كتاب تعليم برنامج بروكن 2033

Page 1

:

Prepared by: Eng. Mohammed Al-Dhabiany

"#$ % &'( ) * + " $ ,-( . / - 0 ) + .10 Prokon2003 ! 89: ; ( -4 < 7 + *# , ( * 45 6 0 3 ( .) "#$ C/ D9; E 0 < (Prokon2003 , ( . / = > ?@ A B .H4/= .<$ 45 F ) 4/ I ,!G 04! A F - ( .) * + ? = * G G )!9 /; G )M/ " N K >( " J=, K + * 0 ) 4 L ( .P , .<$ ) 4/ .,- O ) )M/ > A

Prepared by: Eng. Mohammed Al-Dhabiany

I(G L F (G 8 / P 0 :" 4=5 .<> F/ Q $ #*( 7 + *J 9: ( R ; F/ )/ - - S A * Y S Y S ( (desktop) V < P=* F/ 8 4 4 ) 4 !G F/ EM1 P N S UT (start menu)Z

-G .<$ ' :( )\ + > $ % - ]4* % ^ U[

Prepared by: Eng. Mohammed Al-Dhabiany

file, edit, view, insert, ) .` (Menu) Y S `' A4< - > > A a J .<$ ( U_

.) J (L IJ5 Y 4 8&: Q $ 74S ]4*( (tools, setting, programs, help . - '& Y 4 .N*# - - ( (Tab)I &0 4 4: AG 8 , c& ( :G $ Ub :V - :( (analysis, steel, connections, concrete, timber, masonry, cad and detailing, general, geotechnical) (Concrete, Cad and detailing) :( &0 4 8&: -&0 Q > F d =-#*(

.<$ 0 ' 8&0 % - / EM1 ( (Concrete) /' d40 8L N 6L > f Ue ) * + ,

: -G ' :( )N/ + ) * + D 9 G , `' F/ (Concrete) 6&0 c4 -( Ug CB(continuous beam/slab), Captain(posted tension beam and slab), FESD(finite elements slab design), Slab(rectangular slab panel design), RecCol(rectangular column design), CirCol(circular column design), GenCol(general column design), Wall(retaining wall design), base(base design)

.N* .<$ 4: ' *G d40 8L#N 6L > %! D9 .' * J < !( (continuous beam and slab) ,

` L 0 (Continuous beam) , * Uh

Prepared by: Eng. Mohammed Al-Dhabiany

` L (Continuous beam) ,-

.N*G .<$ 0 ' ) ,- 0 D / (Continuous beam and slab)I ,- F/ EM@ UT (continuous beam and slab) ,

(Continuous beamI ,- 6&0 )) 8&0 - U[

Prepared by: Eng. Mohammed Al-Dhabiany

. / - V )!4 - ( &0 4 8&: V-L#*( ) 0 &0 4 6 ( (File) ) Y S A4< - 8&0 8&: U_ : -G ' ;!L - , ( . / / .<$ 0 ' :(File) Y S UZ

( * A(9+ ,- P N open) % &'( ( ! ,- P N new) F/ ) Y 8&: c4 -( ( , aN save and save as ) F/ 1! c4 -( 4< L 5 4:( (Code of practice) :( , " 4=5 F ( F/ 1! c4 -( ) 8&0 - (Code of practice) F/ EM1 (

3 (Codes) K A a J ( (BS8110-1997 ` 0 4:() ) C0( , H4/= 4< L + .)/ N 3 - % & ( ) 4 Prepared by: Eng. Mohammed Al-Dhabiany

: -G ' &0 4 8&:( ." = I 5 ! ( ) 0 &0 4 6 A4< -( :(Input) 6&0 UH (input) 6&0 UT

input 6&0 ) 0 &0 4 i M,i <) * < /

.D =5G 0 L9 &: F/ EM@ :8&0 .' 0 . N A4<! D =5 4 ( 7 0

Prepared by: Eng. Mohammed Al-Dhabiany

:) -G " 4/ I 5 8&0 8&: 0 !( : (Parameters) 6&0 UT

Fcu: (Compressive strength of concrete ) * + ( ) Fy: (Yield strength of main steel Y !

