SAE AIR 1174B-2001 Index of Starting System Specifications and Standards《启动系统规范和标准索引》.pdf

1、SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirelyvoluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefro

2、m, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions.Copyright 2001 Society of Automotive Engineers, Inc.All rights reserved. Printed in U.S.

3、A.TO PLACE A DOCUMENT ORDER: (724) 776-4970 FAX: (724) 776-0790 SAE WEB ADDRESS: http:/www.sae.org400 Commonwealth Drive, Warrendale, PA 15096-0001AEROSPACE INFORMATION REPORTAIR1174REV.BIssued 1970-07Revised 2001-12Superseding AIR1174AIndex of Starting System Specifications and Standards1. SCOPE:Th

4、is report lists military and industry specifications and standards which are used in aerospace engine starting and auxiliary power systems. Listings are provided as follows:Section 2. Topic ListingSection 3. Numerical ListingSection 4. Alphabetical ListingOnly those hardware standards which have bee

5、n specifically designed for engine starting systems are listed. Revisions and amendments which are current for these specifications and standards are not listed.1.1 Listing Documents:The following documents which list specifications and standardsare used as a basis for this report. Basic document nu

6、mbers are listed without revision letter. Many Military specifications are officially canceled and will no longer be kept up to date but they are available for general use.1.1.1 Military Specifications and Standards: Department of Defense, Index of Specifications and Standards. This document is publ

7、ished annually with bi-monthly supplements.1.1.2 Society of Automatic Engineers, Inc. Documents: Index of Aerospace Standards, Recommended Practices and Information Reports. This document is published annually by SAE, Inc., 400 Commonwealth Drive, Warrendale, PA 15096.SAE AIR1174 Revision B- 2 -1.2

8、Availability of Documents:SAE Publications (SAE, AS, ARP, AIR) are available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001. Military and U.S. Government Publications (DOD, MS, SD, ARDCM, AN, AND, MIL, MS) are available from DODSSP, Subscription Service Desk, Building 4D, 700 Robbins Av

9、enue, Philadelphia, PA 19111-5094.2. TOPIC LISTING:Documents are organized under technical topics and source. 2.1 Engine Starting Characteristics:2.1.1 Military Specifications:Engines, Aircraft, Turbojet and Turbofan, General Specification for MIL-E-5007Engines, Aircraft, Turboshaft and Turboprop, G

10、eneral Specification for MIL-E-85932.1.2 Society of Automotive Engineers Documents:Guide for Determining Engine Starter Drive Torque Requirements AIR781Guide for Determining, Presenting and Substantiating Turbine AIR713Engine Starting and Monitoring CharacteristicsPower Sources, Auxiliary, for Aeros

11、pace Applications AIR744Engines, Aircraft, Reciprocating, General Specification for AS251092.2 Engine Starting System:2.2.1 Military Specifications:Joint Service Specification Guide: Air Vehicle Subsystems JSSG-2009Auxiliary Power Systems, Airborne MIL-A-87229(inactive for new design - see JSSG-2009

12、)SAE AIR1174 Revision B- 3 -2.2.2 Society of Automotive Engineers Documents:Aircraft Accessory Drag Torque During Engine Starts AIR1087A Means of Testing Turbojet Starter Performance ARP715Gasket Type XI, Engine Accessory Drive AS3492Gasket - Type XII, XIV A and XIV B Engine Accessory Drive AS3493Ga

13、sket - Type XVI Engine Accessory Drive AS3496Gasket Engine Accessory Drive AS3498Glossary, Aircraft Engine Starting Systems ARP906Guide for Determining Engine Starter Drive Torque Requirements ARP781Turbine Engine Starting System Design Requirements ARP949Turbine Engine Starting and Motoring Charact

14、eristics Guide AIR713for Determining, Presenting and Substantiating2.2.3 Military Standards:Drive Pad-Accessory, 10.000 BC Round, Design Standard for MS3329Flange Accessory, 5.000 BC Square, Design Standard for MS3331Flange Accessory, 10.000 BC Round, Design Standard for MS3334Adapter Installation -

15、 Type XII or XVI Drive Starter Jaw MS33509Drive Pad-Accessory, 5.000 BC Round, Design Standard for MS3327 (AS)Drive Pad-Accessory 8.000 BC Round, Design Standard for MS3328 (AS)Drive Pad-Accessory 5.000 BC Square, Design Standard for MS3326 (AS)Flange Accessory, 5.000 BC Round, Design Standard for M

