The present invention discloses a
pump jet propeller model with Helmholtz resonant cavities, and a design method thereof. The
pump jet propeller model comprises a conduit, a front
stator, an
impeller, a ring rib and a longitudinal rib that are arranged inside the conduit, a
Helmholtz resonator with two parallel resonant cavities arranged at the inner front end of the conduit, and a
Helmholtz resonator with two parallel neck portions arranged at the inner rear end of the conduit. The resonant frequency of the front
resonator is the
pump jet blade frequency and 2 times blade frequency, and the resonant frequency of the rear
resonator is the 2 times pump jet blade frequency. Compared with the reference pump
water jet model, the hydrodynamic performance of the pump jet model with the Helmholtz resonant cavities is basically the same, and the
spectral noise at the blade frequency and 2 times blade frequency is reduced by 2-3dB. The number of
stator blades is 11 leaves, the number of
impeller blades is 9 leaves, and the
impeller blades have large lateral slope characteristics, and can be used as the main
propeller with the speed of 16 knots, the thrust of 300kN and the power of 3.5MW. According to the technical scheme disclosed by the present invention, pump jet low-frequency
spectral noise can be further prohibited, and total
noise can be further reduced; and the
muffler technical scheme can be applied to the
spectral noise optimization design of the non-axis drive integrated motor pump
water jet model.