Published: 18 September 2015

The substantiating of the dynamic parameters of the shaking conveyor mechanism

Zhauyt Algazy1
1Department of Applied Mechanics and Basics of Machine Design, Kazakh National Technical University, Almaty 050013, Kazakhstan
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Abstract

In this paper is studied a vibratory conveyor that is placed on an elastic base. Using the closed contours method it was determined the system that needs to be solved to obtain graphical representation for the generalized coordinates determining the position of the mechanical system elements. The shaking conveyor represents the chase hanged or supported to the fixed section. The chase commits oscillating motions hereupon the cargo which is in the chase, migrates concerning to the chase. The nature of the flow and its parameters are determined by the nature of the oscillating committed by the chase. Justifying the dynamic parameters of the shaking conveyor and a study of the stress-strain state. Installation causes fluctuations fixed tray. Uniformly distributed load on the tray acts in each element of the mechanism. A proper dynamic model has been developed within MSC ADAMS software. Simulation tests have been carried out and results are discussed to validate the proposed design solution.

1. Introduction

The big application in various fields of the industry was received by the shaking conveyors applied to transportation of hot, poisonous, chemical aggressive cargoes by the supplement of complete tightness of their relocation [4], and also for transportation of the metallic cuttings damped with emulsion and oil, hot earth which has been beaten out from casting forms, small casting, foundry fusion mixture, etc. The shaking conveyor represents the chase hanged or supported to the fixed section. The chase commits oscillating motions hereupon the cargo which is in the chase, migrates concerning to the chase [5-8]. The nature of the flow and its parameters are determined by the nature of the oscillating committed by the chase. Shaking conveyors on the conditions of the chase flow and nature of cargo movement are subdivided on inertial (with variable and constant stress of cargo to the chase) in which [9] cargo under the influence of inertia force glides on the chase, and on vibrating in which cargo tears off the chase and migrates along the chase. The vibrating conveyors [1-3] are widely applied owing to a number of advantages in these latter days. The questions of the kinematic and dynamic study of the vibrating feeder intended for dosing of the fusion mixture loading of the melting furnaces of foundry production are considered in the presented work [11-15]. The principle of operation of the vibrating conveyor is described, and it is devoted the kinematic analysis of the action. The differential equation of the link move of the reduction of the vibrating conveyor is considered in the difference method (the approximate method) solutions of the equation of move of the vibrating conveyor is resulted [10]. It is devoted to the analysis of the equations solutions of conveyor move. Here tables of the results and relocation drawing and velocity of the leading link depending on time are resulted.

2. Materials and methods

2.1. Differential equations of the link move of the reduction of the vibrating conveyor

It is the action of the III class. The crew ВЕD basic crew from which there are three leads FЕ, АВ, GD. The link ОА is a leading link.

This action has one axis of motion, therefore relocation, velocities and speed-up of the driven link and action dots are functions of the relocation, velocities and speed-up of the leading link. Therefore we will find analytical dependences between relocations, velocities of the driven links and leading link. As the leading link enters into the rotational pair with the console we set function:

φ1=φ1t.

Fig. 1Kinematic scheme of the shaking conveyor

Kinematic scheme of the shaking conveyor

Table 1The action has following performances

No.
Links
1
2
3
4
5
Mass, kg
m1= 30
m2= 65
m3= 1160
m4= 59
m5= 59
Length units, mm
l1= 60
l2= 430
l3= 1100
l4= 440
l5= 440

By the solution of the action move problem with one degree of freedom we will use the equation of the action move of the engine aggregate:

1
Ikφ1dω1dt+ω122dΙk(φ1)dφ1=Mk-Mk.

It is known to us dependence MP(ω) and MR(φ1). We determine MR(φ1) the resulted moment of resistance forces from power equalling of the resulted moment of force resistance and the sum of powers of the moments [5] of resistance forces of operating in links E, D, F, G:

MKω1=ME ω4+MD ω5+МF ω4+MG ω5,
MK=ME ω4ω1+MD ω5ω1+MF ω4ω1+MG ω5ω1=ME u41+MD u51+MF u41+MG u51=4u41Mk.