( ) Fyv: (Yield strength of stirrup steel (stirrup)j ! ( ) % Redistribution: (Percentage of moment redistribution to be applied) Downward /Optimized redits.: (Method of redistribution 79 ?!R4- 6 ! k) D for downward or O for optimized :( Cover to the center top (c4/ !

=S l, F c4/ ) * + P=* * + D =M ) Cover to the center bot. ( /N !

=S l, F c4/ ) * + P=* * + D =M ) Dead load factor (in ULS =1.4) Live load factor (in ULS = 1.6) Density of concrete.:?= / - & AR4 H 7 + - ) * + 0 `' % live load permanent: (Portion of the live load to be considered as permanent when calculating the creep component of the long term deflection) φ Creep coefficient: the thirty year creep factor use to calculate the final creep strain C .<$ mN F/ I( ;/ * V -( ξ cs Free shrinkage strain: thirty year drying shrinkage of plain concrete C .<$ mN F/ I( ;/ * V -(

Prepared by: Eng. Mohammed Al-Dhabiany

F/ (Position) `' 0 ) + ?k I 5 ! 8&0 8&: 0( : (Sections) 6&0 U[ .(Continuous beam)I I4k

( * )?k o =

I 5 J5 ! .8 Tn A4< ! I( F/ c4 - 8&0 8&: A a J .<$ IJ5 : -G ' .) + ?k Sec NO. : ?= `' % : A4<! A < ! ) O .(span) 6&0 0 ) + *G ?= SL I 5 Bw: web o D: (flange) c ) 0 ?= / /< C Bf-top: )!4/ (flange) o ? ( . = 3 ?= c ( L or T ?= A ' ^ 0 7 + Hf-top: )!4/ (flange) C ? ( . = 3 ?= c ( L or T ?= A ' ^ 0 7 + Bf-bot: /N (flange) o ? ( . = 3 ?= c ( L or T ?= A ' ^ 0 7 + Hf-bot: /N (flange) C ? ( . = 3 ?= c ( L or T ?= A ' ^ 0 7 + Prepared by: Eng. Mohammed Al-Dhabiany

Y-offset: Vertical offset the section. If zero or left blank, the top surface is aligned with the datum line. A positive value means the section is moved up. Web offset: Horizontal offset of the web portion. If zero or left blank, the web is taken symmetrical about the beam/slab centre line. A positive value means the web is moved to the right. Flange offset: Horizontal offset of both the top and bottom flanges. If zero or left blank, the flanges are taken symmetrical about the beam/slab centre line. A positive value means the flanges are moved to the right. (support) 6&0 03D view \ 5 7 + *# ?= F/ p

- " M J % < ! : ) J M J ( (section) 6&0 0 7 SLG M- .10 .<$ N- ]4*( 8&0 mN F/ * )> > F/ ! ]4* ) G ?= G % 5 D q M a J * '

Prepared by: Eng. Mohammed Al-Dhabiany

(span) .' 0 ) + ?k ( (spans)I I 4k I 5 ! 8&0 8&: 0 :(Spans) 6&0 U_

?k 7 SL ( (spans)I I 4k I 5 G .8 b A4< - 8&0 8&: A a J C .<$ IJ5 : -G ' .(span) .' 0 ) + Span NO.: (span)I SL Section length:

(?= ) 0 7 + * ) (span segment)(span)I ) =S I4k ( (span)I I4k =S F span I * 0 span mN F/ = 7 + * L 0 J`

Sec.No.left: span ) =S I r ) ; ( span I ) ; 0 7 + ?= SL Sec.No.right: span ) = ) ; ( span I ) ; 0 7 + ?= SL 7 SLG I 5 IJ5 % ^( I( ; .N* o = 0 M J % < ! :) J

