A micro gas turbine impeller is a highly challenging component to fabricate given the stringent tolerance requirements. This paper highlights and reports a novel process to machine and fabricate a SS 304 impeller using a 3 axis cnc milling machine with minimum usage of job overhead. The impeller chosen to demonstrate this process is a 12 vaned impeller with outside diameter of 110 mm with an elliptical hub surface and constant radius circular shroud surface. The blade thickness varies from 1.6 mm at tip and 3.5 mm at hub. The intersection region of the blade with the disk has a uniform fillet radius of 1.5 mm. The blade exit height is 16 mm. Blades are not perpendicular to the hub surface, intersecting angle is changing as you move down the blades. The height of the blade varies from exducer to inducer is 4.5 times. It is seen that a considerable saving in time and effort without a compromise on the dimensional tolerances is obtained with the above procedure.
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ASME 2013 Gas Turbine India Conference
December 5–6, 2013
Bangalore, Karnataka, India
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5616-1
PROCEEDINGS PAPER
Manufacturing of a Radial Inflow Turbine for Microgas Turbine in a 3 Axis CNC Milling Machine
M. N. Varadarajan,
M. N. Varadarajan
CSIR - National Aerospace Laboratories, Bangalore, KA, India
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M. E. Mohana Sundaram,
M. E. Mohana Sundaram
CSIR - National Aerospace Laboratories, Bangalore, KA, India
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K. Sampath
K. Sampath
CSIR - National Aerospace Laboratories, Bangalore, KA, India
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M. N. Varadarajan
CSIR - National Aerospace Laboratories, Bangalore, KA, India
M. E. Mohana Sundaram
CSIR - National Aerospace Laboratories, Bangalore, KA, India
K. Sampath
CSIR - National Aerospace Laboratories, Bangalore, KA, India
Paper No:
GTINDIA2013-3541, V001T08A002; 6 pages
Published Online:
February 28, 2014
Citation
Varadarajan, MN, Sundaram, MEM, & Sampath, K. "Manufacturing of a Radial Inflow Turbine for Microgas Turbine in a 3 Axis CNC Milling Machine." Proceedings of the ASME 2013 Gas Turbine India Conference. ASME 2013 Gas Turbine India Conference. Bangalore, Karnataka, India. December 5–6, 2013. V001T08A002. ASME. https://doi.org/10.1115/GTINDIA2013-3541
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