ANALYSIS & DESIGN CALCULATION FOR BFP FOUNDATION
Designed by Checked by Approved by
TABLE OF CONTENTS
SECTION
PAGE NO.
1 GENERAL DESCRIPTION 2
2
2 DESIGN PHILOSOPHY 2
3 DATA 2
4 STATIC DESIGN OF PUMP FOUNDATION 3
5 ECCENTRICITY CHECKS & INERTIA CALCULATIONS 7
6 CALCULATION OF SPRING CONSTANTS & DAMPING RATIOS 10
7 CHECK FOR VARIOUS SHEAR MODULUS VALUES 13
8 STABILITY CHECKS 15
9 REINFORCEMENT CALCULATION 16
APPENDIX-A LOAD INPUT
ANALYSIS & DESIGN CALCULATION FOR BFP FOUNDATION
Designed by Checked by Approved by
1.0 GENERAL DESCRIPTION:
1.1 SCOPE
The purpose of this calculation is to design the foundation of the centrifugal pump (6 HDX 24A).
1.2 STANDARDS
vendor drawing.Flowserve Drawing NO 50015HE0673 Refer Appendix -A
Arya, S., O'Neil, M., & Pincus, G. (1981). Design of Structures and Foundations for Vibrating Machines. Gulf Publishing Company.
ACI 351.3R-04 Foundations for dynamic equipment
DEP 34.00.01.30-GEN Standard design and engineering of onshore structures
DEP 34.11.00.12-GEN Geotechnical and foundation engineering onshore
2.0 DESIGN PHILOSOPHY:
The pump and motor are mounted on an common skid which is supported by a rectangular block foundation resting on soil. The block foundation is designed for the pump and motor weight as per vendor drawing.
3.0 DATA:
3.1 Material Data
Concrete
Design Compr. Strength F'c = 27.5 (4000 psi)
Unit weight of concrete = 24
Unit weight of water = 10
Concrete cover for foundationsCc = 50 mm
Reinforcement
Yield Strength of steel fy = 410 (60000 psi)
unit weight of steel = 78.5
N/mm2
c kN/m3
w kN/m3
N/mm2 KN/m3
4.0 STATIC DESIGN OF PUMP FOUNDATION
4.1. DESIGN DATA 4.1.1 Block Dimensions:
Length in X-direction = 5.4 m
Length in Z-direction = 2.3 m
Height of the Block Above FGL = 0.3 m
Depth of Foundation from FGL D = 1.70 m
Total Height of Block = 2.00 m
Length in Z-direction(Motor/BP Area) Bm = 2.30 m 4.1.2 Pump Data:
Length of the skid in X-direction = 4.50 m
Width of the skid in Z-direction = 2.00 m
Ht.of the skid in Y-direction = 0.25 m
No. of anchor bolts = 12
Anchor Bolts Dia = 42
= 3.84 m
= 1.64 m
Height of shaft from u/s of skid = 0.95 m
Depth of grouting considered = 0.05 m
4.1.3 Motor & BFBP Data:
Length of the skid in X-direction = 5.00 m
Width of the skid in Z-direction = 2.00 m
Ht.of the block in Y-direction = 0.25 m
LB BB HB_AG HB LS BS HS
C/c distance bet. far end bolts along length,La C/C distance bet. far end bolts along width,Ba hS
Lm Bm Hmb
PLAN VIEW SECTION VIEW
X Z CL o f D is ch ar ge Mz Mx LB LS La BB Ba Bs FGL HB_AG Hs D CL of Pump Y hs HB
Designed by Checked by Approved by
4.1.4 Unit Weights:
Unit weight of concrete = 24 kN/m³
Unit weight of Water = 10 kN/m³
Unit weight of soil = 18.87 kN/m³
Co-eff of friction bet. Soil & Concrete µ = 0.35 4.1.5 Stability Limits:
Finished Ground Level Elevation = 100.0 m
Allowable Soil Bearing Pressure at Elevation 98.3 m = 100 kN/m² (Note: Bottom of lean concrete El. is 98.3 m.)