16、S3332 (AS)Flange Accessory, 8.000 BC Round, Design Standard for MS3333 (AS)SAE AIR1174 Revision B- 4 -2.2.4 Society of Automotive Engineers Standards:Power Take-Off Pad Requirements, Gas Turbine Engine ARP748Flange - Accessory, 2.653 BC Square, Design Standard for AS960Splines Involute; Wear Definit

17、ion of ARP1200Drives and Flange Standards, Aircraft Engine and Accessory AIR1160Breech Drive Pad, OAD Assembly AS1259Coupling Clamp, Groove V-Band 6.400, 9.400, 11.400 Flange OD AS976Disconnect Systems, Accessory Drive Shaft AIR853Drive Tachometer Type I AS54Drive Studded, Accessory, 10.000 BC Round

18、, Design Standard for AS967Drive Studded, Accessory, 2.653 BC Square, Design Standard for AS959Drive Studded, Accessory, 5.000 BC Square, Design Standard for AS961Drive Accessory, 10.000 BC Round, QAD, Design Standard for AS971Flange Accessory, 10.000 BC Round, Design Standard for AS968Gasket Copper

19、, Tube Connection, Plain AS3332Flange Accessory, 5.000 BC Square, Design Standard for AS962Drive Accessory, 5.000 BC Round, QAD, Design Standard for AS969Drive Accessory, 8.000 BC Round, QAD, Design Standard for AS970Drive Studded, Accessory, 5.000 BC Round, Design Standard for AS963Drive Studded, A

20、ccessory, 8.000 BC Round, Design Standard for AS965Flange Accessory, 5.000 BC Round, Design Standard for AS964Flange Accessory, 8.000 BC Round, Design Standard for AS966Spline Details, Accessory Drives and Flanges AS972SAE AIR1174 Revision B- 5 -2.3 Cartridge/Pneumatic Starting System:2.3.1 Society

21、of Automotive Engineers Documents:2.3.2 System Components:2.3.2.1 Starter:2.3.2.1.1 Military Specifications:Starter, Engine, Cartridge/Pneumatic, Shaft MIL-S-27266Drive General Specification for2.3.2.2 Energy Control:2.3.2.2.1 Military Specifications:Valve, Starter Control, Pneumatic, Aircraft MIL-V

22、-38398Engine General Specifications forValve, Starter Control, Aircraft Engine, General MIL-V-81995Specification for2.3.2.3 Mechanical Connections:2.3.2.3.1 Ducting:2.3.2.3.1.1 Military Specifications:Bleed Air Systems, General MIL-B-81365Specification forCoupling Half, Quick Disconnect, MIL-DTL-255

23、31Pneumatic Starter, External, Low PressureDuct, Pneumatic Start, Flexible MIL-DTL-22706Pneumatic Power Systems, High MIL-P-87210Pressure (inactive for new design see JSSG 2009)SAE AIR1174 Revision B- 6 -2.3.2.3.1.2 Society of Automotive Engineers Documents:High Temperature Pneumatic Duct ARP699Syst

24、ems for Aircraft2.3.2.3.1.3 Military Standards:Fitting, Pneumatic Starter Duct- MS17833Flanged (Male)Fitting, Pneumatic Starter Duct- MS17835Flanged (Female)Connector, Pneumatic Starter Duct, MS17836Double EndedAdapter, Pneumatic Starter, Duct MS17834Nipple and (Male)Nipple, Pneumatic Starting, 3 in

25、ch MS33740I.D. Outline Dimensions of2.3.2.3.2 Electrical:2.3.2.3.2.1 Military Specifications:Connectors, Electrical Circular, MIL-C-5015Threaded AN type, General Specification forConnectors, Electric, (Circular, MIL-C-83723Environment Resisting), Receptacles and Plugs, GeneralSpecification forSAE AI

26、R1174 Revision B- 7 -2.3.2.3.2.1 (Continued):Slash Sheets for Series III MIL-C-83723/82Threaded Coupling thruMIL-C-83723/85MIL-C-83723/88thruMIL-C-83723/90MIL-C-83723/95thruMIL-C-83723/98Connectors, Electrical, Circular, MIL-C-38999Miniature High Density, Quick Disconnect, Threaded Coupling, Series