Let’s find resulted moment of the flywheel actions Ιk(φ1) from equalling condition of kinematic energy of reduction link to the kinematic energy sum of all links of the action:

2
Ιkφ1=ΙS1+m2ϑS2φ1+ΙS2u222+m3ϑS3φ12+Ι4F+Ι5Gl412.

We determine inertia moments of the first, second, fourth and fifth links.

ΙS1=m1l122, ΙS2=m2l222, Ι4F=ΙS4+m4l'4=m4l422+m4l424,
Ι5G=ΙS5+m5l'5=m5l522+m5l524.

We differentiate the resulted inertia moment on φ1. For this purpose we substituted all above found values in the equation:

dΙkφ1dφ1=2m2(l1sinφ1+l2'sinφ2u21)2+(l1cosφ1+l2'cosφ2u21)2ω1
ω1l1cosφ1-sinφ1+l2'u212cosφ2-sinφ2+l2'du21dφ1sinφ2+cosφ2(lsinφ1+l21sinφ2u21)2+(l1cosφ1+l21cosφ2u21)2+2IS2l1l2sinφ4-φ1sinφ2-φ4
l1l2u41cosφ4-φ1cosφ4-φ1sinφ4-φ2-u21cosφ4-φ2-u41cosφ4-φ2sinφ4-φ1sin2φ4-φ2
+2m3ω12-l1cosφ1+sinφ1-l2u212cosφ2-sinφ2+l2du21dφ1cosφ2-sinφ2-cosφ1-φ2u21-cosφ1-φ2sinφ2-φ1sin2φ2-φ4l1l4sinφ2-φ1sinφ2-φ4
=2m2ω12l1cosφ1-sinφ1+l2'u21cosφ2-sinφ2+l2'du21dφ1sinφ2+cosφ2+2ΙS2
l12l22sinφ4-φ1sinφ2-φ4u41cosφ1-φ4-cosφ4-φ1sinφ2-φ4-u21cosφ4-φ2-u41cosφ4-φ2sinφ4-φ1sin2φ4-φ2
-2m3ω12l1cosφ1+sinφ1+l1'u212cosφ2-sinφ2-l2du21dφ1sinφ2-cosφ2-du51dφ1acosω5t-bsinω5t
+2(Ι4F+Ι5G)l12l42sin(φ2-φ1)sin(φ2-φ4)
u21cosφ1-φ2-cosφ1-φ2sinφ2-φ4-u21cosφ1-φ2-cosφ1-φ2sinφ2φ1sin2φ2-φ4.

The move equation of the reduction link of the action looks like:

3
ΙS1+m2ω12[(l1sinφ1+l2'sinφ2u21)2+l1cosφ1+l2'cosφ2u21)2+ΙS2l12l22sin2φ4-φ1sin2φ2-φ4
+m3ω12(-l1sinφ1+l2sinφ2u21+au51cosω5t)2+(l1cosφ1+l2cosφ2u21-bu51sinω5t)2
+Ι4F+Ι5Gl12l42sin2φ2-φ1sin2φ2-φ4dω1dt
+ω1222m2ω12(l1sinφ1+l2'sinφ2u21)l1cosφ1u212+l'2sinφ2du21dφ1
-l1cosφ1+l2'cosφ2u21l1sinφ1+l2'sinφ2u212-l2'cosφ2du21dφ1
+2ΙS2l12l22cosφ1+φ4-cosφ1+φ4sinφ1-φ4sin2φ2-φ4
+2m3ω12l1sinφ1+l2sinφ2u21-au51cosω5tl1cosφ1+l2cosφ2u212+l1sinφ2du21dφ1-acosω5tdu51dφ1-l1cosφ1+l2cosφ2u21-bu51sinω5tl1sinφ1-l2sinφ2u212-l2cosφ2du21dφ1+bsinω5tdu51dφ1
+2Ι4F+Ι5Gl12l22cosφ1+φ2-cosφ1-φ2sinφ2-φ1sin2φ2-φ4=Мkο-αω1-4u41M'k+K0φ5.

