FIELD: testing equipment.
SUBSTANCE: present invention relates to stands for testing low-pressure axial compressors of a two- (multiple) loop gas turbine engine and can be used to study characteristics of low pressure compressors, as well as their parametric refinement in the course of work on the development of new gas turbine engines.
EFFECT: technical result achieved by using the claimed invention is the possibility of simulating conditions of different modes of operation of the tested compressor as part of two-loop engine in real conditions.
1 cl, 1 dwg
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