Test Rig Dealers in Ramnagar, Roorkee (2 products available)

Clients can stay assured for the products that we offer, as they will remain damage free. For this, we make use of premium packaging material for wrapping them. Buyers can stay rest assured about the quality of our products as we check each and every product at diverse stages.   Range: Pelton Wheel Turbine Test Rig (Capacity : 1 Kw) lKaplan Turbine Test Rig (Capacity : 1 Kw) Steam Turbine Test Rig Centrifugal Pump Test Rig (Three Speed Cone Pulley) Gear Pump Test Rig Submersible Pump Test Rig Hydraulic Ram (Closed Circuit) Hydraulic Tilting Flume / Open Channel - 4 Meter Hydraulic Tilting Flume / Open Channel - 6 Meter Hydraulic Tilting Flume / Open Channel - 10 Meter Experiment Pneumatic Apparatus Hydraulic Tilting Flume / Open Channel - 10 Meter Experiment Hydraulic Apparatus Pelton Wheel Turbine Test Rig (Capacity : 3.7 Kw) Francis Turbine Test Rig (Capacity : 3.7 Kw) Kaplan Turbine Test Rig (Capacity : 3.7 Kw) Centrifugal Pump Test Rig (Constant Speed) Reciprocating Single Stage Pump Test Rig Jet Pump Test Rig Cavitations Test Rig Hydraulic Tilting Flume / Open Channel - 8 Fits Hydraulic Tilting Flume / Open Channel - 5 Meter Hydraulic Tilting Flume / Open Channel - 8 Meter Wind Tunnel Experiment Pneumatic Apparatus Wind Tunnel Hydraulic Ram Model  Turbine & Pumps Models : Centrifugal Pump Deep Well Turbine Pump Francis Turbine Model Kaplan Turbine Model Steam Turbine Model Reciprocating Pump Jet Pump. Submersible Pump Pelton Turbine Model De-level Turbine Model lHydraulic Ram Model

Based in Roorkey, Uttarakhand we have emerged as one of the focused manufacturers, exporters and suppliers of the Pressure Testing Rig. This system that we offer can be used to simulate aircraft fatigue induced by changes in altitude. The design and quality of all the products we offer are stringently checked and monitored at each stage to ensure that the final product meets is on par with industrial standards.   Details : To design a system to simulate few years of aircraft fatigue induced by changes in altitude. The system was required to pressurize and depressurize all voids within the aircraft and be accurate to within 0.1psi at all stages of the operation. A very high level of safety was required, to prevent any potential damage to an aircraft through over pressure. The input control signal would be sent via a PLC and the operation would be recorded.