BS ISO 12334:2000
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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. Hydraulic, pressure-compensated, variable delivery pumps. General requirements for 35000 kPa systems
Hardcopy , PDF
31-03-2016
English
15-04-2000
Foreword
1 Scope
2 Normative references
3 Functional requirements
3.1 Hydraulic fluid
3.2 Rated discharge pressure
3.3 Maximum full-flow pressure
3.4 Inlet pressure
3.4.1 Rated inlet pressure
3.4.2 Cavitation pressure
3.4.3 Minimum inlet pressure
3.5 Case drain pressure
3.5.1 Rated case-drain pressure
3.5.2 Case proof-pressure
3.6 Case drain flow
3.7 Rated temperature
3.8 Maximum displacement
3.9 Rated delivery
3.10 Rated speed
3.11 Endurance
3.12 Torque
3.13 Efficiency
3.14 Discharge pressure pulsations
3.15 Variable delivery control
3.15.1 General
3.15.2 Response time
3.15.3 Stability
3.16 Maximum transient pressure
3.17 Depressurization
3.18 Balance
3.19 Adjustment
3.20 Safety wire sealing
3.21 Directionally critical components
3.22 Environmental requirements
3.23 Installation requirements
3.23.1 Dimensions
3.23.2 Mass
3.23.3 Mounting
3.23.4 Drive coupling
3.23.5 Ports
3.24 Detail requirements
3.24.1 Material
3.24.2 Metals
3.24.3 Corrosion protection
3.24.4 Castings
3.24.5 Seals
3.24.6 Identification marking
3.24.7 Design and construction
3.25 Maintainability
3.25.1 Maintenance concept
3.25.2 Useful life and storage conditions
3.26 Reliability
3.26.1 Equipment compliance
3.26.2 Requirements
4 Quality assurance provisions
4.1 Responsibility for inspection
4.2 Classification of tests
5 Qualification tests
5.1 General
5.2 Qualification procedure
5.2.1 Detail specification
5.2.2 Qualification by analogy
5.2.3 Pump qualification test report
5.3 Samples and programme of qualification tests
5.4 General conditions for qualification tests
5.5 Acceptance tests
5.6 Dimensional check
5.7 Proof-pressure and overspeed test
5.8 Calibration
5.8.1 Pump inlet pressurized
5.8.2 Flow rate and driving torque values
5.8.3 Minimum operating speed
5.9 Maximum pressure, response time and pressure
pulsation tests
5.9.1 General
5.9.2 System impedance
5.9.3 Maximum pressure test
5.9.4 Determination of response time
5.9.5 Pressure pulsation test
5.10 Heat rejection test
5.10.1 Principle
5.10.2 Determination of heat rejection
5.11 Vibration tests
5.11.1 Mounting of the test pump
5.11.2 Pump operating during vibration tests
5.11.3 Resonant frequency vibration test
5.11.4 Cyclic frequency vibration test
5.11.5 Other vibration tests
5.12 Low temperature test
5.13 Endurance testing
5.13.1 Test programme
5.13.2 Filtration for normal endurance tests
5.13.3 Filter check
5.13.4 Calibration
5.13.5 Start-stop cycles
5.13.6 Pump case pressure cycles
5.13.7 Air ingestion
5.13.8 Thermal cycles
5.13.9 Thermal shock
5.13.10 Hydraulic fluid
5.13.11 Failure of parts
5.14 Cavitation test
5.15 Drive Coupling shear test
5.16 Teardown inspection
6 Acceptance tests
6.1 General
6.2 Examination of the product
6.3 Test programme
6.3.1 Break-in run
6.3.2 Proof-pressure and overspeed tests
6.3.3 Teardown inspection examination
6.3.4 Break-in run
6.3.5 Functional tests
6.3.6 External leakage test
6.3.7 Pressure control test
6.3.8 Calibration
6.3.9 Filter patch test
7 Storage and packaging
Defines general requirements for pressure-compensated, variable delivery hydraulic pumps, to be used in aircraft hydraulic systems at 35,000 kPa. To be used in conjunction with detail specifications relative to each pump model.
Committee |
ACE/69
|
DevelopmentNote |
Supersedes 96/703809 DC. (07/2005) Reviewed and confirmed by BSI, December 2013. (11/2013)
|
DocumentType |
Standard
|
Pages |
38
|
PublisherName |
British Standards Institution
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
Standards | Relationship |
ISO 12334:2000 | Identical |
ISO 7320:1992 | Aerospace Couplings, threaded and sealed, for fluid systems Dimensions |
ISO 8078:1984 | Aerospace process Anodic treatment of aluminium alloys Sulfuric acid process, undyed coating |
ISO 2685:1998 | Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones |
ISO 8399-2:1998 | Aerospace — Accessory drives and mounting flanges (Metric series) — Part 2: Dimensions |
ISO 6771:2007 | Aerospace — Fluid systems and components — Pressure and temperature classifications |
ISO 8399-1:1998 | Aerospace — Accessory drives and mounting flanges (Metric series) — Part 1: Design criteria |
ISO 8079:1984 | Aerospace process Anodic treatment of aluminium alloys Sulfuric acid process, dyed coating |
ISO 2093:1986 | Electroplated coatings of tin — Specification and test methods |
ISO 7137:1995 | Aircraft — Environmental conditions and test procedures for airborne equipment |
ISO 3601-1:2012 | Fluid power systems — O-rings — Part 1: Inside diameters, cross-sections, tolerances and designation codes |
ISO 2669:1995 | Environmental tests for aircraft equipment — Steady-state acceleration |
ISO 8081:1985 | Aerospace process Chemical conversion coating for aluminium alloys General purpose |
ISO 2671:1982 | Environmental tests for aircraft equipment — Part 3.4 : Acoustic vibration |
ISO 8077:1984 | Aerospace process Anodic treatment of aluminium alloys Chromic acid process 20 V DC, undyed coating |
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