Depth from finished ground to bottom of the foundation, d = 1.70 m Required depth of lean concrete, t = 0.00 m
Allowable bearing pressure at base of mat, = 100 kN/m²
FOS against Sliding = 1.5
FOS against Overturning = 2
FOS against Buoyancy = 1.25
4.2 STATIC LOADS
4.2.1 Pump, Motor & BFBP Weight:
Pump Weight, = 1900 kg = 18.64 kN
Pump rotor Weight, = 570 kg = 5.59 kN (if no vendor data, assume 30% of Pump wt)
Motor Weight, = 2517 kg = 24.69 kN
Motor rotor Weight, = 755.1 kg = 7.41 kN (if no vendor data, assume 30% of motor wt)
Base Weight of BFP, = 2520 kg = 24.72 kN
BP Weight = kg = 0.00 kN
BP rotor Weight = 0 kg = 0.00 kN (if no vendor data, assume 30% of motor wt)
Base Weight of BP, = 0 kg = 0.00 kN
Other = 0 kg = 0.00 kN
Total weight of pump, WP=Pp+ Pm + Pb+Pbp+Pbp+Po = 68.05 kN
Weight of concrete fill inside the skid = 4.5x 2 x 0.25 x 24 = 54 KN
= 5x 2 x 0.25 x 24 = 60 KN
4.2.2 Buoyancy Force:
Buoyancy Force =
= 5.4x2.3x1.7x10 = 211.14 KN
4.3 PRELIMINARY FOUNDATION CHECK: 4.3.1 Check for Plinth Size:
c w s FSliding FOT FBUO Pp Ppr Pm Pmr Pb Pbp Pbpr Pbp Po Wcf1 Wcf2 Fb LB x BB x D x w
= 150 mm = 0.15 m = 75 mm = 0.075 m
Therefore
Min. plinth length required = (2 xDmin)+La+Lm = (2 x 0.15 ) + (3.84+5) = 4.14 m
= = (2x0.075 ) + (4.5+5) = 4.65 m
Min. plinth length required = Max of the above = 4.65 m < 5.4 m
Hence O.K
Min. plinth width required = = ( 2 x 0.15 ) + 1.64 = 1.94 m
= = ( 2 x 0.075 ) + 2 = 2.15 m
Min. plinth width required = Max of the above = 2.15 m < 2.3 m
Hence O.K
4.3.2 Check for Foundation Depth:
Min. foundation depth = 0.60 + L/30 ( Where L is greater of length or width in meters )
= 0.780 m < 2 m
Hence O.K
4.3.3 Check for Foundation Weight:
Foundation weight should be greater than 3 times the total weight of the pump, Machine or Pump total weight, = 68.05 kN
= (5.4 x 2.3 x 2 x 24 )
= 596.16 KN > 3 times the pump weight
Hence O.K
4.3.4 Preliminary Check for Bearnig pressure:
Total Vertical force =
= 68.05 + 54 + 60 + 596.16 = 718.21 KN
Total Vertical force with 50% impact load =
Fyi = 718.21 + 0.5 x 68.05 = 752.24 KN
Moment due to impact load (i.e.25% of pump weight acting laterally at shaft level)
Total Mom in Long. Direction =
at Bottom of base = 0.25 x 68.05 x (0.95 + 0.3 + 1.7 ) = 50.19 KNm
Total Mom in Tran. Direction =
at Bottom of base = 0.25 x 68.05 x (0.95 + 0.3 + 1.7 ) = 50.19 KNm
Maximum Base Pressure =
at founding depth below HPP Minimum bolt edge distance, Dmin Minimum edge of skid to concrete,Cmin
( 2 x Cmin ) + Ls+Lm ( 2 x Dmin ) + Wa ( 2 x Cmin ) + Bs WP Foundation weight, Wf FY WP + Wcf1 +Wcf2+ Wf FY + 50% WP MX Mx_I Mz Mz_I PMAX P / A + MX / ZX
Designed by Checked by Approved by = (752.24 / (4.5 x 2.3 + 5 x 2.3 )) + (50.19 x 6 / (4.5 x 2.3^2 + 5 x 2.3^2 )) = 40.42 < 80 (80% of allowable) Hence O.K = = (752.24 / (4.5 x 2.3 + 2.3 x 5 )) + (50.19 x 6 / (2.3 x 4.5^2 + 2.3 x 5^2 )) = 37.32 < 80 Hence O.K KN/m2 KN/m2 PMAX P / A + MZ / ZZ KN/m2 KN/m2
4.4 DYNAMIC LOADS INPUT 4.4.1 Pump data:
Location No Description Speed
Dynamic forces from vendor data
Vertical Longitudinal Lateral Rocking Pitching
kN kN Fy (kN) Fx (kN) Fz (kN)
1 Pump 5.59 1800 1.68 0 0 0 0 0
2 Motor 7.41 1800 2.22 0 0 0 0 0
3 BP 0.00 0 0.00 0 0 0 0 0