Prepared by: Eng. Mohammed Al-Dhabiany

: (Supports) 6&0 Ub

: -G ' :( ) YL 8 g F/ c4 - (supports) 6&0 A C .<$ IJ5 a J Sup No.: (support)) SL Code C, F:

(column) ? (beam)I B `- ! k

FV < % & fixed A4<- A :( (column) ? (beam)I B `- ! k I 5 74 4 &: 0 free A4<! I 8&: 0(column f : m A4<! A ( ] c J ) + f 0pin A4<- A ( cantilever F/ ) G C V < ( c& (support)I .< ] c J ) + 8&: f - (simply supported beam) I 0 :) J c J ) + B' - ^ simply (support)I ! AG .L 0 c& ( 0 .]

Prepared by: Eng. Mohammed Al-Dhabiany

(support) .' (beam)I B - 4

Column below: D:

span I 8 s;- s0 D ! c Y A ' ^ 4 =S ( (column)I C

B:

c Y (column)I ! SL J ) + B' - ( N\ A ' 0( 4 o

Code P,F:

(support ).' (beam)I B -column. ] = B `- ! k

(] c J ) + f - ( )F V <!( fixed A4<! A ( P V <!(pin A4<! A ] = ( (support) .' (beam)I F/ 4

Column above: D:

span I 8 s;- s0 D ! c Y A ' ^ 4 =S ( (column)I C

B:

c Y (column)I ! SL J ) + B' - ( N\ A ' 0( 4 o

Code P,F:

(support ).' (beam)I F/ column. ] = B `- ! k

(] c J ) + f - ( ) F V <!( fixed A4<! A ( P V <!(pin A4<! A ] = (

Prepared by: Eng. Mohammed Al-Dhabiany

(Beam)I F/ ) I ( ) I G I 5 ! :(Loads) 6&0 Ue

: -G ' :( 8 Tn A4< - (loads) 6&0 A a J C .<$ IJ5 . )

Case D,L:

(D.L factor)H Y /- ) H 1! A a J ( D V < : ( ) I :( (L.L factor)H Y /- ) H 1! A a J (L V < : ( ) I A4<- A ( (span) I SL

Span:

.) ( ) I D 4* / . ?@( ! - (span)I SL V < Wleft:

(span)I r ) ; 0 . S

Wright:

(span)I ) ; 0 . S

a: b: P: a: M: a: Prepared by: Eng. Mohammed Al-Dhabiany

. C =- ! = . C =- ! )= )* . C =- ! = Concentrated load (concentrated load)I C =- = concentrated moment (concentrated moment)I C =- =

) - Y , F AG ); (Input) ) Y 8&0 / ) ) N &0 4 A ) J input 8&0 ? V F V -#- ( r 5G &0 4 IJ5 % ^( 5 S "J5 F/ (View, Reinforcing, Clcsheet) : &0 4 8&:(

0 "J5 f : 4!G A V ( / N 3 (View, Clacsheet) -&0 A .<$ a JA ? = F '& " 4=+ A V;! / N ( (Input)) Y 8&0 ) N &0 4 (View, Clacsheet) . : '^ C -&0 .' 0 Y . > F (View, Clacsheet) -&0 . 0 A ? = * F )/` G I 5 # 74S#* :) J

Prepared by: Eng. Mohammed Al-Dhabiany

.(View, Clacsheet) -&0 .' B/ N-( Y F/ B/, / ' I ` " = I 5 :) J H V - . - Input F (G ) Y 8&0 B ' :) J (View) ) ` ) Y 8&0 Ut

:) ) N &0 4 c4 - (View) 6&0 A a J .<$ IJ5 ) 4 (deflection ) ] G Y o - 8&0 8&:( :(Deflection) 6&0 UT (deflection) ] J F ) P@4! ' Elastic deflection and the long term deflection : -G .<$ 0 '

Prepared by: Eng. Mohammed Al-Dhabiany

(beam). j F % &'( 79 F F/ c4 - 8&0 8&: :(Moments and shear) 6&0 U[ Span uI I4k F/ j ( 79 .< F ) L P@4- ' : .<$ 4: '

