Appendix F Examples.pdf
PDF 6 MB Posted
- Solicitation number
- W912P6-20-R-0009
About this file
This solicitation notice is for a fish barrier controls replacement project located in Romeoville, Illinois. The U.S. Army Corps of Engineers - Chicago District is seeking to replace the pulse-generating control systems for Barrier IIA and optionally Barrier IIB. The contractor will furnish and install new control systems that include IGBT assembly control, high voltage power supply control, high voltage polarity/position switch control, power monitoring system control, cooling control, backup generator monitoring and control, database control, and other supportive systems. The contractor must also install a remote control system to integrate the existing backup generators at Barriers IIA and IIB with the control system at the Permanent Barrier I Facility. Installation of Barrier IIA controls must begin by April 1, 2021, with optional Barrier IIB controls beginning by November 1, 2021. Both installations must be completed within 120 days, and testing within 30 days. Competition is unrestricted with a 10% price evaluation preference for HUBZone small businesses. The North American Industry Classification code is 334513. The contracting office is the U.S. Army Corps of Engineers Chicago District. The point of contact is listed along with instructions to reference the solicitation number on all correspondence regarding this opportunity.
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Appendix H Examples
Example A Flow Diagram
Best Practices for PAC Project and groov
PAGE
4 TECHNICAL NOTE • Form 2073-130625 the Powerup chart to reset values for important variables in case of a power cycle. Instead of making each variable persistent, you can write their values periodically to a persistent table. The default values block checks to see if a value is zero; if it is, it’s replaced by the value from the table.
Add a block named End (empty) to the end of the Powerup chart (and other flow-through charts) just to make it clear that the chart stops. By the way, you don’t need to put the Stop Chart command at the end of a chart; if there is no more logic, the chart will stop by itself.
Charts that monitor essential or time-critical pieces of your process, such as emergency stops on dangerous equipment or I/O that must be monitored continuously, should use looping logic so they are constantly running. Looping logic should also be used for alarm control and communication with an external program or device.
Take advantage of sample charts and code shared by Opto 22 engineers as well as by other customers on the OptoForums. Here’s a list of the greatest sample hits available on the forums. Pay special attention to the samples under “Our Product Support Group (PSG) Recommends.” Your strategy should include a chart similar to the I/O Enabler, for example, to make sure that any I/O unit that inadvertently goes offline is promptly re-enabled.
For a complex strategy you may want to create a marshalling chart—a chart to monitor all charts. The marshalling chart can gather status data, check chart sequencing, perform simple error checking, and act as the “glue” for a large strategy.
Space within Charts
Keep charts as simple as possible. Lay out your charts neatly, so it’s easy to follow chart logic. Keep all your blocks the same size, and make your connection lines neat and clearly visible.
Try to keep charts compact so you don’t have to scroll side to side. When possible, standardize on a size for Action blocks that is not as tall as the default. The smaller size saves vertical space in the chart. Use the smallest reasonable space between blocks to keep the chart more compact, but make sure connections and arrowheads are clearly visible.
http://www.opto22.com/community/showthread.php?t=453
Example B One Line Network and Peripheral Diagram
H1ECXDMB
Text Box
11"X17" PLOT SET 25 JAN 2010
Example C Table for Data List
RC_Byrd_Local_Pierhouse_1 - Tag Listing Page 3 RC_Byrd_Local_Pierhouse_1 (Controller) 2/27/2012 1:58:58 PM
... Program\Pierhouses\Final Programs\Gate 1\RCB_LTU_PH1_4_12_11_312ctsperrevFinal.ACD
RSLogix 5000
Name Value Data Type Scope Alarm_Ack_from_OS_1_or_2 0 BOOL RC_Byrd_Local_Pierhouse_1
Input for alarm acknowledgment. (This is used to acknowledge all alarms) Alarm_Ack_from_OS_1_or_2 - MainProgram/Alarms - 17(XIO), 19(XIO), 20(XIO), 22(XIO), 23(XIO), 5(XIO), 7(XIO), 8(XIO)
Alarm_at_Gate 0 BOOL RC_Byrd_Local_Pierhouse_1 Alarm_at_Gate - MainProgram/Alarms - *26(OTE)
Alarm_at_Gate_to_Shutdown 0 BOOL RC_Byrd_Local_Pierhouse_1 Alarm_at_Gate_to_Shutdown - MainProgram/Alarms - *25(OTE) Alarm_at_Gate_to_Shutdown - MainProgram/Gate_Position_Setpoint - 7(XIC) Alarm_at_Gate_to_Shutdown - MainProgram/Raise_and_Lower_Gate - 1(XIO), 7(XIO) Alarm_at_Gate_to_Shutdown - MainProgram/Stop_Gate - 1(XIC)
Aux_Lower_Cntacts_Failed_to_Close_in_10s TIMER RC_Byrd_Local_Pierhouse_1 This timer is initiated after the gate is initiated to lower and the gate lowering aux. contact is not energized.
Aux_Lower_Cntacts_Failed_to_Close_in_10s - MainProgram/Alarms - *21(TON) Aux_Lower_Cntacts_Failed_to_Close_in_10s.DN - MainProgram/Alarms - 22(XIC)
Aux_Lower_Contacts_Failed_to_Close 0 BOOL RC_Byrd_Local_Pierhouse_1 Aux_Lower_Contacts_Failed_to_Close - MainProgram/Alarms - *22(OTE), 17(XIC), 22(XIC), 23(XIC), 25(XIC), 26(XIC)
Aux_Raise_Cntacts_Failed_to_Close_in_10s TIMER RC_Byrd_Local_Pierhouse_1 This timer is initiated after gate is initiated to raise and the gate raising aux. contact is not energized.
Aux_Raise_Cntacts_Failed_to_Close_in_10s - MainProgram/Alarms - *18(TON) Aux_Raise_Cntacts_Failed_to_Close_in_10s.DN - MainProgram/Alarms - 19(XIC)
Aux_Raise_Contacts_Failed_to_Close 0 BOOL RC_Byrd_Local_Pierhouse_1 Aux_Raise_Contacts_Failed_to_Close - MainProgram/Alarms - *19(OTE), 17(XIC), 19(XIC), 20(XIC), 25(XIC), 26(XIC)
Battery_not_Detected 0 BOOL RC_Byrd_Local_Pierhouse_1 Battery_not_Detected - MainProgram/Operating_Screens_Interface - *15(OTE)
Commanded_Gate_Pos_In_Counts 0 DINT RC_Byrd_Local_Pierhouse_1 Gate position in feet entered by the operator is converted to counts. 0-68 ft.=100-65,000 counts.
Commanded_Gate_Pos_In_Counts - Gate_Position_Program/Gate_Position_Routine - *0(CPT), *1(CPT), *2(CPT), *3(CPT), *4(CPT), *5(CPT), *6(CPT) Commanded_Gate_Pos_In_Counts - MainProgram/Raise_and_Lower_Gate - 0(LES), 2(ADD) Commanded_Gate_Pos_In_Counts - MainProgram/Stop_Gate - *2(SUB)
Commanded_Gate_Pos_In_Counts_With_Offset 0 DINT RC_Byrd_Local_Pierhouse_1
The addition is needed to compensate for the GTor = to in the Lower Rung.