* Dynamic force (kN) = (Rotor weight )x(Rotor speed,r.p.,m) / 6000 ACI 351.3R-04 eq. 3.7 Cl. 3.2.2.1d
4.4.2 Soil & Foundation parameters for Dynamic loads (From Geo tech report )
= 117877
= 0.35
= 0.02
4.4.3 Alloawable limits for design
Allowable eccentricity of C.G.in X-direction,x = 5% = 0.05 x 5.4 = 0.27 m
Allowable eccentricity of C.G.in Z-direction,z = 5% = 0.05 x 2.3 = 0.115 m
C.G.in Y-direction,y = Below TOC = 2 = 2 m
Damped Natural Frequencies shall be less than = 0.8 = 0.8 x 1800 = 1440 rpm
or more than = 1.2 = 1.2 x 1800 = 2160 rpm
Allowable peak-to-peak amplitude = 16 microns Fig 3.7
Range of shear modulus (G) values to consider = 0.5 to 1
5 ECCENTRICITY CHECK & INERTIA CALCULATIONS
(Eccentricity of C.G. of machine+foundation system to be checked in all 3 directions w.r.t. C.G of foundation) Rotor
weight Dynamic force*
(rpm) T (kNm) T (kNm)
Dynamic Shear Modulus( Gdyn ) KN/m2
Poisson ratio,
Soil internal damping ratio (D)
of LB of BB D CL of Pump X Y HB C.G X Z C.G origin
5.1 COMPUTATION OF CG OF BASE BLOCK
Elements Dimensions(m)
Lxi Lzi Lyi* xi(m) zi(m) yi(m)
Pump - - - 1.23 1.28 3.00 - - -Motor - - - 3.14 1.20 3.00 - - -BP - - - -Skid1 Skid2 Mat_BFP Motor/pump 5.00 2.30 2 11.5 2.50 1.15 1.00 28.8 13.2 11.5 Total 11.50 6.86 3.63 7.00 28.8 13.2 11.5
* Concrete fill in skid and grout thickness included in height of block for CG Calculation
C.G. of Foundation ,x dir-, X = = 28.75 / 11.5 = 2.500 m
C.G. of Foundation ,z dir-, Z = = 13.225 / 11.5 = 1.150 m
C.G. of Foundation ,y dir-, Y = = 11.5 / 11.5 = 1.000 m
5.2 COMPUTATION OF CG OF MACHINE & FOUNDATION BLOCK
Elements Weight
Wi (kN) xi zi yi mixi mizi miyi
BFP 18.64 1.9 1.23 1.28 3.00 2.33 2.42 5.70 Motor 24.69 2.52 3.14 1.20 3.00 7.91 3.02 7.56 BP 0.00 0 0.00 0.00 0.00 0 0.00 0.00 Skid1 0 0 0.00 0.00 0.00 0 0.00 0.00 Skid2 0 0 0.00 0.00 0.00 0 0.00 0.00 Mat_BFP 0 0 0.00 0.00 0.00 0 0.00 0.00 Mat_Motor 552 56.27 2.50 1.15 1.00 141 64.71 56.27 Total 595.33 60.69 6.86 3.63 7.00 151 70 70 = = 150.91154/60.69 = 2.49 m = = 70.157/60.69 = 1.16 m = = 69.53/60.69 = 1.15 m
5.3 ECCENTRICITY OF CG OF FOUNDATION SYSTEM W.R.T. BASE BLOCK(check with limits in 4.4.3) = 2.5 - 2.49
= 0.01 m < 0.27 m Hence OK
Area
(m2) Coordinates of CG of elements Static moment of area
Ai Ai*Xi Ai*Zi Ai*Yi
AiXi/Ai
AiZi/Ai
AiYi/Ai
Mass
mi Coordinates of CG of elements Static moment of mass (kNSec2) kNsec2/m Combined C.G. in X direction,xo mi.xi/mi Combined C.G. in Z direction,zo mi.zi/mi Combined C.G. in Y direction,yo mi.yi/mi Eccentricity in X direction (x-x0) X X origin
= 1.15 - 1.16
= -0.01 m < 0.115 m Hence OK
= 1.15 < 2 m Hence OK
5.4 MASS MOMENTS OF INERTIA AND INERTIA RATIOS (Table 4.6 of Arya, Neil & Pincus)
Elements
mass mi
xoi zoi yoi
BFP 1.9 - - - 1.26 -0.115 -1.85 6.528 3.1 9.5 Motor 2.52 - - - -0.65 -0.04 -1.85 8.629 1.1 9.7 BP 0 - - - 2.49 1.16 1.15 0.000 0.0 0.0 Skid1 0 0.000 0.000 0.000 2.49 1.16 1.15 0.000 0.0 0.0 Skid2 0 0.000 0.000 0.000 2.49 1.16 1.15 0.000 0.0 0.0 BFP_Mat 0 0.000 0.000 0.000 2.49 1.16 1.15 0.000 0.0 0.0 Motor_Mat 56.27 43.562 142.035 135.986 -0.01 0.01 0.15 1.272 0.0 1.3 Total 60.69 43.562 142.035 135.99 16.43 4.13 20.49 Iox = Ix = = Iox/Ix = 43.562 + 16.429 = 59.991 + 60.69 x 1.15^2 = 59.991 / 140.254 = 60.0 = 140.3 = 0.428 Ioz = Iz = = Ioz/Iz = 135.986 + 20.486 = 156.472 + 60.69 x 1.15^2 = 156.472 / 236.735 = 156.5 = 236.7 = 0.661 Ioy = Iy = Ioy = 142.035 + 4.126 = 146.16 = 146.16 = 140.25 = 236.74 = 146.16 Eccentricity in Z direction (z-z0) in Y direction, y0