For solution of the Eq. (3) there are following initial conditions: at t=0, ω1=0, φ1= 60°.

2.2. The approximate method of the equation solutions of the vibrating conveyor

For constructing on the piece t[0,T] of the approximate solution of the move Eq. (3), we copy it in the following kind:

4
R(t)dω1dt+Q(t)ω2(t)=W(t),

where:

R(t)=ΙS1+(m2At+m3Htω12+Bt+DtAt=l12+2l1l2'sinφ1sinφ2+cosφ1cosφ2u21+l2'2u212,
Ht=l12-l22u212+a2cos2ω5t+b2sin2ω5tu512+2l1l2u21sinφ1sinφ2+cosφ1cosφ2
-2l1u51(asinφ1cosω5t+bcosφ2sinω5t)-2l2u21acosω5tsinφ2+bsinω5tcosφ2,
Bt=ΙS2l12sin2φ4-φ1l22sin2φ2-φ4, Dt=Ι4F+Ι5Gl12sin2φ2-φ1l42sin2φ2-φ4,
Qt=m2Et+m3Ft2ω12+2ΙS2l12l22Nt+Mt,
E(t)=(l1sinφ1+l21sinφ2u21)l1cosφ1+l21cosφ2u212+l21sinφ2du21dφ1
-l1cosφ1+l21cosφ2u21l1sinφ1+l21sinφ2u212-l21cosφ2du21dφ1,
Ft=l1sinφ1+l2sinφ2u21-au51cosω5tl1cosφ1+l2cosφ2u212+l1sinφ1du21dφ1-acosω5tdu51dφ1
-(l1cosφ1+l2cosφ2u21-bu51sinω5t)l1sinφ1+l2sinφ2u212-l2cosφ2du21dφ1+bsinω5tdu51dφ1,
Nt=cosφ1+φ4-cosφ1-φ1sinφ1-φ4sin2φ2-φ4,
Mt=Ι4F+Ι5G2l12l22cosφ1+φ2-cosφ1-φ2sinφ2-φ1sin2φ2-φ4,
Wt=MDο-αω1-4u41Mko'+Kοφ5.

3. Results and discussion

A proper dynamic model has been developed within MSC ADAMS software to provide information on the feasibility of the proposed design solution. Simulation tests have been carried out and results are discussed for validating the proposed design and characterizing its operation.

Fig. 2Six bar linkage motion simulation in MD Adams

Six bar linkage motion simulation in MD Adams

Fig. 3Computed plot of the force and momentum joint 1

Computed plot of the force and momentum joint 1

Fig. 4Computed plot of the force and momentum joint 2

Computed plot of the force and momentum joint 2

Fig. 5Computed plot of the force and momentum joint 3

Computed plot of the force and momentum joint 3

Fig. 6Computed plot of the force and momentum joint 7

Computed plot of the force and momentum joint 7

Fig. 7Computed plot of the force and momentum joint 8

Computed plot of the force and momentum joint 8

Fig. 8Computed plot of the force and momentum joint 9

Computed plot of the force and momentum joint 9

Fig. 9Computed plot of the force and momentum joint 10

Computed plot of the force and momentum joint 10

4. Conclusions

1) Formulas for the position determination and velocity of conducted links depending on position and velocity of the leading link are received.

2) The differential equations of the link move of the action reduction are received.

3) On the basis of the profiles variation analysis of the angular rate of the leading link it is possible to make the following concluding:

– with the growth of the starting driving moment middle angulator of the action grows;

– with reduction of the starting driving moment middle angular rate of the action is decays;

– with coefficient increase α0, ωcp grows.

4) The basis of the program MSC Adams software investigated the kinetic energy and translational momentum of each link mechanism with results and calculations.

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About this article

Received
Accepted
03 June 2015
Published
18 September 2015
SUBJECTS
Mechanical vibrations and applications
Keywords
vibratory conveyor mechanism
stress-strain state
closed vector method
equation
Acknowledgements

The first author likes to acknowledge JSC Center of Republic of Kazakhstan for supporting his Ph.D. study and research at LARM in the University of Bielsko-Biala in Poland, in the academic year 2014-2015.