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CHAPTER II

THEORET โCAL CONSIDERATIONS

The analysis of conical rice bin made by Kanoknukul- chai (16) was summarized as the followings.

2.1 Physical Details of Conical Rice Bin

A conical rice bin, as shown in Pig. (1), consists of two conical shells joined at their outer edges by a ring girder of radius R^ and cross-sectional area A-j^. The bottom cone is completed with a semi-vertex angle =<^and H a thickness h^ , while the top cone is truncated with a

semi-vertex angle OC-^ and a thickness h^.. The ring girder at the top edge of the top frustum cone has a radius of R^

and cross-sectional area A_j_.

Two sets of orthogonal co-ordinates Ï y, 9 and z for the top cone, and y, 9 and z for the bottom cone are shown in Pig. (1). The co-ordinates y and y are extended along the generators from the apexes of the top and bottom cones respectively. The value of y at the outer edge of the

bottom cone is denoted by y , i.e., yQ = R^/sinc^1? likewise, y^ and y denote the values of y at the inner and outer

edges of the top cone, i.e., y, = H-j^/sin and y 0 = Rg/sin&j.^

respectively.

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The following conventions concerning the use of

su b sc rip ts and su p erscrip ts should be noted. The su b scrip ts t and b are designed to functions belonging to the top and bottom cones re sp ec tiv e ly , p to the ring g ird e rs, and o and i to those at the outer and inner edges of a cone res p ectiv ely . The su p erscrip ts p and c denote the membrane and bending

p a rts of the t o t a l solution re sp ec tiv e ly . 2•2 Method of Analysis of Conical pice Bin.

The conical rice bin had been analyzed by Kanoknukulchai (16). Initially, the shell will be treated, under the applied loading, as ล membrane (2 5). Under such conditions, the

statically determinate stress resultants in each cone can be obtained without dependence on their geometric continuities.

A consideration is then given to the e ffe c ts of the s t a t i c a l l y indeterm inate forces and couples which must e x is t at the

edges of each cone to preserve the c o n tin u ity . This can be done by applying the corrective shearing forces and couples in the bending an aly sis. F in ally , by combining both p a rts of the so lution, the t o t a l solution of the bin are obtained.

Figure (2) shows the scheme of the approach.

In the an aly sis, i t is assumed th at the contact pressure of the foundation is uniformly d is trib u te d over a h o rizo n tal p ro je c tio n of the bottom cone of the bin. Thus, the contact

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pressura P is determined ๖2/ dividing the total vertical loads by the area of the plane circle of radius

2.2.1 Membrane Solution The membrane solution has been carried out in Ref. (lé) for the structure under various

kinds of loads ; the dead load of the bin, the vertical live load on the top edge of the bin, and the pressure of water.

The solutions are shown in Tables (1), (2) and (3)» The notations and conventions of all forces and stress resultants following those in Ref. (2 5) are shown in Fig. (3)» All other notations, parameters and arguments are defined in the list of symbols.

2»2-? Bending So lu tio n The governing equations, fo r the general case of bending due to boundary loads applied uniformly along the edges of a conical s h e ll, have been derived and solved in Ref. (1 1). The so lutions interms of Kelvin functions are presented in Ref. (1 6), and are again shown in Table (4). The notation s and conventions of a l l s tre s s re s u lta n ts and displacements following those in Ref. (2 5) are shown in Fig. (4). All other n o tatio n s,

fu n ctio n s, parameters and arguments are defined in the l i s t of symbols.

2*2.3 Total Solutio n In obtaining the to t a l so lu tio n by a superposition of the membrane and bending so lu tio n s,

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the in te ra c tin g edge couple MQ as shown in Fig. (5) are f i r s t determined from the kinematic boundary and continuity conditions as shown in Ref. (1 6), Eqs. (54) to (5 7 )« Once ing so lution is completed and the to t a l so lution can be obtained by an appropriate su p er-p o sitio n of the membrane and bending so lutions.

2•3 plate Analysis of Bin Lid.

seated on a ring support of radius ล^, may be analysed as a th in p late subjected to a uniformly d is trib u te d load q.

Employing polar coordinates ( r , 0 ), with the o rig in of r a t the p late center, and le tt in g พ^ (r) and พ2 (r) denote the p late d e flec tio n fo r the domain 0 ^ r < a-^ and

< r < a2 res p ec tiv e ly , the axisymmetrical bending so lu tio n attain ed in Ref. (16), shown below ร

the values of H, . , H, 9 H. and M are determined, the bend" t i to bo 0

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พ2(r) ส ์) »4 ฟ ^

4 ( . i i ) + 2 (5 ± ÿ ) 1+y i+y

4

. ? ri± 5 y \!i

+2( พ ^ r2

“ 2al

2•4 Design Exampl8 of Conical Rice Bin.