mass moment of inertia of individual elements abt its own
axis Distance between common C.G. & C.G. of individual elements (m)
Mass moment of inertia of whole system about common
CG
kNsec2/m *(LyiIx = mi /12 2+Lzi2) *(LxiIy = mi /12 2+Lzi2) *(LxiIz = mi /12 2+Lyi2) xo - xi zo - zi yo - yi (yoiIx = mi* 2+zoi2) (xoiIy = mi* 2+zoi2) (xoiIz = mi* 2+yoi2)
Mass Moment of Inertia of the whole system about each axis passing through the common C.G. & perpendicular to the plane of vibration
Mass Moment of Inertia of the whole system about each axis passing through the centroid of the base area &
perpendicular to the plane of vibration
Ratio between moments of inertia 1/12 x mi(lyi2+l zi2)+mi(yoi2+zoi2) Iox + m.yo 2 x kN sec2-m kN sec2-m 1/12 x mi(lxi2+l yi2)+mi(xoi2+yoi2) Ioz + m.yo2 z kN sec2-m kN sec2-m 1/12 x mi(lxi2+l zi2)+mi(xoi2+zoi2) kN sec2-m kN sec2-m
Mass moment of inertia effective against
rocking excitation , I kN sec2-m
Mass moment of inertia effective against pitching
excitation ,I kN sec2-m
Mass moment of inertia effective against cross
= 60.69
6 CALCULATION OF SPRING CONSTANTS & DAMPING RATIOS
Length in X-direction = 5.4 m
Average Width in Z-direction Bavg = 2.3 m
L/B Ratio / Bav = 5.4 / 2.3 = 2.35
B/L Ratio / = 2.3 / 5.4 = 0.43
depth of foundation embedment below grade, h = 1.70 m
6.1 SPRING CONSTANTS (Table 4.1 & 4.2 of Arya, Neil & Pincus - Refer Appendix-B)
Embedment coefficients Spring Constant
Fig4.1(Arya) Vertical Y Ky = = = = ### = (2.3x5.4/3.14)^0.5 = 1+0.6x(1-0.35)x(1.7/1.988) = 117877/(1-0.35)x2.262x (2.3x5.4)^0.5x1.334 in the Fig 4.1) = ### = 1.334 = 1928524 kN/m Kx = = = = ### = (2.3x5.4/3.14)^0.5 = 1+0.55x(2-0.35)x(1.7/1.988) = 2*(1+0.35)x117877x0.977x (2.3x5.4)^0.5x1.78 = ### = 1.78 = 1950600 kN/m = = = = ### = (2.3x5.4^3/3x3.14)^0.25 = 1+1.2x(1-0.35)x(1.7/2.49)+ = 117877/(1-0.35)x0.635x 0.2x(2-0.35)x(1.7/2.49)^3 (2.3x5.4^2)x1.638 = ### = 1.638 = 12650821 kN/m/radian = = = = ### = (2.3^3x5.4/3x3.14)^0.25 = 1+1.2x(1-0.35)x(1.7/1.625)+ = (117877/(1-0.35)x0.433x 0.2x(2-0.35)x(1.7/1.625)^3 (2.3^2x5.4)x2.194
ratio in Fig 4.1) = ### = 2.194 = 4921411 kN/m/radian
6.2.0 CALCULATION OF DYNAMIC FORCES (in the absence of vendor data)
Location No Description Speed
kN kN X(m) Y(m) Z(m) Xo (m) Yo (m) Zo(m)
1 Pump 5.59 1800 1.677 1.227 3.000 1.275 2.490 1.150 1.160
Effective Mass for translation (both Vertical and
Horizontal) excitation ,mc kN sec2/m
LB LB BB LB Mode of Vibration Geometry
factors Equivalent radius r0
ηy (BL/)0.5 1+0.6(1-)(h/r 0) (G/(1-)) y (B L)0.5 ηy y (Refer z value Horizontal, X,Z ηx (BL/)0.5 1+0.55(2-)(h/r 0) 2(1+)G x(BL)0.5 ηx x Rocking η K (BL3/3)0.25 1+1.2(1-)(h/r 0)+0.2(2-)(h/ro)3 (G/(1-)) (BL2) ηΦ Pitching η K (B3L/3)0.25 1+1.2(1-)(h/r 0)+0.2(2-)(h/ro) 3 (G/(1-)) (B2L) η (Refer for BB/LB Rotor
weight Dynamic force Point of Application at Shaft Location* Combined C.G of machine and foundation w(rpm)
2 Motor 7.41 1800 2.223 3.14 3.000 1.200 2.490 1.150 1.160 *Pump and motor locations assumed at L/4 & 3L/4 in X-direction respectively.