Commanded_Gate_Pos_In_Counts_With_Offset - MainProgram/Raise_and_Lower_Gate - *2(ADD), 4(GEQ), 6(GEQ) Commanded_Gate_Pos_In_Counts_With_Offset - MainProgram/Stop_Gate - *3(ADD)
Counter_for_Counts_to_Feet_PB COUNTER RC_Byrd_Local_Pierhouse_1 Counter_for_Counts_to_Feet_PB - MainProgram/Manual_Feet_to_Counts_via_PB - *0(CTU), *203(RES)
Example D Table for Data List I‐O
AC_Inputs - Ladder Diagram Page 27 RC_Byrd_Local_Pierhouse_1:MainTask:MainProgram 2/27/2012 1:59:04 PM Total number of rungs in routine: 8 ... Program\Pierhouses\Final Programs\Gate 1\RCB_LTU_PH1_4_12_11_312ctsperrevFinal.ACD
RSLogix 5000
AC Input Module 1 Slot 3
Local:3:I.Data.1
Input from Local/Remote Switch
(Local) Sel_Sw_In_Local_Mode
AC Input Module 1 Slot 3
Local:3:I.Data.2
Input from Local/Remote Switch
(Remote) Sel_Sw_In_Remote_Mode
AC Input Module 1 Slot 3
Local:3:I.Data.3
Aux. contact indicating gate is lowering (input from PCLR Lower Relay).
Gate_Lowering_Aux_Cont
AC Input Module 1 Slot 3
Local:3:I.Data.4
Aux. contact indicating gate is rising (input from
PCRR Raise Relay).
Gate_Rising_Aux_Cont
AC Input Module 1 Slot 3
Local:3:I.Data.0
Current Sensing Relay CSRR Relay
(Hoist Motor Overloads)
Gate_Hoist_Motor_OLs
AC Input Module 1 Slot 3
Local:3:I.Data.5
120V Input from Surge Protector
Primary Side
TPD1
AC Input Module 1 Slot 3
Local:3:I.Data.6 Pushbutton_for_Counts_to_Feet
Example E Hardware Inventory List
Hardware Inventory Table
Hostname Make Model Location Funciton IP Address MAC Address OS OS Version Memory Hard Drive Capacity
No. Of Network Interfaces
Special Purpose Communcitaions Cards Video Card(s)
OP_WRKSTA DELL OPTIPLEX 990 Control Room Operator's HMI 192.168.1.150 0A:11:0B:43:12:SV
Microsoft
Windows 7 SP1 4GB 700 GB 1 None None (on board)
Example F Device Wiring Diagrams
0 0
IP
P
W P :d m s \E -1
A .d g n
H E
C X J J
.1
:1
/1
/2
L
R H -N
E T
A P
P \C
A D
A P
P S \A
P P
S \L
R H
W o rk s p a c e \W o rk s p a c e \P ro je c tW is e I n te rP lo t
O rg a n iz e r\ m is c \d e s ig n s c ri p t\ s td v .p e n
C P ro g ra m F il e s x
C o m m o n F il e s \I n te rP lo t\
IP
L O
T \m is c \c o lo r.
c tb
-A
U G -2
:3
W
IR
IN
G D
IA
G R
A M
C H
IC
A G
O S
A N
IT
A R
Y S
H
IP
C
A N
A L
C H
IC
A G
O F
IS
H B
A R
R
IE
R S
R O
M E
O V
IL
L E
IL
B A
R R
IE
R
B
J
H U
N T
IN
G T
O N D
IS
T R
IC
T
U .S
A R
M Y C
O R
P S O
F E
N G
IN
E E
R S
N T
IN
G T
O N
W E
S T V
IR
G
IN
IA
E
E T O
F
E-107 A
E -1
A .d g n
C O
N T
R O
L B
O X
O P
E R
A T
O R R
O O
M
-S
+S
-OUT
+OUT
G N
D
IHN 24-3.6
INTERNATIONAL POWER
POWER SUPPLY
24V DC, 3.6A
4 2 3 1 5
JUMPERS
V
V
V
V
ETHERNET SWITCH
N-TRON 306FX2-N-ST
BLACK
RED
POWER SUPPLIES
CAN USE REDUNDANT
RX
TX
1 2
3 4
CONNECTIONS
ST
CONNECTIONS
RJ45
P R
O C
E S
S O
R
S N
A P P
A C
R
O P
T O
TX
RX
COM
RTS
CTS
COM
DTR
DCD
E-NET
E-NET
OFF
ONAUTO
OFF
ONAUTO
1 2
M0-1
M0-2
M0-3
M0-4
M0-5
M0-6
M0-7
M0-8
M1-1
M1-2
M1-3
M1-4
M1-5
M1-6
M1-7
M1-8
3 4 5 6 8 9
10 11 12
SNAP-PAC-RCK16
OFF
ONAUTO
OFF
ONAUTO
OFF
ONAUTO
IN PARALLEL
BROWN/RED/RED/GOLD
A 1.2KOHM RESISTOR
CHANNELS SHOWN HAS
IN PARALLEL
BROWN/RED/RED/GOLD
A 1.2KOHM RESISTOR
CHANNELS SHOWN HAS
IN PARALLEL
BROWN/RED/RED/GOLD
A 1.2KOHM RESISTOR
CHANNELS SHOWN HAS
13 14 15
POWER SUPPLY
5V,4A LOGIC
SNAP-PS5
OPTO 22
GND
120VAC
GND
RED
BLACK
10A, 120/250V
10VN1
EMI FILTER
LOAD
LINE
M O
D U
L E
S
A
D
A
P
BROWN BLUE
LEGEND
TO 2 POLE CB (BROWN)
TO 2 POLE CB (BLUE)
GND
F
S E
B
R O
W N
E M I F
IL
T E
R
V N
B
L U
E
C A
C A
B L
OPTO 22 CONTROLLER
THE CHART BELOW DETAILS THE CORRELATION.
**NOTE: SOME WIRES HAVE WIRE DESIGNATIONS THAT DIFFER ON EACH END,
L E
A V
G
N
C L
O S
U R
E
F
IB
IC
B L
E S
EXTERIOR
ON ENCLOSURE
INDICATING LIGHT
21 46
12VAC-C
120VAC-H10
120VAC-H11
120VAC-H12
120VAC-H13
120VAC-N
120VAC-N
120VAC-N
120VAC-N
120VAC-N
GREEN
WIRE CORRELATION CHART
NOTES
CUT LINE A
CUT LINE A
CUT LINE A
CUT LINE A
G
R E
Y
T P
U T
S N
A P
O A
C
M A
T P
U T
S N
A P
O A
C
M A
A C
D C
IN
P U
T
S N
A P
ID
C
M A
A C
D C
IN
P U
T
S N
A P
ID
C
M A
A C
D C
IN
P U
T
S N
A P
ID
C
M A
M0-2
M0-4
M0-6
M0-8
M1-2
M1-4
M1-6
M1-8
120VAC-H9
120VAC-H8
120VAC-H7
120VAC-H6
120VAC-H5
120VAC-H4
120VAC-H3
120VAC-H2
120VAC-H1
WIRE NO.
DEVICE
ENCLOSURE
WIRE NO.
BLOCK
TERMINAL
WIRE NO.
DEVICE
ENCLOSURE
WIRE NO.
BLOCK
TERMINAL
WIRE NO.
DEVICE
ENCLOSURE
WIRE NO.
BLOCK
TERMINAL
WIRE NO.
DEVICE
ENCLOSURE
WIRE NO.
