Aircraft System Training Equipment, Aircraft System Training Equipment Equipments, Aircraft System Training Equipment Tools, Aircraft System Training Equipment Tool Kits, Aircraft System Training Equipment Manufacturers, Aircraft System Training Equipment Suppliers from India, China, Kenya
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Electrical Fundamentals 1:
Measuring Voltage and Current
Series and Parallel Circuits
Thermo couples
Photocells
Cells and Batteries
Ohms Law.
Electrical Fundamentals 2:
Series/Parallel Networks
Voltage and Current dividers
Resistors in Series and in Parallel
Power in DC Circuits
Kirchoffs Laws
Power Transfer.
Electrical Fundamentals 3:
Capacitors and Electrostatics
Generator Principals
Transformers and their Construction
Inductors and Inductance
DC Motors
Transformer Losses.
Electrical Fundamentals 4:
AC Measurements
Inductance and Capacitance
LR and CR Parallel AC Circuits
LCR Parallel AC Circuits
LR and CR Series AC Circuits
Low Pass and High Pass Filters
Band Pass and Band Stop Filters
LCR Series AC Circuits
Q Factor for Bandwidth.
Tricycle Landing Gear Trainer can be used by students for hands-on training related tolight aircraft landing gears.
The students task may include:
Inspection and maintenance of nose wheel steering mechanism
The Tricycle Landing Gear Trainer is fitted with actual aircraft parts that includes tires,tubes, wheels, dual Cleve and single-disc brakes, nose-wheel steering mechanism, brake pedals, dual brake-fluid reservoirs, master cylinders and hydraulic plumbing for the brakes.
Shock strut inspection and maintenance
One of the three shock struts has a cutaway to expose the internal mechanism, while the other two are complete, and functional shock struts.
Shock strutd is assembly and reassembly, and Hydraulic brakes inspection and maintenance.
Dimensions: 48L x 48W x 64H inches.
The heat exchanger system is a fully functional Air Cycle Machine (ACM) , driven by simulated turbine-engine bleed air, representing atypical system in a modern turbine engine powered aircraft.
System Components:
The trainer includes the following components:
Primary and Secondary Heat Exchangers
Water Seperator
Air cycle machine (ACM)
Temperature sensor
Temperature control valves
Over Temp Sensor
ACM bypass valve
Cabin ventilation blower
Lag chamber
Simulated bleed air source
Digital display of the temperatures of the cabin chamber,bleed air, and ambient air controller.
Dimensions:
72 L x 35 D x 72 H Inches.
Air-conditioning and Heating system trainer is a fully operational model of a typical light aircraft air-conditioning and heatingsystem. The trainer also allows the students to troubleshoot various faults induced by the instructor. All components are actual aircraft parts, and it allows the instructor to fully demonstrate the operation of the various system components.
System Features:
Vapor Cycle Compressor
Fuel tank and associated plumping
Fuel pump and associated electrical components
Compressor Motor
Thermal Switch
Combustion chamber
Ignition system components
Control Valves
Air Blower and associated ducting
Panel mounted control panel
Receiver Dryer
Condenser
Regulating valve
Thermal control switches
Product Features:
Highlights
Fully labeled electrical wires
Durable powder coating finish
System operates on 110/220V AC and 24VDC
All components are mounted on steel frame with full swivelcasters and brakes
Dimensions: 80 L x 30 D x 80 H Inches.
This fully functional trainer incorporates a pneumatic wing de-ice system using a vacuum/pressure ejector boot control valve and pressure switches. An electric motor driven vacuum pump provides system pressure and suction. The Aircraft Ice & Rain Protection and Control System Trainer incorporate all aspects of de-icing and rain protection system found in an aircraft. Propeller deicing is done with an electrically heated propeller boot. A timer control operates the cycle of the propeller de-ice system. Windshield heating is done through internally built heating elements. The trainer offers the opportunity to the students to physically see the various components and assemblies of the system and to understand the interaction between them.
System Features:
Aircraft components and assemblies
Six separate sub-systems
Actuator
Wiper Arm and Wiper Blade
Windshield Heating System
Windshield Wiper System
Windscreen Wiper
Motor
Windshield with heating elements
Temperature Control Thermostat
Sprayer
Flow regulator
Pitot Tube with electrical heating elements
Windshield De-Icing (Alcohol Dispensing)
Alcohol Tank
Alcohol Pump
Propeller De-Icing System
Prop Slip Ring
Ammeter
De-ice Indicator
Electrically Heated
De-Ice Timer
Brush Block
Propeller Blade with De-ice Boot
Regulator valve
Suction Gauge
Pneumatic De-Ice Boot System
Vacuum pump
Filter assembly
Control valve
Boot Pressure Gauge.
Components:
DC Power Switch with indicator light
Master Power Switch with indicator light
Solder-tail aircraft connector
Audio alarm
Circuit Breakers
DC power buss
Relays
Switches
Terminal strips
Voltmeter
Ammeter
Indicator lamps
Power Requirement: 110V AC or 220V AC
Dimensions: 18 L x 18 W x 10 H inches.
