- GTRE
A turbocharger is indigenously designed, qualified and delivered for 1500 hp engine of Main Battle Tank (MBT) and 600 hp engine of Infantry Combat Vehicle (ICV) under development at CVRDE. The product is expected to provide performance both at sea-level and high-altitude battle fields.
Turbocharger for 1500 hp engines of Main Battle Tank (MBT) and 600 hp engines of Infantry Combat Vehicle (ICV)
Kaveri Derivative Gas Turbine Engine is the indigenous power plant for Indian Unmanned Aerial vehicle. It is a non-afterburning turbofan engine. The engine is based on the Kaveri Engine architecture with specific design improvements for the UAV applications viz High Inlet Distortion Tolerant Fan, Engine Fuel Control System, Autonomous FADEC and Jetpipe.
Aero Engine for Indian Unmanned Aerial vehicle
STFE is a Twin spool, Low By-Pass Turbo Fan, Aero Gas Turbine Engine. It is a turbofan engine intended for use in unmanned air vehicle. The engine is controlled by Digital Engine Control Unit (DECU).
Turbofan engine intended for use in unmanned air vehicle.
Full Authority Digital Engine Controller to control the Kaveri Derivative Aero Engine. FADEC modulates the engine thrust and ensures surge free operation of the engine. It is built around dual redundant architecture with two identical controllers, each with its independent set of sensors to meet mission reliability.
Full Authority Digital Engine Controller for Kaveri Derivative Aero Engine
HISPEL is a high speed gearbox designed to transmit 25Kw power and to step up the output from commercially available electric motor to 1,10,000 rpm. Speed from the input motor is stepped up in three stages and is designed with combined straight and epicyclic gear trains. This gearbox is intended to provide the drive to test the performance of units/ accessories fitted to small turbofan class of engines. Few of the critical technologies in this project include control of high speed gear dynamics, power loss reduction, effective scavenging, coupling and sealing at high speed.
Gearbox is to provide the drive for testing the units/ accessories of small turbofan class engines.
Indigenous Engine Fuel Control System Comprising of Double Pump Fuel Metering Unit for supplying Metered Fuel flow at the required pressure to the Main Combustor and Variable Geometry Actuation System.
Kaveri Derivative Engine for Indian Unmanned Aerial Vehicle
Fan with variable guide vane system designed to improve operability at part speeds and surge margin. 3D stacked aerofoils minimize loss and control secondary flow interaction. Wide chord blades are chosen for flutter avoidance and better distortion tolerance. Indigenous raw material sourcing and manufacturing of all the components.
Fan for Aero Engine of manned and unmanned aerial vehicle