Jet Engine Gas Turbine Manufacturer,Supplier and Exporter in India
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Product Code : SCL-CELE-13932
Indian Lab Suppliers supplies the Jet Engine Gas Turbine (Product ID: 13932) as part of its Civil Engineering Lab Equipment range. It is a small turbojet on a test stand with computer control and data acquisition.
Quick Answer
The engine has a single-stage radial compressor, combustion chamber and axial turbine. It idles at about 50,000 rpm, reaches up to 120,000 rpm and gives up to 167 N of thrust, with an exhaust gas temperature of about 600 °C. It runs on Jet A, Jet A1 or low-sulphur paraffin with a specified turbine oil mix. It is listed with a 16-channel, 16-bit USB DAQ (250 kS/s) and LabVIEW-based software measuring speed, thrust, stage temperatures and pressures and air flow.
Key Specifications
| Parameter | Detail |
|---|---|
| Engine | Radial compressor, combustion chamber, axial turbine |
| Thrust | Up to 167 N |
| Speed | Idle about 50,000 rpm; max 120,000 rpm |
| Exhaust temperature | About 600 °C |
| Fuel | Jet A, Jet A1 or low-sulphur paraffin |
| Data acquisition | 16-channel, 16-bit, 250 kS/s USB; LabVIEW-based software |
| Measurements | Speed, thrust, stage temperatures and pressures, air flow |
Where This Is Used
Aerospace and mechanical students find specific thrust, turbine efficiency, fuel consumption and air-fuel ratio. See also the Turbo-Jet Trainer with Reheat (Product ID: 13935) and Two Shaft Gas Turbines (Product ID: 13929). Browse the full Civil Engineering Lab Equipment range or related Engineering Lab Equipment apparatus.
Frequently Asked Questions
How much thrust does it produce?
Up to 167 N.
What fuel does it use?
Jet A, Jet A1 or low-sulphur paraffin.
How is data recorded?
With a 16-channel USB DAQ and LabVIEW-based software.
Related Categories
Civil Engineering Lab Equipment · Engineering Lab Equipment · Physics Lab Equipment
Request a Quote
For pricing, bulk quantities or tender documentation on the Jet Engine Gas Turbine, reach our team via Contact Us or submit your requirement through our Tenders page.
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