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SECTION 2. Components and connecting

Anschlussschema Kraftstoffstart

Hoppertank

Filzpendel /
felt pendulum

Pumpe/

fuel pump

Kraftstoffventil/
Kerosene valve

Ignitionventil/
ignition valve

Y Festo

Akku / battery

i/o-Platine /

i/o-board

Filter

Messingpendel /
brazen pendulum

Haupttank /
main tank

Ignitionventil/
igniotion valve

Kraftstoffventil/
Kerosene valve

Pumpe/

fuel pump

Akku / 

battery

Hochstrom zur 
Turbine / High 

current to the 

turbine

Datenverbindung 

zur Turbine / 

Data connection

to turbine

Verbindung zur 

Fernbedienung / 

Remote control

connection

Verbindung zu 

I/O Platine und 

GSU/ Connection 

to I/O board and 

GSU

GSU

ECU

Tankentlüftung /

Tank ventilation

Hochstrom / High current

Datenkabel / data

Datenkabel / data

Fernbedienung /

remote control

(a) Connection scheme.

(b) ECU connectors.

Figure 1: Connecting the H

ORNET

-III.

2.3

Fuel system

The overall reliability of the jet engine system depends on a well-made fuel system. New AeroDesignWorks
model jet engines ship with high quality components (fuel pump and valves, connectors, . . . ). If you need to
make adjustments or exchange components, some suggestions are:

• Use a high quality fuel pump like the ones shipped with the corresponding AeroDesignWorks jet engines.

• Use fuel valves of high quality.

• Use a hopper tank with felt pendulum in front of the main fuel tank(s).

• Do not use fuel filters directly before the fuel pump.

• Use a fuel feed line with the largest possible diameter.

2.4

Power supply

Since all components (like glow plug, starter, valves, fuel pump) are supplied by a single battery, its capacity
should be sufficiently high (

2500

mAh

).

5

Summary of Contents for HORNET-III

Page 1: ...HORNET III manual Firmware v3 0 AeroDesignWorks GmbH Wankelstr 57 D 50996 K ln Germany 27th April 2022...

Page 2: ...ermination statuses 12 4 5 Main menu 12 4 5 1 Run time settings 12 4 5 2 User adjustments 12 4 5 3 System and periphery 13 4 5 4 GPS and airspeed value 14 4 5 5 Test functions 15 4 5 6 Expert menu 15...

Page 3: ...ECUs sold by AeroDesignWorks only work with our own range of model jet engines As they are configured for a fuel start we no longer provide information on using an auxiliary gas The firmware version v...

Page 4: ...not supervise the proper installation and operation of the jet engine the electronic components and the radio controller the end user is responsible for all of this The product comes with a 24 month l...

Page 5: ...gure 1a Note that there are two fuel valves for the two fuel lines labeled KEROSENE and IGNITION on the engine These valves and their fuel lines refered to as main and ignition in this manual 2 1 Grou...

Page 6: ...ta Datenkabel data Fernbedienung remote control a Connection scheme b ECU connectors Figure 1 Connecting the HORNET III 2 3 Fuel system The overall reliability of the jet engine system depends on a we...

Page 7: ...several days 2 5 GPS module A GPS module can be connected to the corresponding outlet on the ECU It does not need to be configured via GSU The GPS data is available in the corresponding menu see Secti...

Page 8: ...ry is transmitted if using a telemetry module It is possible to turn off the engine and going into cool down mode 4 Fail safe If the ECU recieves errors from the RC during the Automatic phase e g no s...

Page 9: ...revent overshoots we meas ured the time from the controller signal assuming its maximum value to the engine reaching 98 of the max imum RPM note the vertical green lines in Figure 2 With this definiti...

Page 10: ...EEPROM automatically upon saving them When the engine is in standby mode the start sequence can be initiated by simultaneously pressing up and escape This might be needed if one HORNET III is used to...

Page 11: ...GSU will display e g CONNECTED TO 4711 TYPE 005 In this example the successfully connected to an engine with serial number 4711 of type 005 6 Result of RPM check RPM CHECK OK or RPM CHECK FAILED This...

Page 12: ...p procedure Status Description OFF Engine is is off can be switched to standby by moving the throttle first to neutral and then to full see Section 5 2 2 STANDBY Engine is ready to receive the start s...

Page 13: ...below the acceptable limit during calibration MAX CAL VOLT EXCEEDED The maximum fuel pump voltage allowed was exceeded without reaching the re quired RPM CALCULATED MAX PUMPVOLT EXCEED The calculated...

Page 14: ...e RPM 5 000 DUR ING RAMP UP The engine could not reach the required RPM May be due to a broken starter or a jammed engine BATTERY VOLTAGE TOO LOW The battery voltage fell below the limit set by the us...

Page 15: ...ld be set at the beginning of each session as functions and safety checks depend on it 2 3 BATTERY VOLTAGES Set the voltage at which the battery is considered empty or full here This is important for...

Page 16: ...on the glow plug and escape aborts This program can only be used when the engine is off 5 3 IGNIT FUEL Pressing enter switches the valve from OFF to ON and vice versa 5 4 FUEL VALVE Pressing enter swi...

Page 17: ...menus please get in touch with our support at turbines aerodesignworks com 4 6 Necessary settings before starting At the start of each session i e before the engine s first start of the day the GSU s...

Page 18: ...off position If the throttle is then set to full position within three seconds the ECU will initiate the autostart sequence 3 Running After successfully completing the autostart sequence the ECU puts...

Page 19: ...d black lines corresponding to c1 0 3 and c1 0 7 in Figures 4a 4b result in throttle curves that are easier to control at both low and high RPM 5 3 Autostart The autostart sequence can be triggered wh...

Page 20: ...l reaching full RPM once The RPM between idle and full RPM is controlled by the user s input This is achieved by an RPM and temperature dependent fuel flow Telemetry data is transmitted if a telemetry...

Page 21: ...the GSU menu see Section 4 5 2 e g if the RC uses digital trimming ON replaces the maximum trim setting OFF replaces the minimum trim setting Leave the RC s trimming at maximum when using this switch...

Page 22: ...xes The maximum RPM for the B300F could not be re adjusted to 105 000 after lowering it This has been fixed When the GSU was used to modify values the user could not discard the changes Pressing escap...

Page 23: ...you for your attention Your team at AeroDesignWorks GmbH Wankelstr 57 D 50996 K ln Germany Telefon 49 0 221 98 43 11 50 Telefax 49 0 221 98 43 11 02 https aerodesignworks com turbines aerodesignworks...

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