Cylinder length 200mm, diameter 22.5MM diameter.
The suction nozzle diameter 9mm.
Limit the suction pressure is less than 6.7 * 103Pa (50mmHg).
It is a portable instrument for collecting samples in the atmosphere, such as: sulfur dioxide. It has accurate sampling time by using MCU control technology and it can directly observe sampling time and greatly improve original sampling time accuracy by using highlight Digitron display.
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The Air-to-Water Heat Pump Operation Training Bench Unit is designed to allow students to gain both practical and theoretical knowledge of the operation of heat pumps.
The Air-to-Water Heat Pump Operation Training Bench Unit has been designed and manufactured to incorporate all current safety standards.
The refrigerant used complies with anti-pollution legislation.
An Air-to-Water Heat Pump Operation Training Bench for studying the use of heat pumps to transfer heat from one source at a certain temperature to another source at a higher temperature.
Experiments:
Plant start-up and system monitoring using the protection and safety devices incorporated into the training bench
Studying the operation of a heat pump.
Analysing system behaviour and reactions with the variation of:
Plotting the refrigeration cycle on a p-h diagram
Air flow rate at the evaporator
Water temperature in the tank
Thermostatic valve superheat.
Obtaining data readings and calculation of:
Ideal and actual coefficient of performance (C.O.P.)
Volumetric compression efficiency
Heat balances for the evaporator, condenser and compressor
Refrigerant mass flow.
It is a teaching experimental instrument of physical mechanics, used with digital timer and small air source. It can be used for classroom demonstration experiment and student independent experiment.
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The unit is supplied with manuals which describe all parts of the unit, the installation and utilization procedures, as well as many exercises with experimental results. The Air water Heat Transfer Apparatus allows to perform several experiments relevant to the thermal exchange phenomena connected to convection and conduction and some interesting experiments on fluid dynamics. In particular, it is possible to study the thermal exchange between a gas (air) and a liquid (water) and the thermal exchange between an air flow rate in a forced motion and a wall at different temperature.
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This allows working with original manufacturer documents and circuit diagrams. These components are exposed for easy access. Standard diagnostic testers can be connected via the OBD interface. The training model consists of all the original components of a Golf V airbag system. The connections of all functionally relevant sensors and actuators and the control units andcomponents are original connections as in the vehicle. The training equipment contains non-ignitable airbags and belt tensioners. Thus, asafe handling and troubleshooting is possible.
Characteristics:
Originalcomponents: Airbag control unit, Driver airbag, Coil spring, Steering columnelectronics, Passenger airbag, Side airbag, Crash sensor for front and rearside airbag, Instrument cluster with indicator lamps, Belt pretensioner fordriver and passenger, Belt buckle for driver and passenger with belt buckleretainer, Passenger seat occupancy recognition (for belt check), Switching off the passenger airbag via key-switch, OBD Diagnosis connection.
Aluminum frame profile on castors with extra-large tabletop, control panels, OBDconnector
Fully functional airbag training model, original components VW Golf 5, specially prepared for training purposes.
Airconditioner (1Hp Split Type, Inverter/ R410a), Airconditioner (1Hp Split Type, Inverter/ R410a) Equipments, Airconditioner (1Hp Split Type, Inverter/ R410a) Tools, Airconditioner (1Hp Split Type, Inverter/ R410a) Tool Kits, Airconditioner (1Hp Split Type, Inverter/ R410a) Manufacturers, Airconditioner (1Hp Split Type, Inverter/ R410a) Suppliers from India, China, Kenya
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Aircraft quality electrical shielded wiring, cables, connectors, and harness assemblies and easily removable AD Fantenna with coaxial cable connections. All interconnections are of aircraft quality electrical shielded wiring, cables, connectors, and harnesses. Aircraft Automatic Direction Finder Equipment Trainer is designed to provide hands-on training on a real and operational equipment approved for aircraft installation. Using Avionics Instructors can effectively teach students on installing, removing, and testing an ADF unit. Students also develop proper understanding and learn how to trouble shoot the ADF equipment. The equipment is mounted on a mobile workstation containing air craft ADF unit, ADF indicator, and ADF loop and sense antenna assembly package. The work station includes a test panel console for bench testing of ADF equipment.
Features:
Durable,steel frame, Vertical standing panel with sturdy casters
Adjustable height test panel
ADF Indicator
Wood shelf
Accessories storage case
Adjustable height equipment panels
Avionics panel, complete with Allied Signal KX 155 with Indicator
Aircraft Antenna mounted on rotating machanis
Power Supply with voltage and current meters, power cord
Installation and mounting kit.
