Active silencing system applied to aero-engine test room
A technology for aero-engines and test rooms, which is applied to sound-generating devices and instruments, and can solve problems such as limited noise reduction effects
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[0013] The present invention will be described in detail below with reference to the accompanying drawings and examples. It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other. For the convenience of description, if the words "up", "down", "left" and "right" appear in the following, it only means that the directions of up, down, left and right are consistent with the drawings themselves, and do not limit the structure.
[0014] like figure 1 As shown, an active noise reduction system applied to an aero-engine test room provided by this embodiment is installed in the test room 2, which includes a sound wave generator 3, a sound wave receiver 5, a noise source receiver 6 and a controller 7.
[0015] One side of the test room 2 is provided with an air inlet 8, and the other side is provided with an exhaust air passage 9, and the sound-absorbing element 1 inside the air inle...
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