Current research projects

Image Test procedures for electrical components
Image Helium extraction from natural gas
Image Range of services laboratory analyses
Image Characterisation of Superconductors in Hydrogen Atmosphere
Image In-situ investigation concerning the swelling behaviour of polymer materials under elevated pressures and temperatures
Image State of system and failure analyses
Image Thermal engines
Image Innovative Manufacturing Technologies for Cryosorption Systems
Image CO₂ GAS HYDRATES FOR SUSTAINABLE ENERGY AND COOLING SOLUTIONS
Image ZeroHeatPump
Image Computational fluid dynamics CFD
Image Test method for high - temperature heat pump - oils
Image Certification of efficient air conditioning and ventilation systems through the new "indoor air quality seal" for non-residential buildings
Image Investigation of material-dependent parameters
Image Multifunctional electronic modules for cryogenic applications
Image Hydrogen and methane testing field at the ILK

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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 - Research and Development

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Filter Tests

INDUSTRIAL AND LABORATORY PRECIPITATORS

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Low Temperature Tribology

Tribological studies at cryogenic temperatures

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Refrigerants, lubricants and mixtures

Determination of working fluid properties

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Reduction of primary noise sources of fans

...using numerical and experimental methods with contra-rotating axial fan

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Micro fluidic expansion valve

for increasing of the efficiency of small and compact cooling units