This versatile kit is part of a series that allows manyexperiments using different arrangements of their parts. Students test a universalcoupling, a belt drive and a chain drive to see how they work and how theydiffer in the way they transfer motion. The kit introduces students to key engineering terms such asgear ratio, pulley ratio and efficiency. The kit includes extra parts to helpshow the importance of the angle of lap around a pulley and its relationshipwith friction. Students, teachers orlecturers fit the parts of the kit to the Work Panel to study or show anengineering science topic. This kit includes three different drive systems toshow their relative advantages and disadvantages. The selection of parts in the kits and the choice of fixing points on the Work Panel that teachers or lecturers may extend the experiments to an even greaterrange. It includes all the worksheets, guidancenotes and lecturer notes needed for typical experiments with each kit.
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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.
Three degrees of freedom instrument panel permits full demon stration of attitude and directional gyro functions. The Cockpit Instrumentation System with Electronic Flight Instruments and electronic engine display.
Standard Features:
Functional engine monitoring system connected to engine sensors
Provision of engine sensor simulation
Functional digital primary flight display mounted on a panel that can simulate roll,pitch, and yaw movements controlled by a mechanism operated by a control yoke.
Functional pitot- static system with provision for conducting pitot static system checks
Standby Instruments installed.
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.
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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Set of winter clothing for child aged 5 years.
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Vaccine storage capacity: 72.5 L
Refrigerant: R600a, 45 grams
Volume category: >/= 60, <120L
Energy consumption, stable running (kWh/24 hours): 1.47
Equipment operating voltage and frequency: 220-240 Volt, 50Hz/60Hz or 100-127 Volt 50Hz/60Hz, 1ph.
Operating temperature: Min and Max rated ambient temperature: +10 C and +43°C
UIFPF- Grade A
Prequalified Intermittent Mains Powered Refrigerator for storage of vaccines at +2 ?C to+8?C.
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.
Remote Temperature Monitoring (RTM) system for real time monitoring of storage conditions at different levels of the vaccine cold chain: (a) with data access, setup of alarm thresholds and setup of alarm recipients through internet accessible dashboard (b) capable of alarm notifications via SMS, email and/or iOS & Android mobile applications (c) with automatic transmission of data to a server (d) with integrated audio-visual alarm (e) configurable to suit specific applications and scalable to allow for the later installation of additional temperature monitoring products and/or storage facilities.
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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.
Container, round.
Smooth surface.
Material: Austenitic stainless steel.
Austenitic stainless steel composition: 18 - 20% chromium, 8 - 10% nickel.
Reusable.
Capacity: approx. 4 litres.
Internal diameter: approx. 300 mm.
Height: approx. 100 mm.
Thickness: approx. 0.8 mm.
Newborn resuscitation and support of transition of infants at birth. Additionally, used to provide thermal support for newborns in the delivery suite and for critically ill infants who require constant nursing intervention. Mobile resuscitation table for neonatal patients equipped with a radiant warmer and supplied with accessories.
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Drum, sterilizer.
Air vents system to allow steam to circulate freely during the sterilisation cycle.
Lateral air vents system is preferable to top and bottom air vents.
Closing lid with a clip lock.
Material: Austenitic stainless steel, smooth surface.
Carrying handle.
External diameter: approx. 280 to 290 mm
Height: approx. 160 to 180 mm.
Thickness: approx. 0.6 to 0.7 mm.
Austenitic stainless steel composition: approx. 8-10 % nickel, 18-20 % chromium.
Reusable.
Material: Martensitic steel (quenched, magnetic steel).
Martensitic steel composition: 0.16-0.40 % carbon; 13-14 % chromium.
Blade shape: Oval, fenestrated.
Blade edge type: Sharp.
Uterine curette.
Shank type: Rigid.
Reusable.
Length: Shaft 26 cm.
Width: Spoon 9 mm.
