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Stations

Made in various configurations

depending on customer requirements

They are a great help in the didactic process being an extensive measurement platform. They enable the measurement of flows, pressures and temperatures in various engine spaces. We are the only company offering a stand equipped with a engine with a glass casing enabling observation of processes inside it throughout the entire scope of work.

Available configuration options

01

  • Info
  • Set
  • Parameters


GTM140 engine with a 70mm turbine with automatic starting on JET-A1 fuel. ECU controller adapted to work with a 1-2ms 50Hz digital signal generator (equipped with position from item 13).
The engine version adapted to long-term work on the stand.

  • GTM140 engine
  • ECU controller
  • GSU ​​control panel
  • rack and pinion fuel pump
  • fuel start solenoid valve
  • fuel main solenoid valve
  • optical speed sensor
  • temperature sensor (EGT) - thermocouple
  • electric / pneumatic cable set
  • fasteners
  • max thrust - 140N
  • min. thrust - 8N
  • rotor speed max. - 120,000 1/min
  • rotor speed min. - 33 000 1/min
  • compression ratio - 2.8: 1
  • mass air flow - 350 g/s
  • outlet gas temperature max. - 700 deg. C
  • exhaust gas temperature min. - 550 degrees C
  • fuel consumption - 420 g/min
  • fuel type - JET-A1
  • lubrication - 4% Aeroshell 500/560 mix, Mobil Jet Oil II

02

  • Info
  • Set
  • Parameters

GTM140 engine with a 70mm turbine. Configuration and parameters as in point 1. The motor in a glass enclosure made of borosilicate glass with a wall thickness of 5mm allows observation of processes occurring throughout the entire range of engine operation. Does not allow internal measurements due to the inability to lead measuring points through the glass housing of the chamber.

Dimensions:
length: 800mm | width: 600mm |  height: 600mm | total mass: 60kg

  • GTM140 engine
  • ECU controller
  • GSU ​​control panel
  • rack and pinion fuel pump
  • fuel start solenoid valve
  • fuel main solenoid valve
  • optical speed sensor
  • temperature sensor (EGT) - thermocouple
  • electric / pneumatic cable set
  • fasteners
  • max thrust - 140N
  • min. thrust - 8N
  • rotor speed max. - 120,000 1/min
  • rotor speed min. - 33 000 1/min
  • compression ratio - 2.8: 1
  • mass air flow - 350 g/s
  • outlet gas temperature max. - 700 deg. C
  • exhaust gas temperature min. - 550 degrees C
  • fuel consumption - 420 g/min
  • fuel type - JET-A1
  • lubrication - 4% Aeroshell 500/560 mix, Mobil Jet Oil II

03

  • Info
  • Set
  • Parameters

GTM220 engine with 85mm turbine with automatic starting on JET-A1 fuel.

Dimensions:
diameter: 132mm | length: 390mm |  total mass: 3200g

  • GTM220 engine
  • ECU controller
  • GSU control panel
  • rack and pinion fuel pump
  • fuel start solenoid valve
  • fuel main solenoid valve
  • optical speed sensor
  • temperature sensor (EGT) - thermocouple
  • electric / pneumatic conduit set
  • fasteners
  • max thrust - 220 N
  • min thrust - 12 N
  • rotor speed max. - 105,000 1/min
  • rotor speed min. - 35,000 1/min
  • compression ratio - 3.7: 1
  • mass air flow - 440 g / s
  • exhaust gas temperature - 750 degrees Celsius
  • fuel consumption - 640 g / min
  • fuel type - JET-A1
  • lubrication - 4% Aeroshell 500/560 mix, Mobil Jet Oil II

04

  • Info
  • Parameters

500N engine with 160mm turbine with automatic starting on JET-A1 fuel in the injector system with the fuel swirler (without evaporators). High voltage spark ignition system. Full engine control via FADEC. Lubrication system closed, pressure (oil pump, filter, cooler, pressure regulator). Implementation in the form of a 60x60x80cm module with protected equipment enabling autonomous operation.

Dimensions:
length: 800mm | width: 600mm |  height: 600mm | total mass: 60 kg

  • max thrust - 500N
  • min thrust - 50N
  • rotor speed max. - 50,000 1/min
  • rotor speed min. - 32,000 1/min
  • compression ratio - 2.2:1
  • mass air flow - 1100 g/s
  • exhaust gas temperature - 650 degC (max 970 degC)
  • fuel consumption - 950 g/min
  • fuel type - JET-A1
  • lubrication - Aeroshell 500/560, Mobil Jet Oil II in a closed system (pressure 3.5 bar)

05

Measuring point set behind the compressor diffuser

Number of 3 pieces. Peripherally every 120 degrees. Terminals adapted to connect the apparatus made after arrangements with the customer. This option cannot be used on glass-enclosed motors.

