Arrangement for rotor blade deicing, in particular of helicopters

摘要

Arrangement for rotor blade deicing of rotor blades, in particular of helicopters, characterized in that the arrangement for the rotor blade deicing (1) with the rotor blade (4,4 ') the / the gas turbine / engine (11) and the funnel (9) with the / the gas turbine / motor (11) is in thermal contact, the heating tubes (16) and the flow connection (6,6 ', 6 ", 16') with the valve (17) and the outlet (5,5 '), the manifold Ring housing (13) with at least the nozzle (13 ', 13 "), the temperature sensor (18) and the cover (7) with the flow breaking edge (7') and the connecting element (7"), wherein the rotor head (2) rotates freely in the manifold ring housing (13) and that the flow connection (6 ', 16') in the turbine (8) opens and it is in flow communication with the manifold ring housing (13).