BS ISO 18170:2017
Current
The latest, up-to-date edition.
Aerospace series. AC induction electric motor driven, variable delivery, hydraulic pumps. General requirements
Hardcopy , PDF
English
24-05-2017
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Foreword
1 Scope
2 Normative references
3 Terms and definitions
4 General requirements
5 Functional requirements
6 Detailed design requirements
7 Strength requirements
8 Construction
9 Installation requirements
10 Maintenance
11 Reliability
12 Quality assurance provisions
13 Acceptance tests
14 Qualification tests
Bibliography
Describes the general requirements for electric motor driven, variable delivery, hydraulic pumps suitable for use in aircraft hydraulic systems.
| Committee |
ACE/69
|
| DevelopmentNote |
Supersedes 16/30282578 DC. (05/2017)
|
| DocumentType |
Standard
|
| Pages |
64
|
| PublisherName |
British Standards Institution
|
| Status |
Current
|
| Supersedes |
This document establishes the general requirements for electric motor driven, variable delivery, hydraulic pumps suitable for use in aircraft hydraulic systems.
This document includes the general requirements for Alternating Current (AC) induction electric motor powered units. The AC power electrical power supply can be either controlled to provide a Constant Frequency (CF) or uncontrolled to provide a Variable Frequency (VF) AC supply to the electric motor.
This document is intended to be used in conjunction with the detail specification that is particular to each application.
| Standards | Relationship |
| ISO 18170:2017 | 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 1540:2006 | Aerospace — Characteristics of aircraft electrical systems |
| ISO 8625-2:1991 | Aerospace Fluid systems Vocabulary Part 2: General terms and definitions relating to flow |
| ISO 3323:1987 | Aircraft — Hydraulic components — Marking to indicate fluid for which component is approved |
| ISO 6771:2007 | Aerospace — Fluid systems and components — Pressure and temperature classifications |
| ISO 8625-1:1993 | Aerospace Fluid systems Vocabulary Part 1: General terms and definitions related to pressure |
| ISO 11218:2017 | Aerospace Cleanliness classification for hydraulic fluids |
| 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 8278:2016 | Aerospace series Hydraulic, pressure compensated, variable delivery pumps General requirements |
| ISO 2671:1982 | Environmental tests for aircraft equipment — Part 3.4 : Acoustic vibration |
| ISO 8625-3:1991 | Aerospace Fluid systems Vocabulary Part 3: General terms and definitions relating to temperature |
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