AEROSPACE FLUID POWER - HYDRAULIC FILTER ELEMENTS - METHOD FOR EVALUATING DYNAMIC EFFICIENCY WITH CYCLIC FLOW

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

29-12-2005

Publisher

SAE International

Describes a method for evaluating the performance of filter elements designed for Aerospace hydraulic systems.

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
PD ISO/TR 15640:2011	Hydraulic fluid power contamination control. General principles and guidelines for selection and application of hydraulic filters
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 AIR 4543/1A : 2017	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)