27、IIIConnectors, Series III, Slash MIL-C-38999/20Sheets thruMIL-C-38999/27Contracts, Electrical Connector, MIL-C-39029General Specification forConnector, Accessories, Electrical, MIL-C-85049General Specification forInstalling and Removal Tools, MIL-I-81969Connector Electrical Contact, General Specific

28、ation forCrimping Tools, Terminal, Hand or MIL-DTL-22520Power Actuated, Wire Termination, and Tool Kits,General Specification forSAE AIR1174 Revision B- 8 -2.3.2.3.2.2 Military Standards:Connectors, Receptacle, Electrical, MS3450Wall Mounting Rear Release, Crimp Contact, AN TypeConnectors, Receptacl

29、e, Electrical, MS3451Cable Connecting, Rear Release, Crimp Contact, AN TypeConnectors, Receptacle, Electrical, MS3452Box Mounting, Rear Release, Crimp Contact, AN TypeConnectors, Receptacle, Electrical, MS3454Jam Nut Mounting, Rear Release, Crimp Contact, AN TypeConnectors, Plug, Electrical, Self- M

30、S3459locking Coupling Nut, Rear Release, Crimp Contact, AN Type2.3.3 Power Source:2.3.3.1 Military Specifications:Cartridge, Engine Starter MXU-4A/A MIL-C-27505Power Units, Aircraft Auxiliary, Gas-Turbine-Type, MIL-P-8686General Specification forAuxiliary Power Systems, Airborne MIL-A-87229(inactive

31、 for new design - see JSSG-2009)Power Unit, Aircraft, Auxiliary, Gas Turbine, General MIL-P-85573Specification for2.3.3.2 Society of Automotive Engineers Documents:Pneumatic Power Supplies for Starting Aircraft AIR944SAE AIR1174 Revision B- 9 -2.4 Electric Starting System:2.4.1 Military Specificatio

32、ns:Electrical Power Systems, Aircraft MIL-E-87219Selection and Installation of Aircraft Electric Equipment MIL-STD-70802.4.2 Society of Automotive Engineers Documents:2.4.3 Military Standards:Criteria, Jet Electrical Starting System, DC Aircraft MS17794Electrical Power Characteristics MIL-STD-7042.4

33、.4 System Components:2.4.4.1 Starter:2.4.4.1.1 Military Specifications:Starter, Electric, Constant Current DC MIL-S-7780Starter-Generator, Engine, STU-6A MIL-S-265472.4.4.1.2 Society of Automotive Engineers Documents:Generators/Starter-Generators, Engine Driven AS8020DC, and Associated Voltage Regul

34、ators, Minimum Performance Standards forD-C Starter-Generator, Engine, General ARP892Specification for2.4.4.1.3 Military Standards:Starter-Aircraft, Direct Cranking, 28V DC AN41162.4.4.2 Connections:2.4.4.2.1 Electrical:SAE AIR1174 Revision B- 10 -2.4.4.2.1.1 Military Specifications:Cable Assemblies

35、 and Attachable MIL-C-7974Plugs External Power, Aircraft2.4.5 Power Source:2.4.5.1 Military Specifications:Battery and Cell, Storage, Aircraft, General Specification for MIL-B-8565Battery, Storage, Aircraft, Type MA-2-1 MIL-B-26026Batteries and Cells, Storage, Nickel-Cadmium, Aircraft, MIL-PRF-81757

36、General Specification forBatteries, Storage, Lead Acid, General Specification for MIL-B-837692.4.5.2 Society of Automotive Engineers Documents:Electromagnetic Compatibility (EMC) System Design Checklist AIR1221Electromagnetic Compatibility on Gas Engines for Aircraft Propulsion AIR1423Electromagneti

37、c Interference (EMI) Measurement Impulse ARP1267Generators; Standard Calibration Requirements and Techniques Methods of Achieving Electromagnetic Compatibility of AIR1425Gas Turbine Engine Accessories for Self-Propelled Vehicles Nickel Cadmium Vented Rechargeable Aircraft Batteries AS8033(non-sealed

38、 maintainable type)2.4.5.3 Military Standards:2.5 Gas Turbine Starting System (Jet Fuel Starter):SAE AIR1174 Revision B- 11 -2.5.1 Military Specifications:Starter Auxiliary Power Unit, Aircraft Engine, As Turbine Type, MIL-S-85419Detailed Specification forAuxiliary Power Systems, Airborne MIL-A-8722

