponding X and Y coordinates, when connected by a smooth continuous arc, define one of a plurality of airfoil profile sections at each Z distance, and the plurality of airfoil profile sections, when joined together by smooth continuous arcs, define an airfoil shape.
Description
TECHNICAL FIELD

This application relates to airfoils for a gas turbine and more particularly to an airfoil profile for a turbine nozzle of a gas turbine.


BACKGROUND

Turbines are machines that obtain rotational force by impulsive or reaction force using a flow of a compressible fluid such as steam or gas, and include a steam turbine using steam, a gas turbine using hot combustion gas, and so on.


The gas turbine includes a compressor, a combustor, and a turbine. The compressor includes an air inlet into which air is introduced, and a plurality of compressor vanes and a plurality of compressor blades which are alternately arranged in a compressor housing. The introduced air is compressed by the compressor vanes and the compressor blades while passing through an inside of the compressor.


The combustor supplies fuel to air compressed by the compressor and ignites a fuel-air mixture with an igniter to produce high-temperature and high-pressure combustion gas.


The turbine includes a plurality of turbine vanes and a plurality of turbine blades which are alternately arranged in a turbine housing. In addition, a rotor is arranged to pass through centers of the compressor, the combustor, the turbine, and an exhaust chamber.


The rotor is rotatably supported at both ends thereof by bearings. A plurality of disks are fixed to the rotor, and a plurality of blades are connected to each of the disks while a drive shaft of a generator is connected to an end of the exhaust chamber.


In a gas turbine, many system requirements should be met at each stage of the gas turbine to meet design goals. The design goals may include overall improved efficiency and airfoil loading capability. For example, a turbine nozzle airfoil profile should achieve thermal and mechanical operating requirements for that particular stage. There is thus a desire for an improved turbine nozzle airfoil profile for use in a turbine and the like.


SUMMARY

Aspects of one or more exemplary embodiments provide a unique airfoil profile for the nozzles of a turbine stage capable of enhancing aeromechanics and reducing thermal and mechanical stresses.


Additional aspects will be set forth in part in the description which follows and, in part, will become apparent from the description, or may be learned by practice of the exemplary embodiments.


According to an aspect of an exemplary embodiment, there is provided a turbine nozzle including: an airfoil portion having an uncoated nominal profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1. Here, the X, Y, and Z coordinates are distances in inches measured in a Cartesian coordinate system, the corresponding X and Y coordinates, when connected by a smooth continuous arc, define one of a plurality of airfoil profile sections at each Z distance, and the plurality of airfoil profile sections, when joined together by smooth continuous arcs, define an airfoil shape.


The airfoil shape may lie within an envelope of +1-0.120 inches measured in a direction normal to any of the plurality of airfoil profile sections.


The X and Y coordinate values are scalable as a function of a same constant or number, and a set of corresponding nominal Z coordinate values are scalable as a function of the same constant or number to provide at least one of a scaled up or a scaled down airfoil.


The airfoil shape may include a leaned airfoil section to reduce a secondary flow effect.


The turbine nozzle may further include a coating applied to the airfoil shape, the coating having a thickness of less than or equal to 0.010 inches.


According to an aspect of another exemplary embodiment, there is provided a turbine including: a turbine nozzle extending from a platform to an end wall and having an airfoil-shaped cross section having a leading edge, a trailing edge, and a pressure side and a suction side each of which extends from the leading edge to the trailing edge, wherein the turbine nozzle may include an airfoil portion having an uncoated nominal profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1. Here, the X, Y, and Z coordinates are distances in inches measured in a Cartesian coordinate system, the corresponding X and Y coordinates, when connected by a smooth continuous arc, define one of a plurality of airfoil profile sections at each Z distance, and the plurality of airfoil profile sections, when joined together by smooth continuous arcs, define an airfoil shape.


According to an aspect of another exemplary embodiment, there is provided a gas turbine including: a compressor configured to compress air; a combustor configured to mix compressed air supplied from the compressor with fuel for combustion; and a turbine including a plurality of turbine nozzles and a plurality of turbine blades rotated by combustion gas to generate power, wherein each of the turbine nozzles extending from a platform to an end wall and having an airfoil-shaped cross section having a leading edge, a trailing edge, and a pressure side and a suction side each of which extends from the leading edge to the trailing edge, and wherein the turbine nozzle may include an airfoil portion having an uncoated nominal profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1. Here, the X, Y, and Z coordinates are distances in inches measured in a Cartesian coordinate system, the corresponding X and Y coordinates, when connected by a smooth continuous arc, define one of a plurality of airfoil profile sections at each Z distance, and the plurality of airfoil profile sections, when joined together by smooth continuous arcs, define an airfoil shape.





BRIEF DESCRIPTION OF THE DRAWINGS

The above and other aspects will become more apparent from the following description of the exemplary embodiments with reference to the accompanying drawings, in which:



FIG. 1 is a partially cutaway perspective view illustrating a gas turbine according to an exemplary embodiment;



FIG. 2 is a cross-sectional view illustrating a schematic structure of the gas turbine according to the exemplary embodiment;



FIG. 3 is a schematic diagram of a turbine according to an exemplary embodiment;



FIG. 4 is an aft view of a turbine nozzle including an airfoil according to an exemplary embodiment;



FIG. 5 is a forward view of a turbine nozzle including an airfoil according to an exemplary embodiment; and



FIG. 6 is an airfoil shape including a leaned airfoil section according to an exemplary embodiment.





DETAILED DESCRIPTION

Various modifications and various embodiments will be described below in detail with reference to the accompanying drawings so that those skilled in the art can easily carry out the disclosure. It should be understood, however, that the various embodiments are not for limiting the scope of the disclosure to the specific embodiment, but they should be interpreted to include all modifications, equivalents, and alternatives of the embodiments included within the spirit and scope disclosed herein.


Hereinafter, exemplary embodiments will be described in detail with reference to the accompanying drawings. Throughout the disclosure, like reference numerals refer to like parts throughout the various figures and exemplary embodiments. In certain embodiments, a detailed description of functions and configurations well known in the art may be omitted to avoid obscuring appreciation of the disclosure by a person of ordinary skill in the art. For the same reason, some components may be exaggerated, omitted, or schematically illustrated in the accompanying drawings.



FIG. 1 is a partially cutaway perspective view illustrating a gas turbine according to an exemplary embodiment. FIG. 2 is a cross-sectional view illustrating a schematic structure of the gas turbine according to the exemplary embodiment.


Referring to FIGS. 1 and 2, the gas turbine 1000 may include a compressor 1100, a combustor 1200, and a turbine 1300. Based on a flow direction of gas (e.g., compressed air or combustion gas), the compressor 1100 is disposed at an upstream side of the gas turbine 1000, and the turbine 1300 is disposed at a downstream side of the gas turbine 1000. The combustor 1200 is disposed between the compressor 1100 and the turbine 1300.


The compressor 1100 includes compressor vanes 1120 and compressor rotors in a compressor housing. The turbine 1300 includes turbine vane 1320 and turbine rotors in a turbine housing. The compressor vanes 1120 and the compressor rotors are arranged in a multi-stage arrangement along the flow direction of compressed air. The turbine vanes 1320 and the turbine rotors are arranged in a multi-stage arrangement along the flow direction of combustion gas. The compressor 1100 is designed such that an internal space is gradually decreased in size from a front stage to a rear stage so that air drawn into the compressor 1100 can be compressed. On the contrary, the turbine 1300 is designed such that an internal space is gradually increased in size from a front stage to a rear stage so that combustion gas received from the combustor 1200 can expand.


A torque tube for transmitting a rotational torque generated by the turbine 1300 to the compressor 1100 is disposed between a compressor rotor that is located at the rearmost stage of the compressor 1100 and a turbine rotor that is located at the foremost stage of the turbine 1300. FIG. 2 illustrates a case in which the torque tube includes multiple torque tube disks arranged in a three-stage arrangement, but it is understood that this is only an example and other exemplary embodiments are not limited thereto. For example, the torque tube may include multiple torque tube disks arranged in an arrangement of equal to or greater than four stages or an arrangement of equal to or less than two stages.


Each of the compressor rotors includes a compressor rotor disk and a compressor blade 1110 fastened to the compressor disk. That is, the compressor 1100 includes a plurality of compressor rotor disks, and respective compressor rotor disks are coupled to each other by a tie rod to prevent axial separation in an axial direction. The compressor rotor disks are arranged in the axial direction with the tie rod extending through centers of the compressor disks. Adjacent compressor rotor disks are arranged such that opposing surfaces thereof are in tight contact with each other by being tightly fastened by the tie rod so that the adjacent compressor rotor disks cannot rotate relative to each other. Each of the compressor rotor disks has a plurality of compressor blades 1110 radially coupled to an outer circumferential surface thereof.


The compressor blades 1110 (or referred to as buckets) are radially coupled to an outer circumferential surface of each of the compressor rotor disks in a row. The compressor vanes 1120 (or referred to as nozzles) are provided on an inner circumferential surface of the compressor housing in an annular row in each stage, and rows of the compressor vanes 1120 are arranged between rows of the compressor blades 1110. While the compressor disks rotate along with a rotation of the tie rod, the compressor vanes 1120 fixed to the housing do not rotate. The compressor vanes 1120 guide the flow of compressed air moved from front-stage compressor blades to rear-stage compressor blades.


The tie rod is disposed to pass through centers of the plurality of compressor rotor disks and turbine rotor disks. One end of the tie rod is fastened to a compressor disk located at the foremost stage of the compressor 1100, and the other end thereof is fastened in the torque tube by a fastening nut.


It is understood that the tie rod is not limited to the example illustrated in FIG. 2, and may be changed or vary according to one or more other exemplary embodiments. For example, a single tie rod may be disposed to pass through the centers of the rotor disks, a plurality of tie rods may be arranged circumferentially, or a combination thereof may be used.


Also, a deswirler serving as a guide vane may be provided in the compressor 1100 to adjust an actual inflow angle of the fluid entering into an inlet of the combustor 1200 to a designed inflow angle.


The combustor 1200 mixes the introduced compressed air with fuel, burns a fuel-air mixture to produce high-temperature and high-pressure combustion gas with high energy, and increases the temperature of the combustion gas to a temperature at which the combustor and the turbine components are able to withstand an isobaric combustion process.


A plurality of combustors constituting the combustor 1200 of the gas turbine may be arranged in the housing in a form of a cell. The combustor 1200 may include a plurality of chambers 1210 and fuel nozzle modules 1220 arranged annually.


The high-temperature and high-pressure combustion gas supplied from the combustor 1200 flows into the turbine 1300 and expands while passing through the inside of the turbine 1300, thereby applying an impulsive force or reaction force to the turbine blades 1310 to generate a rotational torque. A portion of the rotational torque is transmitted to the compressor via the torque tube, and a remaining portion which is an excessive torque is used to drive a generator to produce power.


