BS SP 115 to 117-1956 Specifications for hydraulic surface-check type lubricating nipples for aircraft《航空用液压表面止动型润滑脂嘴规范》.pdf
《BS SP 115 to 117-1956 Specifications for hydraulic surface-check type lubricating nipples for aircraft《航空用液压表面止动型润滑脂嘴规范》.pdf》由会员分享,可在线阅读,更多相关《BS SP 115 to 117-1956 Specifications for hydraulic surface-check type lubricating nipples for aircraft《航空用液压表面止动型润滑脂嘴规范》.pdf(12页珍藏版)》请在麦多课文档分享上搜索。
1、BRITISH STANDARD CONFIRMED APRIL 1998 BS SP 115 to 117:1956 Incorporating Amendment Nos. 1, 2, 3 and 4 Specifications for Hydraulic surface-check type lubricating nipples for aircraft UDC 621-729.7 : 629.13BSSP 115 to 117:1956 These British Standards, havingbeen approved by the AircraftIndustry Stan
2、dards Committee and endorsed by theChairman ofthe EngineeringDivisional Council, were published under theauthority of the General Council of the Institution on 29March 1956 BSI 04-2000 Committee Reference ACE/14 Draft for comment CV(ACE) 5063 ISBN 0 580 34447 9 A British Standard does not purport to
3、 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 itself confer immunity from legal obligations. Summary of pages This document comprises a front cover, an inside front cover,
4、pagesi andii, pages1 to7 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 table on the inside front cover. Amendments issued since publication Amd. No. Date of issue Comments 3506 September 1959 52
5、51 May 1964 6390 April 1968 607 September 1970 Indicated by a sideline in the marginBSSP 115 to 117:1956 BSI 04-2000 i Contents Page 1 Scope 1 Section 1. General requirements 2 Construction and performance 1 3 Materials 1 4 Dimensions 1 5 Screw threads 1 6 Anti-corrosion treatment 1 7 Freedom from d
6、efects 1 8 Identification and marking 1 Section 2 9 Inspection and testing 2 10 Batch 2 11 Sampling before components are assembled 2 12 Component dimensions and finish 2 13 Heat treatments and tests on components 2 14 Sampling of complete nipples 3 15 Assembly of components 3 16 Tests 3 Figure 1 En
7、velope dimensions of nipple head 4 Figure 2 1 / 4in. UNF straight nipple 4 Figure 3 1 / 4in. UNF 45 angle nipple 5 Figure 4 1 / 4in. UNF 90 angle nipple 5 Figure 5 Minimum clearance around hydraulic nipple 6 Figure 6 Test block 7 Table 1 British Standard numbers 2 ii blankBSSP 115 to 117:1956 BSI 04
8、-2000 1 1 Scope These British Standards specify the requirements for hydraulic, surface-check type, lubricating nipples having body attachment screw threads 1 / 4in. 28, Unified Fine (UNF), Class 2A limits. Three types of nipple are specified: a) straight and in one piece, with attachment screw thre
9、ads on one end of the body and the nipple on the other (Figure 2); b) a body with attachment screw threads on one end and a nipple set in the other end at 45 to the axis of the attachment screw threads (Figure 3); c) a body with attachment screw threads at one end and a nipple set in the other end a
10、t 90 to the axis of the attachment screw threads (Figure 4). Section 1. General requirements 2 Construction and performance a) The nipples shall incorporate a check valve, located at the surface of the nipple inlet tip, which with its seat shall provide a seal against the ingress of dirt or other fo
11、reign matter, but shall admit lubricant and prevent its escape, as required byd) tof) below. b) Springs shall be of non-collapsing design and of such quality of wire as to withstand the tests specified in this British Standard. c) The external surface of the nipple to be in contact, after installati
12、on, with a gun nozzle or coupler, shall be hardened to a case depth of 0.003 in. 0.005 in. Other parts required by the manufacturers approved drawings to be hardened shall be hardened as specified on the drawings. d) The nipples shall satisfactorily admit lubricant at1 000 lb/sq. in. without appreci
13、able leakage when a hydraulic-type coupler of approved design is connected and inclined to an angle of not less than10 in any radial direction between the axis of the coupler and the axis of inlet tip of the nipple. e) The opening pressure of the check valve shall be between 140 lb/sq. in. and 500 l
14、b/sq. in. f) The nipple shall retain lubricant at a sustained pressure of 5 000 lb/sq. in. without a total leakage in excess of 2 cu.cm in one minute. 3 Materials The nipples shall be made from steel complying with approved specifications see Clause 9 a). The manufacturers drawings and/or the specif
15、ications shall specify the materials and heat treatments and tests required on them. 4 Dimensions The nipples shall conform to the envelope dimensions shown in Figure 1, Figure 2, Figure 3, and Figure 4, and to those shown in the approved drawings (see Section 2, Clause 10), which shall be provided
16、with adequate dimensions and limits. The minimum clearance required around the nipples when they are installed in position is shown in Figure 5. 5 Screw threads a) The nipples shall each embody an attachment screw thread of a form to permit the nipple to be screwed tightly into a boss tapped with a
17、1 / 4in. 28 UNF 2B screw thread complying with the latest issue of BS 1580, “Unified screw threads”. b) Details of attachment screw threads shall be shown on approved manufacturing drawings and shall comprise 1 / 4in. 28 UNF 2A screw thread, complying with the latest issue of BS 1580, having2 1 / 2t
18、hreads run-out (root taper). c) Any other screw threads used in the internal construction of the nipples shall be in accordance with the approved drawing. d) The screw threads, before and after plating, shall be required to pass gauges approved by the Inspecting Authority. 6 Anti-corrosion treatment
19、 The body, and nipples before assembly, shall be uniformly coated with cadmium, in accordance with the latest issue of Ministry of Supply aircraft process specification D.T.D.904. The protective treatment for other parts shall be in accordance with the approved drawings. 7 Freedom from defects a) Th
20、e nipples shall be free from harmful defects. b) The nipples may be rejected at any time for faults in, or revealed by, manufacture, although they have been made from material passed previously for chemical composition and mechanical properties. 8 Identification and marking a) The nipples shall be i
21、dentified as “Unified” by a pattern of contiguous circles, e.g. OOO, of 3 / 32in. diameter indented on one or more flats of the hexagon and parallel to the axis of the nipple. b) The nipples shall be identified for ordering purposes by the relevant British Standard number shown in Table 1. The speci
22、fication number shall not be marked on the part.BSSP 115 to 117:1956 2 BSI 04-2000 c) The nipples shall be made into parcels which shall have the appropriate British Standard number and the Unified symbol of contiguous circles clearly marked on the labels. Table 1 British Standard Numbers Section 2
23、9 Inspection and testing a) For inspection purposes the manufacturers Inspecting Authority shall be provided with approved manufacturing drawings 1)and manufacturers approved specifications 1) , if any. Any changes in the drawings and specifications shall similarly be notified on approved drawings a
24、nd specifications and the Inspecting Authority shall have the right to carry out a complete series of tests before accepting any nipples to the new drawings and/or specifications. b) The nipples shall comply with the inspection and testing requirements specified in this section. The inspections and
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
5000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- BSSP115TO1171956SPECIFICATIONSFORHYDRAULICSURFACECHECKTYPELUBRICATINGNIPPLESFORAIRCRAFT 航空 液压 表面 止动型

链接地址:http://www.mydoc123.com/p-399129.html