ADF Mühendislik

FCU 100V UÇAK TÜRBİN YAKIT SİSTEMİ EĞİTİM SETİ (5 TANK – 2 MOTOR)

Designed to represent a complete aircraft fuel system, Model FCU – 100 Turbine Fuel System Training Set enables trainees to learn the essentials of fuel system components and how these components are linked to each other in a typical aircraft fuel system.
This trainer includes a capacitance fuel system that shows non-linear fuel quantity indications with multiple probes set at various angles. It comes fully plumbed and with a wing tank.
This completely functional fuel system consists of a fuel management panel, fuel transfer system and capacitance fuel quantity indicating system. It also contains an instructor’s panel that makes it possible to add faults to conduct troubleshooting training.
The fuel system panel features fuel quantity indicators, a fuel transfer selector valve, fuel transfer and low fuel warning lights, fuel pressure and flow indicators and complete fuel system drawings.
This system contains, engine driven fuel pump, screen, fuel filter, fuel control unit, system sensors, fuel dispenser system turbine fuel nozzle inside a clear enclosed container etc.

Features:

Understand fundamentals of aircraft fuel system and its components.
Fully functional and configured like a typical aircraft fuel system.
Aircraft fuel system can run automatically and manually.
Fuel tanks are automatically filled and when tank is full system is automatically be shut off.
The control of the fuel that flows to combustion chamber can be observed using the throttle lever.
Some of Trainer Functions
- Mode selector auto/manual function
- Cross feed function
- Pump’s fault function
- ECAM functions
- Single chime functions
- Master caution functions
- Master warning functions
Some of Trainer Processes
- Fuel transfer process
- Refueling process
- Defueling process
- Bonding process
Some of Trainer Cases
- Inner cell full
- Slat extended
- No engine starts
- Center tank low level
- Wing tank full
Fuel dispenser unit and its equipment
Bonding equipment
Aircraft fire scenario is simulated.
Fuel tanks be manually drained for maintenance.
Fuel tanks have transparent window in order to observe fuel filling and refilling.
Combustion chambers is transparent.
Tanks are able to manually or automatically cross-fit.
The hose and tubes used in the trainer are labeled according to aviation standards.
Wirings on the trainer are connected via terminals.
Wires have clear identification labels for each wire.
All wires are coded and labeled for troubleshooting.
All required hoses and pipes
Instructor’s panel for Fault & simulation Insertion panel (Independent unit)
Components:
Fuel Control Unit
Five (5) pieces fuel tank (2 inner, 2 outers, 1 center)
Six (6) pieces fuel pump
Three (3) Level control switches
Two (2) Combustion chamber
Engine no: 1 Combustion chamber
Engine no: 2 Combustion chamber
Two (2) Nozzle
Throttle lever,
- Dual quadrants
- Dual engine start panel
Two transfer valves
Suction Valve
Fuel filter
Cross feed control valve
Fuel System Pressure sensor for each line
Fuel Level sensor for each tank
Fuel System Flow Sensor
Fuel temp sensor
Hi level sensor for each tank
Two Engine Shut-Off Valve
Three (3) manuals drain valve
Check valves
Refueling panel
- Left hi level
- Center hi level
- Right hi level
- Refuel valves open function
- Refuel valves norm function
- Refuel valves shut function
- Refuel mode selector SW
- Transfer valve indicator
- Test SW
- END indicator
Two (2) Refuel valve
Two (2) Refuel coupling
A refueling dispenser vehicle
Refueling equipment
Bonding equipment
Fuel tanks maintenance hatch
Fuel system control computer
Master warning & caution panel
- Aural warning horn
- Master warning resettable illuminated pushbutton
- Master caution resettable illuminated push button
Control Panel
- Mode selector control illuminated pushbutton
- Mode selector fault indicator
- Cross Feed control illuminated pushbutton
- Left tank pump-1 control illuminated pushbutton
- Left tank pump-2 control illuminated pushbutton
- Left tank pump-1 fault indicator
- Left tank pump-2 fault indicator
- Center tank pump-1 control illuminated pushbutton
- Center tank pump-2 control illuminated pushbutton
- Center tank pump-1 fault indicator
- Center tank pump-2 fault indicator
- Right tank pump-1 control illuminated pushbutton
- Right tank pump-2 control illuminated pushbutton
- Right tank pump-1 fault indicator
- Right tank pump-2 fault indicator
Master power panel
Aircraft circuit breaker
Aircraft circuit breaker lockout
10” inch touchable screen (like EICAS or ECAM)
- Wings & Center tank pumps indications
  - In line
  - LOW
  - Cross line
- Cross feed indications
  - Valve is open
  - Valve is closed
- Momo display
- Fault display
- Transfer valve status
- Fuel temperature indicator
- Re-fuel indication
- Left wing tank fuel quantity indicator
- Right wing tank fuel quantity indicator
- Center tank fuel quantity indicator
- Fuel pressure indicator
- Fuel flow indicator
- Valve status
- Fire status
LAN output
Fault & instructor port
Lockable Fault & instructor box
Terminals

The system mounted on a metal/aluminum mobile stand.
Metal/aluminum frame with 4 wheels. 2 of 4 wheels are lockable.
Training video for teachers
Delivered fully assembled tested and ready to operate
Colored Ultraviolet printing method on aluminum composite panel

Documentation:

User’s Manual
Study Guide
Instructor’s Guide
Components Diagrams
Flow Diagrams

Power Specs

Electrical box
Residual current device
Emergency Button
Energy Signal Lamp
110 VAC 60 Hz or 220-240 VAC 50 Hz