The turbine 1300 basically has a structure similar to the compressor 1100. That is, the turbine 1300 may include a plurality of turbine rotors similar to the compressor rotors, and each of the turbine rotor may include a turbine rotor disk and a turbine blade 1310 fastened to the turbine rotor disk. A plurality of turbine blades 1310 (or referred to as buckets) are radially disposed. A plurality of turbine vanes 1320 (or referred to as nozzles) are fixedly arranged on an inner circumferential surface of the turbine housing in an annular row in each stage, and rows of the turbine vanes 1320 are arranged between rows of the turbine blades 1310. The turbine vanes 1320 guide the flow direction of combustion gas passing through the turbine blades 1310.



FIG. 3 is a schematic diagram of the turbine 1300 according to an exemplary embodiment. FIG. 4 is an aft view of a turbine nozzle including an airfoil according to an exemplary embodiment. FIG. 5 is a forward view of a turbine nozzle including an airfoil according to an exemplary embodiment.


Referring to FIG. 3, the turbine 1300 may include a plurality of turbine stages employing a plurality of nozzles and a plurality of buckets. For example, a first stage comprises a plurality of circumferentially spaced nozzles 20 and buckets 10. The nozzles are circumferentially spaced one from the other and fixed about the axis of the rotor. The first stage buckets 10 are mounted on the turbine rotor 17. A second stage of the turbine 1300 includes a plurality of circumferentially spaced nozzles 26 and buckets 16 mounted on the rotor 17. A third stage of the turbine 1300 includes a plurality of circumferentially spaced nozzles 32 and buckets 22 mounted on rotor 17. Although three stages are illustrated in FIG. 3, it is to be understood that any number of stages may be used.


Referring to FIGS. 4 and 5, the turbine nozzle 1320 according to the exemplary embodiment includes an airfoil extending from a platform 1340 to an end wall 1342. The turbine vane airfoil 1330 has an airfoil-shaped cross section having a leading edge 1331, a trailing edge 1332, a pressure side 1333, and a suction side 1334. The pressure side 1333 and the suction side 1334 are formed to extend from the leading edge 1331 to the trailing edge 1332.


The airfoil shape may be defined by a loci of points in space that meet stage design requirements. These points are unique and specific to the system. The list of X, Y, and Z coordinates for the airfoil, which are included as Table 1, has been optimized for stage efficiency, aerodynamic efficiency, and thermal and mechanical life requirements. In one exemplary embodiment, the points may be arrived at by iteration between aerodynamic and mechanical design optimization. Accordingly, these are the only loci of points that allow the gas turbine to run at the most efficient, safe and smooth manner.


Referring to FIGS. 4 and 5, the airfoil shape of the exemplary embodiment is defined by a unique set or loci of points in space that may be delineated. As shown in Table 1, the loci that defines the shape of the airfoil may include a set of approximately 1,440 points with X, Y and Z coordinates. The X, Y and Z coordinates, which represent the airfoil shape, are created in a coordinate system which is defined relative to the cold rotor centerline axis of the gas turbine (i.e., X coordinate axis). The origin of the coordinate system on the cold rotor centerline axis is defined as X=0.0, Y=0.0 and Z=0.0. For example, the coordinate system is set relative to the airfoil and is fully defined by points A, B and C. Points A and B are both located 41.650 inches above the cold rotor centerline axis. Point A lies at an intersection of the airfoil mean camber line and the leading-edge airfoil surface. Point B lies at an intersection of the airfoil mean camber line and the trailing-edge airfoil surface. Point C is located 46.100 inches above the cold rotor centerline axis and lies at the intersection of the airfoil mean camber line and the airfoil trailing-edge surface. Here, a coordinate system origin is located at point A. Points A and B define the positive X-axis. Points A, B and C define the positive X-Z plane. The Y-axis is then defined using the right-hand rule methodology. The coordinate values for the X, Y and Z coordinates are set forth in inches in Table 1, although other units of dimensions may be used if the values are appropriately converted.


The Cartesian coordinate system of X, Y and Z values given in Table 1 below defines the shape of the airfoil according to an exemplary embodiment. More specifically, the shape of the airfoil is defined by the cloud of points listed such that airfoil could be constructed by defining approximately smooth sheet surfaces through the listed points. As one of ordinary skill in the art will appreciate, Table 1 values are generated and shown to three decimal places for determining the profile of airfoil. All of the 1440 points represent a nominal cold or room temperature shape of the airfoil. It will be appreciated that as the nozzle heats up in operation, mechanical loading and temperature will cause a change in X, Y and Z coordinates. Accordingly, values for the airfoil shape given in Table 1 represent ambient, non-operating or non-hot conditions.


The coordinate values set forth in Table 1 below are for a cold condition of the turbine nozzle (e.g., non-rotating state and at room temperature). Further, the coordinate values set forth in Table 1 are for an uncoated nominal three-dimensional (3D) shape of the turbine nozzle. In some aspects, a coating (e.g., corrosion protective coating) may be applied to the turbine nozzle. The coating thickness may up to about 0.010 inches thick.


Further, the turbine nozzle 1320 may be fabricated using a variety of manufacturing techniques, such as forging, casting, milling, electro-chemical machining, electric-discharge machining, and the like. As such, the turbine nozzle may have a series of manufacturing tolerances for the position, profile, twist, and chord that can cause the turbine nozzle to vary from the nominal 3D shape defined by the coordinate values set forth in Table 1. This manufacturing tolerance may be, for example, +1-0.120 inches in a direction away from any of the coordinate values of Table 1 without departing from the scope of the subject matter described herein.


In addition to manufacturing tolerances affecting the overall size of the turbine nozzle, it is also possible to scale the airfoil to a larger or smaller airfoil size. In order to maintain the benefits of this 3D shape, in terms of stiffness and stress, it is necessary to scale the turbine nozzle uniformly in the X, Y, and Z directions.


The Table 1 values are generated and shown for determining the profile of the airfoil. There are typical manufacturing tolerances as well as coatings which must be accounted for in the actual profile of the airfoil. Each section is joined smoothly with the other sections to form the complete airfoil shape. It will therefore be appreciated that +/−typical manufacturing tolerances, i.e., +/−values, including any coating thicknesses, are additive to the X, Y and Z values given in Table 1 below.














