1、BRITISH STANDARD AEROSPACE SERIES BS W 14:1999 ISO 9763:1999 Aircraft control wire rope assemblies Technical specification ICS 49.035BSW14:1999 This British Standard, having been prepared under the directionof the Engineering SectorCommittee, was publishedunder the authority ofthe Standards Committe
2、e andcomes into effect on 15October1999 BSI 04-2000 ISBN 0 580 35018 5 National foreword This British Standard reproduces verbatim ISO9763:1999and implements it as the UK national standard. The UK participation in its preparation was entrusted to Technical Committee ACE/14, Aerospace details and par
3、ts, which has the responsibility to: aid enquirers to understand the text; present to the responsible international/European committee any enquiries on the interpretation, or proposals for change, and keep the UK interests informed; monitor related international and European developments and promulg
4、ate them in the UK. A list of organizations represented on this committee can be obtained on request to its secretary. Cross-references The British Standards which implement international or European publications referred to in this document may be found in the BSI Standards Catalogue under the sect
5、ion entitled “International Standards Correspondence Index”, or by using the “Find” facility of the BSI Standards Electronic Catalogue. A British Standard does not purport to include all the necessary provisions of a contract. Users of British Standards are responsible for their correct application.
6、 Compliance with a British Standard does not of itself confer immunity from legal obligations. Summary of pages This document comprises a front cover, an inside front cover, pages i and ii, theISO title page, pages ii to iv, pages 1 to 7 and a back cover. This standard has been updated (see copyrigh
7、t date) and may have had amendments incorporated. This will be indicated in the amendment table on the inside front cover. Amendments issued since publication Amd. No. Date CommentsBSW14:1999 BSI 04-2000 i Contents Page National foreword Inside front cover Foreword iii Text of ISO 9763 1ii blankBSW1
8、4:1999 ii BSI 04-2000 Contents Page Foreword iii 1 Scope 1 2 Normative references 1 3 Terms and definitions 1 4 Requirements 2 5 Quality assurance 5 6 Marking 6 7 Packing 7 8 Certificate of conformity 7 Figure 1 Swaging of end fittings ISO 9737, ISO 9749, ISO 9759 and ISO 9760 4 Figure 2 Swaging of
9、ISO 9747 end fitting 4 Figure 3 Swaging of ISO 9748 end fitting 4 Figure 4 Cross-section of the swaged part of the end fitting 5 Table 1 Technical requirements and inspections and test methods 2 Table 2 Dimensions of the swaged part 3 Table 3 Inspections and tests for the qualification of control wi
10、re rope assemblies 6 Table 4 Acceptance inspections and tests for control wire rope assemblies 7 Table 5 7BSW14:1999 BSI 04-2000 iii Foreword ISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISO member bodies). The work of preparing Int
11、ernational Standards is normally carried out through ISO technical committees. Each member body interested in a subject for which a technical committee has been established has the right to be represented on that committee. International organizations, governmental and non-governmental, in liaison w
12、ith ISO, also take part in the work. ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of electrotechnical standardization. International Standards are drafted in accordance with the rules given in the ISO/IEC Directives, Part 3. Draft International Sta
13、ndards adopted by the technical committees are circulated to the member bodies for voting. Publication as an International Standard requires approval by at least75% of the member bodies casting a vote. International Standard ISO9763was prepared by Technical Committee ISO/TC 20, Aircraft and space ve
14、hicles, Subcommittee SC 12, Mechanical system parts.iv blankBSW14:1999 BSI 04-2000 1 1 Scope This International Standard specifies the characteristics, inspections and test methods as well as the quality assurance requirements for aircraft control wire rope assemblies equipped with swaged end fittin
15、gs. This International Standard is applicable to control wire rope assemblies as defined in ISO 9762. 2 Normative references The following normative documents contain provisions which, through reference in this text, constitute provisions of this International Standard. For dated references, subsequ
16、ent amendments to, or revisions of, any of these publications do not apply. However, parties to agreements based on this International Standard are encouraged to investigate the possibility of applying the most recent editions of the normative documents indicated below. For undated references, the l
17、atest edition of the normative document referred to applies. Members of ISO and IEC maintain registers of currently valid International Standards. ISO 2020-1, Aerospace Preformed flexible steel wire rope for aircraft controls Part 1: Dimensions and loads. ISO 9001:1994, Quality systems Model for qua
