D. Chatterjee, A.S. Chauhan, Venkat ., D.P. Tigga, D.K Das
{"title":"小型涡轮风扇发动机高压涡轮叶片熔模铸造工艺的实现","authors":"D. Chatterjee, A.S. Chauhan, Venkat ., D.P. Tigga, D.K Das","doi":"10.14429/dsj.73.18719","DOIUrl":null,"url":null,"abstract":"Turbo-fan gas turbine engines, or simply turbo-fan engines (STFEs), are used for powering both manned aircrafts and unmanned air vehicles (UAVs). The high pressure turbine section of such engines use Ni-base superalloy cast rotor blades because of their good mechanical properties at high operating temperatures. The present paper provides the technical/technological details of the various aspects associated with development and manufacturing of high pressure turbine blades (HPTBs) for utilization in an indigenously-developed small turbo-fan engine. Vacuum investment casting process has been adopted for realization of the above equiaxed components using a Ni-base superalloy
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Realization of High Pressure Turbine Blades of a Small Turbo Fan Engine through Investment Casting Process
Turbo-fan gas turbine engines, or simply turbo-fan engines (STFEs), are used for powering both manned aircrafts and unmanned air vehicles (UAVs). The high pressure turbine section of such engines use Ni-base superalloy cast rotor blades because of their good mechanical properties at high operating temperatures. The present paper provides the technical/technological details of the various aspects associated with development and manufacturing of high pressure turbine blades (HPTBs) for utilization in an indigenously-developed small turbo-fan engine. Vacuum investment casting process has been adopted for realization of the above equiaxed components using a Ni-base superalloy
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