06

Measuring point set before the turbine nozzles

Number of 3 pieces. Peripherally every 120 degrees. Terminals adapted to connect the apparatus made after arrangements with the customer. This option cannot be used on glass-enclosed motors.

07

Temperature measurement in one point 10mm behind the turbine in the outlet nozzle. (visual reading – no data transmission)

08

Measurement of rotor speed (visual reading – no data transmission)

09

Supply voltage measurement (visual reading – no data transmission)

10

Measurement of voltage at the fuel pump (visual reading – no data transmission)

11

An additional set of internal nozzles in the evaporators enabling independent injection of fuel or other substances. (12 nozzles circumferentially one for each dish)

12

  • Info
  • Set

Engine stand GTM130 / 220. in the basic version. The stand is equipped with transport handles on both sides and stands – non-slip rubber feet 50 / 60mm. Running platform with linear bearings with elements for mounting the engine and its equipment made of acid-resistant steel. It enables the assembly of a 1-2ms 50Hz digital signal generator to control the engine operation, together with a power setting knob and a switch (optional key switch) from point 22.

  • steel base with galvanic protection in silver or black, with 20mm linear guides
  • Additional platform for equipment under the running platform
  • 12V17Ah battery
  • Fuel tank with a capacity of min. 10L with filter

13

Additional equipment for measuring static thrust: strain gauge, MD150T programmable indicator with USB communication and data acquisition software. Tensometric beam with a measuring range up to 300N mounted on the base of the station.

14

Transducer for testing fuel consumption with an oval-wheel sensor with an operating range of 5ml-1000ml / min, accuracy of 0.5%. Working pressure max 3 MPa. Open collector outlet 0.174ml / pulse.

15

Control system with a three-way valve in the fuel supply system. It is used for automatic, smooth transition to alternative fuel.

16

System for measuring the mass air flow rate at the inlet to engines in a metal housing. It allows collecting data on static and total pressure as well as temperature in the engine inlet duct. Stabilizes the airflow at the compressor inlet. The system prevents the use of an automatic electric starter. The engine can be started by means of compressed air, controlled manually or automatically after the application of the “Automatically controlled start system” from the next position. (the option does not apply to the 500N engine)

17

Automatic compressed air starting system. It is used to start the engine with the mass air flow measurement system installed. (option not intended for 500N engine). The microprocessor-based controller regulates the rotor rotation proportionally by an air solenoid valve, starting it up in accordance with the current stage of turbine operation and the measured parameters.

18

Stand cover

Tunnel made of transparent polycarbonate with a thickness of 8mm with very high resistance to mechanical impacts. Mounted on guides allowing easy access to the engine. The cover additionally increases the safety of operating the station. Rapid disassembly and assembly of the cover is possible during the maintenance of the station.

19

Additional fuel tank with a capacity of 25 liters with a loaded filter in the bottom. Connections in accordance with the fuel installation of the stand.

20

Additional fuel tank with a capacity of 25 liters with a loaded filter in the bottom. Connections in accordance with the fuel installation of the stand.
Tank equipped with a fuel level indicator.

21

An external digital control module equipped with a power adjustment knob / lever and a start switch (optional key switch). Enables motor control on an extended connection e.g. from a separate room.

22

Control panel with module mounting elements: GSU with LCD display and a digital module for engine control. Material – stainless steel. Version for independent assembly outside the stand.

23

Additional gear fuel pump

24

Additional fuel valve kit

25

  • Info
  • Parameters

Modular control and measuring apparatus with data acquisition. Digital and analog inputs adapted to the used sensor set.

  • Recording measurements on memory media (SD card or USB Flash Drive)
  • Transmission of measurement data with a time stamp every 200 ms via a USB port to an external computer (not included in the set)
  • Measurement of environmental conditions - absolute pressure and temperature and calculation of mass flow (using a system for measuring mass flow)
  • The possibility of individual configuration for user needs
  • Local graphic interface on a 7 "touch screen

26

A set of sensors and transducers for measuring pressure, temperature and RPM cooperating with control and measuring equipment. The value of the item depends on the configuration, presented in the individual valuation.

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Design and realization: Aggie Studio