Axial Flow Turbine Engine

Axial Flow Turbine Engine

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Axial Flow Turbine Engine Specification: An aeronautical axial flow gas turbine engine mounted on a stainless steel plinth, suitable for bench mounting. An electronic console and 5L ‘explosafe’ fue...


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Axial Flow Turbine Engine

Specification:
  • An aeronautical axial flow gas turbine engine mounted on a stainless steel plinth, suitable for bench mounting. An electronic console and 5L ‘explosafe’ fuel tank are also provided.
  • An optional mounting frame is available for floor standing operation.
  • The engine has a maximum speed in excess of 100,000 rpm and generates a thrust of at least 195N
  • Full instrumentation to measure rpm, thrust and temperature and pressure at each stage of the jet engine.
  • Stainless Steel air inlet duct to measure air flow.
  • The engine is easy to start, without the need for compressed air.
  • The equipment is fully controlled from a user supplied PC. The software includes powerful educational features together with sophisticated graph plotting and data logging capability.
  • Interface to the PC is via a single USB interface, thus providing easy installation.
Features:
  • Complete aeronautical axial flow gas turbine engine
  • Full instrumentation and sensors
  • Full control by means of software and microprocessor controller
  • Easy installation into a test cell (single USB interface)
  • High performance centrifugal compressor
  • High maximum RPM
  • Fast response to speed changes
  • Single point pivot on engine mounting allows accurate thrust measurement
  • No need for external lubrication system (the lubricant is mixed with the fuel)


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quick overview :

Axial Flow Turbine Engine

Specification:
  • An aeronautical axial flow gas turbine engine mounted on a stainless steel plinth, suitable for bench mounting. An electronic console and 5L ‘explosafe’ fuel tank are also provided.
  • An optional mounting frame is available for floor standing operation.
  • The engine has a maximum speed in excess of 100,000 rpm and generates a thrust of at least 195N
  • Full instrumentation to measure rpm, thrust and temperature and pressure at each stage of the jet engine.
  • Stainless Steel air inlet duct to measure air flow.
  • The engine is easy to start, without the need for compressed air.
  • The equipment is fully controlled from a user supplied PC. The software includes powerful educational features together with sophisticated graph plotting and data logging capability.
  • Interface to the PC is via a single USB interface, thus providing easy installation.
Features:
  • Complete aeronautical axial flow gas turbine engine
  • Full instrumentation and sensors
  • Full control by means of software and microprocessor controller
  • Easy installation into a test cell (single USB interface)
  • High performance centrifugal compressor
  • High maximum RPM
  • Fast response to speed changes
  • Single point pivot on engine mounting allows accurate thrust measurement
  • No need for external lubrication system (the lubricant is mixed with the fuel)

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