6.2.1 Dynamic forces No Description Pitching Fz(kN) Fx(kN) Fy(kN) 1 Pump 1.677 0.000 1.677 3.295 2.118 0.193 2 Motor 2.223 0.000 2.223 4.201 1.438 0.089
Total transmitted force = 3.900 0.000 3.900 7.497 3.556 0.2818
* Longitudinal translation not considered since it is usually lesser than that of Lateral translation
Mass (or Inertia) ratio Embedment factor Damping ratio D
Vertical Y By Dy = = = = (1-0.35)x595.33 / = (1+1.9x(1-0.35)(1.7/1.988))/(1.334)^0.5 = (0.425x1.78)/(0.653)^0.5 (4x18.87x1.988^3) = 0.653 = 1.780 = 0.936 Bx Dx = = = = (7-8x0.35)x595.33 / = (1+1.9x(2-0.35)x(1.7/1.988))/(1.78)^0.5 = (0.288x2.759)/(0.811)^0.5 (32x(1-0.35)x18.87x1.988^3) = 0.811 = 2.759 = 0.882 = = = = (3x(1-0.35)x140.254) / = (1+0.7x(1-0.35)x(1.7/2.49)+ = (0.15x1.27/((1+1.6x0.186)x (8x(18.87/9.81)x2.49^5) 0.6x(2-0.35)x(1.7/2.49)^3)/(1.638)^0.5 (1.6x0.186)^0.5) = 0.186 = ### ** = 1.270 = 0.269 = = = = (3*(1-0.35)x236.735) / = (1+0.7x(1-0.35)x(1.7/1.625)+ = (0.15x1.762/((1+1.122x2.65)x 8x(18.87/9.81)x1.625^5) 0.6x(2-0.35)x(1.7/1.625)^3)/(2.194)^0.5 (1.122x2.65)^0.5) = 2.65 = ### ** = 1.762 = 0.039 5 3 2 1 0.8 0.5 0.2 1.08 1.11 1.143 1.219 1.251 1.378 1.6
6.3.1 SUMMARY OF DAMPING RATIOS
(Final D is 2/3 of Theoritical value + soil internal damping ratio or 0.7 whichever is lesser )
Final Damping ratio
Vertical 0.02 2/3 x 0.936 + 0.02 = 0.644 0.70 Dy = 0.500
Lateral
translation Longitudinal translation* Vertical translation
Rocking (Due to Lateral
translation) shaft ecentricity)Rocking (due to
Mψ1 (kNm) MØ'-kNm Mψ2 -kNm
6.3 CALCULATION OF EQUIVALENT DAMPING RATIO (Tables 4.3 & 4.4 of Arya, Neil & Pincus)
Mode of Vibration y (1-) W / (4r03) (1+1.9(1-h/r 0)) / (ηy)0.5 0.425 y / (By)0.5 Horizontal, X,Z x (7-8) W / (32(1-r03) (1+1.9(2-h/r 0)) / (ηx) 0.5 0.288 x / (Bx)0.5 Rocking B D 3(1-) I /(8 r05) (1+0.7(1-h/r 0)+0.6(2-h/ro) 3))/(η 0.5 0.15 / ((1+nB (nB0.5) n Pitching B D 3(1-) I /(8 r05) (1+0.7(1-h/r 0)+0.6(2-h/ro)3))/(η0.5 0.15 / ((1+nB (nB0.5) n
** Values for nnfor various values of BTable 4.5 of Arya, Neil & Pincus, reproduced below)
B
nn
Mode of
Horizontal 0.02 2/3 x 0.882 + 0.02 = 0.608 0.70 Dx = 0.200
Rocking 0.02 2/3 x 0.269 + 0.02 = 0.199 0.70 = 0.100
Pitching 0.02 2/3 x 0.039 + 0.02 = 0.046 0.70 = 0.046
6.4 CALCULATION OF UNDAMPED NATURAL FREQUENCIES
Vertical (60/(2x3.14))x(1928524/60.69)^0.5 = 1702 (1702x(1-0.5^2)^0.5 = 1474
Horizontal (60/(2x3.14))x(1950600/60.69)^0.5 = 1712 (1712x(1-0.2^2)^0.5 = 1677
Rocking (60/(2x3.14))x(12650821/140.254)^0.5 = 2868 (2868x(1-0.1^2)^0.5 = 2854
Pitching (60/(2x3.14))x(4921411/236.735)^0.5 = 1377 (1377x(1-0.046^2)^0.5 = 1376
6.5 CALCULATION OF FREQUENCY RATIO , MAGNIFICATION FACTOR , AMPLITUDE ,
TRANSMISSIBLITY FACTOR AND TRANSMITTED FORCE (Table 1.4 of Arya, Neil & Pincus, Ref.Appendix-B)
(Since the machine will operate at constant speed, formulae associated with sinusoidal force of constant amplitude are used in the dynamic analysis)
Magnification factor, M Transmissiblity factor, Tr
