《ISO-5856-2008.pdf》由会员分享，可在线阅读，更多相关《ISO-5856-2008.pdf（10页珍藏版）》请在三一文库上搜索。
1、 Reference number ISO 5856:2008(E) ISO 2008 INTERNATIONAL STANDARD ISO 5856 Second edition 2008-08-15 Aerospace Screws, 100 degrees normal countersunk head, internal offset cruciform ribbed or unribbed drive, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, str
2、ength classes less than or equal to 1 100 MPa Dimensions Aronautique et espace Vis tte fraise 100 degrs normale, empreinte cruciforme dporte, avec ou sans saillies antidrapantes, avec tige normale et filetages MJ courts ou de longueur moyenne, en matriau mtallique, revtues ou non revtues, de classes
3、 de rsistance infrieures ou gales 1 100 MPa Dimensions Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=Boeing Co/5910770001 Not for Resale, 10/25/2008 05:36:50 MDTNo reproduction or networking permitted without license from IHS -,-,- ISO 5856:
4、2008(E) PDF disclaimer This PDF file may contain embedded typefaces. In accordance with Adobes licensing policy, this file may be printed or viewed but shall not be edited unless the typefaces which are embedded are licensed to and installed on the computer performing the editing. In downloading thi
5、s file, parties accept therein the responsibility of not infringing Adobes licensing policy. The ISO Central Secretariat accepts no liability in this area. Adobe is a trademark of Adobe Systems Incorporated. Details of the software products used to create this PDF file can be found in the General In
6、fo relative to the file; the PDF-creation parameters were optimized for printing. Every care has been taken to ensure that the file is suitable for use by ISO member bodies. In the unlikely event that a problem relating to it is found, please inform the Central Secretariat at the address given below
7、. COPYRIGHT PROTECTED DOCUMENT ISO 2008 All rights reserved. Unless otherwise specified, no part of this publication may be reproduced or utilized in any form or by any means, electronic or mechanical, including photocopying and microfilm, without permission in writing from either ISO at the address
8、 below or ISOs member body in the country of the requester. ISO copyright office Case postale 56 CH-1211 Geneva 20 Tel. + 41 22 749 01 11 Fax + 41 22 749 09 47 E-mail copyrightiso.org Web www.iso.org Published in Switzerland ii ISO 2008 All rights reserved Copyright International Organization for St
9、andardization Provided by IHS under license with ISO Licensee=Boeing Co/5910770001 Not for Resale, 10/25/2008 05:36:50 MDTNo reproduction or networking permitted without license from IHS -,-,- ISO 5856:2008(E) ISO 2008 All rights reserved iii Foreword ISO (the International Organization for Standard
10、ization) is a worldwide federation of national standards bodies (ISO member bodies). The work of preparing International 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
11、be represented on that committee. International organizations, governmental and non-governmental, in liaison with ISO, also take part in the work. ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of electrotechnical standardization. International Stand
12、ards are drafted in accordance with the rules given in the ISO/IEC Directives, Part 2. The main task of technical committees is to prepare International Standards. Draft International Standards adopted by the technical committees are circulated to the member bodies for voting. Publication as an Inte
13、rnational Standard requires approval by at least 75 % of the member bodies casting a vote. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. ISO shall not be held responsible for identifying any or all such patent rights. ISO 5856 w
14、as prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 4, Aerospace fastener systems. This second edition cancels and replaces the first edition (ISO 5856:1991), which has been technically revised. Copyright International Organization for Standardization Provided
15、by IHS under license with ISO Licensee=Boeing Co/5910770001 Not for Resale, 10/25/2008 05:36:50 MDTNo reproduction or networking permitted without license from IHS -,-,- Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=Boeing Co/5910770001 Not
16、for Resale, 10/25/2008 05:36:50 MDTNo reproduction or networking permitted without license from IHS -,-,- INTERNATIONAL STANDARD ISO 5856:2008(E) ISO 2008 All rights reserved 1 Aerospace Screws, 100 degrees normal countersunk head, internal offset cruciform ribbed or unribbed drive, normal shank, sh
17、ort or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1 100 MPa Dimensions 1 Scope This International Standard specifies the dimensions of 100 normal countersunk head screws with internal offset cruciform ribbed or unribbed drive, with close o
