SAE ARP4205
Current
The latest, up-to-date edition.
Aerospace Fluid Power - Hydraulic Filter Elements - Method for Evaluating Dynamic Efficiency with Cyclic Flow
Hardcopy , PDF
English
29-12-2005
Important note : Users cannot be edited or removed once added to your Multi user PDF.Describes a method for evaluating the performance of filter elements designed for Aerospace hydraulic systems.
| DocumentType |
Standard
|
| Pages |
27
|
| PublisherName |
SAE International
|
| Status |
Current
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This SAE Aerospace Recommended Practice (ARP) describes a method for evaluating the performance of filter elements designed for Aerospace hydraulic systems. The performance is measured and reported in terms of filtration ratios and stabilized contamination level while testing with cyclic flow.
| MIL-DTL-8815-31 Base Document:2009 | FILTER ELEMENTS, NON-CLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 3,000 PSI, 5 MICRON ABSOLUTE, -65 DEGREES F TO 275 DEGREES F |
| BS ISO 14085-3:2015 | Aerospace series. Hydraulic filter elements. Test methods Filtration efficiency and retention capacity |
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| MIL-DTL-8815-32 Base Document:2010 | FILTER ELEMENTS, NON-CLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 3000 PSI, 5 MICRON ABSOLUTE, -65 DEGREES F TO 275 DEGREES F, H-60 AIRCRAFT |
| SAE AIR4543/1A | Aerospace Hydraulics and Actuation Lessons Learned |
| ISO 14085-3:2015 | Aerospace series — Hydraulic filter elements — Test methods — Part 3: Filtration efficiency and retention capacity |
| SAE AIR 1922 : 2017 | AEROSPACE - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE |
| SAE AIR 887 : 2013 | LIQUID FILTER RATINGS, PARAMETERS AND TESTS |
| ISO/TR 15640:2011 | Hydraulic fluid power contamination control General principles and guidelines for selection and application of hydraulic filters |
| 13/30271035 DC : 0 | BS ISO 14085-3 - AEROSPACE SERIES - HYDRAULIC FILTER ELEMENTS - TEST METHODS - PART 3: FILTRATION EFFICIENCY AND RETENTION CAPACITY |
| MIL-DTL-8815-33 Base Document:2011 | FILTER ELEMENTS, NON-CLEANABLE, FLUID PRESSURE, HYDRAULIC LINE, 3500 PSI, 5 MICRON ABSOLUTE, -65 DEGREES F TO 275 DEGREES F, AVIATION GROUND POWER UNIT (AGPU) |
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