ARMY UFGS-33 52 43 14-2010 AVIATION FUEL CONTROL VALVES《航空燃油控制阀》.pdf

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1、*USACE / NAVFAC / AFCESA / NASA UFGS-33 52 43.14 (February 2010)-Preparing Activity: USACE UNIFIED FACILITIES GUIDE SPECIFICATIONSReferences are in agreement with UMRL dated April 2010*SECTION TABLE OF CONTENTSDIVISION 33 - UTILITIESSECTION 33 52 43.14AVIATION FUEL CONTROL VALVES02/10PART 1 GENERAL1

2、.1 REFERENCES1.2 ADMINISTRATIVE REQUIREMENTS1.3 SUBMITTALS1.4 QUALITY ASSURANCE1.4.1 Field Assistance1.4.2 Training1.5 WARRANTYPART 2 PRODUCTS2.1 MATERIALS AND EQUIPMENT2.2 CONTROL VALVES2.2.1 General2.2.1.1 Bodies, Bonnets, and Covers2.2.1.2 Valve Seats2.2.1.3 Valve Discs2.2.1.4 Diaphragm Assembly2

3、.2.1.5 Bolts, Screws and Nuts2.2.1.6 Pilot Control System and Auxiliary Piping2.2.1.7 Pilot Valves2.2.1.8 Solenoids2.2.2 Serviceability of Main Valve Internal Parts2.2.3 Total Lengths2.2.4 Flanges2.2.5 Identification2.2.5.1 Main Valve Body2.2.5.2 Main Valve Cover2.2.5.3 Brass Name Plates2.2.5.4 Inle

4、t Name Plate2.2.5.5 Outlet Name Plate2.2.5.6 Pilot Valves2.3 INDIVIDUAL CONTROL VALVE OPERATIONAL REQUIREMENTS2.3.1 High Liquid Level Shut-Off Valve (HLV-1 AND HLV-2)2.3.1.1 Size2.3.1.2 FlowSECTION 33 52 43.14 Page 1Provided by IHSNot for ResaleNo reproduction or networking permitted without license

5、 from IHS-,-,-2.3.1.3 Operation2.3.1.4 Check Valve Feature2.3.1.5 Manual Test Feature2.3.1.6 Strainer2.3.1.7 Pressure Sensitive Close Feature2.3.1.8 Minimum Differential Pressure Feature2.3.1.9 Opening and Closing Feature2.3.2 Non-Surge Check Valve (CV-1 THRU CV-6)2.3.2.1 Size2.3.2.2 Flow2.3.2.3 Ope

6、ration2.3.2.4 Quick closure2.3.2.5 Flow Control2.3.2.6 Strainer2.3.3 Non-Surge Check/Air Block Valve (AB/CV-1 THRU AB/CV- )2.3.3.1 Size2.3.3.2 Flow2.3.3.3 Operation2.3.3.4 Speed Control2.3.3.5 Check Feature2.3.3.6 Solenoid Control2.3.3.7 Strainer2.3.4 Filter Separator Control Valve (FSCV-1 Thru FSCV

7、-7)2.3.4.1 Size2.3.4.2 Flow2.3.4.3 Operation2.3.4.4 Check Valve Feature2.3.4.5 Water Slug Shut-Off2.3.4.6 Shut-Off Feature at Maximum Differential Pressure2.3.4.7 Emergency Shut-off Operation2.3.4.8 Solenoid Control2.3.5 Filter Separator Float Control Valve and Tester (FC-1 THRU FC-7)2.3.5.1 Operati

8、on2.3.5.2 Float Control Pilot and Tester2.3.6 Back Pressure Control Valve (BPCV-1)2.3.6.1 Size2.3.6.2 Flow2.3.6.3 Operation2.3.6.4 Check Valve Feature2.3.6.5 Solenoid Control2.3.6.6 Speed Control2.3.6.7 Opening Feature2.3.7 Pressure Control Valve (PCV-1)2.3.7.1 Size2.3.7.2 Flow2.3.7.3 Operation2.3.7

