SAE AIR 1899A-2001 Aerospace Military Aircraft Hydraulic System Characteristics《航空航天军用飞机液压系统特征》.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 REPORTAIR1899 REV.AIssued 1985-08Reaffirmed 1991-11Revised 2001-03Superseding AIR1899Aerospace Military Aircraft HydraulicSystem Ch

4、aracteristicsTABLE OF CONTENTS1. SCOPE .41.1 Purpose .41.2 Field of Application 42. APPLICABLE DOCUMENTS52.1 SAE Publications .52.2 U.S. Government Publications.53. ATTACK AIRPLANES 53.1 Northrop Grumman A-6A.53.2 Northrop Grumman A-7E.123.3 Fairchild A-10A 183.4 Lockheed F-117A 244. FIGHTER AIRPLAN

5、ES.294.1 Northrop Grumman F-5E .294.2 Northrop Grumman F-14A .344.3 Boeing F-15A .414.4 Lockheed Martin F-16A .484.5 Boeing F/A-18A .544.6 MRCA 595. BOMBERS 655.1 Boeing B-1B.655.2 Northrop Grumman B-2A.73SAE AIR1899 Revision A- 2 -TABLE OF CONTENTS (Continued)6. ANTI-SUB - FIXED WING AIRCRAFT806.1

6、Lockheed Martin P-3806.2 Lockheed Martin S-3A .857. TRANSPORT AIRPLANES.917.1 Lockheed Martin C-5A .917.2 Boeing C-17A Globemaster III .977.3 Lockheed Martin C-1301047.4 Lockheed Martin C-141B .1108. HELICOPTERS .1188.1 Bell 2141188.2 Sikorsky CH-53E1238.3 Sikorsky S-76 .1289. BOATS1339.1 M-161 Boat

7、 13310. SUMMARY138FIGURE 1 A6-A Aircraft Hydraulic System.10FIGURE 2 A-6A Power System11FIGURE 3 A-7E Aircraft Hydraulic System.16FIGURE 4 A-7E Power System17FIGURE 5 A-10A Aircraft Hydraulic System .22FIGURE 6 A-10A Power System 23FIGURE 7 F-117A Aircraft Hydraulic System .27FIGURE 8 F-117A Power S

8、ystem 28FIGURE 9 F-5E Aircraft Hydraulic System .32FIGURE 10 F-5E Power System 33FIGURE 11 F-14A Aircraft Hydraulic System .39FIGURE 12 F-14A Power System 40FIGURE 13 F-15A Aircraft Hydraulic System .45FIGURE 14 F-15A Flight Power System 46FIGURE 15 F-15A Utility Power System 47FIGURE 16 F-16A Aircr

9、aft Hydraulic System .52FIGURE 17 F-16A Power System 53FIGURE 18 F-18A Aircraft Hydraulic System .57FIGURE 19 F-18A Power System 58FIGURE 20 MRCA Aircraft Hydraulic System 63FIGURE 21 MRCA Power System .64SAE AIR1899 Revision A- 3 -TABLE OF CONTENTS (Continued)FIGURE 22 B-1B Aircraft Flight Control

10、System 69FIGURE 23 B-1B Aircraft Utility System .70FIGURE 24 B-1B Power System71FIGURE 25 B-1B Hydraulic Reservoir 72FIGURE 26 B-2A Aircraft Flight Controls Hydraulic System.77FIGURE 27 B-2A Aircraft Utility System .78FIGURE 28 B-2A Power System79FIGURE 29 P-3 Aircraft Hydraulic System .83FIGURE 30

11、P-3 Power System 84FIGURE 31 S-3A Aircraft Hydraulic System.89FIGURE 32 S-3A Power System90FIGURE 33 C-5A Aircraft Hydraulic System .95FIGURE 34 C-5A Power System 96FIGURE 35 C-17A Aircraft Hydraulic System.102FIGURE 36 C-17A Power System103FIGURE 37 C-130 Aircraft Hydraulic System .108FIGURE 38 C-1

12、30 Power System 109FIGURE 39 C-141B Aircraft Hydraulic System.114FIGURE 40 C-141B Power System 1 .115FIGURE 41 C-141B Power System 2 .116FIGURE 42 C-141B Power System 3 .117FIGURE 43 214 Aircraft Hydraulic System .121FIGURE 44 214 Power System 122FIGURE 45 CH-53E Aircraft Hydraulic System 126FIGURE

