Current research projects

Image Calibration leak for the water bath leak test
Image Tensile and compression testing
Image High temperature heat pump
Image Electrical components in refrigeration circuits
Image Innovative small helium liquefier
Image Filter Tests
Image Behavior of multiphase cryogenic fluids
Image Certification of efficient air conditioning and ventilation systems through the new "indoor air quality seal" for non-residential buildings
Image Practical training, diploma, master, bachelor
Image In-Situ-Swelling Behaviour of Polymer Materials in Flammable Fluids
Image Ionocaloric cooling
Image Testzentrum PLWP at ILK Dresden
Image Humidifier System for High-Purity Gases
Image Cryostats, Non-Metallic and Metallic
Image Verification of storage suitability of cryo tubes
Image Preformance measurements of heat exchangers

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Low temperature – test facilities

Industry and research instituts

Gunar Schroeder

+49-351-4081-5129

thermal cycling tests at very low temperatures

Parts and components of machines such as satellites or space telescopes are subject to mechanical stress. In addition to the mechanical stress, the temperatures at which these components are used also have an influence on their strength and thus also on their lifetime. In the area of materials research, material aging and especially for space applications with the very high temperature changes that occur in a vacuum, temperature change tests are essential. These tests normally are combined with subsequent strength testing. With the knowledge gained, e.g. how the component strength changes due to extreme temperature changes, the components can be optimally designed with regard to the special requirements for reliability and minimum weight.

A test chamber has been build up at the ILK Dresden specifically for such temperature change tests. With the help of this thermal cycling chamber, parts or components can be exposed to changing temperatures for different durations. The temperatures can be specified in the range of 20 – 363 K for defined time intervals. The temperature gradients, performing the change from the lowest temperature to the highest temperature or reverse can also be specified in a range. Using a programmable electronic control, temperature profiles can be defined and run through in automated test operation over several hours to several days.

Sample limits Parameter
Temperature range 20 K ... 363 K / -253°C ... +90°C / -423°F ... 194°F
Temperature stability ± 1 K
Dimension, length x width 0,95 m x 0,6 m / 3 ft x 2 ft
Mass up to 30 kg / 66 lb

 


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Further Projects

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Characterisation of Superconductors in Hydrogen Atmosphere

Are superconductors really compatible with hydrogen?

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Corrosion inhibitor for ammonia absorption systems

An alternative to chromium(VI) compounds

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Development of a Cryogenic Magnetic Air Separation Unit

Oxygen Enrichment by Applied Cryogenic Magnetohydrodynamics

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Software for test rigs

Individual software for complex tests and evaluation