Current research projects

Image Investigation according to DIN EN ISO 14903
Image All-in-one device for freeze-drying and production of biomaterial
Image Cryostats, Non-Metallic and Metallic
Image Low Temperature Tribology
Image Combined building and system simulation
Image Development of a Cryogenic Magnetic Air Separation Unit
Image Hydrogen and methane testing field at the ILK
Image 3D - Air flow sensor
Image Thermal engines
Image Cool Up
Image Behavior of multiphase cryogenic fluids
Image In-Situ-Swelling Behaviour of Polymer Materials in Flammable Fluids
Image Panel with indirect evaporative cooling via membrane
Image Industry 4.0 membrane heat and mass exchanger (i-MWÜ4.0)
Image Brine (water)-water heat pump
Image High temperature heat pump

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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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Investigation of materials

Investigations regarding the compatibility of materials with refrigerants, oils and heat transfer fluids

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Non- invasive flow measurements

PDPA - flow fields and particle sizes

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Computational fluid dynamics CFD

Scientific analysis of flows