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Cinema

fan blades airfoil

0.4093 −0.3942 26 41 −0.4492 0.3484 0.0002 −0.1026 −0.1204 −0.1764 −0.1094 0.0682 −0.2994 −0.3640 0.0374 −0.1298 8 41 32 0.0998 0.0071 40 42 0.0011 3 0.0045 23 −0.3573 21 33 21 0.4011 −0.1196 Referring to FIG. −0.2536 0.2753 −0.1396 −0.3199 0.3462 −0.1425 The axial and circumferential coordinates can be converted to metric (mm) by multiplying by 25.4. 0.0135 −0.4965 0.1388 6 −0.0985 19 0.0750 0.0540 22 −0.2051 0.0386 52 −0.3449 −0.3801 −0.1556 18 0.1833 0.0557 5 0.0000 −0.2594 13 −0.3650 0.0006 18 −0.0007 56 −0.0001 15 −0.3987 28 −0.2754 a combustor fluidly connected to the compressor section; a turbine section fluidly connected to the combustor, the turbine section comprising: a high pressure turbine coupled to the high pressure compressor via a shaft; a fan section operatively coupled to the turbine section, wherein the fan section includes an array of fan blades, wherein at least one fan blade includes an airfoil having leading and trailing edges joined by pressure and suction sides to provide an exterior airfoil surface extending from in a radial direction to a tip; and, Gas turbine engine fan blade airfoil profile, Application filed by United Technologies Corp, Assigned to UNITED TECHNOLOGIES CORPORATION. 0.0026 −0.4594 −0.2886 0.2202 10 45 0.0032 52 −0.2053 0.0002 24 0.0096 0.0002 1 39 34 43 50 42 −0.1995 46 0.0018 0.4917 53 0.1391 0.0045 42 0.2741 4 0.0020 37 −0.2428 0.0949 24 0.0059 −0.1900 0.1815 43 19 All things equal, more span and less chord is more efficient. −0.0796 0.4359 19 42 −0.0002 0.0198 2. The disclosure can be further understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein: FIG. 0.1248 −0.4706 −0.0895 −0.3451 In addition, the airfoil 64 is sometimes rotated with respect to a radial axis or a normal to the platform or shroud surface, for example by up to ±10° or more. −0.1368 −0.3420 −0.0526 −0.3893 0.0412 0.0048 −0.3322 10 0.0691 44 0.3032 −0.3793 0.0036 0.0036 0.0025 0.1072 19 15 44 1 −0.3690 −0.2723 38 The contour of the airfoil 78 is set forth in Table 1, which provides the axial (X), circumferential (Y) coordinates (in inches) and span coordinates. 0.0002 0.3898 −0.2633 −0.4090 −0.2369 29 −0.0379 −0.3075 14 0.0649 −0.1760 0.0662 BOSON’s airfoil fan blades include special construction features, such as solid nose piece utilization, to provide superior resistance to abrasion and wear. 55 53 0.0533 0.0016 35 −0.4994 0.2755 0.2383 During operation, air is pressurized in the compressor section and is mixed with fuel and burned in the combustor section to generate hot combustion gases. 0.0963 40 −0.1486 0.0140 56 −0.4741 0.2144 −0.0529 38 −0.2252 −0.4151 0.0008 0.0290 28

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