BLOCK
TERMINAL
ASSEMBLY (BLUE)
TO RESISTOR
TERMINAL BLOCK-DIN RAIL
JUMPER
FUSE INDICATOR-DIN RAIL
FUSE BLOCK WITH BLOWN
BLOCK-DIN RAIL
MULTI-LEVEL TERMINAL
m
IN
P U
T
S N
A P
A
IM
A iS
R C
CH0
CH1
A-D
CHANNEL
TWO
OFF
ONAUTO
A C
D C
IN
P U
T
S N
A P
ID
C
M A
IN PARALLEL
BROWN/RED/RED/GOLD
A 1.2KOHM RESISTOR
CHANNELS SHOWN HAS
OFF
ONAUTO
A C
D C
IN
P U
T
S N
A P
ID
C
M A
IN PARALLEL
BROWN/RED/RED/GOLD
A 1.2KOHM RESISTOR
CHANNELS SHOWN HAS
OFF
ONAUTO
A C
D C
IN
P U
T
S N
A P
ID
C
M A
IN PARALLEL
BROWN/RED/RED/GOLD
A 1.2KOHM RESISTOR
CHANNELS SHOWN HAS
OFF
ONAUTO
A C
D C
IN
P U
T
S N
A P
ID
C
M A
OFF
ONAUTO
A C
D C
IN
P U
T
S N
A P
ID
C
M A
OFF
ONAUTO
T P
N
A P
O D
C
M A
T.B. 127
IN
P U
T
S N
A P
A
IM
A iS
R C
CH0
CH1
A-D
CHANNEL
TWO
IN
P U
T
S N
A P
A
IM
A iS
R C
CH0
CH1
3.6A P.S.
TO 24VDC
A-D
CHANNEL
TWO
CH0
CH1
3.6A P.S.
TO 24VDC
D-A
CHANNEL
TWO
T P
U T
S N
A P
A O
A iS
R C
CH0
D-A
CHANNEL
SINGLE
V
T P
U T
S N
A P
A O
V
M3-1
M3-2
M3-3
M3-4
M3-5
M3-6
M3-7
M3-8
M4-1
M4-2
M4-3
M4-4
M4-5
M4-6
M4-7
M4-8
M5-1
M5-2
M5-3
M5-4
M5-5
M5-6
M5-7
M5-8
M6-1
M6-2
M6-3
M6-4
M6-5
M6-6
M6-7
M6-8
M7-1
M7-2
M7-3
M7-4
M7-5
M7-6
M7-7
M7-8
M8-1
M8-2
M8-3
M8-4
M8-5
M8-6
M8-7
M8-8
M11-2
M11-4
M11-6
M11-8
(RED)
M15-1
(BLACK)
M15-2
G N
D
G
N D
G
N D
G N
D
G
N D
G
N D
G
R E
Y
G
R E
Y
G
R E
Y
G
R E
Y
G
R E
Y
G
R E
Y
G
R E
Y
G
R E
Y
B
L A
C K
G
R E
Y
B
L A
C K
B
L A
C K
B
L A
C K
B
L A
C K
B
L A
C K
B
L A
C K
B
L A
C K
B
L A
C K
B
L A
C K
R
E D
B
L A
C K
R
E D
B
L A
C K
R
E D
B
L A
C K
R
E D
B
L A
C K
R
E D
B
L A
C K
R
E D
R
E D
R
E D
R
E D
R
E D
B
L A
C K
WIRE NO.
DEVICE
ENCLOSURE
WIRE NO.
BLOCK
TERMINAL
SPARE (PAIR 8)
GENERATOR #1
SPARE (PAIR 7)
GENERATOR #1
SPARE (PAIR 6)
GENERATOR #1
SPARE (PAIR 5)
GENERATOR #1
SPARE (PAIR 4)
GENERATOR #1
SPARE (PAIR 1)
CONTACT CLOSED=AUTO
GENERATOR #1 MAN/AUTO
SPARE (PAIR 2)
CONTACT OPEN=RUN
GENERATOR #1 RUN
SPARE (PAIR 3)
CONTACT OPEN=FAULT
GENERATOR #1 FAULT
B
L A
C K
R
E D
B
L A
C K
B
L A
C K
B
L A
C K
B
L A
C K
B
L A
C K
B
L A
C K
B
L A
C K
R
E D
R
E D
R
E D
R
E D
R
E D
R
E D
R
E D
W H
IT
E
B L
A C
K
IN
P U
T
S P
A R
E m
A T
T
S H
IE
L D
B L
A C
K
R E
D P
O
IN
T
D E
W
B L
A C
K
R E
D
M P
E R
A T
U R
E
C O
N T
R
O M
120VAC-N
120VAC-N
120VAC-N
12VAC-H
12VAC-H
12VAC-H
12VAC-H
12VAC-H
12VAC-H
12VAC-H
12VAC-H
12VAC-H
12VAC-H
12VAC-H
12VAC-H
12VAC-H
RELAY-16
12VAC-H
RELAY24
12VAC-H
12VAC-H
12VAC-H
12VAC-H
12VAC-H
12VAC-H
12VAC-H
24V COM
24V COM
M11-2
M11-4
M11-6
M11-8
M12-2
M12-1
M13-6
M13-5
M13-2
M13-1
M14-1
M14-5
M14-6
M14-2
M15-1
M15-2
(RED)
M14-1
(BLACK)
M14-2
(RED)
M14-5
(BLACK)
M14-6
(RED)
M13-1
(BLACK)
M13-2
(RED)
M13-5
(BLACK)
M13-6
(RED)
M12-1
(BLACK)
M12-2
M3-2
M3-8
M4-2
M4-4
M4-6
M5-4
1. SEE E-31 (AS-BUILT DRAWING DATED 2-28-2011) AND E-107B&C FOR ADDITIONAL DETAILS.
S E
B
R O
W N
I F
IL
T E
R
V N
B
L U
E
SUPPLY (BLUE)
TO OPTO 22 POWER
TO FUSE 6 (BROWN)
TO 1.2A P.S.
TO T.B. 38 WIRE LABELED 52
M10-2
M10-4
M10-6
M10-8
BE LABELED M9-XX.
WHERE THEY SHOULD
ARE LABELED M10-XX
**NOTE**WIRE NUMBERS
TO MOD. 10 M11-7
M10-2
M10-4
M10-6
M10-8
BE LABELED M10-XX.
WHERE THEY SHOULD
ARE LABELED M11-XX
**NOTE**WIRE NUMBERS
SUPPLY OUT+ (RED)
TO 1.2A POWER
M7-1
M7-3
M7-5
M7-7
BE LABELED M11-XX.
WHERE THEY SHOULD
ARE LABELED M7-XX
**NOTE**WIRE NUMBERS
SEE NOTE 2.
TO MOD. 11 AS SHOWN IN CHART AND MODULE NOTES.
2. M10 SERIES WIRED TO MOD. 9, M11 SERIES WIRED TO MOD. 10 AND M7 SERIES WIRED
RELAY-1
RELAY-2
RELAY-3
RELAY-4
RELAY-5
RELAY-6
RELAY-7
RELAY-8
RELAY-9
RELAY-10
RELAY-17
RELAY-18
RELAY-16
RELAY-15
RELAY-14
RELAY-13
RELAY-12
RELAY-11
RELAY-19
RELAY-20
RELAY-21
RELAY-22
RELAY-23
RELAY-24
M3-4,6
2,4,6,8
MOD11-
M7-1
M7-3
M7-5
M7-7
M10-7
TO MOD. 9
M4-8, M7-4
M5-2, M7-2
M5-6, M7-6
M5-8, M7-8
M6-8, M8-2
M6-6, M8-4
M6-4, M8-6
M6-2, M8-8
C O
N N
E C
T
IO
N
N O
12VAC-H 51
CH0
CH1
CH2
CH3
CH0
CH1
CH2
CH3
CH0
CH1
CH2
CH3
CH0
CH1
CH2
CH3
CH0
CH1
CH2
CH3
CH0
CH1
CH2
CH3
CH0
CH1
CH2
CH3
CH0
CH1
CH2
CH3
CH0
CH1
CH2
CH3
CH0
CH1
CH2
CH3
CH0
CH1
CH2
CH3
S O
L
IC
IT
A T
IO
N N
O
F
IL
E N
A M
E
D W
N B
Y
C K
D B
Y
D E
S
IG
N E
D B
Y
D E
S C
R
IP
T
IO
N
D
2 3
C
4 5
A
B
M A
R K
A P
P R
D A
T E
F
IL
E N
U M
B E
R
S
IZ
E
S U
B M
IT
T E
D B
Y
P L
O T S
C A
L E
P L
O T D
A T
E
D A
T E
M A
R K
D E
S C
R
IP
T
IO
N
C O
N T
R A
C T N
O
IDENTIFICATION
SHEET
D A
T E
A P
P R
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US Army Corps
Huntington District
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9 5
10 6
11 7
12 8
RELAY
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
IN PARALLEL AS SHOWN. TYPICAL.