Vertical,Y 1.058 0.940 1.368 5.334 kN 2 Micron
Horizontal,X 1.051 2.306 2.502 0.000 kN 0 Micron
Horizontal,Z 1.051 2.306 2.502 9.758 kN 5 Micron
0.628 1.616 1.628 12.666 kNm 0.00 radians
1.307 1.391 1.401 4.983 kNm 0.00 radians
6.6 FORCES & AMPLITUDES FOR VARIOUS ROTOR POSITIONS 6.6.1 Dynamic loads (Fo) - In-phase & 180 degrees out-of-phase
Rotor Position Pitching
Fz(kN) Fx(kN) Fy(kN)
In Phase 1 3.900 - - 7.497 -
-In Phase 2 - - 3.900 - 0.281775 3.556
Out of Phase 3 0.546 - - 1.010 -
-Out of Phase 4 - - 0.546 - -0.06279 0.680
6.6.2 Transmitted Force (Ftr) on Foundation due to various Rotor positions
Rotor Position Pitching
Fz(kN) Fx(kN) Fy(kN)
D
D
Mode of Vibration
Undamped Natural frequency, n (rpm)
[ (60/2π)x(K/m)0.5]
Damped Natural frequency mr
[n (1-D2)0.5] (rpm)
Mode of
Vibration Frequency ratio, r force/moment Transmitted Displacement response, Ax
n 1/((1-r2)2+(2Dr)2)0.5 (1+(2Dr)2)0.5 / [(1-r2)2+(2Dr)2]0.5 FtrT
rFo M(Fo/K)
Rocking,
Pitching,
Load
Case TranslationLateral Longitudinal Translation TranslationVertical Translation Force)Rocking (Due to Rocking (Due to shaft eccentricity)
MØ' (kNm) M
Ø2 (kNm) Mψ
1 (kNm)
Load
Case TranslationLateral Longitudinal Translation TranslationVertical Translation Force)Rocking (Due to Rocking (Due to shaft eccentricity)
MØ' (kNm) M
Ø
2 (kNm) M
In Phase 1 9.758 - - 12.207 -
-In Phase 2 - - 5.334 - 0.459 4.983
Out of Phase 3 1.366 - - 1.645 -
-Out of Phase 4 - - 0.747 - -0.102 0.953
6.6.3 Amplitudes (Ay)
(Maginfication factor M x Dynamic loads Fo / Spring constants K )
Translation Displacement Rotational Displacement
Rotor Position
In Phase 1 5 - - 9.57E-07 -
-In Phase 2 - - 2 - 3.60E-08 1.01E-06
Out of Phase 3 1 - - 1.29E-07 -
-Out of Phase 4 - - 0 - 0 1.92E-07
6.6.4 Total Amplitudes Calculation
(Maginfication factor M x Dynamic loads Fo / Spring constants K )
Phase Amplitude Calculations
Vertical Ky In phase = 2+0E-06x5.4/2+1E-06x2.3/2 = 2 < 16 microns SAFE
Out of phase = 0+0x5.4/2+0.2E-06x2.3/2 = ### < 16 microns SAFE
Horizontal Kx In phase = 0+1E-06x (3-1.15) = ### < 16 microns SAFE
Out of phase = 0+0.2E-06x (3-1.15) = ### < 16 microns SAFE
Horizontal Kz In phase = 5+1E-06x (3-1.15) = 5 < 16 microns SAFE
Out of phase = 1+0.1E-06x (3-1.15) = 1 < 16 microns SAFE
7.0 CHECK FOR VARIOUS SHEAR MODULUS VALUES
Shear Modulus values considered = 0.50G 0.63G 0.76G 0.89G 1.00G
7.1 SPRING CONSTANTS FOR VARIOUS G VALUES
G Vertical Ky Horizontal kx Translational kz
KN/m KN/m KN/m kN/m/radian kN/m/radian 0.50G 964262 975300 975300 6325410 2460706 0.63G 1214970 1228878 1228878 7970017 3100489 0.76G 1465678 1482456 1482456 9614624 3740273 0.89G 1716386 1736034 1736034 11259230 4380056 1.00G 1928524 1950600 1950600 12650821 4921411
7.2 SUMMARY OF FREQUENCIES FOR VARIOUS 'G' VALUES WITH CHECK FOR FREQUENCY RANGE*
G Vertical,Y Horizontal,X Horizontal,Z
Load
Case Due to Fz ( micron ) Due to Fx ( micron ) Due to Fy ( micron ) Due to M
