■• %,«* ••' -ov*" cCl'^ «^ «5°^ > O. •'^^^'' V -ov*" 'bV •oV" ■0 U^ ^ > -.. ... .*,^te^-. ^..^/ ,^, u^^^ ,^-, *.,^/ ,^^, .,^^^* , V .»: % ^ *l ■ -^ A^ ^'^K'o ^-^r. ^ »V^^ ^0^ \:/ -^o^ a5<^ « '^^^ "- 4^^^"^'/^^ /.c;^^% /-^i'^-^ /.c;^^ °o ,^''\^^i'\. ^oV 4''^>. -.Oilier; *:^'^^. "o'^JAW A^^'^^ ■:"5Plil^*° ^'?'^\. °MW^: a^""^^ •'.s^ii^*'' ^:^""^ " ■" " <■?' 0" * A^"^ -j.^ %. ^^-^^^ .^ .. ^0* ..IV' "> ■r O <* *'..«* ..& > A V *%>. . ^ «4o«. « ■^^. ^*Tr.-* .«,'«•' \ *7 ^ «5^ o V "0, V. .^"^^ « 9^ : «:^^V ^ : ^^.^ * - ->^- «"5 ^ " ' « V *^^ • ""O A? ^ V r \ % nX\\ h^^^\ \ \ 1 \ h \\\ vX-N^ s. N \, h ^ \ \ \N \\ \ \ s. > \ w \ % \ iN\ \\ \ \ \ \ ^. \ ^>^ k k \ k \, K \ ^\ \ \ \ \\ \ \ \ 100 90 80 7C 6 50 403530 25 20 15 109 8 7 6 5 4 3 5 3 2.5 2 SUPPORT LOAD, kips/ft of entry length 1.5 1 10 15 20 ENTRY WIDTH, ft FIGURE 10. - Nomogram for determining support loads. Four different types of beam loadings are shovm in figure 11. They include concentrated loading, uniform loading, uniformly varying loading, and parabolic loading. Formulas for calculating end reaction, maximum shear, maximum moment, and maximum deflection are presented for each case. rock to be carried by each support. The maximum moment to be resisted in terms of the total load and beam length is M 5 WL 5 (164,000) (16) ma X 32 32 = 410,000 fflb. (4) SUPPORT SELECTION The design example is based on the fol- lowing assumptions. A 16-ft-wide entry is to be supported. The roof is composed of shale rock with a density of 160 lb/ ft-'. Support envelope height is esti- mated as 24 ft (3b/2), indicating that heavy loading is expected. The supports will be spaced 4 ft apart along the en- try. Parabolic loading of the supports by the roof rock (case 4) is assumed. A typical yield strength of structural steel is 36,000 psi. It is assumed that the critical load condition causes yield- ing of the section. In other words, the failure load is defined when one element of the supporting structure has reached yield strength of the steel. The nomograph of figure 10 gives a sup- port load of 41 kips per foot of entry length for a 16-ft-wide entry, 160-lb/ft^ rock density, and 24-ft-high support en- velope. Multiplying this number by the 4-ft support spacing gives 164 kips or 164,000 lb as the total weight of roof The required section modulus is obtained by converting the maximum moment to inch pounds and dividing by the yield strength of 36,000 psi. S = M„ (410,000) (12) 36,000 = 137 in^. (5) Referring to the "W Shapes, Properties for Designing" section of a steel con- struction manual (_5 ) , and using the plas- tic modulus (Zj<) column, choose the fol- lowing beams as having at least a 137-in^ section modulus: W 14 X 82, W 16 X 77, W 18 X 71, W 21 X 62. Without concern for headroom or clear- ance, select the lightest weight section, which is the W 21 x 62 beam. The second number in the W designation is the beam weight in pounds per foot. Pertinent properties of the selected beam are listed in figure 12. 12 W R End reaction; R = W Maximum shear; V, Maximum moment: M W WL max Maximum deflection; fS = 0.0 208- max 48EI ^ Case 1 - c o nc e n t r a t e d load Total load: W = End reaction: R = qL w Maximum shear:Vmax~ W qL*^ WL Maximum m o m e n t : M^ a x = T^ = "~5~ Maximum d e f I e c t i o n: 6 m a x = 120EI ^ 60EI Case 3-uniformly varying load A n -* L »► Total load ; W = qL End reaction; R = qL W Maximum shear; V, W 2 Maximum moment;Mmax = Maximum deflection; '^ qJLf_^WL 8 8 _ 5 q L^ ^ 5 W L^ f^a^' 384EI 384EI 0.0 13 WL- Case 2-uniform load FIGURE 11.. Types of CHECKS FOR SUPPORT ADEQUACY The selected beam will now be checked for the following conditions. 1. Shear capacity. 2. Lateral stability. 