13、46 CH-53E Power System .127FIGURE 47 S-76 Aircraft Hydraulic System .131FIGURE 48 S-76 Power System 132FIGURE 49 M-161 Boat Hydraulic System.136FIGURE 50 M-161 Power System 1 .137TABLE 1 Summary .139SAE AIR1899 Revision A- 4 -1. SCOPE:This SAE Aerospace Information Report (AIR) has been compiled to

14、provide information on hydraulic systems fitted to the following categories of military vehicles. Attack Airplanes Fighter Airplanes Bombers Anti-Sub, Fixed Wing Airplanes Transport Airplanes Helicopters Boats1.1 Purpose:The purpose of this document is to provide hydraulic system information to mili

15、tary vehicle system and component designers in order to assist them in future aircraft fluid power system designs.The information provided in this Information Report may be used to find similar type systems, components and materials which will in turn help solve specific problems and lower costs.1.2

16、 Field of Application: Design requirements: Procurement Specifications System pressure: Fluid power system operating pressure Hydraulic fluid: Type of fluid system is designed for No. of hydraulic systems: No. and ID of independent hydraulic systems System temperature: Minimum and maximum operating

17、temperatures Main hydraulic pump: Flow, pressure, displacement Backup pump data: System auxiliary pump or backup pump data Hydraulic motor data: System hydraulic motor requirements Accumulator data: Usage, volume and precharge requirements Reservoir data: Type, volume and pressure Relief valve data:

18、 Usage, crack and reseat press, rated flow Filtration: Usage, filtration rating Tubing data: Materials, sizes, wall thickness Fitting data: Type, size range, material Schematic block diagram: System architecture, services supplied Power circuit schematic: Detail schematic of power system Heat exchan

19、gers: Cooling medium Hand pump data: System hand pump data Miscellaneous: Quiescent flow, seal material, etc.SAE AIR1899 Revision A- 5 -2. APPLICABLE DOCUMENTS:The following publications form a part of this document to the extent specified herein. The latest issue of SAE publications shall apply. Th

20、e applicable issue of other publications shall be the issue in effect on the date of the purchase order. In the event of conflict between the text of this document and references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws a

21、nd regulations unless a specific exemption has been obtained.2.1 SAE Publications:Available from SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001.AS1290 Graphic Symbols for Aircraft Hydraulic and Pneumatic Systems2.2 U.S. Government Publications:Available from DODSSP, Subscription Services Des

22、k, Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094.MIL-H-5440(now AS5440) Hydraulic Systems, Aircraft, Design and Installation Requirements forMIL-H-5606 Hydraulic Fluid, Petroleum Base, Aircraft, Missile and OrdnanceMIL-PRF-83282 Hydraulic Fluid, Fire Resistant, Synthetic Hydrocarbon B

23、ase, Metric, Nato Code Number H-537MIL-PRF-87257 Hydraulic Fluid, Fire Resistant, Low Temperature, Synthetic Hydrocarbon Base, Aircraft and Missile3. ATTACK AIRPLANES:3.1 Northrop Grumman A-6A:3.1.1 Design Requirements: MIL-H-5440B3.1.2 System Pressure: 3000 psi (20,690 kPa)3.1.3 Hydraulic Fluid: MI

24、L-H-5606/MIL-PRF-832823.1.4 Number of Hydraulic Systems: 23.1.5 System Temperature: -65 to 275 F (-54 to 135 C)SAE AIR1899 Revision A- 6 -3.1.6 Main Hydraulic Pump Data:3.1.7 Backup Pump Data:SAE AIR1899 Revision A- 7 -3.1.8 Hydraulic Motor Data:3.1.9 Accumulator Data:3.1.10 Reservoir Data:SAE AIR18

25、99 Revision A- 8 -3.1.11 Relief Valve Data:3.1.12 Filtration:3.1.13 Tubing Data:SAE AIR1899 Revision A- 9 -3.1.14 Fitting Data:3.1.15 Hand Pump Data:3.1.16 Miscellaneous:SAE AIR1899 Revision A- 10 -FIGURE 1 - A-6A Aircraft Hydraulic SystemSAE AIR1899 Revision A- 11 -FIGURE 2 - A-6A Power SystemSAE A

