FIELD: aerospace technology.
SUBSTANCE: invention relates to aviation and rocket and space technology, namely to the thermal protection of parts of the airframes of aircraft flying at supersonic speeds and in air-free layers of the atmosphere. The wing of a supersonic aircraft contains a thermal emission layer made of a material with a low electron output. The area of the leading edge of the wing and the thermal emission layer are a cathode that is electrically connected to the anode. The wing is made of a material with high magnetic permeability. Insulation is fixed between the cathode and the anode.
EFFECT: by reducing the demolition of thermoelectrons by the incoming flow by organizing the movement of thermoelectrons from the thermal emission layer to the anode layer along magnetic induction lines, an increase in the reliability of the wing of a supersonic aircraft with thermal emission cooling is achieved.
1 cl, 1 dwg
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Authors
Dates
2023-03-01—Published
2022-06-21—Filed