) < P@4! ' j / % &'( 7(9 / P / ! ?!R4- N ' o 74 - 8&0 8&: :(Steel) 6&0 U_ : .<$ 0 ' j ( 79 !

r4,

Prepared by: Eng. Mohammed Al-Dhabiany

Z beam . . / Y ? ) . ' l/ o ! 8&0 8&: 0 :(Output file) 6&0 Ub .)= `' (Reaction at the support to the moment and shear I : .<$ 0 '

moment of inertia I H N ' - I( F/ 8&0 8&: c4 - :(Crack file) 6&0 Ue .(for the crack and uncrack sections) )= `' .<$ 0 '

Prepared by: Eng. Mohammed Al-Dhabiany

(Reinforcing))` ` ) Y 6&0 F . ((View)6&0 :( ) ` ) Y 8&0 AG :(Reinforcing) 6&0 U

: ' :( ) 0 &0 4 6& l # - (Reinforcing ) 6&0 A a J C .<$ .<$ 0 ' :(Detailing parameter) 6&0 UT

Prepared by: Eng. Mohammed Al-Dhabiany

^ /5 - " 4/ 1 - : (Detailing parameter) ) N 8&0 A a J C .<$ 74S ]4*( !

v * =S % &'( 04 !

v * I4k .` ) . \ N 79/- A t - B ' :8 F/ D9 .' l! ) + V ; SL .< P@4 l! V e SL F T SL L 5G !

Beam type(1-5)

-G ' . ,N :(

1-Normal beam 2- Slab 3- Flat slab, column strip 4- Flat slab, middle strip Maximum bar length

) * ! - !

v I4k '

Top: Maximum bar diameter

) * ! - (r4/ ) !

v / =S '

Minimum bar diameter

) * ! - (c4/ ) !

v / =S .S

Bottom : Maximum bar diameter

) * ! - ( /N ) !

v / =S '

Minimum bar diameter

) * ! - ( /N ) !

v / =S .S

+ 0 ) mN I 5 E 0 ( 79/- A % < ! :) J STIRRUP : Maximum diameter

) * ! - " < v =S '

Minimum diameter

) * ! - " < v =S .S " </ ) + * ! - c& .<$

Stirrup shape code

BS 4466: 55, 61, 77, 78 and 79. =! 4< 0 8 I <> G First bar mark – Top

F/ G 0 ! v * I( S ) D S ( ] :I ` ’001’ will increment ( ) ! = 9-) to 002, 003 etc.

Cover to stirrup – Top

’A’ will increments( ) ! = 9- ) to B, C, etc. ’B002’ will increment to B003, B004 etc. F/ G " < F ) * + P=* * + D =M

Cover to stirrup – Bot

.N*G " < F ) * + P=* * + D =M

Cover to stirrup – side

V 4; " < F ) * + P=* * + D =M

Minimum stirrups as % of nominal Loose method of detailing:

%Tnn ) &54- (Beam and Slab)I 0

L G &5#- A V;! (Beam and slab)I & N - ! k . +-

Prepared by: Eng. Mohammed Al-Dhabiany

L G &5 - A V;! Supports I BeamI ! . \ N ( : ) " L 5G (

Y or N

&: ?@ A B/10 0 ) )M/ C S F ?@ A ?= * )!9 /; G )M/ " J=, f : AG( : / )!9 /; G )M/ Q $ • With the ’loose method’ of detailing, also referred to as the ’splice-bar method’, span reinforcement and link hangers are stopped short about 100 mm inside each column face. This is done at all internal columns were congestion of column and beam reinforcement is likely to occur. The span bars and stirrups are often made into a cage, lifted and lowered between supports. For continuity, separate splice bars are provided through the vertical bars of each internal column to extend a lap length plus 100 mm into each span. Top bars will extend over supports for the required distance and lapped with nominal top bars or link hangers. Allowance is made for a lap length of 40¡Ď† and a 100 mm tolerance for the bottom splice bars that are acting in compression. • Alternatively, where accessibility during construction allows, the 'normal' method of detailing usually yields a more economical reinforcement layout. This method allows bottom bars to be lapped at support centre lines. Top bars will extend over supports for the required distance and lapped with link hangers. Where more practical, top bars over adjacent supports may be joined. Adjacent spans are sometimes detailed together. LR F/ EM1 G : 8&0 F I45 7 V;! 8&0 8&: 0 " 4/ 0 ' I 5 : .<$ 0 'Generate reinforcing