TABLE 1








X
Y
Z
















Section 1












Point 1
5.994
−0.345
−0.677



Point 2
5.903
−0.290
−0.673



Point 3
5.786
−0.323
−0.676



Point 4
5.669
−0.356
−0.678



Point 5
5.551
−0.388
−0.680



Point 6
5.434
−0.420
−0.683



Point 7
5.316
−0.451
−0.685



Point 8
5.199
−0.481
−0.687



Point 9
5.081
−0.510
−0.689



Point 10
4.962
−0.538
−0.692



Point 11
4.844
−0.565
−0.694



Point 12
4.725
−0.590
−0.695



Point 13
4.606
−0.614
−0.697



Point 14
4.486
−0.636
−0.699



Point 15
4.366
−0.656
−0.700



Point 16
4.246
−0.674
−0.702



Point 17
4.125
−0.690
−0.703



Point 18
4.005
−0.703
−0.704



Point 19
3.884
−0.715
−0.705



Point 20
3.762
−0.724
−0.705



Point 21
3.641
−0.730
−0.706



Point 22
3.519
−0.734
−0.706



Point 23
3.398
−0.735
−0.706



Point 24
3.276
−0.734
−0.706



Point 25
3.155
−0.729
−0.706



Point 26
3.034
−0.722
−0.705



Point 27
2.912
−0.711
−0.704



Point 28
2.792
−0.698
−0.703



Point 29
2.671
−0.682
−0.702



Point 30
2.551
−0.663
−0.701



Point 31
2.431
−0.641
−0.699



Point 32
2.312
−0.617
−0.697



Point 33
2.194
−0.589
−0.695



Point 34
2.076
−0.559
−0.693



Point 35
1.959
−0.527
−0.691



Point 36
1.843
−0.492
−0.688



Point 37
1.727
−0.455
−0.685



Point 38
1.612
−0.415
−0.682



Point 39
1.498
−0.374
−0.679



Point 40
1.384
−0.331
−0.676



Point 41
1.271
−0.286
−0.673



Point 42
1.158
−0.241
−0.670



Point 43
1.046
−0.194
−0.666



Point 44
0.934
−0.146
−0.663



Point 45
0.823
−0.098
−0.659



Point 46
0.711
−0.051
−0.656



Point 47
0.598
−0.005
−0.652



Point 48
0.484
0.038
−0.649



Point 49
0.369
0.075
−0.646



Point 50
0.250
0.101
−0.644



Point 51
0.129
0.103
−0.644



Point 52
0.013
0.068
−0.647



Point 53
−0.092
0.007
−0.651



Point 54
−0.177
−0.078
−0.658



Point 55
−0.239
−0.183
−0.665



Point 56
−0.285
−0.295
−0.674



Point 57
−0.318
−0.411
−0.682



Point 58
−0.341
−0.530
−0.691



Point 59
−0.355
−0.651
−0.700



Point 60
−0.357
−0.772
−0.709



Point 61
−0.349
−0.893
−0.718



Point 62
−0.331
−1.013
−0.727



Point 63
−0.303
−1.131
−0.735



Point 64
−0.264
−1.246
−0.744



Point 65
−0.214
−1.356
−0.752



Point 66
−0.153
−1.460
−0.760



Point 67
−0.080
−1.557
−0.767



Point 68
0.004
−1.645
−0.773



Point 69
0.097
−1.723
−0.779



Point 70
0.198
−1.791
−0.784



Point 71
0.305
−1.848
−0.788



Point 72
0.417
−1.894
−0.792



Point 73
0.533
−1.932
−0.795



Point 74
0.651
−1.960
−0.797



Point 75
0.771
−1.981
−0.798



Point 76
0.892
−1.996
−0.799



Point 77
1.013
−2.003
−0.800



Point 78
1.134
−2.006
−0.800



Point 79
1.256
−2.004
−0.800



Point 80
1.377
−1.997
−0.799



Point 81
1.498
−1.987
−0.799



Point 82
1.619
−1.973
−0.798



Point 83
1.740
−1.956
−0.796



Point 84
1.860
−1.937
−0.795



Point 85
1.979
−1.915
−0.793



Point 86
2.098
−1.891
−0.792



Point 87
2.217
−1.865
−0.790



Point 88
2.335
−1.837
−0.788



Point 89
2.453
−1.807
−0.785



Point 90
2.571
−1.776
−0.783



Point 91
2.688
−1.743
−0.781



Point 92
2.804
−1.709
−0.778



Point 93
2.921
−1.674
−0.776



Point 94
3.037
−1.637
−0.773



Point 95
3.152
−1.600
−0.770



Point 96
3.267
−1.561
−0.767



Point 97
3.382
−1.522
−0.764



Point 98
3.497
−1.481
−0.761



Point 99
3.611
−1.440
−0.758



Point 100
3.726
−1.398
−0.755



Point 101
3.839
−1.356
−0.752



Point 102
3.953
−1.312
−0.749



Point 103
4.066
−1.268
−0.746



Point 104
4.179
−1.224
−0.742



Point 105
4.292
−1.179
−0.739



Point 106
4.405
−1.133
−0.736



Point 107
4.517
−1.087
−0.732



Point 108
4.629
−1.040
−0.729



Point 109
4.741
−0.993
−0.725



Point 110
4.853
−0.945
−0.722



Point 111
4.965
−0.897
−0.718



Point 112
5.076
−0.849
−0.715



Point 113
5.187
−0.800
−0.711



Point 114
5.299
−0.751
−0.707



Point 115
5.409
−0.701
−0.704



Point 116
5.520
−0.651
−0.700



Point 117
5.631
−0.601
−0.696



Point 118
5.741
−0.550
−0.692



Point 119
5.852
−0.499
−0.689



Point 120
5.961
−0.447
−0.685







Section 2












Point 1
6.172
−0.042
−0.103



Point 2
6.078
0.005
−0.100



Point 3
5.960
−0.028
−0.102



Point 4
5.841
−0.062
−0.105



Point 5
5.722
−0.095
−0.107



Point 6
5.603
−0.127
−0.110



Point 7
5.484
−0.159
−0.112



Point 8
5.365
−0.190
−0.114



Point 9
5.245
−0.220
−0.117



Point 10
5.125
−0.249
−0.119



Point 11
5.005
−0.277
−0.121



Point 12
4.885
−0.304
−0.123



Point 13
4.765
−0.330
−0.125



Point 14
4.644
−0.355
−0.127



Point 15
4.523
−0.378
−0.128



Point 16
4.401
−0.400
−0.130



Point 17
4.280
−0.421
−0.131



Point 18
4.158
−0.440
−0.133



Point 19
4.036
−0.458
−0.134



Point 20
3.914
−0.474
−0.135



Point 21
3.791
−0.489
−0.136



Point 22
3.669
−0.501
−0.137



Point 23
3.546
−0.512
−0.138



Point 24
3.423
−0.521
−0.139



Point 25
3.300
−0.527
−0.139



Point 26
3.176
−0.532
−0.140



Point 27
3.053
−0.534
−0.140



Point 28
2.930
−0.534
−0.140



Point 29
2.807
−0.532
−0.140



Point 30
2.683
−0.527
−0.139



Point 31
2.560
−0.520
−0.139



Point 32
2.437
−0.510
−0.138



Point 33
2.315
−0.498
−0.137



Point 34
2.192
−0.482
−0.136



Point 35
2.070
−0.464
−0.135



Point 36
1.949
−0.443
−0.133



Point 37
1.828
−0.420
−0.131



Point 38
1.707
−0.393
−0.129



Point 39
1.588
−0.364
−0.127



Point 40
1.468
−0.332
−0.125



Point 41
1.350
−0.298
−0.122



Point 42
1.233
−0.261
−0.120



Point 43
1.116
−0.221
−0.117



Point 44
1.000
−0.180
−0.114



Point 45
0.884
−0.137
−0.110



Point 46
0.769
−0.093
−0.107



Point 47
0.654
−0.050
−0.104



Point 48
0.537
−0.008
−0.101



Point 49
0.420
0.029
−0.098



Point 50
0.299
0.054
−0.096



Point 51
0.176
0.060
−0.096



Point 52
0.056
0.034
−0.098



Point 53
−0.053
−0.022
−0.102



Point 54
−0.139
−0.110
−0.108



Point 55
−0.199
−0.217
−0.116



Point 56
−0.242
−0.332
−0.125



Point 57
−0.271
−0.451
−0.134



Point 58
−0.289
−0.573
−0.143



Point 59
−0.296
−0.696
−0.152



Point 60
−0.293
−0.819
−0.161



Point 61
−0.280
−0.941
−0.170



Point 62
−0.257
−1.062
−0.179



Point 63
−0.224
−1.180
−0.188



Point 64
−0.179
−1.294
−0.196



Point 65
−0.123
−1.404
−0.204



Point 66
−0.054
−1.506
−0.212



Point 67
0.026
−1.599
−0.219



Point 68
0.117
−1.682
−0.225



Point 69
0.218
−1.753
−0.230



Point 70
0.326
−1.812
−0.234



Point 71
0.440
−1.858
−0.238



Point 72
0.558
−1.893
−0.240



Point 73
0.679
−1.918
−0.242



Point 74
0.801
−1.934
−0.243



Point 75
0.924
−1.942
−0.244



Point 76
1.047
−1.943
−0.244



Point 77
1.171
−1.939
−0.244



Point 78
1.294
−1.929
−0.243



Point 79
1.416
−1.915
−0.242



Point 80
1.538
−1.897
−0.241



Point 81
1.660
−1.875
−0.239



Point 82
1.780
−1.851
−0.237



Point 83
1.901
−1.824
−0.235



Point 84
2.021
−1.795
−0.233



Point 85
2.140
−1.764
−0.231



Point 86
2.259
−1.731
−0.228



Point 87
2.377
−1.696
−0.226



Point 88
2.495
−1.660
−0.223



Point 89
2.612
−1.623
−0.220



Point 90
2.729
−1.584
−0.217



Point 91
2.846
−1.544
−0.214



Point 92
2.962
−1.503
−0.211



Point 93
3.078
−1.461
−0.208



Point 94
3.194
−1.418
−0.205



Point 95
3.309
−1.374
−0.202



Point 96
3.424
−1.330
−0.199



Point 97
3.539
−1.285
−0.195



Point 98
3.653
−1.239
−0.192



Point 99
3.767
−1.193
−0.189



Point 100
3.882
−1.146
−0.185



Point 101
3.995
−1.099
−0.182



Point 102
4.109
−1.051
−0.178



Point 103
4.222
−1.003
−0.174



Point 104
4.336
−0.955
−0.171



Point 105
4.449
−0.906
−0.167



Point 106
4.562
−0.856
−0.164



Point 107
4.675
−0.807
−0.160



Point 108
4.787
−0.757
−0.156



Point 109
4.900
−0.707
−0.153



Point 110
5.012
−0.656
−0.149



Point 111
5.124
−0.605
−0.145



Point 112
5.237
−0.554
−0.141



Point 113
5.349
−0.503
−0.137



Point 114
5.461
−0.451
−0.134



Point 115
5.573
−0.399
−0.130



Point 116
5.684
−0.347
−0.126



Point 117
5.796
−0.295
−0.122



Point 118
5.908
−0.243
−0.118



Point 119
6.019
−0.190
−0.114



Point 120
6.130
−0.139
−0.111







Section 3












Point 1
6.283
0.139
0.461



Point 2
6.239
0.043
0.454



Point 3
6.283
0.139
0.461



Point 4
6.185
0.179
0.464



Point 5
6.066
0.143
0.462



Point 6
5.946
0.109
0.459



Point 7
5.826
0.076
0.457



Point 8
5.706
0.044
0.454



Point 9
5.585
0.012
0.452



Point 10
5.464
−0.019
0.450



Point 11
5.344
−0.049
0.448



Point 12
5.222
−0.079
0.445



Point 13
5.101
−0.108
0.443



Point 14
4.979
−0.135
0.441



Point 15
4.858
−0.162
0.439



Point 16
4.736
−0.188
0.437



Point 17
4.614
−0.213
0.435



Point 18
4.491
−0.237
0.434



Point 19
4.369
−0.260
0.432



Point 20
4.246
−0.282
0.430



Point 21
4.123
−0.303
0.429



Point 22
4.000
−0.323
0.427



Point 23
3.877
−0.341
0.426



Point 24
3.753
−0.358
0.425



Point 25
3.630
−0.374
0.424



Point 26
3.506
−0.389
0.422



Point 27
3.382
−0.402
0.422



Point 28
3.257
−0.413
0.421



Point 29
3.133
−0.423
0.420



Point 30
3.009
−0.431
0.419



Point 31
2.884
−0.437
0.419



Point 32
2.760
−0.441
0.419



Point 33
2.635
−0.444
0.418



Point 34
2.510
−0.444
0.418



Point 35
2.386
−0.441
0.419



Point 36
2.261
−0.437
0.419



Point 37
2.137
−0.429
0.419



Point 38
2.012
−0.420
