ARMY UFGS-33 09 54-2010 AVIATION FUEL PUMP CONTROL AND ANNUNCIATION SYSTEM (TYPE [IV][V])《航空燃油泵控制就警报系统([IV][V]型)》.pdf
《ARMY UFGS-33 09 54-2010 AVIATION FUEL PUMP CONTROL AND ANNUNCIATION SYSTEM (TYPE [IV][V])《航空燃油泵控制就警报系统([IV][V]型)》.pdf》由会员分享,可在线阅读,更多相关《ARMY UFGS-33 09 54-2010 AVIATION FUEL PUMP CONTROL AND ANNUNCIATION SYSTEM (TYPE [IV][V])《航空燃油泵控制就警报系统([IV][V]型)》.pdf(45页珍藏版)》请在麦多课文档分享上搜索。
1、*USACE / NAVFAC / AFCESA / NASA UFGS-33 09 54 (February 2010)-Preparing Activity: USACEUNIFIED FACILITIES GUIDE SPECIFICATIONSReferences are in agreement with UMRL dated April 2010*SECTION TABLE OF CONTENTSDIVISION 33 - UTILITIESSECTION 33 09 54AVIATION FUEL PUMP CONTROL AND ANNUNCIATION SYSTEM (TYP
2、E IVV)02/10PART 1 GENERAL1.1 SYSTEM OVERVIEW1.2 GENERAL REQUIREMENTS1.3 REFERENCES1.4 SUBMITTALS1.5 OPERATION AND MAINTENANCE MANUALS1.5.1 Schedule and Content1.5.2 Assembly1.6 TOOLS AND SPARE PARTS1.7 EXPERIENCE AND QUALIFICATIONS1.8 WARRANTYPART 2 PRODUCTS2.1 PUMP CONTROL PANEL (PCP) AND COMPONENT
3、S2.1.1 Enclosure2.1.2 Ventilation System2.1.3 Ground Bar2.1.4 Standard Indicator Lights2.1.5 Selector Switches2.1.6 Pushbuttons2.1.7 Relays2.1.8 Nameplates2.1.9 Transient Voltage Surge Suppression Devices2.1.10 Terminal Blocks2.1.11 Circuit Breakers2.1.12 Uninteruptable Power Supplies2.1.13 Miscella
4、neous Power Supplies2.1.14 Alarm Annunciator2.1.15 Alarm Horns2.1.16 Laptop Computer2.1.16.1 Hardware2.1.16.2 Software2.1.17 Personal Computer (PC)2.1.17.1 Hardware2.1.17.2 SoftwareSECTION 33 09 54 Page 1Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-
5、,-2.1.18 Printer2.1.19 FCC Computer2.1.19.1 Hardware2.1.19.2 Software2.2 PROGRAMMABLE LOGICAL CONTROLLER (PLC) HARDWARE AND SOFTWARE2.2.1 General2.2.2 Central Processing Unit Module2.2.3 Power Supply Module2.2.4 Program Storage/Memory Requirements2.2.5 Input/Output (I/O) Modules2.2.6 Interfacing2.2.
6、7 Program Requirements2.2.8 Diagnostics2.3 GRAPHICS DISPLAY PANEL2.3.1 Enclosure2.3.2 Display Presentation2.3.3 Digital Flow and Pressure IndicatorsPART 3 EXECUTION3.1 PUMP CONTROL PANEL (PCP) AND COMPONENTS3.1.1 General3.1.2 Wiring3.1.2.1 Methods and Practices3.1.2.2 Control Wiring Data Lists3.1.3
7、Shop Tests3.1.4 Ventilation System3.1.5 Grounding3.1.6 Indicator Lights, Switches, and Pushbuttons3.1.7 Transient Voltage Surge Suppression Devices3.1.8 Terminal Blocks3.1.9 Circuit Breakers3.1.10 Uninteruptable Power supplies3.1.11 Power Supplies3.1.12 Alarm Annunciator and Horns3.1.12.1 Non-critic
8、al Alarms3.1.12.2 Critical Alarms3.1.12.3 Alarm Sequence3.1.13 Personal Computer3.1.13.1 Screen Number 13.1.13.2 Screen Number 23.1.13.3 Screen Number 33.1.13.4 Screen Number 43.1.13.5 Screen Number 53.1.13.6 Screen Number 63.1.13.7 Screen Number 73.1.13.8 Screen Number 83.1.13.9 Screen Number 93.1.
