Measuring device jet engine in conditions of modeling real flight

摘要

The present invention relates to equipment for measuring the jet engine parameters for high speed aircraft in the actual flight conditions. The apparatus comprises a driven, for example, aircraft of the uterus booster controlled advantageously landing aircraft carrier with two diametrically spaced subjects WFD, each mounted on the corresponding face of the bow of the aircraft carrier made knife-like, symmetrical facets and the front length edges, at least equal to the width of the air intake of the test WFD. New essential features of the apparatus are: - execution of the bow of the carrier aircraft with symmetrical faces cultrate; - execution of the front knife-like edge of the bow aircraft carrier length at least equal to the width of the air intake of the test WFD; - installation of two subjects WFD diametrically symmetrically on the sides of the nose. The present device provides the possibility of increasing the measurement accuracy of the test parameters of the SRM by providing the best flow simulation conditions ram air it in a real flight. The prototype of the device is made in the company - the applicant and has been tested with the experimental WFD with a positive result.