RESISTOR GREEN/BLUE/GOLD/GOLD
RELAY SHOWN HAS A 5.6OHM CUT LINE A
CUT LINE A
NOTES
TO T.B. 54
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
9 5
10 6
11 7
12 8
RELAY
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
TYPICAL
12VAC RELAY
OMRON MY4
13 14
9 5
10 6
11 7
12 8
RELAY
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
13 14
RELAY
9 5
10 6
11 7
12 8
TO T.B. 55 TO T.B. 56 TO T.B. 57 TO T.B. 58 TO T.B. 59 TO T.B. 60
TO 4-5
TO T.B. 61
TO T.B. 62 TO T.B. 63 TO T.B. 64 TO T.B. 65 TO T.B. 66 TO T.B. 67 TO T.B. 68 TO T.B. 69
TO T.B. 71 TO T.B. 70
1. SEE E-31 (AS-BUILT DRAWING DATED 2-28-2011) AND E-107A&C FOR ADDITIONAL DETAILS.
TO T.B. 122
SIDE LEFT SIDE (GREY)
TO 3VR1 FILTER LOAD
TO M3-1 TO M3-3 TO M3-5 TO M3-7 TO M4-1 TO M4-3 TO M4-7
CUT LINE A
CUT LINE A
TO M5-1 TO M5-3
RELAY NOT PRESENT
RELAY BASE ONLY
TO M5-5 TO M5-7 TO M6-1 TO M6-3 TO M6-5 TO M6-7
SIDE RIGHT SIDE (GREY)
TO 3VR1 FILTER LOAD
TO T.B. 53
TO M7-1 TO M7-3
TO T.B. 128
TO M7-5
TO T.B. 129
TO M7-7
TO T.B. 130
TO M8-1
TO T.B. 131
TO M8-3
TO T.B. 132
TO M8-5
TO T.B. 133
TO M8-7
TO T.B. 108
TO T.B. 72
TO T.B. 51
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IDENTIFICATION
SHEET
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CONDOR
POWER SUPPLY
24V DC, 1.2A
10 8 6
5 4 2 1
3A, 120/250V
3VR1
EMI FILTER
PRI
SEC
LINE END DETAIL
3VR1
EMI FILTER
PIN
NOT USED
12.6VCT 2.381A
TERM 6- TERM 8- TERM 10:
TERM 4- TERM 5:115V
TERM 1-TERM 2:115V
HAMMOND 186D12 TRANSFORMER
G
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G
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G
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G
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G
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G
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G
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G
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G
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G
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G
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122 (GREY)
NOTES
12VAC-C
THIS ASSEMBLY.
TO THROUGH RESISTORS TO
(COMMON). FUSES 6-18 WIRED
POINTS ARE INTERCONNECTED
RESISTOR ASSEMBLY ALL
09876
G N
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0 1
4 1 5 1
8976 1
LOAD SIDE (BROWN)
TO 10VN1 FILTER
G N
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G N
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TO EXTERNAL POWER (BLACK)
TO EXTERNAL POWER (WHITE)
TO EXTERNAL GROUND (GREEN)
B L
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N
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2-POLE 10A, CB
G
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G
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G
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G
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12VAC-C
116 (BLACK)
BROWN
BROWN
BROWN
BROWN
BROWN
BROWN
BROWN
BROWN
BROWN
BROWN
BROWN
BROWN
BROWN
G
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B
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CONDUIT C33, 15
SUPPRESSION
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EXR-6
B
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EXR-7
EXR-8
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CONDUIT C33, 14
SECURITY
6.8kOHM RESISTOR
1. SEE E-31 (AS-BUILT DRAWING DATED 2-28-2011) AND E-107A&B FOR ADDITIONAL DETAILS.
TRANSFORMER (BROWN)
TO PT.4 ON 120:12VAC
TRANSFORMER (GREY)
TO PT. 6 ON 120:12VAC
SUPPLY 120VAC-H13 (BROWN)
TO OPTO 22 SNAP-PS5 POWER
TO RESISTOR ASSEMBLY (BROWN)
24V,3.6A P.S. PT.3
120VAC-H12 (BROWN) TO
TO RESISTOR ASSEMBLY (BROWN)
120VAC-H9 (BROWN) (M1-7)
LEAVES ENCLOSURE
120VAC-H10 (BLACK)
TO RESISTOR ASSEMBLY (BROWN)
120VAC-H8 (BROWN) (M1-5)
TO RESISTOR ASSEMBLY (BROWN)
TO RESISTOR ASSEMBLY (BROWN)
120VAC-H7 (BROWN) (M1-3)
TO RESISTOR ASSEMBLY (BROWN)
120VAC-H6 (BROWN) (M1-1)
120VAC-H2 (BROWN) (MO-1)
TO RESISTOR ASSEMBLY (BROWN)
120VAC-H3 (BROWN) (MO-3)
TO RESISTOR ASSEMBLY (BROWN)
120VAC-H4 (BROWN) (MO-5)
TO RESISTOR ASSEMBLY (BROWN)
120VAC-H5 (BROWN) (M0-7)
TO RESISTOR ASSEMBLY (BROWN)
24V,1.2A P.S. PT. 2
120VAC-H1 (BROWN) TO
LINE SIDE
EMI FILTER 3VR1
12VAC-C (GREY) TO
TO T.B. 29 (BLUE)LOAD SIDE (BLUE)
TO 10VN1 EMI FILTER
MARKED #8 NOT HOOKED UP
MARKED #9 NOT HOOKED UP
TO TB 63 TOP
TO RELAY 1, PT.13
L
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P T .1
M
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TO T.B. 70 (BLACK)
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TO T.B. 31
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TO FUSE 19
TO T.B. 30 (BLUE)
(BROWN)(BOTTOM)
TO FUSE BLOCK 18
(BLUE)(TOP)
TO FUSE BLOCK 18
TO RELAY 1 PT. 9 (GREY)
TO RELAY 16, PT.13(GREY)
TO FUSE 19 TOP (GREY)
TO PANEL SR1 CKT. #17.
(ROUTED IN CONDUIT Z8
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TO EMI FILTER 10VN1 (BROWN)
TO EMI FILTER 10VN1 (BLUE)
TO RESISTOR ASSEMBLY (BROWN)
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IDENTIFICATION
SHEET
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Example G Fish Barrier Hazard
Assessment
Hazard Assessment for Chicago Sanitary and Ship Canal
Fish Barrier
Prepared for:
Chicago District
Prepared by:
Protective Design Center
U.S. Army Corps of Engineers Omaha, Nebraska
October 2010
Purpose of Assessment
Electrical equipment containing capacitors similar in design to the capacitors used in the fish barriers have failed in a manner that would be hazardous to personnel present in the vicinity. A failure of a capacitor can cause fire, airblast, and fragment hazards to personnel. A comment by SRI on the final design of CSSC Phase IIB indicated a “blast-proof personnel protection system” was needed for the pulsator rooms. Later correspondence from SRI indicates the module walls will contain fragments, and that pressures inside the module will not cause the cabinet to fail. The following assessment is an independent assessment of the hazards caused by the postulated failure condition.
