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In this paper, a dynamic model for clamp band joint system is developed.
Firstly, the mathematical model of the axial stiffness of the clamp band joint was derived.
Finally, the model is adopted to study the dynamic characteristics of the clamp band joint system subjected to axial harmonic excitation and the effects of the wedge angle of the clamp band joint and the preload on the response.
Then static experiments are carried out on a scaled model of the clamp band joint to validate the joint model.
The application of clamp band joint brings local stiffness variation to the launch vehicle and spacecraft (LV/SC) system and affects the dynamic characteristics of the system.
The research results in the paper can provide a reference for the initial engineering design of the clamp band joint of satellite separation systems to guarantee a secure and reliable separation event.
Similar(51)
Clamp band joints are commonly used for connecting circular components together in industry.
Now, we consider the multi-band joint detection when the compressed sensing module A 1 is valid.
The problem with Barton-Band joint model is its underestimation of hydraulic aperture value (Piggott and Elsworth 1991).
The simultaneous spectrum sensing over multiple sub-carriers is performed by using a set of multi-band joint detectors, as proposed in [21].
In this paper, taking advantage of the frequency-domain sparsity of the wideband spectrum, a WSS scheme combining compressed sensing and multi-band joint detection technique is proposed to reduce the energy consumption.
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