The Attitude Director Indicator (ADI)provides a consolidated and easy-to-read display of aircraft roll and pitch attitudes and command bugs. The Horizontal Situation Indicator (HSI) to provide a consolidated display to a pilot for more efficient cockpit resource management. All modern military and commercial aircraft are equipped with autopilots for automatic flight control, and Horizontal Situation Indicator (HSI) for navigational information presentation to the pilot. All wire harnesses are routed through terminal strips to enable students to measure and monitor electrical signals, and to troubleshoot the instructor induced faults. The equipment is mounted on a mobile workstation containing Horizontal Situation Indicator, with bootstrap Directional Gyro, Flux Valve,Slaving Accessory, ADI, and a simulator box to generate all other required signals needed by the system.
Functional Description:
Magnetic Heading and course information from VOR/LOC, and GPS is combined on the HSI.
Remote mounted compass system consisting of Pictorial Navigation Indicator, Remote Directional Gyro, Magnetic Azimuth Transmitter, simulated NAV signals unit, and Slaving Accessory. The ADI system comprises of vacuum driven attitude gyros,and simulated autopilot deviation signal unit. The HSI also provides outputs for autopilot or flight director, OR receivers, and additional compass loads. The HSI provides a pictorial display of the horizontal navigation situation and also provides manual controls for course and heading datum selection. It includes dual glide-slope pointers which are in view during a simulated ILS approach.
Features:
Durable,metal frame with sturdy casters
Control Yoke operated roll, pitch, and yaw simulation
Installed units are actual aircraft equipment
Fault insertion module
Simulated NAV inputs
Interface trainers
CBT included.
It has a modular design. It may be installed and operated as a roll axis only autopilot, roll and pitch axis, or a roll, pitch, and yaw axis autopilot. Autopilot Trainer is based on a Century 2000 Autopilot. The advanced design provides very smooth and precise corrections in aircraft attitude. Theflexible design provides the economy of expand ability. The complete Century 2000 is a true 3-axes, flight director/autopilot.
System Components:
Roll Axis Control
The complete roll axis autopilot features continuous roll/NAV/voltage monitors, heading select, heading hold, NAV, /LOC/BCanticipative intercept and track automatic soft track, about 45 degree intercept and all angle intercept with HSI.
System Components:
Directional Gyro/Indicator
Roll Servo
Autopilot Computer/Control Unit
Attitude Indicator / Flight Director
Moveable Control Surfaces
Turn & Slip Indicator
Altitude Pre-selector
Autopilot Annunciator
Rate of Climb Indicator
Altitude Sensor
Yaw Servo
Pitch Servo.
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.
The Aircraft specification describes how an avionics system transmits information over the unidirectional data bus to other system elements. The Trainer is complete and comprehensive equipment to prepare aircraft maintenance engineers and avionics engineers to understand and maintain modern aircraft. Aircraft specifications define the standard for transfer of digital data between avionics system elements. Aircraft standards are used on virtually all commercial aircraft.
The Aircraft data words define the units, ranges, resolutions, refresh rates, number of significant bits, padbits, etc. for the words transmitted by the different avionics system elements. Trainer simulates signals at two speeds. Words are 32 bits long including a label, parity bit and other fields. The software installed on the trainer is an intuitive, graphical data bus analyzer that simplifies the simulation of Aircraft based avionics systems. The use of this model does not require programming expertise, and trainees do not need to write software programs. All they need to do is consult the comprehensive training manual provided with the trainer, to understand the various menu options. The user-friendly MS Windows-based interfaces allow transmission and reception on data buses with just a few clicks of the mouse. Then, while the bus is running, data and bus activity can be observed in meaningful engineering units, and can be changed on the fly.
Hardware:
The hard ware utilizes a rack-mount PC, 17-inch LCD TFT monitor, ARINC 429 interface, laser printer, instructors panel, patch panel, and power supply unit. The equipment is installed in two 19-inch racks of 18U height.
Aircraft Distance Measuring Equipment (DME) System Trainer is designed to provide hands-on training on a real and operational equipment approved for aircraft installation. The trainer includes aircraft quality electrical shielded wiring, cables,connectors, and harness assemblies and DME antenna with coaxial cable connections. The equipment is mounted on a mobile workstation containing air craft DME unit with built-in indicator, and DME antenna, and a test set. The trainer includes a test panel console for bench testing of DME equipment.