18、lity assurance in design, development, production, installation and servicing. ISO 9002:1994, Quality systems Model for quality assurance in production, installation and servicing. ISO 9003:1994, Quality systems Model for quality assurance in final inspection and test. ISO 9737:, Aerospace Eye-ends,
19、 in corrosion-resistant steel, swaged on aircraft control wire rope Dimensions and loads 1) . ISO 9747:, Aerospace Double-shank ball-ends, in corrosion-resistant steel, swaged on aircraft control wire rope Dimensions and loads 1) . ISO 9748:, Aerospace Ball-ends, in corrosion-resistant steel, swaged
20、 on aircraft control wire rope Dimensions and loads 1) . ISO 9749:, Aerospace Stud-ends, in corrosion-resistant steel, swaged on aircraft control wire rope Dimensions and loads 1) . ISO 9759:, Aerospace Fork ends, in corrosion-resistant steel, swaged on aircraft control wire rope Dimensions and load
21、s 1) . ISO 9760:, Aerospace Fork ends, in corrosion-resistant steel, swaged on aircraft control wire rope for rolling bearings, Dimensions and loads 1) . ISO 9762:, Aerospace Aircraft control wire rope assemblies Combinations and dimensions 1) . 3 Terms and definitions For the purposes of this Inter
22、national Standard, the following terms and definitions apply. 3.1 manufacturing batch quantity of control wire rope assemblies making up the same manufacturing series and of the same composition: with wire ropes from the same spool (identical material and diameter); with the same definitions for the
23、 extremities 3.2 test piece control wire rope assembly taken at random from a given batch 1) To be published.BSW14:1999 2 BSI 04-2000 4 Requirements 4.1 General The requirements specified by this International Standard are given in Table 1 and, apart from where otherwise specified, they also apply t
24、o control wire rope assemblies ready for use. The test temperature shall be, apart from where otherwise specified, ambient temperature. These requirements are to be taken into account along with the conditions which figure in all the other standards or specifications cited in the product or the defi
25、nition documents for control wire rope assemblies. Table 1 Technical requirements and inspections and test methods No. Characteristics Technical requirements Inspections and test methods Q a A b 4.2 Composition of the control wire rope assembly In conformity with the code designation specified in IS
26、O9762. Visual examination. 4.3 External aspect No cracks, distortion or burrs shall be allowed. Visual examination. A slight round-edged punch mark shall be allowed on the end fitting. This stamp shall be applied before swaging for the purpose of holding the wire rope in the fitting. 4.4 Dimensions
27、of the swaged part In accordance with Table 2 and Figure 1, Figure 2 and Figure 3. Usual measuring instruments. 4.5 Length “L 1 ” of the wire rope inserted into the end fitting In accordance with Figure 1 Inspection: After swaging, no trace of the naked wire rope shall appear between the identificat
28、ion mark and the end fitting. by x-ray examination; or by applying a reference mark tothe wire rope before swaging. The choice of the mark (paint, self-adhesive band or other) is left to the manufacturer. 4.6 Internal faults on the swaged part In accordance with Figure 4. On the cross section for th
29、e swaged part, carry out: After swaging: a visual examination; no cracks or folds visible to the naked eye; a micrographic examination at a magnifying power of at least 100. no cracks deeper than 150 4m; no more than six cracks having a depth between 40 4m and 150 4m. 4.7 Length of the control wire
30、rope assembly In accordance with ISO 9762. Unless specified otherwise, the measurement shall be taken with the wire rope held flat along its whole length under a 50 N load. BSW14:1999 BSI 04-2000 3 Table 1 Technical requirements and inspections and test methods Table 2 Dimensions of the swaged part
31、No. Characteristics Technical requirements Inspections and test methods Q a A b 4.8 Performance under a load equal to60% of the minimum breaking load of the wire rope Subjected to a load equal at least to 60% of the minimum breaking load of the wire rope concerned given in ISO 2020-1, the wire rope
32、shall not slip in the end fitting and no wire shall be found to be broken upon visual or tactile inspection. The test shall be carried out with the wire rope in a straight line. Apply the load continuously and progressively (within a minimum of 3 s). Maintain it for 5 s. Then bring it gradually back
33、 to zero. Any sudden variation in the load recorded during the test shall be considered the sign of possible slippage of the wire rope in the end fittings and shall call for a very thorough inspection of the wire rope assembly and of its length. After this test, the control wire rope assembly shall