Hazard Discussion
Electrical discharge and dielectric mist conflagration were observed at LLNL to cause explosive and fragment hazards around the module. This is the cause for concern with the CSSC Barrier capacitors. It is assumed that the potential for hazardous failure is associated with full operation capacity of the fish barrier.
A brief research effort was performed in order to better understand the nature of the capacitor failures. A document was provided to the Protective Design Center (PDC), “Pressure Effects Analysis of National Ignition Facility Capacitor Module Events” (Ref. 1), which was released by Lawrence Livermore National Laboratory (LLNL). This document summarizes the pressure effects analysis performed by LLNL for the failure of capacitors. Referenced in this document is another LLNL document titled “Mechanical Engineering Safety Note: Analysis and Control of Hazards Associated with NIF Capacitors Module Events” (Ref. 2). This document summarizes the failures which were experienced at First Article NIF Test Module (FANTM) at Sandia National Laboratory for which these pressure calculations are based, and includes calculations by numerous methods to attempt to characterize the events.
There were 5 recorded failures at FANTM. LLNL states that there have been well over a million capacitor shots without failures. The probability of failure was calculated to be 3.1x10-4 explosions/module-shot with a 95% confidence level. Four of the recorded failures were determined to be caused by an open circuit which was caused by poorly soldered connections.
The other failure was in a resistor which failed, producing hazardous fragments and cabinet damage. The internal collateral damage from the failures was relatively minor for all cases but one, in which it was significant.
The estimated peak quasi-static pressure in the module cabinet that could occur during such an event was estimated to be on the order of 11 psig. This pressure resulted in bay pressures less than the tolerance of the bay walls and no pressure relief was needed. This overpressure is assumed to be a static load, so no dynamic loading was addressed. The LLNL bay size was much larger than the bays for the fish barrier, so a similar failure would put higher pressures into the CSSC bays.
Fire Hazard The presence of flammables should be kept to a minimum around the equipment. No further consideration of fire hazard is included here.
Fragment Hazard
General fragment considerations: Fragmentation of the capacitor casing generates the hazardous fragment used in this analysis. The driving energy for this calculation is the stored electrical energy in the capacitor and the burning canola oil. Only the stored electrical energy is significant to contribute to the kinetic energy of the fragment. The burning oil deflagrates and does not contribute to the fragment kinetic energy. Two cases were considered to calculate the potential electrical energy to fly the fragment: first, 528kJ which is the result from the maximum design voltage of 3050V; second 650kJ, which is based on 3400V which is the rated capacitor voltage. To convert electrical energy to an equivalent TNT mass the heat of detonation of 4187 kJ/kg for TNT was used (Ref. 4). The corresponding equivalent charge weights are 0.126 kg TNT and 0.155 kg TNT respectively. Based on these charge weights and the capacitor case mass, the gurney equation (Ref. 5) was used to find a mean initial velocity of a fragment from the capacitor case. A steel cube fragment with a thickness of approximately
0.25 inches was used as the critical fragment.
Capacitor Enclosure Description: The pulsator enclosure drawings shows building 2A enclosures have walls are ¾ inch thick plywood encased in 1/8 inches thick aluminum sheet metal. The building 2A enclosures have discharge covers that are 0.08 inches thick aluminum and filter covers that are 1/8 inches thick aluminum sheet metal. The filter cover thickness was used as the worst case scenario because of the amount of capacitor rack material in-between the capacitors and the discharge covers.
Personnel Hazards: Personnel are located outside of the building 2B pulser room during capacitor operation; therefore a fragment would have to leave the pulsar room to be considered a hazard. The ways for a fragment to leave the pulser room are that the fragment could go through the blast damper, pulsator enclosure, blast door, personnel door, pulser room wall or roof. Based on possible the travel paths the discharge cover on the enclosure in building 2A can be eliminated as possible materials in the travel path. The remaining possible materials that may come in contact with a fragment were evaluated.
Building 2B: The steel blast door has steel sheet metal 0.1046 inches thick (12ga) on each face.
The steel personnel door has steel sheet metal 0.0635 inches thick (16ga) on each face. The cubical walls are 12 inches thick 4 ksi concrete, and the roof at its thinnest is 3.5 inches thick 4 ksi concrete. The building exterior double door has steel sheet metal 0.0516 inches (18ga) thick on each face. The galvanized steel blast damper has galvanized steel 0.1382 inches thick (10ga) per blade.
Building 2A: The walls and roof are considered to be galvanized steel 0.0217 inches thick (26ga).
Table 1: Structural Considerations Element Material Thickness (in)
Building 2B Blast Door Steel 0.2092 Building 2B or 2A Personnel Door
Steel 0.127
Building 2A Pulsator Enclosure Wall
Al and Plywood .25 and .75
Building 2A Pulsator Enclosure Vent
Al 0.08
Building 2B Wall Concrete 12 Building 2B Roof Concrete 3.5 Building 2A Wall Galvanized Steel 0.0217 Building 2A Roof Galvanized Steel 0.0217 Building 2B Exterior Door
Galvanized Steel 0.1032
Building 2B Blast Damper
Galvanized Steel 0.2764
The fragment penetration into material was calculated by the computer software ConWep which is based on UFC 3-340-01. The maximum design fragment penetration into materials at a range of 0.00001 feet is shown in the table below and in Appendix B. The maximum penetration shown in this table is the amount of the specific material thickness required to stop a fragment with the given mass and velocity.
Table 2: Fragment Considerations
Volt s
(kJ)
Charge Weight
(kg-TNT)
Fragment Mass (oz)
Fragment Velocity
(ft/s)
Maximum Penetration Aluminum
(in)
Maximum Penetration
Steel (in)
Maximum Penetration
Concrete (in)
528 0.126 0.00214 3110 0.154 0.0671 0.337
650 0.155 0.00214 3434 0.172 0.0747 0.365 Maximum Fragment Penetrations values from ConWep
Blast Pressure Hazard
Blast pressures are potentially generated by release of electrical energy, and by detonation or deflagration of hydrocarbons. The blast would originate in the module cabinet, and vent to the module bay, then vent to outside. Important parameters to consider are module size, room size, air available for burning oil, vent sizes, electrical energy release, and oil properties.
Two methods of estimating blast and gas pressures are considered. First, the energy release is considered as an equivalent TNT detonation in the module cabinet. The analysis is based on finding the gas pressures generated by an amount of TNT with a heat of detonation that is the same as the energy release due to the electrical and oil energy involved. Venting from the module cabinet and room is analyzed.
The second method is based on a method of estimating effects of electrical energy release from a circuit breaker failure used in page 215 of Ref 4.
Method 1: To find the energy produced and convert it to an equivalent TNT, it must be decided if the canola oil will participate in initial gas pressure production, or if it will burn in later times.