The bin, as shown in Fig. (6), is designed for water loading which is more critical than the loading of rice grain and the vertical live load on the top edge of the bin and the bin lid. The bin has a storage capacity of 3*5 metric tons of rice (bulk density = 630 kg/cu.m.), a volume

capacity = 5*57 cu.m., a surface area of revolution = 1 7 * 1 5

sq.m, = 38 cm. and p_2 = 136 cm. The topmost level of the bin is 175 cm. above ground and the bottommost level is 59 cm. below ground.

The designed bamboocement conical section, the top and bottom ring girders and the bin lid are shown in Fig. (6).

The gross area of the top and bottom ring girders, A^ and

are 5 0 * 0 0 sq.cm. and 45*00 sq.cm. respectively. The

mortar used has a cement-sand ratio of 1;2 by weight, and a water-cement ratio of 0 .4 5“ The properties of materials used in the analysis are shown in Table (5)5 the properties

of bamboocement are determined by the formulae listed in

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Appendix - c . T h i s d e s i g n b a s e s on th e d i s t r i b u t i o n s of the s t r e s s . r e s u l t a n t s a lo n g th e s h e l l domains due t o th e dead w e i g h t of the b i n t h e edge load of the b i n and t h e l o a d i n g

o f w a t e r o b t a i n e d i n P i g s (7 )ร (8)» The edge d i s p l a c e m e n t , r i n g f o r c e s and u n i f o r m c o n t a c t p r e s s u r e of t h e f o u n d a t i o n due t o c o m b i n a t i o n o f l o a d i n g c a s e s a r e shown i n Tabla ( 6 a ) . The f o r c e s and s t r e s s e s i n b i n cap ( c i r c u l a r p l a t e ) a re shown i n Table ( 6 b ) . S t r e s s e s i n th e extrem e f i b e r s and i n t h e s k e l e t a l bamboos a t some c r i t i c a l s e c t i o n s a r e c a l c u l a t e d by the t e c h n i q u e d i s c u s s e d i n Appendix - c. The most s e v e r e

te n s ile s tre s s in bamboocement is found to be 27 kg/sq.cm.

o c c u r i n g a t t h e o u t e r f i b e r of the s e c t i o n

y/y 0

= 8 . 9 0 in

t h e l o n g i t u d i n a l d i r e c t i o n . Tne most s e v e r e c o m p r e s s i v e

s tre s s is 1 5 2 . 2 7 kg/sq.cm. at the inner extreme f ib e r of the sectio n y/y = 0 . 9 0 in the lo n g itu d in al d ire c tio n . The

maximum s t r e s s i n th e s k e l e t a l bamboo i s 359»57 k g / s q . c m . a t th e s e c t i o n y / y 0 = 0 . 9 0 in th e l o n g i t u d i n a l d i r e c t i o n . Comparing t h e s e v a l u e s w i t h th e y i e l d s t r e n g t h s o f the d e s i g n

sectio n , the bamboocement has been loaded up to 96 percent in tension and to 5 0 percent in compression, of the yield

s t r e n g t h s . I t sh o u ld be n o te d t h a t t h i s maximum s t r e s s i n c o m p r e s s i o n i s 94 p e r c e n t of t h e c o n v e n t i o n a l a l l o w a b l e c o m p r e s s i v e s t r e s s c o r r e s p o n d i n g t o 0 . 4 5 f c . The s k e l e t a l /

bamboo h a s been lo a d e d up t o 1 9 p e r c e n t o f i t s y i e l d s t r e n g t h

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and 39 p e r c e n t o f i t s a l l o w a b l e s t r e n g t h . Shown the l i m i t i n g s t r e s s e s a t y i e l d c o n d i t i o n and a l l o w a b l e c o n d i t i o n i n Table (7)» The t e n s i l e s t r e s s 5 c o m p r e ssiv e s t r e s s i n bamboocement and s t r e s s i n th e s k e l e t a l bamboo o f any s e c t i o n s a lo n g the s h e l l domains a r e shown i n Table ( 8 ) i n l o n g i t u d i n a l

d i r e c t i o n and i n Table (9) i n c i r c u m f e r e n t i a l d i r e c t i o n .

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