3. Deflection, 4. Localized buckling. 5. Support length (web crippling). Total load: W = 2qL q L w End r e a c t i on: R = — -- = — q L w Maximum s h e a r: V^ a x ~ ""T~~ T 5qL^ _ 5WL 32 Maximum moment:M max 48 Maximum d e f le c t io n:5 , eiqL^ 6 1WL' f"^^ 5,760EI 3,840EI Case 4-parabolic loading beam loading conditions. All steel design and review calcula- tions are based on the specifications of the American Institute of Steel Construc- tion. Plastic design methods have been used throughout this example. Shear Capacity The maximum shear on the beam is V„,, . f . i^MOO , 82.000 lb. (6) 13 ill 1,375 + 25, (8) 'w Y f ZxPlastic section m o d u I u s = 1 4 4 In-' d:beam depth=21 in tyy:web thick ness=«04 in r;radlus of gyration about Y axis=1.77 in l:tnoment of inertia about X axis»1,330 in^ bfiflange width=8.24 in t|:flange t tiic k ness= . 6 1 5 in k:distance from outer face of flange to web toe of fillet* 1 25 in E: modulus of e la s 1 1 c i t y= 2 9 , , 00 psi Fyiyield strengfti of steel»36.000 psi FIGURE 12. • Pertinent properties for selected beam. The allowable shear for the selected beam in terms of the yield strength (Fy), web thickness, and beam depth (see figure 12 for symbols and values) is Va = 0.55 (Fy) (tj (d) = 0.55 (36,000) (0.4) (21.0) = 166,300 lb. (7) Since the allowable shear is greater than the maximum shear, this size beam is ac- ceptable for the shear loading. Lateral Stability The critical length for lateral stabil- ity is calculated by the formula where the yield strength of the steel (F ) is used in kips per square inch. Substituting in the formula gives cr = (1.77) = HI in. 1,375 36 + 25 (9) As the beam is 16 ft long, it should be braced (struts from beam to beam) on the compression flange at the midspan of the beam. This lateral bracing will prevent buckling of the compression flange. Deflection The deflection formula (figure 11, case d) is = 61 WL^ •"^x 3^840 EI = 61 (164,000) (16)^ (12)3 3,840 (29,000,000) (1,330) = 0.478 = 0.5 in. (10) Measurement of beam deflection permits a quick check on the condition of the beam. The midspan deflection can be measured with a pocket tape by stretching a string from one support to the other. For exam- ple, if 0.25-in deflection is measured, the beam still retains approximately 50 pet of its load capacity. Localized Flange or Web Buckling Beams are made with different flange and web thicknesses and may be subject to localized buckling, even though their section modulus is adequate for the load. Flange thickness is checked with the following formula: 14 2t, < 8.5. (11) R Substituting the selected beam values in the formula. 8.24 = 6.70 < 8.5; 2 (0.615) beam is acceptable. (12) The equation for checking web thickness assuming no axial load is 412 Where the yield strength of the steel (Fy) is used in kips per square inch, substituting beam values in the equation 21 0.4 412 = 52.5 < -7^ = 68.7; 7jh beam is acceptable. (13) Support Length (Web Crippling) This test is to check for localized web buckling from the concentrated loading that occurs over the supporting posts. The appropriate equation is 0.75 Fy (t„) - k. (14) where N = the required bearing length be- tween the beam and its support, in, R = the end reaction, lb, and t^^ and k are defined in figure 12. Substituting beam values into the equation, 82,000 N = 0.75 (36,000) (0.4) - 1.25 = 6.34. (15) If a bearing length between the bot- tom of the beam and the supporting post of less than 6.3 in is used, a stiff- ener should be used at the end of the beam. This reinforcement can be provided by welding plates to both sides of the web. The selected beam has been checked, us- ing plastic theory based upon the recom- mendations