9、.4 Check Valve Feature2.3.7.5 Solenoid Control2.3.7.6 Speed Control2.3.8 Defuel/Flush Valve (D/FV-1)2.3.8.1 Size2.3.8.2 Flow2.3.8.3 Operation2.3.8.4 Check Valve Feature2.3.8.5 Solenoid Control2.3.8.6 Speed Control2.3.9 Hydrant Control Valve (HCV)2.3.9.1 Size2.3.9.2 FlowSECTION 33 52 43.14 Page 2Prov

10、ided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-2.3.9.3 Operation2.3.9.4 Quick Closure2.3.9.5 Deadman Control2.3.9.6 Defuel2.3.9.7 Speed Control2.3.9.8 Thermal Relief2.3.9.9 Adapter2.3.9.10 Strainer2.3.9.11 Minimum Differential Pressure Feature2.3.10 Ove

11、rfill Valve for Product Recovery Tank (OV-1)2.3.10.1 Size2.3.10.2 Capacity2.3.10.3 Operation2.3.10.4 Control Float2.3.10.5 Pressure Reservoir2.3.10.6 Thermal Relief2.3.10.7 Limit Switch2.3.10.8 Strainer2.3.11 Truck Fill Stand Control Valve (TFV)2.3.11.1 Size2.3.11.2 Flow2.3.11.3 Operation2.3.11.4 Qu

12、ick Closure2.3.11.5 Opening Speed Control2.3.11.6 Deadman Control2.3.11.7 Thermal Relief2.3.11.8 Strainer2.3.11.9 Solenoid Control2.3.12 Pantograph Control Valve (PTCV)2.3.12.1 Size2.3.12.2 Flow2.3.12.3 Operation2.3.12.4 Closing Speed Control2.3.12.5 Thermal Relief2.3.12.6 Strainer2.3.13 Flushing Va

13、lve (FV-1)2.3.13.1 Size2.3.13.2 Flow2.3.13.3 Operation2.3.13.4 Solenoid Control2.3.14 Pantograph Pressure Control Valve (PPCV-1 thru PPCV- )2.3.14.1 Size2.3.14.2 Operation2.3.14.3 Check Valve FeaturePART 3 EXECUTION3.1 VALVE TESTING AND START-UP SUPPORT- End of Section Table of Contents -SECTION 33

14、52 43.14 Page 3Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-*USACE / NAVFAC / AFCESA / NASA UFGS-33 52 43.14 (February 2010)-Preparing Activity: USACE UNIFIED FACILITIES GUIDE SPECIFICATIONSReferences are in agreement with UMRL dated April 2010*SE

15、CTION 33 52 43.14AVIATION FUEL CONTROL VALVES02/10*NOTE: This guide specification covers the requirements for diaphragm type automatic control valves used in aircraft refueling systems constructed to the requirements of the DoD Type III/IV/V, and Cutn Cover Hydrant Refueling System Standards. DoD Ty

16、pe III systems shall conform to Standard Design 078-24-28 PRESSURIZED HYDRANT FUELING SYSTEM (TYPE III). DoD Type 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, deletin

17、g, or revising text. For bracketed items, choose applicable items(s) or insert appropriate information.Remove information 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 t

18、echnical proponent of the specification. A listing of the technical proponents, including their organization designation and telephone number, is on the Internet.Recommended changes to a UFGS should be submitted as a Criteria Change Request (CCR).*PART 1 GENERAL1.1 REFERENCES*NOTE: This paragraph is

19、 used to list the publications cited in the text of the guide specification. The publications are referred to in the text by basic designation only and listed in this paragraph by organization, designation, date, and title.SECTION 33 52 43.14 Page 4Provided by IHSNot for ResaleNo reproduction or net