1 (Rad) Due to M 2 (Rad) Due to M' (Rad) Mode of Vibration AY+ψ/2+Ø*LB/2 AY+ψ/2+Ø*LB/2 AX+ØY-Yo) AX+ØY-Yo) Az+ψY-Yo) Az+ψY-Yo) Rocking KØ1 Pitching K ψ 1 Rocking, Pitching,
G
rpm Check rpm Check rpm Check rpm Check rpm Check
0.50G 1042 <20% ok 1186 <20% ok 1186 <20% ok 2018 - 973 <20% ok
0.63G 1170 <20% ok 1331 <20% ok 1331 <20% ok 2265 >20% ok 1092 <20% ok
0.76G 1285 <20% ok 1462 Not ok 1462 Not ok 2488 >20% ok 1199 <20% ok
0.89G 1391 <20% ok 1582 Not ok 1582 Not ok 2692 >20% ok 1298 <20% ok
1.00G 1474 - 1677 - 1677 - 2854 >20% ok 1375 <20% ok
* Frequencies are damped natural frequencies
** Here G is maximum value of G. For clays 88% of this value shall be used. (Ref: Page 66 AOP)
7.3 SUMMARY OF AMPLITUDES FOR VARIOUS 'G' VALUES WITH CHECK FOR AMPLITUDE LIMIT G Check Vertical,Y 0.50G 1.727 0.380 0.759 2.960 2 2 microns SAFE 0.63G 1.538 0.486 0.892 3.479 2 2 microns SAFE 0.76G 1.401 0.588 1.013 3.949 2 2 microns SAFE 0.89G 1.294 0.685 1.121 4.371 2 2 microns SAFE 1.00G 1.221 0.760 1.199 4.677 2 2 microns SAFE Horizontal,X 0.50G 1.518 0.695 0.813 0.000 0 0 microns SAFE 0.63G 1.352 1.011 1.150 0.000 0 0 microns SAFE 0.76G 1.231 1.403 1.564 0.000 0 0 microns SAFE 0.89G 1.138 1.843 2.025 0.000 0 0 microns SAFE 1.00G 1.073 2.197 2.391 0.000 0 0 microns SAFE Horizontal,Z 0.50G 1.518 0.695 0.813 3.171 3 3 microns SAFE 0.63G 1.352 1.011 1.150 4.484 3 3 microns SAFE 0.76G 1.231 1.403 1.564 6.099 4 4 microns SAFE 0.89G 1.138 1.843 2.025 7.899 4 4 microns SAFE 1.00G 1.073 2.197 2.391 9.326 4 4 microns SAFE 0.50G 0.892 3.687 3.745 29.129 4.53E-06 0.63G 0.795 2.495 2.526 19.649 2.44E-06 0.76G 0.723 2.005 2.026 15.760 1.62E-06 0.89G 0.669 1.759 1.775 13.807 1.22E-06 1.00G 0.631 1.626 1.639 12.750 1.00E-06 0.50G 1.85 0.412 0.418 1.485 5.95E-07 0.63G 1.648 0.581 0.587 2.088 6.66E-07 0.76G 1.501 0.793 0.801 2.848 7.54E-07 0.89G 1.387 1.072 1.081 3.845 8.71E-07 1.00G 1.309 1.382 1.392 4.950 9.99E-07 Mode of
Vibration Frequency ratio, r Magnification factor, M Transmissiblity factor, Tr force/moment Transmitted
Amplitude (Microns/rad ) Amplitude, Total Rocking, Pitching,
8 STABILITY CHECKS
8.1 SUMMARY OF TRANSMITTED FORCE /MOMENT
S.No Mode of Vibration
1 Vertical Translation 4.677
2 Lateral Translation -Z 9.326
3 Rocking about X-axis 29.129
4 Pitching about Z-axis 4.950
8.1.1 Calculation of additional loads due to Transmitted force /moment
Total Horizontal load in Z-direction = 9.326+29.129/(2+0.25+0.95+0.05)
= 18.29 kN
8.2 CHECK FOR BEARING PRESSURE:
Total Vertical force = 718.21 kN
Total Vertical force(with impact load) = 752.24 kN
Total Mom in Tran. Direction =
at Bottom of base = 50.19+18.29x(2+0.25+0.95+0.05) = 109.63 KNm
Maximum Base Pressure =
at founding depth below HPP = 752.24/(5.4x2.3)+109.63x6/(5.4x2.3^2)
= 83.594 > 80
Revise the size 8.3 CHECK FOR BUOYANCY:
The critical case for buoyancy check is, when the pump is under maintenance condition. So the self weight of the block itself has to resist the buoyancy force.