34、be carefully examined. 4.9 Performance under the minimum breaking load of the wire rope No slippage of the wire rope in the end fittings shall be allowed under the minimum breaking load of the wire rope concerned given in ISO 2020-1. Any eventual fracture shall only occur under a load equal or super
35、ior to the minimum breaking load and then never in or at the limit of the end fitting. The load shall be applied continuously and progressively until a load equal to 80% of the minimum breaking load is obtained. The remaining load shall be applied at a rate of about 10 N/s. A visual check shall be c
36、arried out to see whether the wire rope has slipped. a Q = conditions for executing qualification inspections and tests (in accordance with 5.2) b A = conditions for executing acceptance inspections and tests (in accordance with 5.3) Dimensions in millimetres Nominal diameter of wire rope a D 1 b D
37、2 c D 3 L 1 L 2 L 3 L 4 0,12 0 0,12 min. max. max. 1,6 3,5 2,84 0 0,12 4,83 18 4,5 10 4 2,4 4,83 3,63 6,43 21 5 15,5 6 3,2 5,56 4,83 8 27 6,4 20 8 4 6,35 5,64 9,63 33 8 26 10 4,8 7,95 6,48 11,23 34 7,3 30 12 5,6 9,52 7,67 0 0,17 12,83 39 8,4 35 14 6,4 11,12 8,84 14,4 43 41 16 a In accordance with IS
38、O 2020-1. b Executable along the whole length L 1(see Figure 1). c Executable along the whole length L 4(see Figure 3).BSW14:1999 4 BSI 04-2000 Figure 1 Swaging of end fittings ISO 9737, ISO 9749, ISO 9759 and ISO 9760 Figure 2 Swaging of ISO 9747 end fitting Figure 3 Swaging of ISO 9748 end fitting
39、BSW14:1999 BSI 04-2000 5 5 Quality assurance 5.1 General 5.1.1 Approval of the manufacturer The manufacturer shall satisfy the quality assurance and approval procedures as defined by ISO 9001, ISO9002 or ISO 9003. The aim of these procedures is to ensure that the manufacturer has a quality system an
40、d is capable of manufacturing, on a regular basis, control wire rope assemblies which fulfil the specified quality conditions. The manufacturer shall be approved by the certification authorities or their delegated representative, who may be the first supervisor. 5.1.2 Qualification of control wire r
41、ope assemblies The purpose of qualification inspections and tests of control wire rope assemblies is to verify that the conception and the manufacturing conditions of a control wire rope assembly and shall be such that the conditions of this International Standard are satisfied. The qualification of
42、 control wire rope assemblies shall be granted by the certification authorities in the buyers country, or their delegated representative, who may be the first supervisor. 5.1.3 Acceptance of control wire rope assemblies The purpose of acceptance inspections and tests for control wire rope assemblies
43、 is to verify as simply and cheaply as possible and with the inherent uncertainty of a statistical test, that the conditions of this International Standard can be satisfied. Acceptance tests shall be carried out by the manufacturer, or under his responsibility. The manufacturer shall be responsible
44、for the quality of the manufactured products. 5.2 Conditions for the execution of qualification tests The qualification tests are given in Table 1. They shall be carried out for each nominal diameter of the control wire rope assembly to the following combinations: a) an ISO 9737 or ISO 9749 or ISO 9
45、759 or ISO 9760 end fitting at the two extremities, b) an ISO 9737 or ISO 9749 or ISO 9759 or ISO 9760 end fitting at one extremity and an ISO 9747 or ISO 9748 end fitting at the other. For a control wire rope assembly, of a given nominal diameter, perform the checks and inspections given in Table 3
46、 on six control wire rope assemblies (two in each of the above combinations). Figure 4 Cross-section of the swaged part of the end fittingBSW14:1999 6 BSI 04-2000 Table 3 Inspections and tests for the qualification of control wire rope assemblies The test specimen shall consist of a 500 mm length wi
47、re rope, with the same characteristics as the naked wire rope used on the control wire rope assembly and from the same spool; end fittings identical to those used on the control cable assembly, swaged on the wire rope sample under the same swaging conditions as for the control wire rope assemblies f
48、rom the batch. These swagings shall be carried out during the manufacture of the batch in question and under the same execution conditions as this batch. If a control wire rope assembly is made up of two end fittings and an intermediary fitting (ISO 9747), each sample shall made up of two specimens
49、on which the following are swaged at the ends: one of the end fittings; an intermediary fitting (ISO 9747). 5.3 Conditions for the execution of acceptance inspections and tests The acceptance inspections and tests are given in Table 1. They shall be carried out on each identity batch in accordance with Table 4. 6 Marking In addition to the manufacturers own marking, each control wire rope assembly shall be marked using th