0.420



Point 39
1.888
−0.407
0.421



Point 40
1.764
−0.391
0.422



Point 41
1.641
−0.372
0.424



Point 42
1.519
−0.350
0.425



Point 43
1.396
−0.325
0.427



Point 44
1.275
−0.296
0.429



Point 45
1.155
−0.264
0.432



Point 46
1.035
−0.228
0.434



Point 47
0.917
−0.190
0.437



Point 48
0.799
−0.149
0.440



Point 49
0.682
−0.106
0.443



Point 50
0.565
−0.064
0.447



Point 51
0.447
−0.024
0.449



Point 52
0.326
0.007
0.452



Point 53
0.202
0.020
0.453



Point 54
0.079
0.000
0.451



Point 55
−0.031
−0.056
0.447



Point 56
−0.116
−0.147
0.440



Point 57
−0.175
−0.256
0.432



Point 58
−0.217
−0.373
0.424



Point 59
−0.244
−0.494
0.415



Point 60
−0.260
−0.617
0.406



Point 61
−0.265
−0.742
0.396



Point 62
−0.260
−0.866
0.387



Point 63
−0.246
−0.989
0.378



Point 64
−0.220
−1.111
0.369



Point 65
−0.184
−1.230
0.360



Point 66
−0.136
−1.345
0.352



Point 67
−0.076
−1.453
0.344



Point 68
−0.003
−1.554
0.336



Point 69
0.083
−1.645
0.330



Point 70
0.180
−1.723
0.324



Point 71
0.286
−1.787
0.319



Point 72
0.400
−1.838
0.315



Point 73
0.519
−1.875
0.313



Point 74
0.641
−1.901
0.311



Point 75
0.764
−1.916
0.310



Point 76
0.889
−1.922
0.309



Point 77
1.014
−1.921
0.309



Point 78
1.138
−1.914
0.310



Point 79
1.262
−1.900
0.311



Point 80
1.385
−1.883
0.312



Point 81
1.508
−1.861
0.314



Point 82
1.630
−1.836
0.315



Point 83
1.752
−1.808
0.318



Point 84
1.873
−1.777
0.320



Point 85
1.993
−1.744
0.322



Point 86
2.113
−1.709
0.325



Point 87
2.232
−1.673
0.328



Point 88
2.350
−1.634
0.330



Point 89
2.469
−1.595
0.333



Point 90
2.586
−1.554
0.336



Point 91
2.704
−1.512
0.339



Point 92
2.821
−1.469
0.343



Point 93
2.937
−1.425
0.346



Point 94
3.054
−1.380
0.349



Point 95
3.170
−1.334
0.353



Point 96
3.285
−1.288
0.356



Point 97
3.401
−1.241
0.359



Point 98
3.516
−1.193
0.363



Point 99
3.631
−1.145
0.367



Point 100
3.746
−1.096
0.370



Point 101
3.860
−1.047
0.374



Point 102
3.975
−0.998
0.377



Point 103
4.089
−0.948
0.381



Point 104
4.203
−0.898
0.385



Point 105
4.317
−0.847
0.389



Point 106
4.431
−0.797
0.392



Point 107
4.544
−0.746
0.396



Point 108
4.658
−0.694
0.400



Point 109
4.771
−0.643
0.404



Point 110
4.885
−0.591
0.408



Point 111
4.998
−0.539
0.411



Point 112
5.111
−0.487
0.415



Point 113
5.224
−0.434
0.419



Point 114
5.337
−0.382
0.423



Point 115
5.450
−0.329
0.427



Point 116
5.563
−0.276
0.431



Point 117
5.676
−0.223
0.435



Point 118
5.789
−0.170
0.439



Point 119
5.902
−0.117
0.443



Point 120
6.014
−0.064
0.446







Section 4












Point 1
6.366
0.218
1.019



Point 2
6.267
0.257
1.022



Point 3
6.146
0.222
1.019



Point 4
6.025
0.188
1.017



Point 5
5.903
0.154
1.014



Point 6
5.781
0.122
1.012



Point 7
5.659
0.090
1.009



Point 8
5.537
0.059
1.007



Point 9
5.414
0.029
1.005



Point 10
5.292
0.000
1.003



Point 11
5.169
−0.029
1.001



Point 12
5.046
−0.057
0.999



Point 13
4.923
−0.084
0.997



Point 14
4.799
−0.110
0.995



Point 15
4.676
−0.135
0.993



Point 16
4.552
−0.159
0.991



Point 17
4.428
−0.183
0.989



Point 18
4.304
−0.205
0.988



Point 19
4.180
−0.227
0.986



Point 20
4.055
−0.247
0.984



Point 21
3.931
−0.267
0.983



Point 22
3.806
−0.285
0.982



Point 23
3.681
−0.303
0.980



Point 24
3.556
−0.319
0.979



Point 25
3.431
−0.334
0.978



Point 26
3.306
−0.347
0.977



Point 27
3.180
−0.359
0.976



Point 28
3.054
−0.370
0.975



Point 29
2.929
−0.380
0.975



Point 30
2.803
−0.388
0.974



Point 31
2.677
−0.394
0.974



Point 32
2.551
−0.398
0.973



Point 33
2.425
−0.400
0.973



Point 34
2.299
−0.401
0.973



Point 35
2.172
−0.399
0.973



Point 36
2.046
−0.395
0.974



Point 37
1.921
−0.389
0.974



Point 38
1.795
−0.379
0.975



Point 39
1.669
−0.367
0.976



Point 40
1.544
−0.352
0.977



Point 41
1.419
−0.333
0.978



Point 42
1.295
−0.311
0.980



Point 43
1.172
−0.285
0.982



Point 44
1.049
−0.254
0.984



Point 45
0.928
−0.220
0.986



Point 46
0.808
−0.183
0.989



Point 47
0.689
−0.142
0.992



Point 48
0.570
−0.099
0.995



Point 49
0.451
−0.057
0.998



Point 50
0.330
−0.023
1.001



Point 51
0.205
−0.009
1.002



Point 52
0.081
−0.030
1.000



Point 53
−0.030
−0.089
0.996



Point 54
−0.115
−0.181
0.989



Point 55
−0.174
−0.292
0.981



Point 56
−0.216
−0.411
0.972



Point 57
−0.244
−0.533
0.963



Point 58
−0.260
−0.658
0.954



Point 59
−0.266
−0.783
0.945



Point 60
−0.261
−0.909
0.936



Point 61
−0.246
−1.034
0.926



Point 62
−0.220
−1.157
0.917



Point 63
−0.183
−1.277
0.908



Point 64
−0.134
−1.393
0.900



Point 65
−0.072
−1.502
0.892



Point 66
0.005
−1.602
0.884



Point 67
0.094
−1.691
0.878



Point 68
0.196
−1.765
0.872



Point 69
0.307
−1.825
0.868



Point 70
0.424
−1.870
0.864



Point 71
0.546
−1.901
0.862



Point 72
0.671
−1.920
0.861



Point 73
0.797
−1.928
0.860



Point 74
0.923
−1.929
0.860



Point 75
1.049
−1.922
0.861



Point 76
1.174
−1.909
0.862



Point 77
1.299
−1.891
0.863



Point 78
1.423
−1.869
0.865



Point 79
1.547
−1.843
0.866



Point 80
1.669
−1.814
0.869



Point 81
1.792
−1.783
0.871



Point 82
1.913
−1.749
0.873



Point 83
2.034
−1.713
0.876



Point 84
2.154
−1.675
0.879



Point 85
2.274
−1.636
0.882



Point 86
2.393
−1.595
0.885



Point 87
2.512
−1.553
0.888



Point 88
2.631
−1.510
0.891



Point 89
2.749
−1.466
0.894



Point 90
2.866
−1.421
0.898



Point 91
2.984
−1.375
0.901



Point 92
3.101
−1.328
0.905



Point 93
3.218
−1.281
0.908



Point 94
3.334
−1.232
0.912



Point 95
3.450
−1.184
0.915



Point 96
3.567
−1.135
0.919



Point 97
3.682
−1.085
0.922



Point 98
3.798
−1.035
0.926



Point 99
3.914
−0.985
0.930



Point 100
4.029
−0.934
0.934



Point 101
4.144
−0.883
0.937



Point 102
4.259
−0.832
0.941



Point 103
4.374
−0.780
0.945



Point 104
4.489
−0.728
0.949



Point 105
4.604
−0.676
0.953



Point 106
4.719
−0.624
0.957



Point 107
4.833
−0.571
0.960



Point 108
4.948
−0.519
0.964



Point 109
5.062
−0.466
0.968



Point 110
5.177
−0.413
0.972



Point 111
5.291
−0.360
0.976



Point 112
5.405
−0.306
0.980



Point 113
5.519
−0.253
0.984



Point 114
5.634
−0.199
0.988



Point 115
5.748
−0.146
0.992



Point 116
5.862
−0.092
0.996



Point 117
5.976
−0.038
1.000



Point 118
6.090
0.015
1.004



Point 119
6.204
0.069
1.008



Point 120
6.318
0.123
1.012







Section 5












Point 1
6.459
0.245
1.572



Point 2
6.410
0.150
1.565



Point 3
6.459
0.245
1.572



Point 4
6.359
0.283
1.575



Point 5
6.236
0.248
1.573



Point 6
6.113
0.213
1.570



Point 7
5.990
0.180
1.568



Point 8
5.867
0.147
1.565



Point 9
5.743
0.115
1.563



Point 10
5.619
0.084
1.560



Point 11
5.495
0.053
1.558



Point 12
5.371
0.024
1.556



Point 13
5.247
−0.005
1.554



Point 14
5.122
−0.033
1.552



Point 15
4.997
−0.061
1.550



Point 16
4.872
−0.087
1.548



Point 17
4.747
−0.113
1.546



Point 18
4.622
−0.138
1.544



Point 19
4.497
−0.162
1.542



Point 20
4.371
−0.185
1.541



Point 21
4.245
−0.207
1.539



Point 22
4.119
−0.229
1.537



Point 23
3.993
−0.249
1.536



Point 24
3.867
−0.269
1.534



Point 25
3.741
−0.287
1.533



Point 26
3.614
−0.304
1.532



Point 27
3.488
−0.321
1.531



Point 28
3.361
−0.336
1.529



Point 29
3.234
−0.350
1.528



Point 30
3.107
−0.362
1.527



Point 31
2.980
−0.374
1.527



Point 32
2.852
−0.384
1.526



Point 33
2.725
−0.392
1.525



Point 34
2.597
−0.399
1.525



Point 35
2.470
−0.403
1.524



Point 36
2.342
−0.407
1.524



Point 37
2.214
−0.408
1.524



Point 38
2.087
−0.406
1.524



Point 39
1.959
−0.403
1.524



Point 40
1.832
−0.397
1.525



Point 41
1.704
−0.387
1.526



Point 42
1.577
−0.375
1.526



Point 43
1.450
−0.359
1.528



Point 44
1.324
−0.340
1.529



Point 45
1.199
−0.317
1.531



Point 46
1.074
−0.289
1.533



Point 47
0.950
−0.257
1.535



Point 48
0.828
−0.220
1.538



Point 49
0.707
−0.180
1.541



Point 50
0.587
−0.137
1.544



Point 51
0.466
−0.094
1.547



Point 52
0.344
−0.057
1.550



Point 53
0.218
−0.039
1.551



Point 54
0.093
−0.060
1.550



Point 55
−0.020
−0.119
1.545



Point 56
−0.105
−0.213
1.538



Point 57
−0.165
−0.326
1.530



Point 58
−0.207
−0.446
1.521



Point 59
−0.234
−0.570
1.512



Point 60
−0.250
−0.696
1.503



Point 61
−0.255
−0.824
1.493



Point 62
−0.250
−0.951
1.484



Point 63
−0.234
−1.077
1.475



Point 64
−0.208
−1.202
1.465



Point 65
−0.170
−1.323
1.456



Point 66
−0.119
−1.440
1.448



Point 67
−0.055
−1.551
1.440



Point 68
0.023
−1.651
1.432



Point 69
0.114
−1.740
1.426



Point 70
0.218
−1.814
1.420



Point 71
0.332
−1.872
1.416



Point 72
0.452
−1.915
1.413



Point 73
0.576
−1.943
1.411



Point 74
0.703
−1.960
1.409



Point 75
0.830
−1.966
1.409



Point 76
0.958
−1.964
1.409



Point 77
1.085
−1.955
1.410



Point 78
1.212
−1.940
1.411



Point 79
1.338
−1.919
1.412



Point 80
1.463
−1.895
1.414



Point 81
1.588
−1.867
1.416



Point 82
1.712
−1.836
1.418



Point 83
1.835
−1.803
1.421



Point 84
1.958
−1.767
1.424



Point 85
2.080
−1.729
1.426