20、working permitted without license from IHS-,-,-Use the Reference Wizards Check Reference feature when you add a RID outside of the Sections Reference Article to automatically place the reference in the Reference Article. Also use the Reference Wizards Check Reference feature to update the issue date

21、s.References not used in the text will automatically be deleted from this section of the project specification when you choose to reconcile references in the publish print process.*The publications listed below form a part of this specification to the extent referenced. The publications are referred

22、 to in the text by basic designation only.ASME INTERNATIONAL (ASME)ASME B16.24 (2006) Cast Copper Alloy Pipe Flanges and Flanged Fittings: Classes 150, 300, 600, 900, 1500, and 2500ASME B16.5 (2009) Standard for Pipe Flanges and Flanged Fittings: NPS 1/2 Through NPS 24ASME BPVC SEC VIII D1 (2007; Ad

23、denda 2008; Addenda 2009) Boiler and Pressure Vessel Code; Section VIII, Rules for Construction of Pressure Vessels Division 1ASTM INTERNATIONAL (ASTM)ASTM A 194/A 194M (2009) Standard Specification for Carbon and Alloy Steel Nuts for Bolts for High-Pressure or High-Temperature Service, or BothASTM

24、A 216/A 216M (2008) Standard Specification for Steel Castings, Carbon, Suitable for Fusion Welding, for High-Temperature ServiceASTM A 269 (2008) Standard Specification for Seamless and Welded Austenitic Stainless Steel Tubing for General ServiceASTM A 320/A 320M (2008) Standard Specification for Al

25、loy/Steel Bolting Materials for Low-Temperature ServiceASTM A 536 (1984; R 2009) Standard Specification for Ductile Iron CastingsASTM A 743/A 743M (2006) Standard Specification for Castings, Iron-Chromium, Iron-Chromium-Nickel, Corrosion Resistant, for General ApplicationSECTION 33 52 43.14 Page 5Pr

26、ovided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-ASTM B 26/B 26M (2009) Standard Specification for Aluminum-Alloy Sand CastingsASTM D 2000 (2008) Standard Classification System for Rubber Products in Automotive ApplicationsASTM D 751 (2006) Coated Fabri

27、csNATIONAL FIRE PROTECTION ASSOCIATION (NFPA)NFPA 70 (2008; AMD 1 2008) National Electrical CodeSOCIETY OF AUTOMOTIVE ENGINEERS INTERNATIONAL (SAE)SAE AMS 3216 (2005; Rev G) Fluorocarbon (FKM) Rubber High-Temperature - Fluid Resistant Low Compression Set 70 To 80SAE J200 (2008) Classification System

28、 for Rubber MaterialsSAE J429 (1999) Mechanical and Material Requirements for Externally Threaded FastenersU.S. DEPARTMENT OF DEFENSE (DOD)MIL-A-8625 (2003; Rev F; Am 1) Anodic Coatings, for Aluminum and Aluminum Alloys1.2 ADMINISTRATIVE REQUIREMENTSDesign conditions shall be as specified in Section

29、 33 52 43.11 AVIATION FUEL MECHANICAL EQUIPMENT. Components shall be suitable for ANSI Class 150 ( 2 MPa 275 psig at 38 degrees C 100 degrees F).a. Control valves specified herein shall be of one manufacturer. The valve manufacturer shall also produce the hydraulically-operated pilots. For each type

30、 control valve required and specified, submit the following:(1). Flow diagrams.(2). Operational description of the control valve and pilot control system.(3). Complete valve assembly list of materials, along with material Certificates of Conformance, used in the manufacture of the control valves and

31、 pilot systems.(4). sectional drawings of main valve and control pilot systems.b. Before shipment, each individual control valve shall be operationally tested and adjusted by manufacturer under actual flow conditions utilizing a hydrocarbon test fluid with a specific gravity comparable to JP-4 JP-5