39、9(inactive for new design - see JSSG-2009)2.6 Hydraulic Starting System:2.6.1 Military Specifications:Starter, Aircraft Engine, Hydraulic General Specification for MIL-S-22999Hydraulic Power Systems MIL-H-87227(inactive for new design - see JSSG-2009)2.6.2 Society of Automotive Engineers Documents:A

40、erospace Hydraulic and Pneumatic Specifications and Standards AIR737Determination of Hydraulic Pressure Drop ARP24Hydraulic Fluid Characteristics AIR81Fluid System Characteristics Affecting Hydraulic Pump Operation ARP819Fluid Properties AIR1116 Hydraulic Systems, Aircraft, Design and Installation R

41、equirements AS54402.6.3 System Components:2.6.3.1 Military Specifications:Starter, Aircraft Engine, Hydraulics MIL-S-22999SAE AIR1174 Revision B- 12 -2.6.3.1.2 Society of Automotive Engineers Documents:Aircraft Hydraulic Starters AS714AAircraft Hydraulic Starter/Pumps AS838Hydraulic System Component

42、s, General AS8775Specifications forHydraulic Energy Limited Starting Systems AIR14662.6.4 Power Source:2.6.4.1 Military Specifications:Filter and Filter Elements, Fluid Pressure, Hydraulic MIL-F-8815Line, 15 Micron Absolute and 5 Micron Absolute,Type II Systems, General Specifications forAccumulator

43、s, Aircraft Hydropneumatic Pressure MIL-A-5498Pump, Hydraulic Ram, Hand Driven MIL-P-5515Motors Aircraft, Hydraulic, Constant Displacement, MIL-M-7997General Specification for2.6.4.2 Society of Automotive Engineers Documents:Hose Assemblies, Metal, Medium Pressure, High Temperature ARP1424Hose Assem

44、blies: Aircraft and Missile, High ARP604Temperature (400 F), High Pressure (3000 psi)Hose Characteristics and Selection Chart AIR797Tubing Installations, Recommended Practice for the ARP994Design of, for Aerospace Fluid Power SystemsPumps, Hydraulic, Variable Flow, General Specification for AS19692S

45、AE AIR1174 Revision B- 13 -2.6.4.3 Military Standards:Accumulator, Cylindrical, 3,000 PSI MS28700Pump-Hydraulic Hand AN6201Pump-Hydraulic Hand, Type 3000 AN62482.7 Mechanical Starting System:2.7.1 System Components:2.7.1.1 Starter:2.8 Pneumatic Starting System:2.8.1 Society of Automotive Engineers D

46、ocuments:Safety Criteria for Pneumatic Starting Systems AIR1639Gas Energy Limited Starting Systems AIR14672.8.2 System Components:2.8.2.1 Starter:2.8.2.1.1 Military Specifications:Starter, Aircraft Engine, Air Turbine MIL-S-19557Starter and Accessory Drive, Combination: MIL-S-22518Aircraft Engine, A

47、ir Turbine Type I, Detail Model Specification forStarter, Engine, Air Turbine STU-16/A MIL-S-38043Starter, Pneumatic, Aircraft Engine, General MIL-S-38399Specification forSAE AIR1174 Revision B- 14 -2.8.2.1.2 Society of Automotive Engineers Documents:Starting Aircraft, Pneumatic Power Supplies for A

48、IR944Symbols Graphic, for Aircraft Hydraulic Wear Definition of ARP1200Electromagnetic Interference (EMI) Measurement Impulse ARP1267Generators; Standard Calibration Requirements and TechniquesHose Assemblies, Metal, Medium Pressure, High Temperature ARP1424Valve, Starter Control, Pneumatic, Aircraf

49、t Engine ARP1607General Specification for3.6 AS (SAE Aerospace Standard):Drive Tachometer Type I AS54Aircraft Hydraulic Starters AS714Aircraft Hydraulic Starter/Pumps AS838Starter, Pneumatic, Aircraft Engine, General Specification for AS943Flange - Accessory, 2.653 BC Square, Design Standard for AS960Flange Accessory, 5.000 BC Square, Design Standard for AS962Drive Studded, Accessory, 5.000 BC Round, Design Standard for AS963Drive Studded, Accessory, 8.000 BC Round, Design Standard for AS965Drive Studded, Accessory, 10.000 BC Round, D