Features:
Durable,steel frame, Vertical standing panel with sturdy casters
Built-in DCP ower Supply
Simulation of Distance, and Speed
Avionics panel complete with Honeywell DME with built-in Indicator for distance, speed,and time
Accessories storage drawers & cabinet.
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
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 GPS trainer provi desin-depth knowledge and hands-on experience to maintain and troubleshoot GP S equipment. A fault panel lets the instructor insert commonly encountered faults so that trainees can learn how to troubleshoot and repair the GPS equipment in actual situations. GPS has become an indispensable aid for airborne, land and marine navigation. Correct usage and effective maintenance of GPS equipment require a good knowledge of GPS principles, operation and equipment circuitry. Optional system components may be added and interfaced to the system which increase its features and capabilities. Some of these optional components include an external course deviation indicator (CDI) or horizontal situation indicator (HSI), autopilot, and external annunciators. The GPS Trainer equipment consists of a panel mounted IFR- approved GPS receiver, a GPS antenna, and a GPS signal simulator. Asimul at or for altitude input is included to provide full navigation and operational capabilities.
GPS Functional Features:
Panel-mount IFR GPS capable of performing GPS approaches
Eight- channel parallel GPS receiver
Direct- To feature for easy navigation
Easy-to-readmap display
Comprehensive Jeppesen database
Altitude input for increased accuracy
Database can store up to 500 user-defined way points along with user comments for up to 200airports
Capable of B- RNAV compliance.
Can beinter faced to external CDI or HSI, RMI, fuel management system, external moving map display, and air data system
Operates on any voltage 11-33Vdc.
The trainer includes secondary radar equipment, and radio navigation equipment. The may be upgraded with the optional feature to include satellite navigation(GPS). The Aircraft Navigation Systems Trainer consists of fully functional aircraft navigational equipment used in a typical general aviation aircraft. The trainer is a realistic mock-up of aircraft navigational systems with functions and capabilities that facilitate the following aspects of hands-on training:
Test the equipment using simulated navigation/flight data in compliance with standard technical procedures.
The emphasis in design is to allow the students gain hands-on experience.
Conduct practical training for flight line tasks like physical removal, installation, operation, and maintenance testing by using ramp tester.
Perform diagnostic testing as done in an avionics maintenance shop, using real time navigation transmission and reception with aDME/Transponder bench test set.
The engine is operated from a semi-enclosed test cell cabin that has all the necessary instrumentation and controls to run the engine. The trainer comes complete with an operational piston engine. The engine is connected to propeller assembly including spinner and governor. The engine trainer may be mounted on wheels for easy mobility as shown above. The engine is mounted with all necessary electrical wiring, engine accessories, controls, and instruments that are needed for running the engine. The students may also be trained to remove and replace parts for field level maintenance practice. For fixed installations, the trainer is provided with heavy duty vibration and shear mounts to absorb vibrations, as shown below.
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Aircraft Propeller Trainer comprising a three blade propeller mounted on a free standing fixture. The range of propeller blade movement is demonstrated by the application of air pressure. The propellers are mounted on a moveable stand. The trainer equipped with a constant speed, feathering and reverse pitch propeller.
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Air craft Radio Altimeter System Trainer is a fully functional radio altimeter system comprising of actual airborne avionics equipment. They are also abbreviated as Rad. Alt. in avionics terminology. The terms Radio Altimeter and Radar Altimeter are used interchangeably and essentially mean the same.
The Radio Altimeter System Trainer is comprised of the following items:
Bench-mounted mobile workstation
Radio Altimeter Tx and Rx Antennas
Radio Altimeter Transmitter/Receiver
Radio Height Indicator
Test Set Antenna Couplers, qty. 2
Test Set
Power Supply
All necessary wiring harnesses
Features:
Solid-stat eRadio Altimeter Receiver/ Transmitter Unit
Digital altitude processor for long, drift-free operation
Rugged,die-cast construction of the Receiver/Transmitter Unit
Radio Altitude Indicator
Operates on28 volt DC power
Has serial digital output for use by other avionics equipment like FMS and Autopilots
Self test to enable rapid verification of proper system function
Standard radio altimeter antenna used in general aviation aircraft
Adjustable Decision Height function provided to alert pilot via lamp and aural tone that the aircraft has descended to a selected altitude
Aircraft in the air simulation
Fixed, linear variable, and flight profile altitude simulation
Aircraft on Ground simulation
Para metrictesting functions.
