Capacitance fuel quantity fuel system comes with awing tank and all associated plumbing. This functional fuel system is designed to represent a complete turbine engine fuel system. It includes a fuel management panel, fuel transfer system and capacitance fuel quantity in dicating system. Turbine Fuel System Trainer is specially designed to allow trainees to understand the fundamentals of turbine fuel system components and how they are inter connected in a typical aircraft fuel system. An instructors panel is included allowing faults to be added to assistin teaching troubleshooting. The fuel system panel includes 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. The system is mounted on a mobile stand. This completely functional Turbine Fuel System Trainer includes a capacitance fuel system, with multiple probes set at different angles to demonstrate non-linear fuel quantity indications.
Features:
Fully functional and configured like a typical turbine engine aircraft fuel system.
Training manuals including troubleshooting charts, explanatory text, symbols charts,wiring diagrams, flow schematics, and component cut-away diagrams.
Includes over head transparencies and laminated fuel system drawings.
Instructors panel for introduction of usual system faults and errors Aircraft hydraulic cylinder sequenced by a sequencing valve
Designed with aircraft parts
Works with 28 volt DC power or with an APU.
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.
Designed for the reduction of test samples which are too large in volume to be conveniently handled. Complete with two collecting pans. Clam shell hopper: 30 litres capacity. Very sturdily constructed, it is totally Cadmium Plated for rust protection. It handles any material from Sand sizes up to diameter 108 mm. Each Chute bar is 12 mm wide so that openings of 12-24-36-48-60-72-84-96-108 mm are possible.
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The Fluid Science Energy Losses in BendsSystems Tray provides hands on experimentation designed to demonstrate energylosses due to the geometry of the flow path at different flow rates.
Differential pressure reading is takenusing a digital manometer against varying flow rates.
Utilising the service unit theexperiments rapidly mount onto the multifunctional work panel and is connectedto the built-in water supply via quick connect couplings.
The tray includes the following Hydraulic Circuits:
Energy losses in Bends
Mitre Bend, 6mm diameter.
Shallow bend Radii 75mm, 6mm diameter
Tight Bend Radii 25mm, 6mm diameter.
Internal pressure is applied to the cylinder by mean of a hydraulic hand pump. Pressure in the cylinder is indicated on a pressure gauge. A hand screw is attached to one end of the frame to operate a piston on one side of the cylinder. Thin Cylinder Experiment is used for studying the stresses in a thin wall cylinder. The strain gauges are fixed onto the cylinder at different angles. Each strain gauge is wired to form a full bridge with temperature compensation gauge and zero adjustment in a bridge box with strain gauge indicator. A thin wall aluminum alloy cylinder is mounted on a rigid steel frame. By applying the hand screw, only circumferential stress occurs on the cylinder or both circumferential and axial stresses occur.
Experiments:
Measurement of strains and stresses under internal pressures.
Comparison of theoretical stresses and strains with experimental values.
Determination of Youngâ„¢s modulus an Poissons ratio.
Rectangular mosquito net, polyethylene 120-150 DENIER, treated with WHO PQ qualified insecticide, color white/blue/green, dimensions 180 x 160 x 150 cm (length x width x height) +/-5%.
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Intended use:
Applicable for molecular/PCR & sterile microbiological works.
Various clinical laboratory usage conditions including; Sample cold storage, sample preparation/extractions with water bath, incubator, and centrifuge.
Mixing of reagents in bottles, flasks and beakers in horizontal orbital motion.
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Used for multiple techniques to accurately dispense required volumes of liquid
8-channel, adjustable pipetting volumes 5-50ul
Manual air displacement micropipette
Compatible with universal fit pipette tips ranging 5-50ul
Autoclavable, and Resistant to UV sterilization
A handle with digital setting and read-out of delivered volumes
Built-in tips ejector
Sturdy and chemical resistant parts.
Used for multiple tests.
Heparin coated internally
Capillary glass tube
Length approx. 75 mm
Diameter approx. 1.2 mm
Seal-packing of smaller units (such as 100 tubes).
Set of winter clothing for child aged 5 years.
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Icepack with screw cap
Capacity: 0.6 litres
External dimensions: 190 x 120 x 34mm, +/- 2mm
Water content: 0.55 to 0.6 litres
Removable cap, with internal water seal to prevent leakage.
Filling line indicated on one side.
Walls to be reinforced to prevent swelling.
Supplied empty.
Vaccine storage capacity: 57 L
Volume category: <60L
Solar radiation reference period of 3.5 kWh/m²/day and hot zone (+43°C) test temperatures.
Refrigerant: R600a, 100 grams
Operating temperature: Min and Max rated ambient temperature: +5 °C and +43°C
UIFPF: Grade A
PQS prequalified Solar direct drive combined refrigerator and freezer with no battery for storage of vaccines at +2?C to+8?C and freezing of ice packs in areas without any electricity, or where there is less than eight hours of reliable electricity over a typical day.
Capacity: 598L
Cabinet Type: Upright
Volume Category: ≥ 300 <600L
Power requirement: 230V /50Hz and upon request 220V/60 Hz
Operating ambient temperature: +10 °C to +43°C (Hot zone)
Storage temperature: up to-86°C
Adjustable cabinet temperature set point -40°C to -86°C in 0.5°C increment., the temperature regulation accuracy is 0.1°C.
The composition of the paper should be homogenous with no inclusions/alien particles and be suitable for a range of art activities(painting, colouring, sticking etc.)
Roll of white, plain (un-ruled) paper, 70 cm wide and 25 m long ,preferably with an internal cardboard tube strengthener. Paper to be 75% recovered paper fibres (post and pre-consumer waste) and of 80 gsm.
Decal, vehicle, permanently adhesive, 1000 x 280mm
Size: Rectangular, length 1000 mm x height 280 mm, with corners in a 90-degree angle.
Material: White gloss PVC, with permanent adhesive; 0.1mm thickness; lifespan 2-3 years from date of delivery; Kraft liner 130 grams.
Color: Background color: cyan blue. The logo printed in white, positioned in the middle of the decal, running 80% of the length.
Hacky Sack or Footbag made from PU material in 6 panels with loose metal filling. The diameter of the Hacky Sack is 53mm.
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Compartment 1:
Inside Pockets:
Two inner pockets; mesh sides with elastic tops, located on the back side of the main compartment.
Large compartment zip closure around three sides of the compartment with a 2 way zip pull. Mesh lining stitched to the base of the bag and a 1mm PVC board reinforcement secured on the base.
Size: H400 x Depth100 x W270 mm.
Compartment 2:
Small pocket H230 x Depth 40 x W280 mm with side gussets, zip closure around top of pocket with one zip pull.
Portable ultrasonic scanning systems are used in physician offices, radiology departments, cardiology departments, emergency departments, critical care units and by mobile imaging service providers. The main benefit of point of care ultrasounds units is that it allows physicians to quickly determine whether an abnormality is present so they can make appropriate patient management decisions. They can also have important applications in disaster triage and mass casualty incidents.
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Full term newborn life-size manikin with realistic anatomical features. Fully articulated head, neck and jaw with tongue. With soft, lifelike skin and moulded hair.
Features: Head tilt/chin lift to open the airway; Realistic chest rise on positive pressure ventilation; brachial artery pulse examination point.