26、IR1899 Revision A- 12 -3.2 Northrop Grumman A-7E:3.2.1 Design Requirements: MIL-H-5440D3.2.2 System Pressure: 3000 psig (20,690 kPa)3.2.3 Hydraulic Fluid: MIL-H-5606/MIL-PRF-832823.2.4 Number of Hydraulic Systems: 33.2.5 System Temperature: -65 to 275 F (-54 to 135 C)3.2.6 Main Hydraulic Pump Data:3

27、.2.7 Backup Pump Data:3.2.8 Hydraulic Motor Data: NoneSAE AIR1899 Revision A- 13 -3.2.9 Accumulator Data:3.2.10 Reservoir Data:3.2.11 Relief Valve Data:SAE AIR1899 Revision A- 14 -3.2.12 Filtration:3.2.13 Tubing Data:3.2.14 Fitting Data:3.2.15 Hand Pump Data:0.7 in3/cycle at 3000 psigSAE AIR1899 Rev

28、ision A- 15 -3.2.16 Miscellaneous:SAE AIR1899 Revision A- 16 -FIGURE 3 - A-7E Aircraft Hydraulic SystemSAE AIR1899 Revision A- 17 -FIGURE 4 - A-7E Power SystemSAE AIR1899 Revision A- 18 -3.3 Fairchild A-10A:3.3.1 Design Requirements: MIL-H-5440F3.3.2 System Pressure: 3000 psi (20,690 kPa)3.3.3 Hydra

29、ulic Fluid: MIL-PRF-832823.3.4 Number of Hydraulic Systems: 23.3.5 System Temperature: -65 to 275 F (-54 to 135 C) Fluid, -65 to 160 F Amb3.3.6 Main Hydraulic Pump Data:3.3.7 Backup Pump Data:SAE AIR1899 Revision A- 19 -3.3.8 Hydraulic Motor Data:3.3.9 Accumulator Data:3.3.10 Reservoir Data:SAE AIR1

30、899 Revision A- 20 -3.3.11 Relief Valve Data:3.3.12 Filtration:3.3.13 Tubing Data:3.3.14 Fitting Data:3.3.15 Hand Pump Data:NoneSAE AIR1899 Revision A- 21 -3.3.16 Miscellaneous:SAE AIR1899 Revision A- 22 -FIGURE 5 - A-10A Aircraft Hydraulic SystemSAE AIR1899 Revision A- 23 -FIGURE 6 - A-10A Power Sy

31、stemSAE AIR1899 Revision A- 24 -3.4 Lockheed F-117A:3.4.1 Design Requirements: MIL-H-5440G3.4.2 System Pressure: 3000 psi (20,690 kPa)3.4.3 Hydraulic Fluid: MIL-PRF-832823.4.4 Number of Hydraulic Systems: 2, Utility and Flight3.4.5 System Temperature: -65 to 275 F (-54 to 135 C) Fluid3.4.6 Main Hydr

32、aulic Pump Data:3.4.7 Backup Pump Data:3.4.8 Hydraulic Motor Data:NoneSAE AIR1899 Revision A- 25 -3.4.9 Accumulator Data:3.4.10 Reservoir Data:3.4.11 Relief Valve Data:SAE AIR1899 Revision A- 26 -3.4.12 Filtration:3.4.13 Tubing Data:3.4.14 Fitting Data:3.4.15 Hand Pump Data:None3.4.16 Miscellaneous:

33、NoneSAE AIR1899 Revision A- 27 -FIGURE 7 - F-117A Aircraft Hydraulic SystemSAE AIR1899 Revision A- 28 -FIGURE 8 - F-117A Power SystemSAE AIR1899 Revision A- 29 -4. FIGHTER AIRPLANES:4.1 Northrop Grumman F-5E:4.1.1 Design Requirements: MIL-H-5440B, also D & F4.1.2 System Pressure: 3000 psi (20,690 kP

34、a)4.1.3 Hydraulic Fluid: MIL-H-5606/MIL-PRF-832824.1.4 Number of Hydraulic Systems: 24.1.5 System Temperature: -65 to 275 F (-54 to 135 C) Fluid, -65 to 160 F Ambient4.1.6 Main Hydraulic Pump Data:4.1.7 Backup Pump Data:None4.1.8 Hydraulic Motor Data:None4.1.9 Accumulator Data:NoneSAE AIR1899 Revision A- 30 -4.1.10 Reservoir Data:4.1.11 Relief Valve Data:4.1.12 Filtration: