TURBO JET ENGINE, 70N Thrust
GENERAL DESCRIPTION
The engine is a bench top unit for a
small turbo jet engine with a radial flow compressor and an axial flow
turbine as in modern jet plane.
Inlet air through an orifice flow measuring device is compressed by a
single stage radial flow compressor. The turbine is motor started and
runs on Jet A fuel. Fuel is injected and ignited in the combustion
chamber providing hot gas for a single stage axial flow turbine which
inturn drives the compressor. The gas is exhausted through a nozzle at
high velocity providing a thrust. The turbine unit runs on ceramic
bearings. Lubrication is provided by jet oil in the fuel, and no
separate lubrication system is required. A fan is provided for engine
cooling.
An Electronic Control Unit (ECU) controls the basic turbine
operation. Additional instruments are provided for monitoring and
controlling engine operation and performance.
A touch screen computer with an interface unit, and software are
provided for speed control, data display and analysis, and to assist the
ECU.
A transparent engine cover, and over speed shutdown are provided.
TYPICAL EXPERIMENTS
- Understanding the thermodynamic process.
- Static thrust vs turbine speed.
- Power input and output and propulsive efficiency.
TECHNICAL DATA
| Engine construction |
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| - Diffuser |
: High strength aluminium. |
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| - Combustion chamber |
: Inconel. |
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| - Turbine |
: Vacuum cast inconel. |
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| - Compressor |
: High grade aluminium alloy. |
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| . Engine performance specifications. |
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| - Maximum static thrust |
: Upto 70 N at 150,000 rpm. |
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| - Running fuel |
: Jet A or Kerosene with jet oil. |
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| . Sensors |
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| - Temperatures : Inlet air, diffuser exit, turbine guide vane entry and exit and nozzle exit. |
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| - Pressures : Diffuser exit and turbine exit. |
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| - Thrust. |
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| - Speed. |
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| - Fuel flow rate. |
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| - Air flow rate |
: Differential pressure at inlet orifice. |
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| . Accessories |
: Engine cooling fan, 2 ear muffs, jet oil and barometer. |
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| . Power supply |
: 220V 1Ph 50Hz. |
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| Net (unpacked) shipping dimensions WxLxH : 85 x 115 x 60 cm |
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| Net weight : Approx. 65 kg |
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Motesta Instruments is one of India's most trusted Civil & Mechanical Engineering Lab Equipment Manufacturers for bulk tender supply of TURBO JET ENGINE, 70N Thrust. We deliver against Ministry of Education tenders, World Bank funded projects, ITI/Polytechnic supply contracts and turnkey lab setup orders for Engineering Colleges and Universities worldwide.
For tender quotations on TURBO JET ENGINE, 70N Thrust (Code: Civil-MCE-0135), our tender desk provides:
- Detailed Technical Specifications matched line-by-line to your tender BOQ
- OEM Authorization Letters and ISO/CE compliance certificates
- EMD & Bank Guarantee support documentation
- Custom branding on labels & control panels for institute identity
- Voltage variants (110V/220V/three-phase) for the destination country
- Multi-language documentation (English, French, Spanish, Arabic on request)
- Container loading photos and pre-shipment inspection reports
Read more about MoE Tender Supply
Worldwide Delivery
Door-to-door logistics to 50+ countries — sea freight, air freight or express courier depending on order size. We handle export packing, marine insurance, customs clearance and delivery to your institute address.
Export Packing & Inspection
Sea-worthy export packing in plywood crates with desiccant; pre-shipment photos, inspection reports and container loading documentation provided for every order.
Installation & Commissioning
On-site installation, calibration, commissioning and acceptance testing performed by our trained engineers (subject to order value & geography).
Faculty Training
Hands-on faculty & lab-technician training included with bulk tender deliveries — both on-site and remote video sessions available.
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