SAE AIR 1922 : 2017
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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AEROSPACE - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE
Hardcopy , PDF
26-11-2022
English
13-02-2017
1. SCOPE
2. REFERENCES
3. PUMP INLET LINE
4. PUMP OUTLET LINE
5. PUMP CASE DRAIN LINE
6. MOUNTING PAD ACCESSORY DRIVE
7. FLUID PROPERTIES AND CLEANLINESS
8. NOTES
APPENDIX A - ASSOCIATED TECHNICAL DOCUMENTS
APPENDIX B - EXAMPLE CALCULATION OF REQUIRED RESERVOIR
PRESSURE
APPENDIX C - PUMP DRIVE SPLINE STANDARDS
Provides the following factors that affect hydraulic pump life and performance: a. The need to supply hydraulic fluid at the correct pressure and quality to the pump inlet port, b. Considerations for the pump output, c. Factors to be considered for the pump case drain lines, d. The mounting of the hydraulic pump; and e. Hydraulic fluid properties, including cleanliness.
Committee |
A-6C4
|
DocumentType |
Standard
|
Pages |
42
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
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SAE ARP4752B | Aerospace - Design and Installation of Commercial Transport Aircraft Hydraulic Systems |
SAE ARP6025 | Duty Cycle Considerations for Electrohydrostatic Actuators |
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SAE AIR 5829 : 2008 | AIR IN AIRCRAFT HYDRAULIC SYSTEMS |
SAE AS5586 | Aerospace - General Requirements for Hydraulic System Reservoirs |
SAE ARP4925B | Aerospace Design and Installation of Commercial Transport Helicopter Hydraulic Systems |
SAE ARP 4943 : 2008 | GROUND SUPPORT EQUIPMENT HYDRAULIC SYSTEMS, DESIGN AND INSTALLATION, RECOMMENDED PRACTICES FOR |
SAE ARP5376B | Methods, Locations And Criteria For System Sampling And Measuring The Solid Particle Contamination Of Hydraulic Fluids |
MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
SAE ARP4752B | Aerospace - Design and Installation of Commercial Transport Aircraft Hydraulic Systems |
SAE AS5440A | Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For |
SAE AIR1362C | Aerospace Hydraulic Fluids Physical Properties |
SAE AIR 5829 : 2008 | AIR IN AIRCRAFT HYDRAULIC SYSTEMS |
SAE AIR5277A | Aerospace Fluid Power - Waste Reduction Practices for Used Phosphate Ester Aviation Hydraulic Fluid |
SAE AIR4543C | Aerospace Hydraulics and Actuation Lessons Learned |
MIL-PRF-87257 Revision C:2017 | HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE |
SAE AS19692B | Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump |
SAE AS1241D | Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft |
SAE ARP4205 | Aerospace Fluid Power - Hydraulic Filter Elements - Method for Evaluating Dynamic Efficiency with Cyclic Flow |
MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
MIL F 8815 : D | FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR |
SAE AS 4059F : 2013 | AEROSPACE FLUID POWER - CONTAMINATION CLASSIFICATION FOR HYDRAULIC FLUIDS |
SAE AS595D | Aerospace – Civil Type Variable Delivery, Pressure Compensated, Hydraulic Pump |
ISO 16889:2008 | Hydraulic fluid power Filters Multi-pass method for evaluating filtration performance of a filter element |
SAE AIR810D | Degradation Limits of Hydrocarbon-Based Hydraulic Fluids, MIL-PRF-5606, MIL-PRF-83282, and MIL-PRF-87257 Used in Hydraulic Test Stands |
SAE ARP4925B | Aerospace Design and Installation of Commercial Transport Helicopter Hydraulic Systems |
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