BLEED VALVE ASSEMBLY WITH RESONATOR CHAMBER

Bleed valve assemblies (300) in a gas turbine engine (100) are disclosed herein. A bleed valve assembly (300) in a low pressure compressor (150) may include a bleed valve (230; 310) and a resonator chamber (500; 610, 620). A manifold (400) may allow passage of air from a bleed duct (230; 310) into the resonator chamber (500; 610, 620). The resonator chamber (500; 610, 620) may alter resonation properties of the bleed duct (230; 310) in order to prevent damage to components in the low pressure compressor (150).