Bleed valve of a turbine engine compressor

摘要: The invention relates to a turbofan aviation turbojet compressor, said compressor comprising, in known manner, relief valves (7) placed housings of the external wall for discharging part air flow. According invention, comprise means (14a) which remain pressed against vein as long valve has not reached determined opening angle (α) and are suitable, greater (β), project into (2) collect excess water entering compressor.