Buoyancy Force = 211.14 KN (Cl.4.2.2) Transmitted Force/Moment kN / kNm Thz FY FYi
Mx Mz_I + Thz x distance b/w shaft & bottom of base
PMAX P / A + MX / ZX
KN/m2 KN/m2
Resisting Force =
= 5.4x2.3x(1.7+0.3)x24 = 596.16 KN
FOS for Buoyancy Check = 596.16 / 211.14
= 2.82 > 1.25
Hence O.K 8.4 CHECK FOR OVERTURNING:
Resisting Moment in Tran. Direction = (718.21 - 211.14) x2.3 / 2 = 583.13 KN-m
FOS against Overturning in Z-axis, = 583.13 / 109.63 = 5.3 > 2
Hence O.K
8.5 CHECK FOR SLIDING
Frictional co-efficient m = = 0.35
Sliding Force along Z-axis = = 35.30 KN
Frictional Resistance = = 0.35x(718.21-211.14) = 273.2 KN
Actual Factor of Safety against Sliding, FOS = 273.163 / 35.3025 = 7.74 > 1.5
Hence O.K
9 REINFORCEMENT CALCULATION:
Provide T 20 @ 200 c/c E/W Top and Bottom of Footing
Provide T 20 @ 200 c/c Sides of Footing
Provide T 12 @ 600 c/c Triaxial Vertical Only for blocks with depth more than 1.0 m
Provide T 12 @ 600 c/c Triaxial Horizontal
9.1 CHECK FOR WEIGHT OF REINFORCEMENT
Weight of reinf. required(footing) = 5.4 x 2.30 x 2.00 x 30 = 745.20 kg
Reinforcement provided : Footing
Top 28 bars x ( 2.30 + 2.000 ) 2.47 = 297.39 kg
13 bars x ( 5.4 + 2.000 ) 2.47 = 237.61 kg
Bottom same as that in top = 535.00 kg
Sides (horz) 9 bars x 7.7 x 2.47 = 171.17 kg
Fresist LB x BB x (D+HB_AG) x c
Considering water table at ground level, vertical force will be taken as FY - Fb
MRz
FOSZ
Considering water table at ground level, vertical force will be taken as FY - Fb
FSz Fz_I
FRr x (FY - Fb)
As the foundation is designed as a block foundation, a minimum shrinkage reinforcement of 30kg/m3 shall be
9 bars x 7.7 x 2.47 = 171.17 kg
Triaxial (Horz) 8 bars x 2.3 x 0.89 = 16.38 kg
3 bars x 5.4 x 0.89 = 14.42 kg
Triaxial (Ver) 16 bars x 2 x 0.89 = 28.48 kg
Total Reinforcement in Foundation = 1471.62 kg > 745.200 kg
Hence O.K
9.2 REINFORCEMENT SKETCH:
T20 - 200 c/c E/W Top and Bottom
T20 - 200 c/c T.O.G EL+100.300
F.G.L EL+100.000
Triaxial 16Nos of T12 - 600 c/c
B.O.F EL+98.300
Triaxial 8Nos of T12 - 600 c/c Triaxial 3Nos of T12 - 600 c/c
SECTIONAL ELEVATION
9.5 9.7 0.0 0.0 0.0 0.0 1.3 20.49
Mass moment of inertia of whole system about common
CG
Iz = mi* (xoi2+yoi2)
Ratio between moments of inertia
Spring Constant 117877/(1-0.35)x2.262x 2*(1+0.35)x117877x0.977x 117877/(1-0.35)x0.635x (117877/(1-0.35)x0.433x Zo(m) 1.160 Combined C.G of machine and foundation
1.160 0.193 0.089 0.2818 Damping ratio D Rocking (due to shaft ecentricity) Mψ2 -kNm
2 Micron 0 Micron 5 Micron 0.00 radians 0.00 radians Pitching -3.556 -0.680 Pitching Displacement response, Ax M(Fo/K) Mψ1 (kNm) Mψ1 (kNm)
-4.983 -0.953 Rotational Displacement -1.01E-06 -1.92E-07 Amplitude Calculations SAFE SAFE SAFE SAFE SAFE SAFE Due to M' (Rad)
Check SAFE SAFE SAFE SAFE SAFE SAFE SAFE SAFE SAFE SAFE SAFE SAFE SAFE SAFE SAFE
Table 4-1 Ref. Suresh Arya , O'Neill & Pincus - Equivalent Spring Constants for Rigid Circular and Rectangular Footings
Figure 4-2 Ref. Suresh Arya , O'Neill & Pincus - Embedment coefficients for spring constants
Table 4-4 Ref. Suresh Arya , O'Neill & Pincus - Effect of Depth of Embedment on Damping Ratio
Table 4-5 - Ref. Suresh Arya, O'Neil & Pincus