AeroDesignWorks HORNET-III Скачать руководство пользователя страница 3

1

Introduction

The H

ORNET

-III is an engine control unit (ECU) for model jet turbines, originally developed and produced

by ProJET electronic components GmbH, Fuchsmühl, Germany. Its home builder version (still distributed by
ProJET) can be used for engines of a wide range of manufacturers. All H

ORNET

-III variants have the following

features in common:

• ECU settings accessible via Ground Support Unit (GSU).

• Engine can be started using standard fuel or an auxiliary gas.

• Controls an analogue (brushed) fuel pump.

• RPM sensor can be optic or magnetic (Hall).

• Dynamic throttle response depending on the temperature and RPM sensor signals.

• Fail-safe mode in case run time errors (e.g. one or both sensors fail and other errors).

• Support for connecting to a GPS module.

• Support for a smoker valve.

• Communication with XBee modules for saving telemetry data.

After acquiring the BF Turbines product line in 2017, AeroDesignWorks GmbH purchased the H

ORNET

-

III firmware source code together with a license to use, modify and redistribute the firmware in 2018. The goal

was to be able to make modifications for the BF range of engines. AeroDesignWorks and ProJET continue
to work together on the hardware, but starting in 2021, AeroDesignWorks distributes their H

ORNET

-III ECUs

with a new firmware starting at version v3.0.

• All H

ORNET

-III 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 v3.0 brought some changes that affect the end user and hence a long overdue update

to the manual.

ProJET developed a H

ORNET

-III capable of powering and controlling brushless fuel pumps called H

ORNET

-

III-BLC (Brushless Controller), which uses different hardware and cannot be used with analogue fuel pumps.

There are some notable differences, which will be mentioned in the manual where appropriate.

1.1

Hardware information

The H

ORNET

-III is powered by an Atmel Atmega2560 processor, which has 256 KB of program memory and

4 KB of EEPROM to persistently store settings. The EEPROM has an unlimited amount of read cycles and a
limited but large (100,000+) amount of write cycles per byte.

• The maximum supported battery voltage is 12

.

8

V

for continuous operation.

• The receiver input supports 5 cells with a maximum voltage of 7

.

5

V

and a minimum pulse amplitude of

2

.

7

V

.

• The fuel pump can be supplied with a current of 10

A

for continuous operation, with peaks of 20

A

for up

to 0

.

2

s

.

• The starter can be supplied with a current of 10

A

for continuous operation, with peaks of 20

A

for up to

0

.

2

s

.

• The glow plug can be supplied with a current of 10

A

for continuous operation, with peaks of 20

A

for up

to 0

.

2

ms

.

• The fuel valves can be supplied with a current of 0

.

25

A

for continuous operation, with peaks of 0

.

5

A

for

up to 1

s

.

2

Содержание HORNET-III

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Отзывы: