FIELD: aviation technology.
SUBSTANCE: invention relates to the field of aviation technology for carrying out flight studies of the characteristics and demonstration of technologies for aircraft power plants with small engines. The flying laboratory contains an aircraft-type unmanned aerial vehicle, consisting of a main fuselage, a rectangular wing, a front horizontal tail, a V-shaped tail and a power plant with N aircraft engines. Aircraft engine attachment points are installed on the wing and fuselage. The front horizontal tail is made removable, and the fuselage is equipped with a compartment with a hatch to accommodate an energy source.
EFFECT: invention is aimed at expanding the functionality of a flying laboratory for carrying out flight research of the characteristics and demonstration of technologies for aircraft power plants with small-sized gas turbine, piston, electric engines, as well as hybrid power plants, taking into account the type of energy source and the interference of the elements of the power plant and airframe.
1 cl, 5 dwg
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Authors
Dates
2022-12-05—Published
2022-06-14—Filed