Turbo Jet Engine Test Bench Manufacturer,Supplier and Exporter in India
Product Code : EL-TELE-10706
Engineering Labs Equipment is a leading Turbo Jet Engine Test Bench Manufacturer,and suppliers in India, Turbo Jet Engine Test Bench Uruguay (Montevideo), Turbo Jet Engine Test Bench Uzbekistan (Tashkent), Turbo Jet Engine Test Bench Venezuela (Caracas), Turbo Jet Engine Test Bench Vietnam (Hanoi), Turbo Jet Engine Test Bench Yemen (Sana'a), Turbo Jet Engine Test Bench Zambia (Lusaka), Zimbabwe (Harare), Eswatini (Mbabane) (Lobamba), Ethiopia (Addis Ababa), Fiji (Suva), Gabon (Libreville), Gambia (Banjul), Georgia (Tbilisi), Ghana (Accra), India (Delhi, Mumbai, Kolkatta, Chennai), Indonesia (Jakarta), Iraq (Baghdad), Ivory Coast (Yamoussoukro), Jamaica (Kingston), Jordan (Amman), Kazakhstan (Astana), Kenya (Nairobi), Kiribati (Tarawa), Kosovo (Pristina), Kuwait (Kuwait City), Kyrgyzstan (Bishkek), Laos (Vientiane), Latvia (Riga), Lebanon (Beirut), Lesotho (Maseru), Liberia (Monrovia), Libya (Tripoli), Lithuania (Vilnuis), Luxembourg (Luxembourg), Malawi (Lilongwe), Malaysia (Federal Territory of Kuala Lumpur), Maldives (Malle), Mali (Federal Territory of Kuala Lumpur), Malta (Male), Mauritania (Nouakchott), Mauritius (Port Louis), Mexico (Mexico City), Mongolia (Ulaanbaatar), Bulgaria (Sofia), Burkina Faso (Ouagadougou), Burundi (Gitega), Cambodia (Phnom Penh), Cameroon (Yaoundé), Cape Verde (Praia), Central African Republic (Bangui), Chad (N'Djamena), Chile (Santiago), Colombia (Bogota), Comoros (Moroni), Congo (Kinshasa), Costa Rica (San José), Croatia (Zagreb), Cuba (Havana), Cyprus (Nicosia), Czech Republic (Prague), Denmark (Copenhagen) ,Djibouti (Djibouti City), Dominican Republic (Santo Domingo), DR Congo (Kinshasa), Ecuador (Quito), Egypt (Cairo), El Salvador (San Salvador), Equatorial Guinea (Malabo), Eritrea (Asmara), Estonia (Tallinn)
The Turbo Jet Engine Test Bench experimental test stand trainer investigates the behavior during operation of a jet engine.
Includes the following components: jet engine (with compressor, annular combustion chamber, turbine, and propelling nozzle), fuel system, starter and ignition system, and measurement and control equipment.
The gas turbine works as an open cyclic process, with the ambient air being drawn out and fed back in.
In the jet engine, the ambient air drawn in is first brought to a higher pressure in the single-stage radial compressor.
In the downstream combustion chamber, fuel is added to the compressed air and the resulting mixture is ignited.
The temperature and flow velocity of the gas increase.
The gas flows out of the combustion chamber into the single-stage axial turbine and discharges a portion of its energy to the turbine.
This turbine drives the compressor.
In the propelling nozzle, the partially expanded and cooled gas expands to ambient atmospheric pressure and the gas accelerates to almost the speed of sound.
The high-speed gas outflow generates the thrust.
In order to reduce the outlet temperature, the exhaust gas stream is mixed with the ambient air in a mixing pipe.
The gas turbine is started fully automatically with the aid of an electric starter.
The speed, temperatures, and mass flow rates of the air and fuel is recorded using sensors.
The measured values can be read on digital displays.
At the same time, the measured values can also be transmitted directly to a PC via USB.
The data acquisition software is included.
FEATURES:
Behavior during operation of a jet engine including start-up procedure
Determination of the specific thrust
Determination of the specific fuel consumption
Determination of lambda (fuel-air ratio)
SPECIFICATION:
230V, 50Hz, 1 phase
230V, 60Hz, 1 phase
120V, 60Hz, 1 phase
Jet engine :
Max. thrust: 82N at 117000min-1
Speed range: 35000…117000min-1
Fuel consumption: max. 22L/h (full load)
Exhaust gas temperature: 610°C
Sound level at 1m distance: max. 130dB(A)
Fuel: kerosene or petroleum + turbine oil
Starting system: electric starter
1 tank for fuel: 5L
Measuring ranges :
Dfferential pressure: 0…150mbar
Pressure: 0…2,5bar (combustion chamber)
Temperature: 2x 0…1200°C / 1x 0…400°C
Speed: 0…120000min-1
Consumption: 0…25L/h (fuel)
Force: 0…+/-200N
DIMENSIONS AND WEIGHT:
L x W x H: 1200x 900 x 330 mm
Weight (approx.): 120kg
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