9、14 Laptop Computer3.2 PROGRAMMABLE LOGICAL CONTROLLER (PLC) HARDWARE AND SOFTWARE3.2.1 General3.2.2 Programs3.3 GRAPHICS DISPLAY PANEL3.4 GRAPHICS DISPLAY SCREEN3.4.1 General3.4.2 Display Presentation3.4.3 Process Schematic3.4.4 Digital Flow and PressureIndicators3.5 INSTALLATIONSECTION 33 09 54 Pag
10、e 2Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-3.5.1 Shop Drawing3.5.2 System Start-Up and Testing3.5.3 Training Plan for Instructing Personnel3.6 PLC CONTROL SYSTEM SEQUENCE OF OPERATION3.6.1 General3.6.1.1 Abbreviations3.6.2 Operating Tanks3.6.
11、2.1 Level Control3.6.2.2 Level Control3.6.2.3 Outlet Valve3.6.3 Product Recovery Tank3.6.3.1 Fuel Transfer Pump (FTP)3.6.3.2 Overfill Valve (OV)3.6.3.3 High Level Alarm3.6.3.4 High-High Level Alarm3.6.3.5 Leak Detection3.6.4 Fueling Pumps (FP)3.6.5 Flow Switch, Fueling Pump3.6.6 Transmitters3.6.6.1
12、Pressure Indicating Transmitter (PIT)3.6.6.2 Differential Pressure Transmitter (DPT)3.6.6.3 Pressure Sensors (PS)3.6.7 Control Valves3.6.7.1 Flushing Valve (FV)3.6.7.2 Pressure Control Valve (PCV)3.6.7.3 Backpressure Control Valve (BPCV)3.6.8 Safety Circuit3.6.8.1 Emergency Stop Status3.6.8.2 Emerge
13、ncy Shutoff Valves (ESO) Status3.6.8.3 Circuit Power Status3.6.9 Pump Control Panel3.6.9.1 CPU Faults3.6.9.2 Input Select Switch3.6.9.3 Mode Select Switch3.6.9.4 Lead Pump Selector Switch3.6.9.5 PCP Temperature Alarm3.7 OPERATING PROGRAM REQUIREMENTS3.8 AUTOMATIC MODE - IDLE CONDITION3.9 AUTOMATIC M
14、ODE - REFUELING CONDITION3.10 RE-FUELING MODE - REFUELING CONDITION3.11 LOOP FLUSH MODE3.12 PANTAGRAPH FLUSH MODE3.13 TIGHTNESS TEST MODE3.13.1 High Pressure Test Preparation3.13.2 Run High Pressure Test3.13.3 Low Pressure Test Preparation3.13.4 Run Low Pressure Test3.13.5 Second High Pressure Test
15、Preparation3.13.6 Run Second High Pressure Test3.14 OFF MODE3.15 MANUAL OPERATION OF FUELING PUMPS3.16 4-VALVE MANIFOLD SUPERVISION- End of Section Table of Contents -SECTION 33 09 54 Page 3Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-*USACE / NAV
16、FAC / AFCESA / NASA UFGS-33 09 54 (February 2010)-Preparing Activity: USACEUNIFIED FACILITIES GUIDE SPECIFICATIONSReferences are in agreement with UMRL dated April 2010*SECTION 33 09 54AVIATION FUEL PUMP CONTROL AND ANNUNCIATION SYSTEM (TYPE IVV)02/10*NOTE: This guide specification covers the requir
17、ements for the Pump Control and Annunciation System for aircraft refueling systems constructed to the requirements of the DOD Type IV or V Direct Aircraft Refueling System Standards. DoD Type III systems shall conform to Standard Design 078-24-28 PRESSURIZED HYDRANT FUELING SYSTEM (TYPE III). DoD Ty
18、pe IV/V systems shall conform to Standard Design 078-24-29 AIRCRAFT DIRECT FUELING SYSTEM (TYPE IV) DESIGN Edit this guide specification for project specific requirements by adding, deleting, or revising text. For bracketed items, choose applicable items(s) or insert appropriate information.Remove i
19、nformation and requirements not required in respective project, whether or not brackets are present.Comments and suggestion on this specification are welcome and should be directed to the technical proponent of the specification. A listing of the technical proponents, including their organization de
20、signation and telephone number, is on the Internet.*PART 1 GENERAL1.1 SYSTEM OVERVIEWThe Aircraft Direct Fueling System Aircraft In-Shelter Fueling System consists of fueling pumps that pump fuel to pantagraph type fueling stations located on the airfield apron. in Aircraft Shelters. Using Scheme A,
21、 the lead pump is started manually by the start/stop station located at the fueling station. The other pump is started and stopped automatically by the PCP. Using Scheme B, all pumps are started and stopped automatically by the PCP. Automatic pump starts and stops are based on system pressure and fl
22、ow. Programmable Logic Controllers (PLCs) receive information from pressure transmitters and other devices to control the pumps and control valves. There are two PLCs that are connected in a SECTION 33 09 54 Page 4Provided by IHSNot for ResaleNo reproduction or networking permitted without license f
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