Altitude Temperature (& Humidity) Chamber;Altitude Simulation Cabinet
With the proliferation of more diverse and portable electronic and electrical devices today, devices are being subject to use and storage in complex environments, and evaluation testing is required in those environments.
Combined pressure, temperature, and humidity environments can be reproduced to perform usage environment evaluation and storage evaluation at high altitude for electronic and electrical devices.
Furthermore, this chamber provides a testing environment under reduced pressure. It is perfect for the detection of malfunctions of automobiles for which more electronic components are used during driving at higher elevations and for the evaluation of components intended for use in aircraft.
On Lab Companion's testing chamber, you can set the pressure up to an altitude of 45,000 meters, so you can evaluate operation at low-pressure, low-temperature highlands and evaluate air transport.
Altitude Test Chambers combine temperature and altitude environments with optional humidity for simultaneous environmental testing. An Altitude Chamber allows users to control the test chamber temperature while subjecting the product under test to various levels of altitude up to 100,000 feet, with optional extended altitude range to 150,000 feet. This combination of elements allows precise simulation of real-life conditions a product might encounter at various altitude levels.
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Conformed test standards for aircraft components
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JIS C 8712
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Safety requirements for portable sealed secondary cells
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(UN manual of Test and Criteria , PartⅢ, 38.3.4.1 Test T.1)
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UL1642
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Lithium batteries
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MIL-STD-810C
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Altitude temperature test
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method 504.1 category 4
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JIS W 0812
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Aircraft on-board devices
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(RTCA/D0-160D)
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JIS W 7114
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Electric connector for aircraft
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Conformed test standards for air transport and cabin environment
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JIS C 60068-2-13
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Environment test method (electricity/electronics) Low pressure tests
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JIS C 60068-2-40
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Combined cold/low air pressure tests
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JIS C 60068-2-41
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Combined dry heat/low air pressure tests
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ASTM D 6653, ISO 2873
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Reduced pressure test for filled transport package and unit load
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Other testing standards, and compatibility with system devices
Please contact our sales representatives for more information on the support status for RTCA/DO-160 Section 24 Icing.
Specifications
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Model
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Temperature range
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Humidity range
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Pressure range
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Inner dimensions (mm)
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AT/220/40/L
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-40°C to +100°C
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101.3 to 33.4kPa
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W700×H900×D350
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AT/500/40/L
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W700×H900×D800
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AT/1000/40/L
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W1000×H1000×D1000
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AT/1500/40/L
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W1000×H1000×D1500
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AT/220/40/H
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101.3 to 0.1kPa
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W700×H900×D350
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AT/500/40/H
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W700×H900×D800
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AT/1000/40/H
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W1000×H1000×D1000
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AT/1500/40/H
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W1000×H1000×D1500
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AT/220/70/L
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-70°C to +180°C
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101.3 to 33.4kPa
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W700×H900×D350
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AT/500/70/L
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W700×H900×D800
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AT/1000/70/L
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W1000×H1000×D1000
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AT/1500/70/L
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W1000×H1000×D1500
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AT/220/70/H
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101.3 to 0.1kPa
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W700×H900×D350
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AT/500/70/H
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W700×H900×D800
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AT/1000/70/H
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W1000×H1000×D1000
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AT/1500/70/H
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W1000×H1900×D1500
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AC/220/40/L
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-40°C to +100°C
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20 to 95%rh
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101.3 to 33.4kPa
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W700×H900×D350
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AC/500/40/L
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W700×H900×D800
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AC/1000/40/L
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W1000×H1000×D1000
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AC/1500/40L
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W1000×H1000×D1500
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AC/220/70/L
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-70°C to +180°C
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W700×H900×D350
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AC/500/70/L
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W700×H900×D800
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AC/1000/70/L
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W1000×H1000×D1000
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AC/1500/70/L
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W1000×H1000×D1500
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Pressure & temperature control range
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Figure: Pressure/temperature control range of altitude test chamber (A Series)
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Figure: Pressure/temperature control range of altitude test chamber (A Series)
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Temperature & humidity control range under atmospheric pressure
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AC Type
Temperature and humidity control range under atmospheric pressure
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AC Type
Atmospheric pressure and temperature and humidity control range under reduced pressure
Controllable range of vacuum-temperature and humidity, 93.3 ~ 70.9kPa (altitude 3,000m, 10,000ft)
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* This model supports tests which require the control of temperature and humidity under reduced pressure. We can make suggestions to meet the requirements of customers. Please contact our sales representatives.
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Option
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· The addition of the wall surface control function (3 kPa -1.1 kPa) can expand the temperature/pressure control range to an equivalent altitude of 78,000 ft - 100,000 ft.
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Examples
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· Altitude Temperature (& Humidity) Chamber, Temperature and Humidity Chamber + Precision Air Supply Device
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Specimen: H/V system
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· Equips with high voltage-application terminal
10kV AC
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Specimen: In-vehicle insulation materials
* This specification is for the validation of functional requirements of hybrid automobiles in use at high altitude.
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