Numerical Modeling of Block Caving at the Grace Mine

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NUMERICAL MODELING OF BLOCK CAVING AT THE GRACE MINE-ES UN EJEMPLO DEL MODELAMIENTO NUMERICO EN UNA MINA BLOCK CAVING.

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  • Chapter 15

    NUMERICAL MODELING OF BLOCK CAVING AT THE GRACE MINE

    Giovanni B. Barla

    Department of Structural Engineering Politecnico di Torino

    Torino, Italy

    Stefan H. Boshkov

    Henry Krumb School of Mines Columbia University New York, New York

    ABSTRACT

    The block caving method is examined in this paper on the basis of experi- mental results and observations in the field, and through the use of numerical modeling by the Finite Element Method. The Grace Mine, developed by a panel caving method, served as a reference case. However, the results obtained and the simulation techniques which have been developed may find useful application in more general conditions as encountered in other mining operations by block caving. Following a brief description of the Grace Mine and of the mining method, the problems associated with the behavior of underground drifts at the production levels, during undercutting and caving, are addressed. The most important results obtained through monitoring of strains and loads in the supports of a runway are discussed, while giving relevance to the sequence of mining operations in the immediate vicinity. The most important geomechanical data, as provided for subsequent modeling, are described with reference to: (a) rock mass characterization and (b) in situ state of stress. Then, the numerical modeling procedures, developed by the Finite Element Method in order to predict the caving phenomena and the behavior of underground openings during undercutting, are discussed. Finally, an attempt is made to compare the pre- dictions of the numerical analyses with,the measurements carried out at the instrumented site. Suggestions as to how to improve the results both quali- tatively and quantitatively are also given.

  • NUMERICAL MODELING OF BLOCK CAVING AT GRACE MINE

    INTRODUCTION

    A s i g n i f i c a n t problem i n mining by BZock Caving i s t h e evaluat ion of t h e e f f e c t s o f undercu t t ing and caving on t h e behavior of underground develop- ment and e x t r a c t i o n openings and t h e i r supports (Merr i l and Johnson, 1964) . I n recogni t ion of t h e need t o provide r e l i a b l e s o l u t i o n s t o such a prob- lem, a research program was c a r r i e d ou t from 1974 through 1979, with t h e Grace Mine, near Reading (Pennsylvania) , being considered a s a u s e f u l exem- p l i f i c a t i o n of t h e method ( ~ a r l a and Boshkov, 19791

    This program encompassed i n s i t u s t r e s s de te rmi na t ion , monitoring of equipment i n s t a l l a t i o n (Agac wal e t a l . , 1973) , and subsequent accumulation o f d a t a from 1974 through 1976. Subsequently, t h e fol lowing ob jec t ives were posed: 1. t o r e l a t e f i e l d observat ions and experimental d a t a t o f i e l d experience, and 2 . t o a t t empt t o f i n d a l inkage between t h e two, through t h e des ign o f a numerical model based upon the F i n i t e Element Method. The r e s u l t s of t h e i n v e s t i g a t i o n s c a r r i e d ou t a r e de- sc r ibed i n t h e p resen t paper .

    MINE DESCRIPTION

    The Grace Mine i s s i t u a t e d approximately 1 0 km south of Reading ( ~ e n n s ~ l v a n i a ) . Up t o t h e end of 1978, a magnetite orebody, wi th an average th ick- ness of 100 m , about 400 m wide, has been mined a t a depth of 700 m by t h e panel caving method.

    ?'he o r e v a r i e s from moderately weak t o moderate l y s t rong . The foo twal l , d ipp ing approximately 25 degrees t o North-East, i s d iabase , a f i n e grained and r a t h e r competent rock . A moderately s t r o n g q u a r t z i t e form; t h e hanging w a l l . The mine p lan is shown i n Figure 1, where a completely dep le ted a r e a i n t h e orebody i s r e p r e s e n t e d , t o g e t h e r with t h e runways used f o r o r e p roduc t ion . Figure 2 il- l u s t r a t e s t h e method of mining.

    Runways (4.5x4.0 m) a r e d r iven along t h e s t r i k e , approximately 20 m below t h e ore-diabase c o n t a c t . E n t r i e s (draw p o i n t s ) a r e turned o f f a t 60 degrees each 15 m from t h e runway. Concurrent ly a d r i f t (2x3 m) (undercu t t ing d r i f t ) i s dr iven p a r a l l e l t o t h e runway, 11 m t o t h e down-dip s i d e . Access t o t h i s d r i f t i s secured by d r i v i n g a p i l o t d r i f t through a t every t h i r d e n t r y . D r a ~ - ~ o i n t s a r e c rea ted by en eleven-*,ole i n c l i n e d f a n p a t t e r n d r i l l e d on 1.5 m cen te rs throughout t h e l e n g t h of t h e undercut t ing d r i f t . A f t e r a s u f f i c i e n t number of e n t r i e s a r e completed i n suppor t requirements , t h e fan holes a r e b l a s t e d . Both t h e runways and e n t r i e s a r e heav i ly supported by r e i n f o r c e d con- c r e t e and s t e e l s e t s .

    A l l openings experienced l a r g e s t r e s s and de- formation changes during u n d e r c u t t i n g and caving. This r e s u l t e d i n supports f a i l u r e , c o s t l y r e p a i r o r replacement. I n o rder t o a l l e v i a t e t h e s e prob- lems, p rogress ive ly heav ie r s t e e l s e c t i o n s and t h i c k e r concrete l i n i n g s have been used a t t h e mine w i t h apparent small improvement i n r e s u l t i n g condit ions. No f ixed p a t t e r n t o t h e f a i l u r e o f supports could be defined. Also, t h e f a i l u r e i n

    no case was v i o l e n t , b u t gradual and unre len t ing .

    FIGURE 1 - Mine p lan .

    FIGURE 2 - Method of mining. S e c t i o n through t h e runways showing f o o t w a l l and undercut .

    IXSTRUMENTED RUNWAY

    With t h e purpose o f determining t h e load on s t e d s e t s and s t r a i n s i n t h e concre te l i n i n g , it was de- c ided t o instrument an o r e haulage runway (Runway 6 0 9 ~ , 6 t h l e v e l ) , a t tvo a d j a c e n t e n t r i e s t o t h e caved o r e , a s shown i n Figure 3.

    This runway was instrumented between November 1973 and October 1974 (Agarwal e t a l . , 1973). The equipment i n s t a l l e d included concre te s t r a i n t r a n s - m i t t e r s and load c e l l s . The s t r a i n t r a n s m i t t e r s

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