High Thrust EDF
por KevinJohnson123
Archivos imprimibles (26)
-
stlAxial_Compressor_-_m3x6_screw-1.STL
26 Ko · 5 067 descargas
-
stlAxial_Compressor_-_m3x15_screw-4.STL
21 Ko · 5 063 descargas
-
stlAxial_Compressor_-_m3x15_screw-3.STL
21 Ko · 5 059 descargas
-
stlAxial_Compressor_-_m3x15_screw-8.STL
21 Ko · 5 057 descargas
-
stlAxial_Compressor_-_m3x6_screw-5.STL
26 Ko · 5 060 descargas
-
stlAxial_Compressor_-_m3x15_screw-2.STL
21 Ko · 5 048 descargas
-
stlAxial_Compressor_-_m3x15_screw-7.STL
21 Ko · 5 040 descargas
-
stlAxial_Compressor_-_m3x15_screw-12.STL
21 Ko · 5 040 descargas
-
stlAxial_Compressor_-_m3x15_screw-10.STL
21 Ko · 5 040 descargas
-
stlAxial_Compressor_-_m3x15_screw-5.STL
21 Ko · 5 052 descargas
-
stlAxial_Compressor_-_m3x15_screw-6.STL
21 Ko · 5 042 descargas
-
stlAxial_Compressor_-_m3x15_screw-14.STL
21 Ko · 5 040 descargas
-
stlAxial_Compressor_-_m3x6_screw-4.STL
26 Ko · 5 046 descargas
-
stlAxial_Compressor_-_m3x15_screw-9.STL
21 Ko · 5 039 descargas
-
stlAxial_Compressor_-_m3x15_screw-15.STL
21 Ko · 5 034 descargas
-
stlAxial_Compressor_-_m3x15_screw-13.STL
21 Ko · 5 036 descargas
-
stlAxial_Compressor_-_O-ring_plate-2.STL
85 Ko · 5 045 descargas
-
stlAxial_Compressor_-_Motor_Mount_Trailing_Air_Spike-1.STL
139 Ko · 5 055 descargas
-
stlAxial_Compressor_-_turbine_duct_cover-1.STL
71 Ko · 5 053 descargas
-
stlAxial_Compressor_-_Turbine_Shaft-1.STL
7 Ko · 5 042 descargas
-
stlAxial_Compressor_-_O-ring_plate-1.STL
85 Ko · 5 037 descargas
-
stlAxial_Compressor_-_m3x15_screw-11.STL
21 Ko · 5 035 descargas
-
stlAxial_Compressor_-_compressor_case-1.STL
253 Ko · 5 084 descargas
-
stlAxial_Compressor_-_Leading_Air_Spike_-_rounded-1.STL
257 Ko · 5 048 descargas
-
stlAxial_Compressor_-_Cowling-1.STL
364 Ko · 5 067 descargas
-
stlAxial_Compressor_-_stator-1.STL
438 Ko · 5 183 descargas
Descripción
3d Printable 80mm EDF. It should produce around 1-2 Kg of thrust @ 35,000-40,000 RPMs
It's part of a numerical experiment in computer Virtualization and the SolidWorks API. The goal is to use numerical solutions to find the optimal single-stage turbine configuration which is both Energy Efficient and High Thrust producing.