Most fuel-air-explosives use an initial dispersing blast, and a second detonating blast is used to detonate the vapor cloud generated by the dispersing blast. In the case of a capacitor failure there is only a dispersing blast. Some fuel-air-explosives use only one blast, but these have a mixture of liquid fuel and solids. Accidental generation of the oil mist and detonation is unlikely, especially with the safeguards designed into the capacitors. The inside of the module cabinet would not allow good dispersal of the oil, or allow a flame front to propagate in any uniform manner. There is enough oxygen in the cabinet to support the chemical reaction for a burn of 229 ml of oil, but the flammability of canola is much lower than hydrocarbon fuels. A blast based on the 100% review comment would account for 528 KJ electrical and 7800 KJ oil combustion for a total of 8.3 MJ energy. This is the energy equivalent of 2 kg (4.4 lb) TNT, which has heat of detonation of 4187 KJ/kg (Ref 4, table 2-4). The blast pressures and impulses from this explosion would be extensive and destroy the equipment and cabinet. The evidence from the LLNL accidents indicates that there was not a detonation of the oil. Therefore, in this first method of calculating pressures, the oil is not included in calculating an equivalent TNT blast. A model of the module, bay, and outdoors was made in BlastX to model the gas pressures and venting from the module to the bay, to outdoors. Shock pressure calculation was not included since there is not a high order detonation occurring.
BlastX model description: Three rooms are in the models with properties as follows. Output from the program is included in Appendix B.
Building 2A BlastX Model:
Room 1 Building 2A– Pulsator Enclosure: It is sized to have a volume equal to the air volume in the module so that gas pressure and venting will be modeled correctly. The module cabinet is 204” x 92” x 68” inside dimensions. Internal equipment volume was reported to be 1,233,000 cubic inches, but this is almost the entire cabinet volume. So, room 1 is sized based on having 40% air in the cabinet. The explosive source is located in room 1, and since gas only calculation is done, the charge is not located by x, y, z coordinates. The charge in room 1 represents the electrical energy release is 528kJ/4187 kJ/kg = 0.126 kg TNT.
Room 2 Building 2A: Building 2A is approximately 26’ x 70’ x 12.7’.
Room 3 Outside: The maximum room size allowed in BlastX is 1000 ft3 and represents the outdoors.
Building 2B BlastX Model:
Room 1 Building 2B: The pulsator bay is 23’ x 20’ x 16’ but is adjusted to account for volume taken up by equipment. The explosive source is located in room 1, and since gas only calculation is done, the charge is not located by x, y, z coordinates. The charge in room 1 represents the electrical energy release is 528kJ/4187 kJ/kg = 0.126 kg TNT.
Room 2 Outside: The maximum room size allowed in BlastX is 1000 ft3 and represents the outdoors.
Building 2B BlastX Results Summary: The room in building 2B pressure peaked at 0.59 psi with an impulse equal to 11.01 psi-msec.
Building 2A BlastX Results Summary: Building 2A pressure peaked at 0.185 psi with an impulse equal to 27.7 psi-msec.
Pulsator Enclosure: Pressures in the enclosure are a peak of 73.0 psi with an impulse of 45.0 msec. The enclosure wall panels could be damaged by this pressure, and potentially injure personnel in building 2A. Personnel and building components in the room will not be injured or damaged by the pressures.
BlastX output and SBEDS analysis of a wall and a roof beam of building 2B, a wall panel of building 2A and pulsator enclosure wall are include in Appendix B.
Electrical Energy Release Blast Method
The module room has a total volume of 20.9 m3 and a venting area of 3.05 m2. The worst-case 650KJ energy release over one second was used for the maximum rate of energy dissipation for the analysis. With the initial shockwave produced over 10s to 100s of microseconds. The effective heat capacity ratio of 1.4 was also used for the arc. The actual effective heat capacity ratio of the arc will be much less, so therefore 1.4 was conservative. The point used to find the pressure was 0.5 meters from the arc. The method of calculating blast from an electrical circuit breaker was from Fundamental Studies in Engineering 5 by Baker, Cox, Westine, Kulesz and Strehlow. This method produced a shock pressure of 29.19 kPa (4.23 PSI) and a stress rate of
8885.9 Pa/s (1.29 PSI/S). Some assumptions that may need to be adjusted are, over one second the 650KJ is released to get to watts, the effective module volume and the distance from the arc.
Human Tolerance
DOE criteria for protecting personnel is limiting pressure to 5 psi, limiting fragments to11 ft-lb energy, and preventing structural collapse. For DoD there is criteria presented in Reference 4.
Human tolerance for blast with a fast rising pressure wave is about 5 psi for the threshold of eardrum rupture, and 50 percent rupture would be at 15 psi. Lung damage and body impact from translation occur with higher pressures, so the 5 psi threshold for eardrum rupture can be used as a limiting criteria for worker exposure. Fragment tolerance of humans depends on where a person is impacted, and is shown in the table below from Ref 4.
Conclusions:
The calculated blast pressure will not fail either building or the module and create a safety hazard from structural collapse. The design fragment is the controlling safety hazard. The thickness of the structural elements which could be impacted by a fragment and the maximum penetration capability of the design fragment were compared and led to the following conclusion. The design fragment will not perforate building 2A enclosure walls, building 2B blast door or damper, building 2B personnel or exterior double door sheet metal, wall or roof of either building 2A or 2B. The difference in mass of the design fragment and blast damper components engaged in movement will prevent the fragment from escaping the facility though opening of the blast damper. The design fragment can perforate the building 2A capacitor enclosure filter cover (1/8 inches of aluminum), but does not have enough kinetic energy to perforate the walls, roof, or doors of building 2A for either explosive case.
Recommended thickness of the shield plate during startup testing: Any steel plate with a thickness greater than a ¼ inch should work, and during earlier discussions, it was mentioned that street plate of one inch and one and half inch thick were available. The installation of 18 gage galvanized steel exterior double doors would have a thickness of 0.103 inches of steel total. This thickness would be greater than the required 0.0747 inches of steel to stop the design fragment and therefore would stop the design fragment from exiting the facility.
A-1
Appendix A
Data for Phase IIA and IIB capacitor modules:
There are 3 parts to a pulsator module contained in one cabinet enclosure. Overall outside dimensions of the cabinet is 5’-10” high, 8’-0” wide, 17’-6” long.
• Capacitor section with 2 low intake louvers and 4 exhaust vent fans on top
• ABB section with 2 hinged top doors (35” x 61” each)
• polarity switch with 1 low intake vent louver
3 modules per phase – module 1 and 2 have 50 capacitors, module 3 has 25 capacitors. All capacitors are 46 kg in stainless steel case, capacitors are 2270 micro Farads each, 3400 volts.
100% review comment by SRI indicated the hazard they thought was possible:
“A realistic estimate of energy release is for a single capacitor to rupture and ignite a small fraction of the available oil. Specifically, only 229mL of oil vaporized and ignited resulting in the release of 7.8x10^6J. To this number we need to add the electrical energy, 5.27x10^5 resulting in a total energy release of 8.3x10^6J. This figure should probably be used for overpressure calculations and blow-out panel design.”
Later correspondence (July 17, 2009) indicates a 650 KJ energy release from stored electrical energy and the resulting pressure in the cabinet of 1.89 psi.
Room size for phase IIB is 20’ long, 23’ wide, and 16’ height to bottom of roof deck. Personnel and overhead coiling door are on room end by capacitor section, and louver or blast damper is on other end by polarity switch section.
