Advanced Technocracy Inc.
Grain Market, Ambala, Haryana
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Gas Turbine

Our product range includes a wide range of two shaft gas turbine apparatus and turbojet engine test stand.

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Features

  • Self-contained complete teaching facility
  • Designed for safe easy operation with low noise levels
  • Data logging option available for all measured variables
  • Comprehensive controls and instrumentation displayed in multi-colour flow diagram

Experimental Capacity / Teaching Objectives

  • Performance of a simulated single shaft unit
  • Performance of a two shaft unit
  • Characteristics of individual components: gas generator compressor, combustion chamber characteristics, power turbine characteristics.

Specifications

  • Self-contained moveable stand
  • Melamine laminate instrument panel and steel cladded panels
  • Single shaft compressor/turbine
  • Combustion chamber for operation on propane, butane or propane/butane mixtures
  • Power absorption system and data logging
  • Calibrated electrical machine for torque and power measurement
  • Circulating pump
  • Cooler and filter
  • Five colour instrument panel with flow diagram
  • Oil pressure gauge and fuel supply pressure gauge
  • Air compressor set
  • Tropicalized for use in conditions up to 40ºC ambient and 80% relative humidity
  • Consumption at full load approx. 7 kg/hr.

 


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Description

ATICO have developed a turbo jet engine test stand to provide a cost effective method of testing the performance of an operational aero jet engine. The turbo jet test stand is mounted on a wheeled trolley allowing it to be moved to an operational area or stored in a convenient location.

Experimental Capability

  • Demonstration of the Turbo jet principle
  • Performance analysis of a Turbojet at varying power

Specification

A trolley mounted single shaft turbojet designed for flight is to be supplied so as to demonstrate the turbojet principle. It is to be instrumented, so as to all allow a performance analysis of the turbojet at various speeds to be undertaken. The unit should alternatively be provided with a physical mimic diagram plate or be instrumented for data acquisition and a digital mimic diagram. Thrust produced must greater than the range up to 230N and be measured electronically. Speed is to be up to 110,000 rpm and full power pressure is to be over 2 bar. The fuel is to be kerosene.


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Advanced Technocracy Inc.

Kunal Chopra (CEO)
ATICO House, 5309 Grain Market, Near B. D. Senior Secondary School Aticoindia@gmail.com
Ambala - 133001
Haryana, India
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