Point 86
2.201
−1.689
1.429



Point 87
2.322
−1.648
1.432



Point 88
2.442
−1.606
1.436



Point 89
2.562
−1.562
1.439



Point 90
2.682
−1.517
1.442



Point 91
2.801
−1.472
1.445



Point 92
2.920
−1.425
1.449



Point 93
3.038
−1.377
1.452



Point 94
3.156
−1.329
1.456



Point 95
3.274
−1.280
1.460



Point 96
3.392
−1.231
1.463



Point 97
3.510
−1.181
1.467



Point 98
3.627
−1.131
1.471



Point 99
3.744
−1.080
1.474



Point 100
3.861
−1.029
1.478



Point 101
3.978
−0.977
1.482



Point 102
4.094
−0.925
1.486



Point 103
4.211
−0.873
1.490



Point 104
4.327
−0.820
1.494



Point 105
4.443
−0.768
1.497



Point 106
4.559
−0.715
1.501



Point 107
4.676
−0.662
1.505



Point 108
4.792
−0.608
1.509



Point 109
4.907
−0.555
1.513



Point 110
5.023
−0.501
1.517



Point 111
5.139
−0.447
1.521



Point 112
5.255
−0.393
1.525



Point 113
5.370
−0.339
1.529



Point 114
5.486
−0.285
1.533



Point 115
5.602
−0.231
1.537



Point 116
5.717
−0.177
1.541



Point 117
5.833
−0.122
1.545



Point 118
5.948
−0.068
1.549



Point 119
6.063
−0.013
1.553



Point 120
6.179
0.041
1.557







Section 6












Point 1
6.563
0.239
2.123



Point 2
6.512
0.143
2.116



Point 3
6.563
0.239
2.123



Point 4
6.461
0.276
2.126



Point 5
6.337
0.240
2.123



Point 6
6.212
0.205
2.121



Point 7
6.088
0.171
2.118



Point 8
5.962
0.139
2.116



Point 9
5.837
0.106
2.114



Point 10
5.712
0.075
2.111



Point 11
5.586
0.044
2.109



Point 12
5.460
0.014
2.107



Point 13
5.334
−0.015
2.105



Point 14
5.208
−0.043
2.103



Point 15
5.082
−0.071
2.101



Point 16
4.955
−0.098
2.099



Point 17
4.829
−0.124
2.097



Point 18
4.702
−0.149
2.095



Point 19
4.575
−0.174
2.093



Point 20
4.448
−0.198
2.091



Point 21
4.321
−0.221
2.089



Point 22
4.193
−0.243
2.088



Point 23
4.066
−0.264
2.086



Point 24
3.938
−0.284
2.085



Point 25
3.810
−0.304
2.083



Point 26
3.682
−0.322
2.082



Point 27
3.554
−0.340
2.081



Point 28
3.426
−0.356
2.079



Point 29
3.297
−0.371
2.078



Point 30
3.168
−0.385
2.077



Point 31
3.040
−0.398
2.076



Point 32
2.911
−0.409
2.075



Point 33
2.782
−0.419
2.075



Point 34
2.653
−0.427
2.074



Point 35
2.524
−0.433
2.074



Point 36
2.394
−0.437
2.073



Point 37
2.265
−0.440
2.073



Point 38
2.136
−0.440
2.073



Point 39
2.006
−0.438
2.073



Point 40
1.877
−0.433
2.074



Point 41
1.748
−0.425
2.074



Point 42
1.619
−0.414
2.075



Point 43
1.491
−0.399
2.076



Point 44
1.363
−0.380
2.078



Point 45
1.235
−0.358
2.079



Point 46
1.109
−0.330
2.081



Point 47
0.984
−0.298
2.084



Point 48
0.860
−0.262
2.086



Point 49
0.737
−0.220
2.089



Point 50
0.616
−0.176
2.093



Point 51
0.495
−0.131
2.096



Point 52
0.372
−0.091
2.099



Point 53
0.245
−0.069
2.101



Point 54
0.117
−0.086
2.099



Point 55
0.003
−0.145
2.095



Point 56
−0.084
−0.240
2.088



Point 57
−0.145
−0.354
2.080



Point 58
−0.186
−0.476
2.071



Point 59
−0.213
−0.602
2.061



Point 60
−0.227
−0.730
2.052



Point 61
−0.231
−0.859
2.042



Point 62
−0.224
−0.988
2.033



Point 63
−0.208
−1.116
2.023



Point 64
−0.181
−1.242
2.014



Point 65
−0.142
−1.365
2.005



Point 66
−0.091
−1.483
1.996



Point 67
−0.027
−1.595
1.988



Point 68
0.052
−1.698
1.980



Point 69
0.144
−1.788
1.974



Point 70
0.248
−1.864
1.968



Point 71
0.363
−1.924
1.964



Point 72
0.484
−1.968
1.960



Point 73
0.610
−1.997
1.958



Point 74
0.738
−2.014
1.957



Point 75
0.868
−2.020
1.956



Point 76
0.997
−2.017
1.957



Point 77
1.126
−2.007
1.957



Point 78
1.254
−1.991
1.958



Point 79
1.382
−1.970
1.960



Point 80
1.508
−1.945
1.962



Point 81
1.635
−1.916
1.964



Point 82
1.760
−1.883
1.966



Point 83
1.884
−1.849
1.969



Point 84
2.008
−1.812
1.972



Point 85
2.131
−1.773
1.975



Point 86
2.254
−1.732
1.978



Point 87
2.376
−1.689
1.981



Point 88
2.498
−1.646
1.984



Point 89
2.619
−1.601
1.987



Point 90
2.740
−1.555
1.991



Point 91
2.861
−1.508
1.994



Point 92
2.981
−1.460
1.998



Point 93
3.100
−1.411
2.001



Point 94
3.220
−1.362
2.005



Point 95
3.339
−1.312
2.009



Point 96
3.458
−1.261
2.012



Point 97
3.577
−1.210
2.016



Point 98
3.695
−1.158
2.020



Point 99
3.814
−1.106
2.024



Point 100
3.932
−1.054
2.028



Point 101
4.050
−1.002
2.032



Point 102
4.168
−0.949
2.036



Point 103
4.286
−0.895
2.040



Point 104
4.403
−0.842
2.043



Point 105
4.521
−0.788
2.047



Point 106
4.639
−0.734
2.051



Point 107
4.756
−0.680
2.055



Point 108
4.873
−0.626
2.059



Point 109
4.991
−0.571
2.063



Point 110
5.108
−0.517
2.068



Point 111
5.225
−0.462
2.072



Point 112
5.342
−0.407
2.076



Point 113
5.459
−0.353
2.080



Point 114
5.576
−0.298
2.084



Point 115
5.693
−0.243
2.088



Point 116
5.810
−0.188
2.092



Point 117
5.927
−0.132
2.096



Point 118
6.044
−0.077
2.100



Point 119
6.161
−0.022
2.104



Point 120
6.278
0.033
2.108







Section 7












Point 1
6.670
0.209
2.673



Point 2
6.566
0.246
2.675



Point 3
6.440
0.210
2.673



Point 4
6.314
0.175
2.670



Point 5
6.187
0.142
2.668



Point 6
6.061
0.109
2.665



Point 7
5.934
0.077
2.663



Point 8
5.807
0.046
2.661



Point 9
5.679
0.015
2.658



Point 10
5.552
−0.014
2.656



Point 11
5.424
−0.043
2.654



Point 12
5.296
−0.072
2.652



Point 13
5.168
−0.099
2.650



Point 14
5.040
−0.126
2.648



Point 15
4.911
−0.152
2.646



Point 16
4.783
−0.177
2.644



Point 17
4.654
−0.202
2.642



Point 18
4.526
−0.226
2.641



Point 19
4.397
−0.249
2.639



Point 20
4.268
−0.271
2.637



Point 21
4.138
−0.293
2.636



Point 22
4.009
−0.313
2.634



Point 23
3.880
−0.333
2.633



Point 24
3.750
−0.352
2.631



Point 25
3.620
−0.369
2.630



Point 26
3.490
−0.386
2.629



Point 27
3.360
−0.402
2.628



Point 28
3.230
−0.416
2.626



Point 29
3.100
−0.429
2.625



Point 30
2.969
−0.441
2.625



Point 31
2.839
−0.451
2.624



Point 32
2.708
−0.460
2.623



Point 33
2.577
−0.467
2.623



Point 34
2.447
−0.472
2.622



Point 35
2.316
−0.476
2.622



Point 36
2.185
−0.477
2.622



Point 37
2.054
−0.475
2.622



Point 38
1.923
−0.471
2.622



Point 39
1.792
−0.464
2.623



Point 40
1.662
−0.453
2.624



Point 41
1.531
−0.439
2.625



Point 42
1.402
−0.421
2.626



Point 43
1.273
−0.399
2.628



Point 44
1.145
−0.371
2.630



Point 45
1.018
−0.338
2.632



Point 46
0.893
−0.300
2.635



Point 47
0.769
−0.257
2.638



Point 48
0.647
−0.209
2.642



Point 49
0.525
−0.161
2.645



Point 50
0.402
−0.117
2.649



Point 51
0.274
−0.093
2.650



Point 52
0.144
−0.108
2.649



Point 53
0.027
−0.166
2.645



Point 54
−0.062
−0.261
2.638



Point 55
−0.124
−0.376
2.629



Point 56
−0.165
−0.499
2.620



Point 57
−0.191
−0.627
2.611



Point 58
−0.204
−0.757
2.601



Point 59
−0.207
−0.888
2.592



Point 60
−0.199
−1.018
2.582



Point 61
−0.181
−1.148
2.572



Point 62
−0.154
−1.275
2.563



Point 63
−0.115
−1.400
2.554



Point 64
−0.064
−1.520
2.545



Point 65
0.001
−1.634
2.536



Point 66
0.079
−1.739
2.529



Point 67
0.170
−1.832
2.522



Point 68
0.275
−1.910
2.516



Point 69
0.390
−1.973
2.511



Point 70
0.512
−2.019
2.508



Point 71
0.639
−2.050
2.506



Point 72
0.769
−2.068
2.504



Point 73
0.900
−2.075
2.504



Point 74
1.031
−2.073
2.504



Point 75
1.161
−2.063
2.505



Point 76
1.291
−2.047
2.506



Point 77
1.420
−2.026
2.507



Point 78
1.549
−2.000
2.509



Point 79
1.676
−1.970
2.512



Point 80
1.803
−1.938
2.514



Point 81
1.929
−1.902
2.517



Point 82
2.055
−1.864
2.519



Point 83
2.179
−1.825
2.522



Point 84
2.304
−1.783
2.525



Point 85
2.427
−1.740
2.529



Point 86
2.550
−1.695
2.532



Point 87
2.673
−1.650
2.535



Point 88
2.795
−1.603
2.539



Point 89
2.917
−1.555
2.542



Point 90
3.039
−1.507
2.546



Point 91
3.160
−1.457
2.549



Point 92
3.281
−1.407
2.553



Point 93
3.402
−1.356
2.557



Point 94
3.522
−1.305
2.561



Point 95
3.642
−1.253
2.565



Point 96
3.762
−1.201
2.568



Point 97
3.882
−1.148
2.572



Point 98
4.002
−1.095
2.576



Point 99
4.121
−1.042
2.580



Point 100
4.241
−0.988
2.584



Point 101
4.360
−0.934
2.588



Point 102
4.479
−0.880
2.592



Point 103
4.598
−0.826
2.596



Point 104
4.717
−0.771
2.600



Point 105
4.836
−0.716
2.604



Point 106
4.955
−0.662
2.608



Point 107
5.074
−0.607
2.612



Point 108
5.193
−0.552
2.616



Point 109
5.311
−0.496
2.621



Point 110
5.430
−0.441
2.625



Point 111
5.549
−0.386
2.629



Point 112
5.667
−0.330
2.633



Point 113
5.786
−0.275
2.637



Point 114
5.904
−0.219
2.641



Point 115
6.023
−0.164
2.645



Point 116
6.141
−0.108
2.649



Point 117
6.260
−0.053
2.653



Point 118
6.378
0.003
2.657



Point 119
6.497
0.058
2.662



Point 120
6.616
0.114
2.666







Section 8












Point 1
6.770
0.161
3.221



Point 2
6.665
0.197
3.223



Point 3
6.538
0.162
3.221



Point 4
6.410
0.128
3.218



Point 5
6.282
0.094
3.216



Point 6
6.153
0.062
3.213



Point 7
6.025
0.031
3.211



Point 8
5.896
0.000
3.209



Point 9
5.767
−0.030
3.207



Point 10
5.638
−0.059
3.204



Point 11
5.508
−0.087
3.202



Point 12
5.379