A-2
References:
1. S.Brereton, C. Ma et al, “Pressure Effects Analysis of National Ignition Facility Capacitor Module Events” Proceedings of 8th International Conference on Nuclear Engineering, Apr 2000
2. S. Brereton, LLNL “Mechanical Engineering Safety Note: Analysis and Control of Hazards Associated with NIF Capacitor Module Events” Aug 2001
3. Conwep “Conventional Weapons Effects” computer program, USACE-ERDC
4. Baker, Cox, Westine, Kulez, Strehlow “Explosion Hazards and Evaluation” Elsevier 1983
5. UFC 3-340-01 “Design and Analysis of Hardened Structures to Conventional Weapons Effects” 1 June 2002
5. UFC 3-340-02 “Structures to Resist the Effects of Accidental Explosions” 5 Dec 2008
6. F.D.Gunstone, “Rapeseed and Canola Oil, Production, Processing, Properties and Uses,” CRC Press, p91
8. BlastX computer program, Version 6.4.2.2, Science Applications International Corp.
9. SBEDS “Single degree of freedom Blast Effects Design Spreadsheet”, Version 4.1a, USACE
B-1
Appendix B
BlastX Analysis Output Building 2B
BlastX - Explosions Inside Multiple Room Structures
ERDC/SAIC Version 6.4.2.2 (10 January 2006 Watcom Fortran)
Date 10-22-2010
Electrical discharge .127 kg gas pressure
General units 2.0000 tmax 150.0000 maxord 5.0000 icalc 1.0000 mchamsx 2.0000 mventsx 1.0000 mtargsx 0.0000 mexplsx 1.0000 mwallsx 8.0000 iprint 0.0000 plot 2.0000 tcont 0.00000E+00 ht 1.0000
Ambient pressure 15.6959 temperature 59.0000
Room 1 volume 6739.2002 xlength 18.7000 ylength 18.7000 zlength 18.7000 file \\nwo-nas04\pdc_data\projects\assessment\blast\chicago ssc fish barrier\blastx\campbell\\Pulsar room
Room 2 volume 1.00000E+09 xlength 1000.0000 ylength 1000.0000 zlength 1000.0000 file \\nwo-nas04\pdc_data\projects\assessment\blast\chicago ssc fish barrier\blastx\campbell\\Outside
Opening 1 area 24.7500 r1 1 r2 2
Explosion 1 x0 2.6000 y0 2.6000 z0 0.0000 weight 0.2790 iroom 1.0000
B-2 wburn 9.9500 ld 1.0000 Composition Decimal Fraction
314 1.00000 TNT
Summary of Gas Pressure and Temperature Last Time (ms) = 1.5000E+02
Peak Peak Final Final Pressure Time Temperature Time Pressure Temperature Impulse Room (psi) (ms) (Deg F) (ms) (psi) (Deg F) psi*sec 1 5.947E-01 1.000E-03 7.747E+01 0.000E+00 -7.782E-04 7.182E+01 1.101E-02 2 0.000E+00 0.000E+00 5.900E+01 0.000E+00 0.000E+00 5.900E+01 0.000E+00
Opening Summary
Primary Secondary Differential Pressure Opening Room # Room # Failure Failure Pressure Impulse # Side A Side B Time(msec) Time(msec) (psi) (psi*s) 1 1 2 0.000E+00 1.000E+20 5.947E-01 1.101E-02
--- End of case. Elapsed time (msec) Memory(megabytes) 300 1.40
Opening Summary
Primary Secondary Differential Pressure Opening Room # Room # Failure Failure Pressure Impulse # Side A Side B Time(msec) Time(msec) (psi) (psi*s) 1 1 2 0.000E+00 1.000E+20 7.302E+01 3.391E-02 2 2 3 0.000E+00 1.000E+20 5.502E-01 1.107E-02
490 1.43
B-3
Building 2A
BlastX - Explosions Inside Multiple Room Structures
ERDC/SAIC Version 6.4.2.2 (10 January 2006 Watcom Fortran)
Date 10-20-2010
Electrical discharge .127 kg gas pressure
General units 2.0000 tmax 150.0000 maxord 5.0000 icalc 1.0000 mchamsx 3.0000 mventsx 1.0000 mtargsx 0.0000 mexplsx 1.0000 mwallsx 8.0000 iprint 0.0000 plot 2.0000 tcont 0.00000E+00 ht 1.0000
Ambient pressure 14.6959 temperature 59.0000
Room 1 volume 42.0000 xlength 6.6400 ylength 6.6400 zlength 6.6400 file \\nwo-nas04\pdc_data\projects\assessment\blast\chicago ssc fish barrier\blastx\campbell\\Module
Room 2 volume 23114.0000 xlength 70.0000 ylength 26.0000 zlength 12.7000 file \\nwo-nas04\pdc_data\projects\assessment\blast\chicago ssc fish barrier\blastx\campbell\\Room2A
Room 3 volume 1.00000E+09 xlength 1000.0000 ylength 1000.0000 zlength 1000.0000 plot 0.0000
Opening 1 area 32.8000 r1 1 r2 2
Explosion 1 x0 2.6000
B-4 y0 2.6000 z0 0.0000 weight 0.2790 iroom 1.0000 wburn 9.9500 ld 1.0000 Composition Decimal Fraction
314 1.00000 TNT
Summary of Gas Pressure and Temperature Last Time (ms) = 1.5000E+02
Peak Peak Final Final Pressure Time Temperature Time Pressure Temperature Impulse Room (psi) (ms) (Deg F) (ms) (psi) (Deg F) psi*sec 1 7.298E+01 5.637E-04 2.447E+03 0.000E+00 1.852E-01 1.478E+03 6.193E-02 2 1.852E-01 1.423E+00 6.388E+01 1.423E+00 1.852E-01 6.388E+01 2.771E-02 3 0.000E+00 0.000E+00 5.900E+01 0.000E+00 0.000E+00 5.900E+01 0.000E+00
Opening Summary
Primary Secondary Differential Pressure Opening Room # Room # Failure Failure Pressure Impulse # Side A Side B Time(msec) Time(msec) (psi) (psi*s) 1 1 2 0.000E+00 1.000E+20 7.296E+01 3.421E-02
170 1.43
B-5
10/22/2010
Time, msec
Pr es su re
, p si
Im pu ls e, p si
-m se c
Electrical discharge 0.127 kg gas pressure Room 001
0 15 30 45 60 75 90 105 120 135 150 -0.08 0
0 1.5
0.08 3
0.16 4.5
0.24 6
0.32 7.5
0.4 9
0.48 10.5
0.56 12
0.64 13.5
Module Blast Load
Building 2B Blast Load
B-6
Building 2A Blast Load
B-7
Fragment Results from ConWep
The controlling case for containing a fragment which is in building 2A is shown below. The two thinnest layers that were analyzed in the critical path are 1/8 inches of aluminum then
0.0217 inches (26ga) of galvanized steel. Two explosive cases, 0.126 kg and 0.155 kg of TNT were used for the fragment analysis.
0.126 kg of TNT
First layer 1/8 inches of Aluminum.
ConWep 2.1.0.8
Fragment Penetration into Aluminum (2024-T3) Weapon .......................................................... Cube Design fragment weight ................................ 0.002144 ounces Initial fragment velocity ................................ 3110 feet/sec Range to target ............................................... 0.25 feet Target thickness ............................................. 0.125 inches
Fragment striking velocity ............................. 3086 feet/sec Fragment penetration ..................................... 0.1527 inches Residual velocity of fragment after perforation ........................................... 574.5 feet/sec Residual fragment mass after perforation ........................................... 0.00174 ounces
Second layer 0.0217 inches of galvanized steel.
Fragment Penetration into Steel, Mild Homogeneous Weapon .......................................................... Cube Design fragment weight ................................ 0.00174 ounces Initial fragment velocity ................................ 574.5 feet/sec Range to target ............................................... 1 feet Target thickness ............................................. 0.0217 inches
Fragment striking velocity ............................. 555.7 feet/sec Fragment penetration ..................................... 0.00922 inches
B-8
0.155kg of TNT
First layer 1/8 inches of Aluminum.
