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Overview in PDF format - Tallinna Tehnikaülikool

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2 2( kl − J p + Aωp )ob M la1= b2=,2 22( kl − J o p + Aωb p − β l ω b )3M l β pb1= −a2=2 22(2.38)( kl − J o p + Aωbp − β l ωb)( k + k ) 2 , M = ( M M )/2k = y z / y + z(2.39)2 *( k2yl− Joω) Fall1c1=2 * 2,2 2 * 2 * 2( k yl− Joω) + ( βlω ) + ( Aωbω)2 *2Aωb( k yl− Joω) Fall1c2=2 2 *2,2 2 * 2 * 2βl[( k yl− Joω) + ( βlω ) + ( Aωbω) ]* 2 2 * 2ω [( β l ) + ( Aωbω) ] Fall1d1=2 2 * 2 2 * 2 * 2β [( ω2(2.40)l k yl− Jo) + ( β l ω ) + ( Aωbω) ]The general solution of Eqs (2.22) is the sum of Eqs (2.36)–(2.37):z = z+ z2= exp( − n1t)( D1cos ω1t− D3s<strong>in</strong> ω1t)( − n t)( D cos ω t + D s<strong>in</strong> ω t)1+ expy = y+ exp222*+ a2 cos pt + b2s<strong>in</strong> pt + c2cos ω t ,1+ y2= exp( − n1t)( D1s<strong>in</strong> ω1t+ D3cosω1t)( − n t)( − D s<strong>in</strong> ω t + D cosωt)+2224**+ a1 cos pt + b1s<strong>in</strong> pt + Frl1/ k yl+ c1cosω t + d1s<strong>in</strong>ωt , (2.41)422++where D 1 , D 2 , D 3 and D 4 are constants of <strong>in</strong>tegration to be determ<strong>in</strong>ed from the<strong>in</strong>itial conditions, ω 1 and ω 2 are the natural frequencies of vibrations withgyroscopic forces and damp<strong>in</strong>g.2.6. Experimental Analysis2.6.1. Prelim<strong>in</strong>ary experimental test2.6.1.1. Experimental test of the spr<strong>in</strong>g constant of the latheThe accuracy of the accepted models was tested on the lathe 1K62. Dur<strong>in</strong>g thetheoretical analysis, calculation accuracy depends both on the degree of fitness ofthe accepted models of the real system and on how accurately mechanicalcharacteristics of the lathe are determ<strong>in</strong>ed. One of these characteristics is the spr<strong>in</strong>g30

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