Aircraft Cabin Pressurization Trainer
Product Code : EDS-AT-15054
Eduscope India is a leading Aircraft Cabin Pressurization Trainer
Description :
The Cabin Pressurization trainer demonstrates how an aircraft cabin pressurization and air conditioning system function.
The compact construction of the set allows trainees to conceive the system as understanding the connection between the various parts of the system in regulating the cabin environment.
The trainer includes two chambers simulating altitude and cabin pressure.
The vacuum simulating chamber is able to simulate up to roughly 0 - 40,000 ft.
Features :
Understanding fundamentals of aircraft Cabin Pressurization and its components.
The set is functional and configured like a typical aircraft Cabin Pressurization system.
The trainer include the following panels that will work functionally.
Aircraft Cabin Pressurization panel
Aircraft air condition panel
Aircraft auto-pilot panel
Test panel
Master power panel
Master caution panel
Two transparent cabin in the training set to simulate the interior of the cabin.
2 outflow valves, 1 negative pressure safety valve, and positive pressure safety valve (as a substitution) are in the transparent cabin.
Out Flow Valves are engine controlled.
The valves in the cabin pressurization system operate automatically during the take off and landing.
Cabin pressurization valves are both controlled manually and automatically.
The trainer is able to perform full automatic take off and landing.
Indicators, panels and valves work simultaneously in landing and take-off simulations.
Take off and landing simulations are controlled from the autopilot panel.
Vertica speed and altitude are determined and selected during take-off and landing.
Valve failures are easily observed on gauges and panels.
PACK, BLEED, PACK FLOW and TEMPERATURE selections are made at the air condition panel.
LDG elevation, MODE SELECT, MAN V/S CONTROL and DITCHING are done at the cabin pressurization.
The selections made in the panels are visible on the screen.
Wirings on the trainer are connected via terminals.
Wires should have clear identification labels for each wire.
All wires should be coded and labeled for troubleshooting.
Instructor’s panel for Fault Insertion
The system mounted on a metal/aluminum mobile stand.
Metal/aluminum frame with 4 wheels. 2 of 4 wheels are lockable.
Colored Ultraviolet printing method on aluminum composite panel
Components :
Heat Exchanger
Muffler
Relief Valve
Shut-Off Valve
Vaccum Pump
System Indicators
PSU( Passenger Service Unit)
10 inch Lower ECAM
Vertical speed indicator
Altimeter indicator
Cabin Altimeter
Cabin pressure
Air pressure
Differential pressure
Status area
Flow status
Pack flow status
Bleed status
Auto pilot status
Pressurization mode
Temp
Air/ground
Min 2 Outflow valve
Min 2 outflow control computers
Aircraft Cabin Pressurization panel
Man V/S Control Switch
Mode selector
LDG ELEV Knop
Aircraft air condition panel
Pack-1 control
Pack-2 control
ENG 1 Bleed
ENG 2 Bleed
APU Bleed
Pack Flow Selector
Aircraft auto-pilot control panel
Vertical Speed Selector
Altitude Knop
Control Siwitch
Terminals
Master power panel
Master power light
Master caution panel
Aural warning horn
Test panel
Circuit Breakers,
LAN output
Fault Panel for instructor.
Outflow valve control boxes
Outflow valve terminals
Vacuum chamber (altitude simulator)
Cabin pressure chamber (cabin simulator)
Regulator (simulates air to cabin)
Cabin pressure sensor
24 VDC power supply
Power Specs :
Electrical box
Residual current device
Emergency Button
Energy Signal Lamp
110 VAC 60 Hz or 220-240 VAC 50 Hz