−0.115
3.200



Point 13
5.249
−0.142
3.198



Point 14
5.119
−0.168
3.196



Point 15
4.989
−0.193
3.194



Point 16
4.859
−0.218
3.193



Point 17
4.729
−0.242
3.191



Point 18
4.599
−0.266
3.189



Point 19
4.468
−0.288
3.187



Point 20
4.338
−0.310
3.186



Point 21
4.207
−0.331
3.184



Point 22
4.076
−0.351
3.183



Point 23
3.945
−0.370
3.181



Point 24
3.814
−0.389
3.180



Point 25
3.683
−0.406
3.179



Point 26
3.551
−0.423
3.177



Point 27
3.420
−0.438
3.176



Point 28
3.288
−0.452
3.175



Point 29
3.156
−0.465
3.174



Point 30
3.024
−0.477
3.173



Point 31
2.892
−0.488
3.173



Point 32
2.760
−0.496
3.172



Point 33
2.628
−0.504
3.172



Point 34
2.496
−0.509
3.171



Point 35
2.363
−0.513
3.171



Point 36
2.231
−0.514
3.171



Point 37
2.098
−0.513
3.171



Point 38
1.966
−0.509
3.171



Point 39
1.834
−0.502
3.172



Point 40
1.702
−0.492
3.172



Point 41
1.570
−0.479
3.173



Point 42
1.439
−0.461
3.175



Point 43
1.308
−0.438
3.176



Point 44
1.179
−0.410
3.178



Point 45
1.051
−0.377
3.181



Point 46
0.924
−0.337
3.184



Point 47
0.800
−0.292
3.187



Point 48
0.678
−0.241
3.191



Point 49
0.556
−0.188
3.195



Point 50
0.433
−0.141
3.198



Point 51
0.304
−0.114
3.200



Point 52
0.173
−0.128
3.199



Point 53
0.053
−0.184
3.195



Point 54
−0.040
−0.277
3.188



Point 55
−0.103
−0.392
3.180



Point 56
−0.145
−0.518
3.170



Point 57
−0.171
−0.647
3.161



Point 58
−0.184
−0.779
3.151



Point 59
−0.185
−0.911
3.141



Point 60
−0.177
−1.042
3.132



Point 61
−0.159
−1.173
3.122



Point 62
−0.130
−1.302
3.112



Point 63
−0.091
−1.428
3.103



Point 64
−0.040
−1.550
3.094



Point 65
0.024
−1.665
3.086



Point 66
0.102
−1.772
3.078



Point 67
0.193
−1.868
3.071



Point 68
0.297
−1.949
3.065



Point 69
0.412
−2.014
3.060



Point 70
0.535
−2.063
3.056



Point 71
0.663
−2.097
3.054



Point 72
0.794
−2.117
3.052



Point 73
0.926
−2.125
3.052



Point 74
1.059
−2.124
3.052



Point 75
1.191
−2.115
3.052



Point 76
1.322
−2.100
3.053



Point 77
1.453
−2.079
3.055



Point 78
1.583
−2.053
3.057



Point 79
1.712
−2.024
3.059



Point 80
1.840
−1.991
3.062



Point 81
1.968
−1.956
3.064



Point 82
2.095
−1.918
3.067



Point 83
2.221
−1.878
3.070



Point 84
2.347
−1.836
3.073



Point 85
2.472
−1.793
3.076



Point 86
2.597
−1.748
3.079



Point 87
2.721
−1.703
3.083



Point 88
2.845
−1.656
3.086



Point 89
2.968
−1.608
3.090



Point 90
3.091
−1.559
3.093



Point 91
3.214
−1.509
3.097



Point 92
3.336
−1.459
3.101



Point 93
3.458
−1.408
3.105



Point 94
3.580
−1.356
3.108



Point 95
3.702
−1.304
3.112



Point 96
3.823
−1.251
3.116



Point 97
3.945
−1.198
3.120



Point 98
4.066
−1.145
3.124



Point 99
4.187
−1.092
3.128



Point 100
4.308
−1.038
3.132



Point 101
4.429
−0.984
3.136



Point 102
4.549
−0.929
3.140



Point 103
4.670
−0.875
3.144



Point 104
4.790
−0.820
3.148



Point 105
4.911
−0.765
3.152



Point 106
5.031
−0.710
3.156



Point 107
5.152
−0.655
3.160



Point 108
5.272
−0.600
3.164



Point 109
5.392
−0.545
3.168



Point 110
5.513
−0.489
3.173



Point 111
5.633
−0.434
3.177



Point 112
5.753
−0.379
3.181



Point 113
5.873
−0.323
3.185



Point 114
5.993
−0.267
3.189



Point 115
6.113
−0.212
3.193



Point 116
6.233
−0.156
3.197



Point 117
6.354
−0.101
3.201



Point 118
6.474
−0.045
3.205



Point 119
6.594
0.010
3.210



Point 120
6.714
0.066
3.214







Section 9












Point 1
6.858
0.098
3.767



Point 2
6.752
0.134
3.770



Point 3
6.624
0.099
3.768



Point 4
6.494
0.066
3.765



Point 5
6.365
0.034
3.763



Point 6
6.235
0.002
3.760



Point 7
6.105
−0.028
3.758



Point 8
5.975
−0.058
3.756



Point 9
5.844
−0.086
3.754



Point 10
5.714
−0.114
3.752



Point 11
5.583
−0.142
3.750



Point 12
5.452
−0.168
3.748



Point 13
5.321
−0.194
3.746



Point 14
5.190
−0.219
3.744



Point 15
5.059
−0.244
3.742



Point 16
4.927
−0.268
3.740



Point 17
4.796
−0.291
3.739



Point 18
4.664
−0.313
3.737



Point 19
4.532
−0.335
3.735



Point 20
4.401
−0.356
3.734



Point 21
4.269
−0.376
3.732



Point 22
4.136
−0.395
3.731



Point 23
4.004
−0.414
3.730



Point 24
3.872
−0.431
3.728



Point 25
3.739
−0.448
3.727



Point 26
3.607
−0.464
3.726



Point 27
3.474
−0.479
3.725



Point 28
3.341
−0.492
3.724



Point 29
3.208
−0.505
3.723



Point 30
3.075
−0.516
3.722



Point 31
2.942
−0.526
3.721



Point 32
2.809
−0.534
3.721



Point 33
2.675
−0.541
3.720



Point 34
2.542
−0.546
3.720



Point 35
2.408
−0.550
3.720



Point 36
2.275
−0.551
3.719



Point 37
2.141
−0.550
3.720



Point 38
2.008
−0.547
3.720



Point 39
1.874
−0.540
3.720



Point 40
1.741
−0.530
3.721



Point 41
1.608
−0.517
3.722



Point 42
1.476
−0.499
3.723



Point 43
1.344
−0.477
3.725



Point 44
1.214
−0.449
3.727



Point 45
1.085
−0.415
3.730



Point 46
0.957
−0.374
3.733



Point 47
0.832
−0.328
3.736



Point 48
0.710
−0.275
3.740



Point 49
0.589
−0.219
3.744



Point 50
0.466
−0.167
3.748



Point 51
0.336
−0.135
3.750



Point 52
0.204
−0.145
3.750



Point 53
0.083
−0.199
3.746



Point 54
−0.014
−0.290
3.739



Point 55
−0.080
−0.406
3.730



Point 56
−0.124
−0.531
3.721



Point 57
−0.151
−0.662
3.711



Point 58
−0.165
−0.794
3.702



Point 59
−0.167
−0.927
3.692



Point 60
−0.159
−1.060
3.682



Point 61
−0.141
−1.192
3.672



Point 62
−0.112
−1.322
3.662



Point 63
−0.072
−1.449
3.653



Point 64
−0.020
−1.572
3.644



Point 65
0.044
−1.688
3.635



Point 66
0.122
−1.796
3.627



Point 67
0.213
−1.894
3.620



Point 68
0.317
−1.977
3.614



Point 69
0.432
−2.044
3.609



Point 70
0.555
−2.096
3.605



Point 71
0.684
−2.132
3.603



Point 72
0.815
−2.154
3.601



Point 73
0.949
−2.165
3.600



Point 74
1.082
−2.166
3.600



Point 75
1.215
−2.158
3.601



Point 76
1.348
−2.144
3.602



Point 77
1.480
−2.124
3.603



Point 78
1.611
−2.100
3.605



Point 79
1.742
−2.071
3.607



Point 80
1.872
−2.039
3.609



Point 81
2.000
−2.005
3.612



Point 82
2.129
−1.967
3.615



Point 83
2.256
−1.928
3.618



Point 84
2.383
−1.887
3.621



Point 85
2.510
−1.844
3.624



Point 86
2.636
−1.800
3.627



Point 87
2.761
−1.754
3.631



Point 88
2.886
−1.707
3.634



Point 89
3.011
−1.660
3.638



Point 90
3.135
−1.611
3.641



Point 91
3.259
−1.562
3.645



Point 92
3.383
−1.512
3.648



Point 93
3.506
−1.461
3.652



Point 94
3.630
−1.410
3.656



Point 95
3.753
−1.358
3.660



Point 96
3.876
−1.306
3.664



Point 97
3.998
−1.253
3.668



Point 98
4.121
−1.200
3.671



Point 99
4.243
−1.147
3.675



Point 100
4.366
−1.093
3.679



Point 101
4.488
−1.040
3.683



Point 102
4.610
−0.986
3.687



Point 103
4.732
−0.931
3.691



Point 104
4.854
−0.877
3.695



Point 105
4.976
−0.823
3.699



Point 106
5.097
−0.768
3.703



Point 107
5.219
−0.713
3.707



Point 108
5.341
−0.658
3.712



Point 109
5.463
−0.604
3.716



Point 110
5.584
−0.549
3.720



Point 111
5.706
−0.494
3.724



Point 112
5.827
−0.438
3.728



Point 113
5.949
−0.383
3.732



Point 114
6.071
−0.328
3.736



Point 115
6.192
−0.273
3.740



Point 116
6.314
−0.218
3.744



Point 117
6.435
−0.163
3.748



Point 118
6.557
−0.108
3.752



Point 119
6.678
−0.053
3.756



Point 120
6.800
0.002
3.760







Section 10












Point 1
6.936
0.022
4.313



Point 2
6.830
0.060
4.316



Point 3
6.700
0.026
4.314



Point 4
6.569
−0.006
4.311



Point 5
6.438
−0.037
4.309



Point 6
6.308
−0.067
4.307



Point 7
6.176
−0.097
4.305



Point 8
6.045
−0.125
4.303



Point 9
5.913
−0.152
4.300



Point 10
5.782
−0.179
4.299



Point 11
5.650
−0.205
4.297



Point 12
5.518
−0.230
4.295



Point 13
5.386
−0.254
4.293



Point 14
5.254
−0.278
4.291



Point 15
5.121
−0.301
4.289



Point 16
4.989
−0.324
4.288



Point 17
4.856
−0.346
4.286



Point 18
4.723
−0.367
4.285



Point 19
4.591
−0.387
4.283



Point 20
4.458
−0.407
4.282



Point 21
4.325
−0.426
4.280



Point 22
4.191
−0.444
4.279



Point 23
4.058
−0.461
4.278



Point 24
3.925
−0.478
4.276



Point 25
3.791
−0.493
4.275



Point 26
3.658
−0.508
4.274



Point 27
3.524
−0.522
4.273



Point 28
3.390
−0.534
4.272



Point 29
3.256
−0.546
4.271



Point 30
3.122
−0.556
4.271



Point 31
2.988
−0.565
4.270



Point 32
2.854
−0.573
4.269



Point 33
2.720
−0.579
4.269



Point 34
2.586
−0.584
4.269



Point 35
2.451
−0.587
4.268



Point 36
2.317
−0.588
4.268



Point 37
2.183
−0.586
4.268



Point 38
2.048
−0.582
4.269



Point 39
1.914
−0.575
4.269



Point 40
1.780
−0.565
4.270



Point 41
1.646
−0.552
4.271



Point 42
1.513
−0.534
4.272



Point 43
1.381
−0.512
4.274



Point 44
1.249
−0.484
4.276



Point 45
1.119
−0.451
4.278



Point 46
0.991
−0.410
4.281



Point 47
0.865
−0.363
4.285



Point 48
0.742
−0.309
4.289



Point 49
0.621
−0.251
4.293



Point 50
0.499
−0.195
4.297



Point 51
0.370
−0.158
4.300



Point 52
0.237
−0.164
4.300



Point 53
0.114
−0.216
4.296



Point 54
0.015
−0.306
4.289



Point 55
−0.055
−0.420
4.281



Point 56
−0.102
−0.545
4.271



Point 57
−0.131
−0.676
4.262



Point 58
−0.147
−0.809
4.252



Point 59
−0.151