: EM@

:.<$ 0 ' Y /- (Main reinforcing) 8&0 F . * C L9 F/ EM1 Prepared by: Eng. Mohammed Al-Dhabiany

:(Main reinforcing) 6&0 U[

%- /= ? V* / M 0 ! 8 x A4< ! I( F/ c4 - 8&0 8&: A a J .<$ : ' :( YJ 0 : ' f - ( ) , V - P / ! =S ( y4 (

Bars

(Parameters) 6&0 0Fy,Fyv I 5 Y /-

! ]4* !

y4 A O F/ G D P / ! . / -

Mark

7 SL ( ] D 4* ) 8&0 0 )- 5 c& E mN 7 + ! ]4* ..! ( ) + F/ EM1 E M- % < ! ' SC

!

v 0 = .<>

Span

: =! 4< 0 8 I <>G 20, 32, 33, 34, 35, 36, 37, 38, 39 and 51. Span I SL

Offset

v ! F span . r ) ; )0 .) Span I L ! F/ Span I !

v * ! A4<- V * SL ' 0

Prepared by: Eng. Mohammed Al-Dhabiany

v * ! ) ) 5 F/ 8L#N 6L > A4<- ) C .<$ 0 o > > F/ a J :) J . G A4/ 8L#N 6L ># ) L $ !

Y 0 M J ( 7 SLG M-( )*L F t ! < ( / . * A L ' Y ( :) J . 0 D9 .' 6 Y 0( . l$ <- ]4* ( 8&0 mN F/ * 0 ! ' v I4k

Length

Hook or bend F/ c4 ! v A ' ^

Hook

L or R (left or Right) L 0 ( !

v * 0 L F @ N! A 0 )3L 0 B' - 0

!

v * ?S4

Layer

.N*G 0 7 l, 0 F/ G 0 .:T or M or B (dLRG A4/ ) H4/= Y !

?!R4- ! 8&0 /N D9; 0 *L 4 ( a J :) J .) L . V F ( G A4/ ) C = Y !

P!R4-( E+ A4<! A 6 ? * F/ = * c& M J ( !

z * ( L =S M- % < ! dLRG A4/ E+ E ! G A4/

Prepared by: Eng. Mohammed Al-Dhabiany

:( Stirrup) 6&0 Ub

: ' :( 8 e F/ c4 - 8&0 A a J C .<$ IJ5 ) < SL

Stirrup Number

`' 7 + * F #;/- S ) O 8&0 8&: /- 8&0 0 + * ! F ) </ SL 7 + * - c& A < 0 + *G ) ' `' ] - V;! ) ( j r4S - " </ .<> .) 0 ?= SL

Section Number

(u Sections) 6&0 0 ) 0 ' ?= SL V ' " < 0 ) + * !

v * =S( y4

Bar

Mild steel ! " < 0 7 + ! :) J (High strength steel. 9 - GY or T )m (R V <! % & ( Mark Shape Code

" </ . / - ! c .5 ) < .<> : : =! 4< 0 8 I <>G BS4466: 55, 61, 77, 78 and 74.

