AIRCRAFT TECHNOLOGIES
AIRCRAFT TECHNOLOGIES
SIMULATORS:
TWIN-ENGINE AIRCRAFT ELECTRICAL SYSTEM
MOD. AQ-1/EV
4
TWIN-ENGINE AIRCRAFT HYDRAULIC SYSTEM
MOD. AQ-2/EV
5
TWIN-ENGINE AIRCRAFT AIR CONDITIONING
AND PRESSURIZATION SYSTEM
MOD. AQ-3/EV
6
Note: This publication is constantly updated. Please send any suggestion you have to export@elettronicaveneta.com. We would also like to remind
you that, due to the continuous technological upgrades, the described products may be subjected to design and/or technical modifications.
Nevertheless, we guarantee that the educational content of our equipment remains unchanged.
ELETTRONICA VENETA S.P.A. - 31045 Motta di Livenza (TV) Italy - Via Postumia 16 - Tel. +39 0422 765 802 - Fax +39 0422 861 901 - E-mail: export@elettronicaveneta.com
3
TWIN-ENGINE AIRCRAFT
ELECTRICAL SYSTEM
Mod. AQ-1/EV
INTRODUCTION
The aircraft electrical system simulator mod. AQ-1/EV, is
included in a complete set of educational equipment for the
basic training on aircraft systems.
The simulator consists of a computer-assisted panel, with silkscreen mimic diagram for a clear location of its components.
Various zones of the mimic diagram are represented with
different colours to emphasize peculiar aspects of the system.
Light and displays indicators, installed in the mimic diagram
enable to assess the evolutions of the control.
The graphic display of the information available at the control
input, such as aircraft status (park, APU …) on the computer
screen enables the permanent monitoring of the system.
The operational conditions are set by students according to the
educational path indicated in the courseware, carried out by
the PC.
TRAINING PROGRAM:
• POWER GENERATION
- DC battery
- APU (Auxiliary unit)
- Alternator (Integrated Drive Generators)
- Transformers-rectifiers (TR)
- Electronic inverter DC-AC
- External power
- Random air turbine (RAT)
- Emergency generator
- Hydraulic circuits (Green, blue, yellow)
• POWER NETWORK
- DC BAT bus
- DC BUS1 – DC BUS2
- DC ESS BUS ( emergency bus)
- AC BUS1
- AC ESS bus (emergency bus)
- AC BUS2
- BUS TIE contactor
4
- MAINT bus (Ground handling bus)
• SYSTEM SUPERVISION SIMULATIONS
• STATUS
- Park
- Airport service support
- APU power supply
- APU engine starting
- Take off
- Landing
• ELECTRICAL PROBLEMS HANDLING
TECHNICAL SPECIFICATIONS:
The system is arranged on a silk-screen, panel provided with:
• Color silk screen panel
• Selection of the operational conditions with switches and
pushbuttons
• Displays and LED visualisation
• Dynamic display of the parameters, on the computer screen,
with high graphic performance software (LabVIEW)
• USB connexion with the computer
Power supply: 230 Vca 50 Hz single-phase - 50 VA
(Other voltage and frequency on request)
REQUIRED
PERSONAL COMPUTER
- NOT INCLUDED -
SUPPLIED WITH
SOFTWARE:
SIMULATOR CONTROL MANAGEMENT WITH
GRAPHICAL DISPLAY ON THE PC SCREEN
THEORETICAL-EXPERIMENTAL
HANDBOOK
ELETTRONICA VENETA S.P.A. - 31045 Motta di Livenza (TV) Italy - Via Postumia 16 - Tel. +39 0422 765 802 - Fax +39 0422 861 901 - E-mail: export@elettronicaveneta.com
TWIN-ENGINE AIRCRAFT
HYDRAULIC SYSTEM
Mod. AQ-2/EV
INTRODUCTION
The aircraft hydraulic system simulator mod. AQ-2/EV, is
included in a complete set of educational equipment for the
basic training on aircraft systems.
The simulator consists of a computer-assisted panel, with silkscreen mimic diagram for a clear location of its components.
Various zones of the mimic diagram are represented with
different colours to emphasize peculiar aspects of the system.
Light and displays indicators, installed in the mimic diagram
enable to assess the evolutions of the control.
The graphic display of the information available at the control
input, such as aircraft status (park, APU …) on the computer
screen enables the permanent monitoring of the system.
The operational conditions are set by students according to the
educational path indicated in the courseware, carried out by the PC.