The system is laid out to depict a typical aircraft electrical system, and contains standard aircraft components and wiring. This is a complete functional simulation of adual-engine 28 V DC electrical system of a typical turbine aircraft. The aircraft electrical system trainer is an ideal resource to teach about an aircraft multi engine electrical system. By using this trainer, students not only learn the functionality of each component, but they also develop logical and systematic approach to perform troubleshooting tasks.
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The Landing Gear Mechanism Trainer includes all assemblies and components of the standard hydraulically operated landing gear system. Two types of trainers are available; comprises of three wheels comprising two main landing gears and one nose gear, and has one wheel. The Landing Gear Mechanism Trainer is very valuable equipment for the hands-on training for aircraft maintenance training schools. Trainer is a very effective hands on training system for landing gear system. Both models depict the landing gear mechanism as found in actual aircraft. The model is mounted on a move able stand to facilitate easy positioning of the trainer for a clear view from all directions. It is essential to ensure that trainees not only understand the theory but they are also well prepared to maintain the landing gear system in the best possible manner, and in compliance with the prevailing safety standards.
Features:
1-Tire Assembly
Filter
Fluid Reservoir
Actuating Cylinder
Wheel
Tires
2-Hydraulic Brake Components
Fluid Reservoir
Brake Assembly
Master Brake Cylinder
3- Hydraulically Operated Landing Gear
Electrically Driven Hydraulic Pump
Relief Valves
Emergency Hand Pump.
The trainer is manufactured using fully functional aircraft components. Due to the close proximity of all the components, students can comprehend how the total system works and how the interaction between various components regulates the cabin environment. The Cabin Pressurization System simulates the function of a complete aircraft cabin atmosphere and pressurization control system. The trainer has two sealed chambers simulating altitude and cabin pressure. The cabin chamber simulates the pressurized aircraft cabin, and contains cabin components. The vacuum chamber can simulate altitude up to approximately 22,000 ft. above the mean sea level.
System Features:
Pressure monitored in cabin chamber
Altitude controlled in vacuum chamber
Operates from115/ 220 VAC electrical power
24 VDC power supply included
Differential controller
Rate of climb indicator
Aircraft components
Cabin pressure sensor
Altimeter
Cabin pressure chamber (cabin simulator)
Vacuum chamber (altitude simulator)
Cabin dump valve
Regulating valve
Regulator(simulates air to cabin).
The Anti skid Brake System Trainer includes standard hydraulic brake system plus the anti skid assemblies and components. The system is designed to meet or exceed the FAR requirements for instruction on aircraft anti-skid braking system. The Anti skid braking system is an essential part of a modern jet aircraft. There is a definite need for training aircraft maintenance technicians in this area. Our Trainer is an effective hands-on training system for anti skid braking system. Hands-on training is the only effective method of training to ensure that trainees not only understand the theory but they are also well prepared to maintain the anti skid braking system in the best possible manner.
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Features:
Fire warning horn with latching horn-silencing relay switch-found on large transports
Continuous-loop temperature sensor and control box
Control unit
Loop detector
Fenwall spot detector
Smoke Detection System
Fenwall spot detector sensor hybrid into the fire detection alarm system.
Fire warning lights
All electrical wires marked with ATA codes corresponding to the electrical schematics provided.
Electro mech guarded and unguarded switches and lights
Resetable Discharge Indicator
Press-to-test illuminated switch wired to reset the system after discharge
Guarded fire extinguish discharge illuminated switch
The alarm system is the same as found in all single-engine through four-engine transports
Complete full color operations manual.
A simulated flight control surface is operated to demonstrate the principle of hydraulic-actuated flight controls. This is a complete standalone trainer designed such that each component can be removed, overhauled, reinstalled, and functionally tested. The Hydraulic System Trainer provides hands-on training to the students so that they could understand the function, identify components, and troubleshoot a fully functional hydraulic system.
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This display may be used for demonstration and for hands-on training assignments for the students. The nose gear is mounted on a sturdy steel frame, allowing full access to the landing gear.
Features:
1-Tire Assembly
Shimmy dampener
Nose steering mechanism
Shock absorber
Taxi Light
Oleo strut
Dimensions: 36 L x 32 D x 50 H inches
Aircraft Brake System Trainer is a training aid that displays two functional brakes representing multiple-disk brake and single disk brake. The trainer also demonstrates the functionality of parking brakes. The system is mounted on a display stand with caster wheels for easy mobility. The system includes Master Cylinder,Reservoir, Parking Brake Valve, and a Selector Valve which allows the selection of any of the two brakes for operation by the Brake Pedal. The students can be taught how to bleed the brakes. Also, the instructor can explain the procedures for the maintenance of brake system.
Features:
Ergonomic design
Hydraulic Reservoir
Parking Brake Valve
Master Cylinder
A complete and functional single-disk brake system.
A complete and functional multiple-disk brake system
Selector Valve to choose one of the two brakes for operation / demonstration
Dimensions: 32 Wide x 19 Deep x 48 High.