32、JP-7 JP-8 fuel. Manufacturer shall submit certified records of test data.c. Operation and maintenance information shall be submitted for each individual type control valve specified herein. Refer to Section 01 78 23.33 OPERATION AND MAINTENANCE MANUALS FOR AVIATION FUEL SYSTEMS for the information t

33、o be submitted.SECTION 33 52 43.14 Page 6Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-1.3 SUBMITTALS*NOTE: Review submittal description (SD) definitions in Section 01 33 00 SUBMITTAL PROCEDURES and edit the following list to reflect only the submi

34、ttals required for the project. Submittals should be kept to the minimum required for adequate quality control.A “G” following a submittal item indicates that the submittal requires Government approval. Some submittals are already marked with a “G”. Only delete an existing “G” if the submittal item

35、is not complex and can be reviewed through the Contractors Quality Control system. Only add a “G” if the submittal is sufficiently important or complex in context of the project.For submittals requiring Government approval on Army projects, a code of up to three characters within the submittal tags

36、may be used following the “G“ designation to indicate the approving authority. Codes for Army projects using the Resident Management System (RMS) are: “AE“ for Architect-Engineer; “DO“ for District Office (Engineering Division or other organization in the District Office); “AO“ for Area Office; “RO“

37、 for Resident Office; and “PO“ for Project Office. Codes following the “G“ typically are not used for Navy, Air Force, and NASA projects.Choose the first bracketed item for Navy, Air Force and NASA projects, or choose the second bracketed item for Army projects.*Government approval is required for s

38、ubmittals with a “G“ designation; submittals not having a “G“ designation are for Contractor Quality Control approval. information only. When used, a designation following the “G“ designation identifies the office that will review the submittal for the Government. Submit the following in accordance

39、with Section 01 33 00 SUBMITTAL PROCEDURES:SD-02 Shop DrawingsControl Valves; G; G, _.SD-03 Product DataControl Valves; G; G, _.SD-06 Test ReportsControl Valves; .SD-07 CertificatesPrevious Air Force/Military Projects; G; G, _.SECTION 33 52 43.14 Page 7Provided by IHSNot for ResaleNo reproduction or

40、 networking permitted without license from IHS-,-,-Qualified Engineers; G; G, _.Field Assistance; G; G, _.SD-10 Operation and Maintenance DataOperation and Maintenance Manuals; G; G, _.1.4 QUALITY ASSURANCE1.4.1 Field AssistanceProvide the following:a. Proof of experience on previous Air Force/Milit

41、ary projects.b. Number of qualified engineers (factory trained)available to provide startup support.c. Written assurance as to ability to respond to specified time for field assistance.1.4.2 TrainingThe manufacturer shall conduct two eight hour training classes for Liquid Fuels Maintenance Technicia

42、ns which include valve overhaul procedures, pilot overhaul procedures, valve adjustments, and valve diagnostics. The manufacturer shall provide a 100 mm 4-inch valve mock-up with various trim components (i.e., rate of flow, solenoid control, and speed control features) to be used during training. Vi

43、deo taping of training shall be allowed or provided at the time of the class, and an attendance roster maintained by the Contractor. The 100 mm 4-inch valve mock-up shall become the property of the Government and shall be turned over to the Contracting Officer. Submit copies of the Operation and Mai

44、ntenance Manuals for approval.1.5 WARRANTY*NOTE: Modify hours for projects outside the UNITED STATES.*If a problem attributable to the valves manufacturer or installation arises after the initial system start-up has been accomplished, and after system final acceptance date, the Contractor shall have

45、 48 _ hours from the time of notification that a problem exists to solve the problem. The problem shall be solved to the satisfaction of the Contracting Officer, the Base Civil Engineer and/or the Command Fuel Facilities Engineer Contracting Officer. If the Contractor cannot effectuate a proper resolution to the problem as outlined above in the 48 _ hour period, provide a factory trained enginee