TRAINING PROGRAM:
• PRESSURE GENERATION
- Engine Driven Pump (green hydraulic circuit)
- Engine Driven Pump (yellow hydraulic circuit)
- Electric pump (blue hydraulic circuit)
- Power Transfer Unit (PTU)
• PRESSURE ACCUMULATOR
- Circuit 1 accumulator
- Circuit 2 accumulator
- Circuit 3 accumulator
• HYDRAULIC ACTUATORS
Green circuit
- Flaps, Rudder, Spoilers, Nose wheel steering
Blue circuit
- Spoilers, Rudder, Elevator
Yellow circuit
- Elevator, Spoiler, Landing gear
• SYSTEM SUPERVISION SIMULATIONS
• MODE
- Ground
- Takeoff
- Flight
- Landing
• CONFIGURATIONS
- APU start
- Hydraulic pumps ON
- Electric pumps ON
- PTU automatic
- Wheel pedal disc angle control
- 5 Flaps/Slats position selection
- 6 Flight control pushbuttons
- Speed and Park brake
- Hydraulic emergency situations (PTU, RAT …)
TECHNICAL SPECIFICATIONS:
The system is arranged on a silk-screen, panel provided with:
• Color silk screen panel
• Selection of the operational conditions with switches and
pushbuttons
• Displays and LED visualisation
• Dynamic display of the parameters, on the computer screen,
with high graphic performance software (LabVIEW)
• USB connexion with the computer
Power supply: 230 Vca 50 Hz single-phase - 50 VA
(Other voltage and frequency on request)
REQUIRED
PERSONAL COMPUTER
- NOT INCLUDED -
SUPPLIED WITH
SOFTWARE:
SIMULATOR CONTROL MANAGEMENT WITH
GRAPHICAL DISPLAY ON THE PC SCREEN
THEORETICAL-EXPERIMENTAL
HANDBOOK
ELETTRONICA VENETA S.P.A. - 31045 Motta di Livenza (TV) Italy - Via Postumia 16 - Tel. +39 0422 765 802 - Fax +39 0422 861 901 - E-mail: export@elettronicaveneta.com
5
TWIN-ENGINE AIRCRAFT
AIR CONDITIONING AND
PRESSURIZATION SYSTEM
Mod. AQ-3/EV
INTRODUCTION
The aircraft air conditioning and pressurization simulator mod.
AQ-3/EV, is included in a complete set of educational equipment
for the basic training on aircraft systems.
The simulator consists of a computer-assisted panel, with silkscreen mimic diagram for a clear location of its components.
Various zones of the mimic diagram are represented with
different colours to emphasize peculiar aspects of the system.
Light and displays indicators, installed in the mimic diagram
enable to assess the evolutions of the control.
The graphic display of the information available at the control
input, such as aircraft status (park, APU …) on the computer
screen enables the permanent monitoring of the system.
The operational conditions are set by students according to the
educational path indicated in the courseware, carried out by
the PC.
• STATUS
- Park
- Airport service support
- APU bleed
- PACK 1 and 2
- Engine starting
- Pressurization cycle
• AIR MANAGEMENT PROBLEMS HANDLING
TECHNICAL SPECIFICATIONS:
The system is arranged on a silk-screen, panel provided with:
• Color silk screen panel
• Selection of the operational conditions with switches and
pushbuttons
• Displays and LED visualisation
• Dynamic display of the parameters, on the computer screen,
with high graphic performance software (LabVIEW)
• USB connexion with the computer
TRAINING PROGRAM:
• AIR INTAKE
- BLEED valve 1 and 2
- FAN AIR VALVE 1 AND 2
- APU BLEED valve
- External group
- Cross BLEED valve
• AIR CONDITIONING CIRCUIT
- PACK 1 and 2
- HEAT EXCHANGER 1 and 2
- COMPRESSOR 1 and 2
- AIR distribution
• AIR PRESSURIZATION
- OUTFLOW valve
- Pressurization profile
• SYSTEM SUPERVISION SIMULATIONS
6
Power supply: 230 Vca 50 Hz single-phase - 50 VA
(Other voltage and frequency on request)
REQUIRED
PERSONAL COMPUTER
- NOT INCLUDED -
SUPPLIED WITH
SOFTWARE:
SIMULATOR CONTROL MANAGEMENT WITH
GRAPHICAL DISPLAY ON THE PC SCREEN
THEORETICAL-EXPERIMENTAL
HANDBOOK
ELETTRONICA VENETA S.P.A. - 31045 Motta di Livenza (TV) Italy - Via Postumia 16 - Tel. +39 0422 765 802 - Fax +39 0422 861 901 - E-mail: export@elettronicaveneta.com
ELETTRONICA VENETA S.P.A. forbids the duplication or the disclosure of the information contained in this catalogue without written authorization.
Elettronica Veneta S.p.A.
Via Postumia, 16
31045 Motta di Livenza (Treviso) Italy
Tel. +39 0422 765 802 - Fax +39 0422 861 901
E-mail: export@elettronicaveneta.com
www.elettronicaveneta.com