−0.943
4.242



Point 60
−0.144
−1.077
4.232



Point 61
−0.126
−1.210
4.222



Point 62
−0.097
−1.340
4.213



Point 63
−0.057
−1.468
4.203



Point 64
−0.004
−1.591
4.194



Point 65
0.061
−1.709
4.185



Point 66
0.140
−1.817
4.177



Point 67
0.231
−1.915
4.170



Point 68
0.336
−1.999
4.164



Point 69
0.451
−2.068
4.159



Point 70
0.574
−2.122
4.155



Point 71
0.703
−2.160
4.152



Point 72
0.835
−2.184
4.150



Point 73
0.969
−2.197
4.149



Point 74
1.103
−2.200
4.149



Point 75
1.237
−2.195
4.149



Point 76
1.371
−2.183
4.150



Point 77
1.504
−2.164
4.152



Point 78
1.636
−2.141
4.153



Point 79
1.768
−2.114
4.155



Point 80
1.899
−2.083
4.158



Point 81
2.029
−2.050
4.160



Point 82
2.158
−2.013
4.163



Point 83
2.287
−1.975
4.166



Point 84
2.415
−1.935
4.169



Point 85
2.543
−1.893
4.172



Point 86
2.670
−1.849
4.175



Point 87
2.797
−1.804
4.178



Point 88
2.923
−1.758
4.182



Point 89
3.049
−1.711
4.185



Point 90
3.174
−1.664
4.189



Point 91
3.299
−1.615
4.192



Point 92
3.424
−1.566
4.196



Point 93
3.549
−1.516
4.200



Point 94
3.673
−1.465
4.203



Point 95
3.798
−1.414
4.207



Point 96
3.922
−1.362
4.211



Point 97
4.046
−1.310
4.215



Point 98
4.169
−1.258
4.219



Point 99
4.293
−1.206
4.223



Point 100
4.417
−1.153
4.226



Point 101
4.540
−1.100
4.230



Point 102
4.663
−1.047
4.234



Point 103
4.787
−0.993
4.238



Point 104
4.910
−0.940
4.242



Point 105
5.033
−0.886
4.246



Point 106
5.156
−0.832
4.250



Point 107
5.279
−0.778
4.254



Point 108
5.402
−0.724
4.258



Point 109
5.525
−0.670
4.262



Point 110
5.648
−0.616
4.266



Point 111
5.771
−0.562
4.270



Point 112
5.894
−0.507
4.274



Point 113
6.016
−0.453
4.278



Point 114
6.139
−0.399
4.282



Point 115
6.262
−0.344
4.286



Point 116
6.385
−0.290
4.290



Point 117
6.508
−0.236
4.294



Point 118
6.631
−0.182
4.298



Point 119
6.754
−0.127
4.302



Point 120
6.877
−0.073
4.306







Section 11












Point 1
7.010
−0.062
4.859



Point 2
6.904
−0.023
4.862



Point 3
6.773
−0.055
4.859



Point 4
6.641
−0.086
4.857



Point 5
6.510
−0.116
4.855



Point 6
6.377
−0.145
4.853



Point 7
6.245
−0.172
4.851



Point 8
6.113
−0.199
4.849



Point 9
5.980
−0.224
4.847



Point 10
5.847
−0.250
4.845



Point 11
5.714
−0.274
4.843



Point 12
5.581
−0.297
4.841



Point 13
5.448
−0.320
4.840



Point 14
5.315
−0.343
4.838



Point 15
5.182
−0.364
4.836



Point 16
5.048
−0.385
4.835



Point 17
4.914
−0.405
4.833



Point 18
4.781
−0.425
4.832



Point 19
4.647
−0.443
4.830



Point 20
4.513
−0.461
4.829



Point 21
4.379
−0.479
4.828



Point 22
4.245
−0.495
4.827



Point 23
4.111
−0.511
4.825



Point 24
3.976
−0.526
4.824



Point 25
3.842
−0.540
4.823



Point 26
3.708
−0.554
4.822



Point 27
3.573
−0.566
4.821



Point 28
3.438
−0.577
4.821



Point 29
3.304
−0.588
4.820



Point 30
3.169
−0.597
4.819



Point 31
3.034
−0.605
4.819



Point 32
2.899
−0.611
4.818



Point 33
2.764
−0.616
4.818



Point 34
2.629
−0.620
4.817



Point 35
2.494
−0.622
4.817



Point 36
2.359
−0.622
4.817



Point 37
2.224
−0.620
4.817



Point 38
2.089
−0.615
4.818



Point 39
1.954
−0.608
4.818



Point 40
1.819
−0.597
4.819



Point 41
1.685
−0.583
4.820



Point 42
1.551
−0.566
4.821



Point 43
1.417
−0.543
4.823



Point 44
1.285
−0.516
4.825



Point 45
1.154
−0.483
4.828



Point 46
1.025
−0.443
4.831



Point 47
0.899
−0.396
4.834



Point 48
0.775
−0.341
4.838



Point 49
0.653
−0.282
4.842



Point 50
0.531
−0.224
4.847



Point 51
0.403
−0.183
4.850



Point 52
0.269
−0.186
4.849



Point 53
0.145
−0.238
4.846



Point 54
0.045
−0.327
4.839



Point 55
−0.027
−0.441
4.831



Point 56
−0.077
−0.566
4.821



Point 57
−0.110
−0.697
4.812



Point 58
−0.129
−0.830
4.802



Point 59
−0.136
−0.965
4.792



Point 60
−0.131
−1.100
4.782



Point 61
−0.114
−1.233
4.772



Point 62
−0.085
−1.365
4.762



Point 63
−0.045
−1.493
4.753



Point 64
0.008
−1.617
4.744



Point 65
0.075
−1.735
4.735



Point 66
0.154
−1.843
4.727



Point 67
0.247
−1.941
4.720



Point 68
0.353
−2.025
4.713



Point 69
0.468
−2.095
4.708



Point 70
0.592
−2.150
4.704



Point 71
0.721
−2.189
4.701



Point 72
0.853
−2.216
4.699



Point 73
0.987
−2.230
4.698



Point 74
1.122
−2.235
4.698



Point 75
1.257
−2.232
4.698



Point 76
1.392
−2.221
4.699



Point 77
1.526
−2.204
4.700



Point 78
1.660
−2.183
4.702



Point 79
1.792
−2.157
4.704



Point 80
1.924
−2.128
4.706



Point 81
2.055
−2.095
4.708



Point 82
2.186
−2.060
4.711



Point 83
2.316
−2.023
4.714



Point 84
2.445
−1.984
4.717



Point 85
2.574
−1.943
4.720



Point 86
2.702
−1.900
4.723



Point 87
2.830
−1.856
4.726



Point 88
2.957
−1.811
4.729



Point 89
3.084
−1.765
4.733



Point 90
3.211
−1.719
4.736



Point 91
3.337
−1.671
4.740



Point 92
3.463
−1.622
4.743



Point 93
3.589
−1.573
4.747



Point 94
3.715
−1.524
4.751



Point 95
3.840
−1.473
4.754



Point 96
3.965
−1.423
4.758



Point 97
4.090
−1.372
4.762



Point 98
4.215
−1.321
4.766



Point 99
4.340
−1.269
4.769



Point 100
4.465
−1.217
4.773



Point 101
4.589
−1.165
4.777



Point 102
4.714
−1.113
4.781



Point 103
4.838
−1.060
4.785



Point 104
4.963
−1.008
4.789



Point 105
5.087
−0.955
4.793



Point 106
5.211
−0.902
4.797



Point 107
5.336
−0.849
4.800



Point 108
5.460
−0.796
4.804



Point 109
5.584
−0.743
4.808



Point 110
5.708
−0.690
4.812



Point 111
5.832
−0.637
4.816



Point 112
5.957
−0.584
4.820



Point 113
6.081
−0.530
4.824



Point 114
6.205
−0.477
4.828



Point 115
6.329
−0.424
4.832



Point 116
6.453
−0.370
4.836



Point 117
6.577
−0.317
4.840



Point 118
6.701
−0.264
4.844



Point 119
6.825
−0.211
4.848



Point 120
6.950
−0.157
4.852







Section 12












Point 1
7.086
−0.151
5.404



Point 2
6.980
−0.111
5.407



Point 3
6.848
−0.142
5.404



Point 4
6.715
−0.172
5.402



Point 5
6.582
−0.200
5.400



Point 6
6.449
−0.227
5.398



Point 7
6.316
−0.253
5.396



Point 8
6.182
−0.278
5.394



Point 9
6.048
−0.302
5.392



Point 10
5.914
−0.325
5.391



Point 11
5.780
−0.347
5.389



Point 12
5.646
−0.369
5.387



Point 13
5.512
−0.390
5.386



Point 14
5.377
−0.411
5.384



Point 15
5.243
−0.430
5.383



Point 16
5.108
−0.449
5.382



Point 17
4.974
−0.468
5.380



Point 18
4.839
−0.485
5.379



Point 19
4.704
−0.502
5.378



Point 20
4.569
−0.518
5.376



Point 21
4.434
−0.534
5.375



Point 22
4.299
−0.549
5.374



Point 23
4.164
−0.563
5.373



Point 24
4.028
−0.576
5.372



Point 25
3.893
−0.588
5.371



Point 26
3.758
−0.600
5.370



Point 27
3.622
−0.610
5.370



Point 28
3.487
−0.620
5.369



Point 29
3.351
−0.629
5.368



Point 30
3.215
−0.636
5.368



Point 31
3.079
−0.643
5.367



Point 32
2.944
−0.648
5.367



Point 33
2.808
−0.651
5.367



Point 34
2.672
−0.653
5.366



Point 35
2.536
−0.654
5.366



Point 36
2.400
−0.653
5.366



Point 37
2.264
−0.649
5.367



Point 38
2.128
−0.643
5.367



Point 39
1.993
−0.635
5.368



Point 40
1.857
−0.624
5.369



Point 41
1.722
−0.609
5.370



Point 42
1.587
−0.591
5.371



Point 43
1.453
−0.568
5.373



Point 44
1.320
−0.541
5.375



Point 45
1.189
−0.507
5.377



Point 46
1.059
−0.468
5.380



Point 47
0.931
−0.421
5.384



Point 48
0.806
−0.368
5.388



Point 49
0.684
−0.309
5.392



Point 50
0.560
−0.251
5.396



Point 51
0.431
−0.211
5.399



Point 52
0.296
−0.216
5.399



Point 53
0.172
−0.270
5.395



Point 54
0.073
−0.362
5.388



Point 55
0.001
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Point 56
−0.052
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Point 57
−0.088
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Point 58
−0.110
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Point 59
−0.120
−1.001
5.341



Point 60
−0.117
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5.331



Point 61
−0.102
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5.321



Point 62
−0.074
−1.404
5.311



Point 63
−0.034
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5.301



Point 64
0.019
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5.292



Point 65
0.086
−1.775
5.283



Point 66
0.167
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5.275



Point 67
0.261
−1.982
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Point 68
0.368
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5.262



Point 69
0.485
−2.135
5.257



Point 70
0.609
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5.253



Point 71
0.739
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5.250



Point 72
0.872
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5.248



Point 73
1.007
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Point 74
1.142
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5.246



Point 75
1.278
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5.246



Point 76
1.414
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5.247



Point 77
1.549
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5.248



Point 78
1.683
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5.250