Fragment Penetration into Aluminum (2024-T3) Weapon .......................................................... Cube Design fragment weight ................................ 0.002144 ounces Initial fragment velocity ................................ 3434 feet/sec Range to target ............................................... 0.25 feet Target thickness ............................................. 0.125 inches
Fragment striking velocity ............................. 3407 feet/sec Fragment penetration ..................................... 0.1704 inches Residual velocity of fragment after perforation ........................................... 930.3 feet/sec Residual fragment mass after perforation ........................................... 0.001656 ounces
Second layer 0.0217 inches of galvanized steel.
ConWep 2.1.0.8
Fragment Penetration into Steel, Mild Homogeneous Weapon .......................................................... Cube Design fragment weight ................................ 0.001656 ounces Initial fragment velocity ................................ 930.3 feet/sec Range to target ............................................... 1 feet Target thickness ............................................. 0.0217 inches
Fragment striking velocity ............................. 899.4 feet/sec Fragment penetration ..................................... 0.01538 inches
B-9
ConWep results for maximum design fragment penetration shown in Table 2: Fragment Considerations.
0.126 kg of TNT
ConWep 2.1.0.8
Fragment Penetration into Steel, Mild Homogeneous Weapon .......................................................... Cube 0.2477" Design fragment weight ................................ 0.002144 ounces Initial fragment velocity ................................ 3110 feet/sec Range to target ............................................... 1e-005 feet Target thickness ............................................. 1 inches
Fragment striking velocity ............................. 3110 feet/sec Fragment penetration ..................................... 0.06698 inches
ConWep 2.1.0.8
Fragment Penetration into Aluminum (2024-T3) Weapon .......................................................... Cube 0.2477" Design fragment weight ................................ 0.002144 ounces Initial fragment velocity ................................ 3110 feet/sec Range to target ............................................... 1e-005 feet Target thickness ............................................. 1 inches
Fragment striking velocity ............................. 3110 feet/sec Fragment penetration ..................................... 0.154 inches
ConWep 2.1.0.8
Fragment Penetration into Concrete Weapon .......................................................... Cube 0.2477" Design fragment weight ................................ 0.002144 ounces Initial fragment velocity ................................ 3110 feet/sec Range to target ............................................... 1e-005 feet Concrete slab thickness ................................. 1 inches Concrete compressive strength ...................... 4000 psi
Fragment striking velocity ............................. 3110 feet/sec Penetration into massive concrete ................. 0.3366 inches Minimum concrete thickness required to prevent perforation .................... 0.4166 inches Minimum concrete thickness required to prevent spalling ......................... 0.5115 inches
B-10
0.155 kg of TNT
ConWep 2.1.0.8
Fragment Penetration into Steel, Mild Homogeneous Weapon .......................................................... Cube 0.2477" Design fragment weight ................................ 0.002144 ounces Initial fragment velocity ................................ 3434 feet/sec Range to target ............................................... 1e-005 feet Target thickness ............................................. 1 inches
Fragment striking velocity ............................. 3434 feet/sec Fragment penetration ..................................... 0.07472 inches
ConWep 2.1.0.8
Fragment Penetration into Aluminum (2024-T3) Weapon .......................................................... Cube 0.2477" Design fragment weight ................................ 0.002144 ounces Initial fragment velocity ................................ 3434 feet/sec Range to target ............................................... 1e-005 feet Target thickness ............................................. 1 inches
Fragment striking velocity ............................. 3434 feet/sec Fragment penetration ..................................... 0.1719 inches
ConWep 2.1.0.8
Fragment Penetration into Concrete Weapon .......................................................... Cube 0.2477" Design fragment weight ................................ 0.002144 ounces Initial fragment velocity ................................ 3434 feet/sec Range to target ............................................... 1e-005 feet Concrete slab thickness ................................. 1 inches Concrete compressive strength ...................... 4000 psi
Fragment striking velocity ............................. 3434 feet/sec Penetration into massive concrete ................. 0.3653 inches Minimum concrete thickness required to prevent perforation .................... 0.4421 inches Minimum concrete thickness required to prevent spalling ......................... 0.5389 inches
B-11
Information from Drawings:
Building 2B
B-12
Building 2A
B-13
SBEDS Results
Building: Component: By: Date:
Span, L: 26 ft Elastic Plastic 4 ft 0.11 0.12
Boundary Conditions: 0.39 0.38
Response Type:
Axis of Bending: Shape Type: Time Pressure Shape Size: (ms) (psi)
Self-Weight, w: 67.00 lb/ft 0 0 Moment of Inertia, I: 954.00 in4
10 0 Section Modulus: Z (hot-rolled beam) or S (cold-formed beam): 130.00 in3 20 0 Inbound Natural Period: 103.11 ms Web Thickness, tw: 0.40 in 30 0 Rebound Natural Period: 103.11 ms Depth, d: 16.33 in 40 0 Max Recommended Time Step: 0.05 ms Area, A: 19.70 in2 50 0 0.05 ms Supported Weight, W: 73 psf 60 0 % of Critical Damping: 2 % Loaded Area Factor Applied to L*B, Af: (Note:Af<=1) 1 70 0 Initial Velocity: 0 in/ms Inbound Unbraced Length for Compression Flange, Lbr,i: ft (0 for fully braced) Rebound Unbraced Length for Compression Flange, Lbr,r: 13 ft (0 for fully braced)
Material Type: W R Inbound Rebound Units Yield Strength, fy: 50,000 psi (lbs TNT) (ft) Mass, M 1613.0 1613.0 psi-ms2/in Ultimate Strength, fu: 70,000 psi Load-Mass Factors, K LM
Elastic Modulus, E: 29000000 psi KLM1 0.78 0.78 Static Strength Increase Factor: 1.05 KLM2 0.78 0.78 Dynamic Increase Factor: 1.19 KLM3 0.66 0.66 Dynamic Yield Stress, fdy: 62,475 psi Stiffness, K
4 Static Axial Load, P: lb K1 4.67 4.67 psi/in Leave blank for No Dynamic Axial Load Wall Height (ft)1 K2 4.67 4.67 psi/in Leave Blank Wall Width (ft)1 K3 0.00 0.00 psi/in
Incidence Angle2 Resistance, R
Inbound Moment Capacity, Mi: 8,121,750 lb-in See notes under error messages R1 13.91 -12.67 psi Rebound Moment Capacity, Mr: 7,400,959 lb-in R2 13.91 -12.67 psi Rebound/Inbound Moment Capacity Ratio, MR: 0.91 Ratio of Axial Load to Axial Load Capacity 0.00 Yield Displacement, x x1 2.98 -2.71 in x2 2.98 -2.71 in
LOP/Type θ (deg) μ Equiv Yield Defl., X E 2.98 -2.71 in 10 12 θmax = 0.05 deg. Design Criteria:
μ = 0.05
0.14 in at time = 39.80 msec -0.13 in at time = 92.50 msec
Notes: 0.67 psi at time = 39.80 msec 1 Used for clearing of reflected load -0.61 psi at time = 92.50 msec 2 Angle in degrees from normal Shortest Yield Line Distance to Determine θ: 156.0 in 3 Entering data in white cells will OVERWRITE formulas and cause ERRONEOUS results!!
To recover formulas, save your input data and reinitiate Component Type on Intro worksheet.
4 Axial load per unit width on analyzed component from saved Dynamic Shear History file for 104,125 lb supported component. The total dynamic axial load is this axial load per unit width multiplied 104,125 lb by the input axially loaded width, Ba. Dynamic axial load includes roof static load.
5 Shear controlled response typically has very limited response criteria, although exact values 221,642 lb are not specified in SBEDS - see Shear Flag section in User's Guide for additional guidance. Shear is OK
* Based on larger of inbound and rebound ultimate…
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