Axial Flow Turbine Test Bed Manufacturer,Supplier and Exporter in India

The Axial Flow Turbine Test Bed experimental axial flow engine-start turbine comprising a single-stage radial compressor, an annular combustion chamber and a low mass, high-performance axial flow turbine.

The engine has been integrated into a sturdy metal frame that holds it firmly, while enabling accurate measurement of the thrust produced by the engine.

The engine inlet has been replaced with a custom fabricated frontal duct, to enable the air mass flow rate to be accurately measured.

A tough, transparent polycarbonate screen is fitted in order to make the apparatus completely safe, but still provides excellent visibility of the engine when in use. 

An electronic preprogrammed controller constantly supervises the engine, ensuring safe operating conditions at all times.

The engine is easy to start and stop from the software interface, and automatic, optimal start-up and power-down sequences are already set to assure minimum mechanical stresses. 

There is no requirement for compressed air supply or propane gas to start the engine.

The screen is removable, enabling full access to the engine and instrumentation.

The engine software runs on a personal computer, requiring only a single USB interface between the electronic console and the PC. 

This enables simple installation into a test cell or soundproof enclosure.

FEATURES:

Complete aeronautical axial flow gas turbine engine

Full instrumentation and sensors

Easy installation into a test cell (single USB interface)

High-performance centrifugal compressor

Simple ignition system, based on a common Rossi R8 glow plug

Data acquisition and educational software included

Small-scale equipment minimizes laboratory space needed

Fully tested for high performance and safety

High maximum RPM

Fast response to speed changes

Single point pivot on engine mounting enables accurate thrust measurement

No need for external lubrication system; the lubricant is mixed with the fuel

No need for external battery and charger

Can be fuelled with common paraffin or kerosene – no need for difficult-to-find aviation fuel

Tough, transparent polycarbonate safety screen

An optional floor-standing frame is available to house the unit together with its fuel tank and electronic console

SPECIFICATIONS:

Thrust: 200N typical

Exhaust gas temperature: 800°C typical

Mass flow: 450 g/s

Ignition system: Glow plug

Compressor type: Single-stage radial

Turbine type: Single-stage, low-mass axial flow

Engine rpm: 105,000rpm typical

Engine mount: Single pivot point

Typical fuel:

One of the following choices:

Paraffin

Jet A-1

JP-4/Kerosene

DIMENSIONS AND WEIGHT:

L x W x H: 880 x 510 x 1185 mm

Weight (approx.): 150 kg

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