BS 2SP 106-1955 Specification for swaged cable-end assemblies (Unified threads) for preformed non-corrodible steel wire rope (W 11) for aircraft《飞行器用预成型不可腐蚀的钢丝绳(W 11)的挤压钢索端部组件(统一螺纹.pdf
《BS 2SP 106-1955 Specification for swaged cable-end assemblies (Unified threads) for preformed non-corrodible steel wire rope (W 11) for aircraft《飞行器用预成型不可腐蚀的钢丝绳(W 11)的挤压钢索端部组件(统一螺纹.pdf》由会员分享,可在线阅读,更多相关《BS 2SP 106-1955 Specification for swaged cable-end assemblies (Unified threads) for preformed non-corrodible steel wire rope (W 11) for aircraft《飞行器用预成型不可腐蚀的钢丝绳(W 11)的挤压钢索端部组件(统一螺纹.pdf(22页珍藏版)》请在麦多课文档分享上搜索。
1、BRITISH STANDARD CONFIRMED APRIL 1998 BS 2 SP 106: 1955 Incorporating Amendment Nos. 1, 2 and 3 Specification for Swaged cable-end assemblies (unified threads)* for preformed non-corrodible steel wire rope (W. 11) for aircraft * Assemblies with fittings incorporating B.A. and B.S.F. threads are spec
2、ified in BS SP 53 and BSSP54. Assemblies suitable for use with British Standard W. 9 steel wire rope are specified in BS SP 105.BS2 SP 106:1955 This British Standard, having been approved by the Aircraft Industry Standards Committee and endorsed by the Chairman ofthe Engineering Divisional Council,
3、was published under theauthority of the General Council of the Institution on 29March 1955 BSI 05-2000 The following BSI references relate to the work on this standard: Committee reference ACE/14 Draft for comment CT (ACE) 6748 ISBN 0 580 34454 1 Foreword This revision of BS SP 106 has been prepared
4、 under the authority of the Aircraft Industry Standards Committee to provide a distinctive coding for assemblies with all-Unified threads to replace the B.A./UNF assemblies, included in the first issue of the standard, following a decision to extend the range of fittings in BS SP 101BS SP 104, “Turn
5、barrels, tension rods and swaged cable-end connections (UNF threads) for aircraft”, to include sizes with No. 8 (0.164)32. UNC and No. 10 (0.190)32. UNF threads. In addition, the requirement in regard to the distance of the swage from the inspection hole (Figure 1) has been modified and a requiremen
6、t for a magnetic flaw detection test (Clause 6) has been included in the standard. 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. Compliance with a British Standard does not of itsel
7、f confer immunity from legal obligations. Summary of pages This document comprises a front cover, an inside front cover, pagesi andii, pages1 to16 and a back cover. This standard has been updated (see copyright date) and may have had amendments incorporated. This will be indicated in the amendment t
8、able on the inside front cover. Amendments issued since publication Amd. No. Date of issue Comments 2472 May 1956 4202 June 1961 4421 January 1962 Indicated by a sideline in the marginBS2 SP 106:1955 BSI 05-2000 i Contents Page Foreword Inside front cover 1 Scope 1 2 Selection of fittings 1 3 Swage
9、form 1 4 Proof loading 1 5 Length of assemblies 2 6 Flaw detection 2 7 Production tests 2 8 Identification 2 9 Marking 3 10 Protective treatment 3 Figure 1 Typical swage form 1 Figure 2 Lengths of assemblies 2 Figure 3 Assembly identification 3 Table 1 Assembly loads 1 Table 2 Sizes of identificatio
10、n tags 3 Table 3 5 cwt cable and swaged end assembly code 4 Table 4 10 cwt cable and swaged end assembly code 6 Table 5 15 cwt cable and swaged end assembly code 8 Table 6 20 cwt cable and swaged end assembly code 10 Table 7 25 cwt cable and swaged end assembly code 12 Table 8 30 cwt cable and swage
11、d end assembly code 14 Table 9 40 cwt cable and swaged end assembly code 16ii blankBS2 SP 106:1955 BSI 05-2000 1 1 Scope This British Standard specifies the fittings, requirements and coding for aircraft swaged cable-end assemblies incorporating Unified threadson preformed non-corrodible steel wire
12、ropecomplying with the requirements of BritishStandard W. 11. Requirements for the locking of the assemblies are not covered by this British Standard. For this information reference should be made to the relevant publications of the appropriate airworthiness authority. The fittings comprising the as
13、semblies, and turnbarrels and tension rods for use with them, are covered by British Standards in the aircraft series, as follows: 2 Selection of fittings The fittings comprising the swaged cable-end assemblies shall be selected in accordance with the relevant tables of this British Standard. 3 Swag
14、e form Dimensional details of individual end fittings are specified in the relevant British Standards, listed in Clause 1. A typical swage form is shown in Figure 1. 4 Proof loading With the exception of assemblies 05790591 (Table 3), which have an ultimate tensile value of448 lb and a proof load of
15、 224 lb, the complete cable assembly shall be proof loaded as indicated in Table 1. Table 1 Assembly loads Fittings British Standard No. Turnbarrels BS SP 101 Screwed ends BS SP 102 Tension rods BS SP 103 Tapped ends BS SP 104 Eye ends BS SP 37 Fork ends BS SP 38 Eye ends for chain BS SP 39 Ball end
16、s with shank BS SP 49 without shank BS SP 50 Identification tags BS SP 51 and BSSP52 Cable Load for measuring length (2per cent ultimate) Proof load ( 1 / 2 ultimate) Minimum ultimate breaking load Capacity BS W. 11 Item No. cwt lb lb lb 5 4 PNC 11 280 560 10 5 PNC 22 560 1 120 15 6 PNC 34 840 1 680
17、 20 3 PNC 45 1 120 2 240 25 51 PNC 56 1 400 2 800 30 52 PNC 67 1 680 3 360 40 53 PNC 90 2 240 4 480 Figure 1 Typical swage formBS2 SP 106:1955 2 BSI 05-2000 5 Length of assemblies The positions to which the cable assemblies shall be measured for length and the tolerance on length are illustrated in
18、Figure 2. Lengths should be quoted to the nearest 1 / 4in. Except for assembled cables under 4 ft in length, which shall be measured without a tension load applied, the assembled cable shall be measured to the satisfaction of the Inspecting Authority with a tension of 1 cwt or two per cent of the ul
19、timate load, whichever is the less, immediately after proof loading (see Clause 4) and before coiling. 6 Flaw detection After proof loading, the assembly shall be examined for flaws to the satisfaction of the Inspecting Authority, by the electro-magnetic method or by any other method agreed by the I
20、nspecting Authority. The presence of any crack shall involve rejection of the fitting. 7 Production tests Production samples of swaged cable-end assemblies or test samples typical thereof shall be periodically submitted to the following tests: a) Sectioning and critical examination of the swaged end
21、s. b) Tensile tests to verify that the swaging does not slip and that the assembly does not fail at a load below that specified on the product or in the specification. The minimum frequency of such tests shall be as follows: i) at the beginning of manufacture on any one machine by any one operator o
22、f each size of cable; ii) during manufacture, one cable of each size in every 500 produced on any one machine by any one operator; iii) one cable of each size manufactured on any one machine by any one operator at not greater intervals than six months. 8 Identification The cable assemblies shall be
23、identified on drawings and for ordering purposes by the number of this British Standard unless it is indicated in the relevant table (Table 3Table 9) that the British Standard number BS SP 54 is to be used, the appropriate code number given in the relevant table and the length of the assembly in inc
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