BS M 65:1987
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Specification for pressure compensated variable delivery hydraulic pumps
Hardcopy , PDF
31-03-2016
English
30-06-1987
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National foreword
Committees responsible
Specification
1 Scope
2 References
3 Functional requirements
4 Quality assurance provisions
5 Qualification tests
6 Acceptance tests
7 Storage and packing
Annex
Schematic summary of the contents of this
International Standard
Tables
1 Temperature relationship
2 Duration of endurance test
3 Relation between displacement and flange type
4 Format for nameplate
5 Endurance testing - Normal test
6 Endurance testing - Overload test
Figures
1 Delivery/pressure characteristic curve of pumps
2 Nomograph of maximum recommended values for rated
speeds against pump displacement
3 Typical variation of pressure against time -
Transient from maximum full-flow pressure to rated
discharge pressure (zero flow)
4 Typical variation of pressure against time -
Transient from rated discharge pressure to maximum
full-flow pressure (full flow)
Pumps for use in aircraft hydraulic systems. Quality assurance provisions and acceptance tests are included.
| Committee |
ACE/69
|
| DevelopmentNote |
Supersedes 85/70937 DC (08/2005) Reviewed and confirmed by BSI, November 2010. (11/2010)
|
| DocumentType |
Standard
|
| Pages |
28
|
| PublisherName |
British Standards Institution
|
| Status |
Superseded
|
| SupersededBy |
| ISO 8078:1984 | Aerospace process Anodic treatment of aluminium alloys Sulfuric acid process, undyed coating |
| BS 3G 100-2.3.6:1972 | Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Acceleration requirements |
| BS M 51:1982 | Classification for pressure and temperature for fluid systems and components |
| ISO 8399-2:1998 | Aerospace — Accessory drives and mounting flanges (Metric series) — Part 2: Dimensions |
| BS 3G 100-2.3.13:1973 | Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Resistance to fire in designated fire zones |
| BS M 63:1987 | Specification for dimensions for fluid system port connection, seal and fitting end |
| BS 3G 100-2.3.4:1972 | Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Differential pressure requirements |
| ISO 8399-1:1998 | Aerospace — Accessory drives and mounting flanges (Metric series) — Part 1: Design criteria |
| BS 3G 100-2.3.9:1972 | Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Ice formation |
| ISO 8079:1984 | Aerospace process Anodic treatment of aluminium alloys Sulfuric acid process, dyed coating |
| ISO 3601-1:2012 | Fluid power systems — O-rings — Part 1: Inside diameters, cross-sections, tolerances and designation codes |
| ISO 8081:1985 | Aerospace process Chemical conversion coating for aluminium alloys General purpose |
| ISO 8077:1984 | Aerospace process Anodic treatment of aluminium alloys Chromic acid process 20 V DC, undyed coating |
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