FIELD: transmitters of air parameters used on aircraft. SUBSTANCE: invention refers specifically to transmitters of parameters of air medium built into structure of wing. Ram temperature transducer has temperature-sensitive element determining temperature of air current. Additional cavity is arranged at angle with respect to main cavity so that particles entrapped in current are directed into outlet hole. Aerodynamic support has holes to remove gas of boundary layer. Transducer of air parameters also has cylindrical element determining gas pressure. Such design of transducer allows weight and aerodynamic resistance of structure to be diminished. EFFECT: diminished weight and aerodynamic resistance of transducer. 14 cl, 4 dwg
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