Prepared by: Eng. Mohammed Al-Dhabiany

:( Shear Reinforcing) 6&0

: ' 8 e A4< ! I( F/ c4 - 8&0 8&: A a J C .<$ ) 8&0 0 .5 ' ) < SL

Stirrup Number

/- ) < ( ) ' .' )0

Spacing Span

Span I SL

Offset

) ' I( F Span . r ) ; )0 J5 " < ?!R4- ) = I4k

Length

.%- /= V )0 @G ( .! / L + % f !( 1!( ) 4/= " 74 ! :) J A4/ )C = j ! ( (dLRG A4/ ) H4/= j ! ?!R4- P@4! *L )> $ .N* 0 a J ' .) L / ( G .dLRG A4/ E+ F/ G A4/ E+ E ! A V;! ) J

Prepared by: Eng. Mohammed Al-Dhabiany

u:(Sections) 6&0 Ue Span I ] k 0 !

. \ N- l/ +- % ^(Span I mN F/ ?= `' ?1- A ? = :8&0 8&: P@4! .<$ ( J` =*(

: -G ' 8 _ l # ! I( F/ c4 - 8&0 8&: A a J C .<$ Label Span

Span I 0 @ ?= F/ ) G ( 9 L Span I SL @ ?= &5 Span I SL (Span) 8&0 0 )/5 7 SLG

Offset

@ ?= . ?S4 Span . r ) ; )0 ' &5 !

Prepared by: Eng. Mohammed Al-Dhabiany

:( Bending schedule) Y 0 Ug PAD l/ .<> F/ . aN 8&0 8&: F -# ) 8&0 D G F 8 ! ,-( * F/ " M- . PROKON PAD 7 + * r 5 8 ) N % ^( * F/ "J! - c . A { utoCad : .<$ 8&0 8&: -

*G & l/ aN / $- A ! - Spans 5 ( I( SL F/ :L @ ( * ( aN / 0 ( ( 8 5G ( F (G ) ) )> $ : EM@ % ^ : .<$ 8&0 8&: -Generate schedule F/ EM1

Prepared by: Eng. Mohammed Al-Dhabiany

: : r 5 ) YL 8&0 F . ( (Reinforcing) ) Y 8&0 S AG A4< :(Calcsheet) 6&0 U8

)/ B S > .' F/ l/ c4 ! Y /; F l/ .

.<$ 0 ' 8&0 .N* L9 F/ EM1 l/ &: 0 8 - A ! - !

- % < ! '

( ! - 5 ) )> $ 8&: -

l/ " !4 M : EM@

Prepared by: Eng. Mohammed Al-Dhabiany

" /== 0 ' F/ 5G j N . &0 4 . AG % < !( J ' . "9; S AG A4<. , (r 5 8 ) 0 ? = - F *# . aN )aN q File Y S P N . aN S :) J .CO1 # l/ A a J * O ) / ) * + ,- - CO A O Continuous Beam and Slab ,- - T (

D $ 7 S L 0AUTOCAD F l/ ! ,- / . ' *(

Prepared by: Eng. Mohammed Al-Dhabiany

! " Export the file to the AUTOCAD AS DXF FILE Bending schedule %&' ' # $ .PAD ( )* +, - . / ' ( 6 7 8* 9 ) 01 ' &2 +34

.PAD ( ; , )* <(, CAD and Detailing %&' = 6( 01 '

B&' B&2 * >?@

01 ' Padds * >?@ 9A

2 >?@ Prepared by: Eng. Mohammed AL-dhabiany

:

8 ( B&' # # $

Open�File C D - <('

8 (, 8 )* ,3 E& = 0 F2&

Prepared by: Eng. Mohammed AL-dhabiany

:

: ( 01 9 B&' ' )* !

File C D - G H B F2$ Write DXF/CEX * >?@ 9A

Prepared by: Eng. Mohammed AL-dhabiany

:

DXF ! I ( )* +,3 = 0 (H B&' # $ J K(7 G H B 8 (,( 8 )* +,3 ! E& = 0 (H 9-

! I (

Prepared by: Eng. Mohammed AL-dhabiany

:

<(' ( & +, C *

( 01 ' 7 )* <(, 9-File C D - L

Prepared by: Eng. Mohammed AL-dhabiany

:

Turn static files into dynamic content formats.

Create a flipbook
Issuu converts static files into: digital portfolios, online yearbooks, online catalogs, digital photo albums and more. Sign up and create your flipbook.