ADF Mühendislik

SKT 100V KAYMAZ&OTOMATİK FREN SİSTEMİ İKİ TEKERLEKLİ EĞİTİM SETİ V.2

Our Anti-skid and Auto Braking System trainer is designed to represent the anti-skid braking system that is one of the most essential components of modern jet aircraft.

This training set gains more importance as the need for training maintenance technicians in this area keep increasing. Hands-on training provided by this set ensures that trainees not only comprehend the theory, but they are also well prepared in practice to maintain the anti-skid braking system. Anti-skid and Auto Braking System Training Set includes a typical hydraulic brake system as well as the anti-skid assemblies and components.

This training set contains two wheels.

Features:

Understanding fundamentals of aircraft auto-brake/anti-skid and its components.
Anti-skid and auto-brake system able to work together and independently
Non operations of auto-brake scenario are implemented
Operations of auto-brake scenario are implemented
Take off scenario is implemented
Landing scenario is implemented
Auto-brake scenarios is implemented
Rejected take off scenario is implemented
Some of Trainer Functions
- Auto-brake function
- Anti-skid function
- Food brake function
- Rejected take off function
- WOW switch function
- Brake fan function
- Pump’s fault function
- ECAM functions
- Single chime functions
- Master caution functions
- Master warning functions
Some of Trainer Processes
- Take-off process
- Landing process
- Anti-skid fault process
- System test process
Some of Trainer Cases
- Brake hot
- Park brake fault
- Hydraulic fault
- Auto brake fault
Instructor’s panel for Fault Insertion

Components:

Control Panel
- Aural warning horn
- Master warning resettable illuminated pushbutton
- Master caution resettable illuminated pushbutton
- Auto brake – low illuminated pushbutton
- Auto brake – medium illuminated pushbutton
- Auto brake – max illuminated pushbutton
- Auto brake – RTO illuminated pushbutton
- Auto brake – disarm instrument
- Anti-skid INOP instrument
- Brake fan control illuminated pushbutton
- Brake fan hot instrument
- Nose landing gear instrument light
- Left wing landing gear instrument light
- Right wing gear instrument light
- Landing gear unlock instrument light
- Hydraulic pump control illuminated pushbutton
- Hydraulic pump fault instrument light
- Three (3) aircraft circuit breaker
- Guarded master power switch
- Master power lamp
- Lockable Landing gear control lever
AC engine on/off switch
Air/ground switch
Skid simulation panel
10” inch screen (like EICAS or ECAM)
- Landing gear position
- Landing door position
- Numeric pressure value
- Sensor’s status
- Anti-Skid/Auto-Brake position status
- Numeric Simulated air speed value
Electronic Control Box (Antiskid Control Computer)
Antiskid Valve
TQ – throttle quadrant
Electrically Driven Hydraulic Pump
Hydraulics Filter
Hydraulic Fluid Reservoir
Hydraulics tank Drain Valve
Check valve
Brake fan
0-100 bar Hydraulic System analog pressure gauge
0-100 bar Hydraulic System Pressure sensor
Aircraft landing gear module
- Two (2) pieces Aircraft Tire
- Two (2) pieces Aircraft Wheel
- Two (2) pieces Aircraft Brake system
- Two (2) pieces AC motor for turning the wheels
- Plexiglass cover
Aircraft foot Brake Pedal
Aircraft foot Brake master cylinder
Brake microswitch
Two (2) pieces AC motor for turning the wheels
Two (2) pieces AC motor driver
Fault & instructor port
Lockable Fault & instructor box

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

Power Specs

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

Dimensions and weight

Height: 200cm Width: 140cm Depth: 85cm
Weight: 150kg