of the AISC specifications, and has been found to satisfy the assumed loading conditions. SUMMARY The major source of injuries appears to be handling the steel supports, primarily due to their weight and awkwardness. Ac- ceptable mechanical methods for quicker and safer installation of the heavy steel supports in the confining mine environ- ment are needed. The arch is a more efficient configura- tion than the flat crossbar, as the load is transmitted as compression rather than bending forces. Yielding arches are more effective than rigid arches under se- vere conditions that produce large de- formations. The void space between the arch and the strata must be backfilled or blocked to provide uniform load- ing. Steel supports should be installed close to the face exposure. and shortly after roof The load to be carried by steel sup- ports can be calculated by assuming a parabolic-shaped roof support envelope. The actual height of this support enve- lope in a particular mine can be esti- mated by observing roof falls. A nomo- gram is provided for determining support loads per foot of entry length for vari- ous entry widths, rock densities, and support envelope heights. The support beam can then be designed by referring to 15 any steel construction manual. A design example is provided with pertinent equa- tions and calculations. Equations are provided for checking the selected beam for adequacy, with respect to shear ca- pacity, lateral stability, deflection, localized buckling, and web crippling. REFERENCES 1. Peng, S. S, Coal Mine Ground Con- trol. Wiley, 1978, 405 pp. 2. Hawkins, S. A. Health and Safe- ty Analysis on Support Walls. Volume 2: Steel Supports Design Criteria: A Sum- mary of European Data (contract JO295036, Management Eng. , Inc.). BuMines OFR 121(2)-82, 1980, 61 pp.; NTIS PB 82- 251968. 3. Spruth, F. Steel Roadway Supports: A Practical Handbook. Collier Guardian Co., Ltd., London, v. 2, 1960, 750 pp. 4. Proctor, R. V., and T. L. White. Rock Tunneling With Steel Supports, Com- mercial Shearing, Inc., Youngs town, OH, 1946, 278 pp. 5. American Institute of Steel Con- struction, Inc. Manual of Steel Con- struction. 7th ed., 1973, 1200 pp. 6. Salmon, C. G. , and J. F, Johnson. Steel Structures. Harper & Row, 2d ed., 1980, 945 pp. 7. McCormac, J. C. Structural Steel Design. Harper & Row, 3d ed., 1982, 662 pp. 8. Kuzraanovic, B. 0., and N. Willems, Steel Design Structures. Prentice-Hall, 2d ed. , 19 78, 600 pp. 16 . APPENDIX. —EXPLANATION OF SYMBOLS A Area b Entry width bf Flange width d Beam depth E Modulus of elasticity Fy Yield strength of steel Y Density of rock h Height of roof envelope I Moment of inertia about Y axis k Distance from outer face of flange to web toe of fillet L Beam length l(,p Critical length for lateral stability Mn,ax Maximum moment N Required length between beam and support P Weight of rock that must be supported q Magnitude of distributed load on beam R End reaction r Radius of gyration about Y axis S Section modulus tf Flange thickness ty, Web thickness V Volume Vg Allowable shear V^ax Maximum shear W Total load Zx Plastic section modulus 6n,ax Maximum deflection fiU.S. CPO: 1981-505-019/5068 I N T.- BU.O F M IN ES, P GH., P A. 277 25 D DD 2 Q_ O a "> _. =r 9tcE Q " O 70 O O 3 <*-,- — - ;;;• ° -O 3- W — a- ™ (t O 3 O -t Q- l/i (t O " 8 •■' 3 i % 5: O (A ^^ So X > ■0 r- m z S f" ffi CO «« u CD Oo C o "1 )<■ :«^ ^. 5 m O < m Z > zm zc w O m > ii m "n CO 3:>. > H m zco H m O m O c > I— o TJ TJ O J) H C Z m ■o r- O < m ^ 209 85 .^ c w ^s go -ml" z z > i o o 0> TI -Tl H m I m m w 15 O L~ .r '>% ^-..-^^ ^ '^^^ ' 0° .c:;^^ °o ay ^ « CO, ^^ ,o''_l''*. 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