Point 79
1.817
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5.252



Point 80
1.950
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5.254



Point 81
2.082
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5.256



Point 82
2.214
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5.259



Point 83
2.345
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5.261



Point 84
2.475
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5.264



Point 85
2.605
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Point 86
2.734
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5.270



Point 87
2.863
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5.273



Point 88
2.992
−1.869
5.277



Point 89
3.120
−1.824
5.280



Point 90
3.248
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5.283



Point 91
3.376
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5.287



Point 92
3.503
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5.290



Point 93
3.630
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5.294



Point 94
3.757
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5.297



Point 95
3.883
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5.301



Point 96
4.010
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5.305



Point 97
4.136
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5.308



Point 98
4.262
−1.388
5.312



Point 99
4.389
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5.316



Point 100
4.515
−1.287
5.320



Point 101
4.640
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5.323



Point 102
4.766
−1.184
5.327



Point 103
4.892
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5.331



Point 104
5.018
−1.081
5.335



Point 105
5.143
−1.029
5.339



Point 106
5.269
−0.978
5.342



Point 107
5.395
−0.926
5.346



Point 108
5.520
−0.874
5.350



Point 109
5.646
−0.822
5.354



Point 110
5.771
−0.770
5.358



Point 111
5.896
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5.362



Point 112
6.022
−0.665
5.366



Point 113
6.147
−0.613
5.369



Point 114
6.273
−0.561
5.373



Point 115
6.398
−0.508
5.377



Point 116
6.524
−0.456
5.381



Point 117
6.649
−0.404
5.385



Point 118
6.774
−0.352
5.389



Point 119
6.900
−0.299
5.393



Point 120
7.025
−0.247
5.396











FIG. 6 illustrates an airfoil shape including a leaned airfoil section 1360 according to an exemplary embodiment. As the nozzles come into direct contact with the high-temperature and high-pressure combustion gas, a secondary flow occurs. That is, secondary flows are flow effects that occur after the high-temperature and high-pressure combustion gas path flow contacts the nozzles. The effects are not good as they negatively affect aerodynamic performance, causing turbulence in the flow path. Further, the turbulences may increase the heat transfer coefficients on the gas path surface which also increases heat transfer/metal temperature rise by increasing the heat transfer coefficient of the gas path surface. In order to reduce losses caused by the secondary flows, a newly designed airfoil shape is needed. According to the newly designed airfoil shape of the exemplary embodiment which includes a leaned airfoil section 1360 as illustrated in FIG. 6, it is possible to reduce the secondary flow effects aerodynamically by changing the shape/contour of the airfoil.


While one or more exemplary embodiments have been described with reference to the accompanying drawings, it is to be understood by those skilled in the art that various modifications and changes in form and details can be made therein without departing from the spirit and scope as defined by the appended claims. Therefore, the description of the exemplary embodiments should be construed in a descriptive sense only and not to limit the scope of the claims, and many alternatives, modifications, and variations will be apparent to those skilled in the art.

Claims
  • 1. A turbine nozzle comprising: an airfoil portion having an uncoated nominal profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1,wherein the X, Y, and Z coordinates are distances in inches measured in a Cartesian coordinate system,wherein, at each Z distance, the corresponding X and Y coordinates, when connected by a smooth continuous arc, define one of a plurality of airfoil profile sections, andwherein the plurality of airfoil profile sections, when joined together by smooth continuous arcs, define an airfoil shape.
  • 2. The turbine nozzle according to claim 1, wherein the airfoil shape lies within an envelope of +/−0.120 inches measured in a direction normal to any of the plurality of airfoil profile sections.
  • 3. The turbine nozzle according to claim 1, wherein the X and Y coordinate values are scalable as a function of a same constant or number and a set of corresponding nominal Z coordinate values are scalable as a function of the same constant or number to provide at least one of a scaled up or a scaled down airfoil.
  • 4. The turbine nozzle according to claim 3, wherein the airfoil shape includes a leaned airfoil section to reduce a secondary flow effect.
  • 5. The turbine nozzle according to claim 1, further comprising a coating applied to the airfoil shape, the coating having a thickness of less than or equal to 0.010 inches.
  • 6. A turbine comprising: a turbine nozzle extending from a platform to an end wall and having an airfoil-shaped cross section having a leading edge, a trailing edge, and a pressure side and a suction side each of which extends from the leading edge to the trailing edge,wherein the turbine nozzle comprises an airfoil portion having an uncoated nominal profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1,wherein the X, Y, and Z coordinates are distances in inches measured in a Cartesian coordinate system,wherein, at each Z distance, the corresponding X and Y coordinates, when connected by a smooth continuous arc, define one of a plurality of airfoil profile sections, andwherein the plurality of airfoil profile sections, when joined together by smooth continuous arcs, define an airfoil shape.
  • 7. The turbine according to claim 6, wherein the airfoil shape lies within an envelope of +/−0.120 inches measured in a direction normal to any of the plurality of airfoil profile sections.
  • 8. The turbine according to claim 6, wherein the X and Y coordinate values are scalable as a function of a same constant or number and a set of corresponding nominal Z coordinate values are scalable as a function of the same constant or number to provide at least one of a scaled up or a scaled down airfoil.
  • 9. The turbine according to claim 8, wherein the airfoil shape includes a leaned airfoil section to reduce a secondary flow effect.
  • 10. The turbine according to claim 6, further comprising a coating applied to the airfoil shape, the coating having a thickness of less than or equal to 0.010 inches.
  • 11. A gas turbine comprising: a compressor configured to compress air;a combustor configured to mix compressed air supplied from the compressor with fuel for combustion to generate combustion gas; anda turbine comprising a plurality of turbine nozzles and a plurality of turbine blades rotated by the combustion gas to generate power,wherein each of the turbine nozzles extending from a platform to an end wall and having an airfoil-shaped cross section having a leading edge, a trailing edge, and a pressure side and a suction side each of which extends from the leading edge to the trailing edge,wherein the turbine nozzle comprises an airfoil portion having an uncoated nominal profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1,wherein the X, Y, and Z coordinates are distances in inches measured in a Cartesian coordinate system,wherein, at each Z distance, the corresponding X and Y coordinates, when connected by a smooth continuous arc, define one of a plurality of airfoil profile sections, andwherein the plurality of airfoil profile sections, when joined together by smooth continuous arcs, define an airfoil shape.
  • 12. The gas turbine according to claim 11, wherein the airfoil shape lies within an envelope of +/−0.120 inches measured in a direction normal to any of the plurality of airfoil profile sections.
  • 13. The turbine according to claim 11, wherein the X and Y coordinate values are scalable as a function of a same constant or number and a set of corresponding nominal Z coordinate values are scalable as a function of the same constant or number to provide at least one of a scaled up or a scaled down airfoil.
  • 14. The gas turbine according to claim 13, wherein the airfoil shape includes a leaned airfoil section to reduce a secondary flow effect.
  • 15. The gas turbine according to claim 11, further comprising a coating applied to the airfoil shape, the coating having a thickness of less than or equal to 0.010 inches.
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