18、r large tolerance normal shank and short or medium length MJ threads, in metallic material, coated or uncoated, with strength classes less than or equal to 1 100 MPa. This International Standard is applicable to the compilation of aerospace product standards. 2 Normative references The following ref
19、erenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. ISO 286-2, ISO system of limits and fits Part 2: Tables of standar
20、d tolerance grades and limit deviations for holes and shafts ISO 3353-1, Aerospace Lead and runout threads Part 1: Rolled external threads ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts ISO 7913, Aerospace Bolts and screws, metric Tolerances of form and position ISO 142
21、75, Aerospace Drives, internal, offset cruciform, ribbed Metric series ISO 14276, Aerospace Drives, internal, offset cruciform Metric series 3 Configuration and dimensions See Figure 1 and Table 1. Dimensions and tolerances are expressed in millimetres. They are applicable after any coating (toleran
22、ce on shank diameter before coating is also specified for heat cured matrix coatings), but before the application of any lubricant. Details of form not stated are left to the manufacturers discretion. Tolerances of form and position shall be as specified in ISO 7913 if not otherwise stated on produc
23、t standard. Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=Boeing Co/5910770001 Not for Resale, 10/25/2008 05:36:50 MDTNo reproduction or networking permitted without license from IHS -,-,- ISO 5856:2008(E) 2 ISO 2008 All rights reserved Dime
24、nsions in millimetres Break sharp edges 0,1 to 0,4 Key 1 thread a Blended convex form permitted. b In accordance with ISO 3353-1. Figure 1 Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=Boeing Co/5910770001 Not for Resale, 10/25/2008 05:36:50
25、 MDTNo reproduction or networking permitted without license from IHS -,-,- ISO 5856:2008(E) ISO 2008 All rights reserved 3 Blank page Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=Boeing Co/5910770001 Not for Resale, 10/25/2008 05:36:50 MDTN
26、o reproduction or networking permitted without license from IHS -,-,- ISO 5856:2008(E) 4 ISO 2008 All rights reserved Table 1 D1 Coated screws Uncoated screws Tol. Tol. D2 D3 D4 D5 D6 One hole, optional Diameter code Thread a nom. before coatingb close largeclose largemax. min. nom. Tol. H13 c 030 M
27、J3 0,5-4h6h 3 0,026 0,041 0,006 0,031 6 5,4 4,5 2,3 040 MJ4 0,7-4h6h 4 8 7,2 5,78 3 , 0 0 5 1,1 050 MJ5 0,8-4h6h 5 10 9 7,71 3,4 060 MJ6 1-4h6h 6 0,030 0,045 0,010 0,035 12 10,8 9 4,2 1,5 070 MJ7 1-4h6h 7 14 12,8 10,28 5,2 080 MJ8 1-4h6h 8 16 14,8 12,21 6,2 1,9 100 MJ10 1,25-4h6h 10 0,033 0,048 0,01
28、3 0,038 20 18,8 15,43 7,9 120 MJ12 1,25-4h6h 12 24 22,8 18 9,8 2,4 140 MJ14 1,5-4h6h 14 28 26,8 20,57 11,5 160 MJ16 1,5-4h6h 16 32 30,8 24,43 13,5 3 180 MJ18 1,5-4h6h 18 0,036 0,051 0,016 0,041 36 34,8 25,71 15,5 200 MJ20 1,5-4h6h 20 0,040 0,055 0,020 0,045 h12 cf7 c h12 c 40 38,8 28,92 17,5 0,5 3,8
29、 Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=Boeing Co/5910770001 Not for Resale, 10/25/2008 05:36:50 MDTNo reproduction or networking permitted without license from IHS -,-,- ISO 5856:2008(E) ISO 2008 All rights reserved 5 Table 1 (contin
30、ued) L2 L3 E F G H L1 0,2 d Thread Thread R min. , 0 0 08 short medium short medium nom. Tol. Drive code e 0,06 0,63 0,3 1,27 3 to 30 6 7,5 R3 0,08 0,93 0,4 1,69 3 to 40 7,5 10 5 6 0,4 R4 0,96 0,5 2,12 4 to 50 9 12 6 7,5 0,5 R5 1,26 2,54 5 to 60 10 14 8,5 1,57 2,96 6 to 70 11 15 7 9,5 R6 1,6 3,39 6
31、to 80 11,5 16,5 7,5 10,5 0,7 R8 1,93 4,23 8 to 100 14,5 20,5 9 13 0,8 , 0 0 2 R10 2,53 5,08 10 to 120 16 22,5 10 14,5 0,9 R12 3,14 5,93 10 to 140 19 26 12 17 R14 3,2 6,77 10 to 160 20,5 28,5 12,5 18,5 1,1 R16 4,35 7,62 11 to 180 22,5 31 14,5 21 0,1 4,68 0,6 8,47 12 to 200 24,5 33,5 15 22,5 1,3 , 0 0
32、 3 R18 a In conformity with ISO 5855-2, except for the maximum thread major diameter, dmax, of bolts with a close tolerance on D1, which shall be equal to (D1,min 0,025). b Heat cured organic matrix coatings for close tolerance normal shanks. c See ISO 286-2. d Increments: 1 for L1 u 30; 2 for 30 10
33、0. If greater lengths are required, they shall be chosen using these increments. e In accordance with ISO 14275 or ISO 14276. Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=Boeing Co/5910770001 Not for Resale, 10/25/2008 05:36:50 MDTNo reprod
34、uction or networking permitted without license from IHS -,-,- ISO 5856:2008(E) ICS 49.030.20 Price based on 4 pages ISO 2008 All rights reserved Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=Boeing Co/5910770001 Not for Resale, 10/25/2008 05:36:50 MDTNo reproduction or networking permitted without license from IHS -,-,-