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Continuous research led to the development of an elaborate method for gear noise evaluation.
The tested results show that the profile modification can greatly reduce gear noise.
This paper presents the development of a framework for aircraft landing gear noise prediction.
This is a relevant problem in many applications, in particular aircraft landing gear noise.
In specific, planetary gear noise with multi-sidebands and high magnitude will not only fail the former gear noise elimination algorithms but also affect the methods designed for highlighting bearing-fault-related content.
These include rolling noise, bridge structure noise, pantograph spark noise, pantograph aerodynamic noise, other aerodynamic noise and gear noise.
Similar(43)
The aim is to establish a method for accurately estimating gear noises radiated by the flexural vibration of gear blanks.
Strong vortex shedding from the axle is the second major contributor to landing-gear noise.
We survey experimental studies of landing-gear noise, and argue that the observed power of M is often well below 6.
These optimized specification limits are expected to reduce the bevel gears noise level during operation.
The algorithm's control abilities are sufficiently checked by single-input single-output and multiple-input multiple-output experiments via different feedback strategies progressively: (1) control gear meshing noise through attenuating vibrations at the key points on the transmission path, (2) directly control the gear meshing noise in the cabin using the actuators.
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