EN 6101-2016 en Aerospace series - Rivet 100 edium flush head close tolerance - Inch series《航空航天系列-紧公差100缩减埋头铆钉-英制系列》.pdf

1、BS EN 6101:2016Aerospace series Rivet,100 medium flush head, closetolerance Inch seriesBSI Standards PublicationWB11885_BSI_StandardCovs_2013_AW.indd 1 15/05/2013 15:06BS EN 6101:2016 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 6101:2016.The UK participation

2、 in its preparation was entrusted to TechnicalCommittee ACE/12, Aerospace fasteners and fastening systems.A list of organizations represented on this committee can beobtained on request to its secretary.This publication does not purport to include all the necessaryprovisions of a contract. Users are

3、 responsible for its correctapplication. The British Standards Institution 2016.Published by BSI Standards Limited 2016ISBN 978 0 580 92621 1ICS 49.030.60Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStan

4、dards Policy and Strategy Committee on 30 September 2016.Amendments/corrigenda issued since publicationDate Text affectedBS EN 6101:20162“ EN 6101 trsx vrurxr srr srr srrss trsx 22 “ o CEN-CENELECManagement Centre: Avenue Marnix 17, B-1000 Brussels 9trsx xsrstrsxBS EN 6101:2016EN 6101:2016 (E) 2 Con

5、tents Page European foreword 3 1 Scope 4 2 Normative references 4 3 Requirements 5 3.1 Configuration, dimensions, tolerances and mass 5 3.2 Material and surface treatment 5 4 Designation 9 5 Marking . 10 5.1 Material identification . 10 5.2 Manufacturers identification 11 5.3 Identification of overs

6、ize rivets . 11 6 Technical specification 11 6.1 Aluminium alloy rivet 11 6.2 Heat resisting alloy NiCu31 rivets . 11 6.3 Titanium alloy rivet 11 BS EN 6101:2016EN 6101:2016 (E) 3 European foreword This document (EN 6101:2016) has been prepared by the Aerospace and Defence Industries Association of

7、Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member countries of ASD, prior to its presentation to CEN. This European

8、Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by March 2017, and conflicting national standards shall be withdrawn at the latest by March 2017. Attention is drawn to the possibility that some of the elements of

9、this document may be the subject of patent rights. CEN and/or CENELEC shall not be held responsible for identifying any or all such patent rights. According to the CEN-CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European S

10、tandard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia,

11、 Spain, Sweden, Switzerland, Turkey and the United Kingdom. BS EN 6101:2016EN 6101:2016 (E) 4 1 Scope This European Standard specifies the dimensions, tolerances and mass of rivets with 100 medium flush head, close tolerance, inch series, for aerospace application. 2 Normative references The followi

12、ng documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2114, Aluminium

13、 1050A-H14 Wire for solid rivets D Q 10 mm1)EN 2115, Aerospace series Aluminium alloy 2117-T42 Wire for solid rivets D Q 10 mmEN 2116, Aerospace series Aluminium alloy 2017A-T42 Wire for solid rivets D Q 10 mmEN 2117, Aerospace series Aluminium alloy AL-P5056A (5056A)-H32 Wire for solid rivets D Q 1

14、0 mm EN 2424, Aerospace series Marking of aerospace products EN 2941, Aerospace series Nickel alloy rivets Technical specification EN 3115, Aerospace series Aluminium alloy 7050-T73 Wire for solid rivets D Q 10 mm EN 4372, Aerospace series Heat resisting nickel alloy with copper NI-PD9001 (NiCu31) W

15、ire for solid rivets D Q 10 mm EN 6104, Aerospace series Rivets, solid, in aluminium or aluminium alloy Inch series Technical specification EN 6118, Aerospace series Process specification Aluminium base protection for fasteners1)ISO 8080, Aerospace Anodic treatment of titanium and titanium alloys Su

16、lfuric acid process SAE AMS 4982, Titanium alloy wire 44.5 Cb2) SAE AMS-QQ-P-416, Plating, cadmium (electrodeposited)2)MIL-A-8625, Anodic coatings for aluminum and aluminum alloys3)MIL-C-5541, Chemical conversion coatings on aluminium and aluminium alloys3)NAS 9800, Head protrusion gaging, 100 flush

17、 head fasteners, gage block, gage diameters and stylus4)NASM 5674, Rivets, structural, aluminium alloy, titanium columbium alloy, general specification for4) 1)Published as ASD-STAN Prestandard at the date of publication of this standard (www.asd-stan.org). 2)Published by: Society of Automotive Engi

18、neers (SAE), 400 Commonwealth Drive, Warrendale, PA 15096-0001. 3)Published by: Department of Defense(DoD), the Pentagon, Washington, D.C. 20301. 4)Published by: Aerospace Industries Association of America, Inc. (AIA), 1250 Eye Street, N.W., Washington, D.C. 20005-3924, USA BS EN 6101:2016EN 6101:20

19、16 (E) 5 3 Requirements 3.1 Configuration, dimensions, tolerances and mass The configuration shall conform with Figure 1. The dimensions, tolerances and mass shall conform with Figure 1 and Tables 1 and 3. The dimensions and tolerances of oversizes (for repair purposes only) shall conform with Figur

20、e 1 and Tables 2 and 3. Dimensions and tolerances are expressed in millimetres. 3.2 Material and surface treatment See Table 4. Key 1 Angular misalignment of rivet head to rivet shank axis 0,5max. 2 Marking (see clause 5) a 0,025 mm increase of shank diameter is permissible within 2,54 mm of the bas

21、e of the head b Chamfered ends with radius to the R1dimensions or a 20 chamfer to dimension “S” c Maximum head diameters are to theoretical sharp corners as measured by projection d Measurement method for inspection of head characteristics in accordance with NAS9800 Figure 1 Configuration BS EN 6101

22、:2016EN 6101:2016 (E) 6 Table 1 Dimensions and tolerances Diameter code D Nominal diameter A A1 B C E F P R1 S W +0,03 F 0,03 max. min. min. Ref. +0,05 0 Ref. 0,13 max. min. 0,25 0,25 max. min. 2 1,58 2,90 2,80 2,44 0,53 0,08 0,08 to 0,15 2,07 0,287 0,238 0,48 0,41 2,228 2,223 3 2,38 4,55 4,45 4,09

23、0,89 3,29 0,471 0,419 0,74 0,58 3,443 3,438 4 3,18 5,70 5,60 5,24 1,04 4,14 0,545 0,492 0,99 0,79 4,418 4,413 5 3,97 7,18 7,10 6,74 1,33 5,25 0,861 0,810 1,24 0,99 5,151 5,146 6 4,76 8,43 8,35 7,99 1,52 0,10 6,20 0,946 0,894 1,50 1,19 6,200 6,195 7 5,56 9,67 9,59 9,23 1,70 7,15 1,001 0,948 1,75 1,37

24、 7,310 7,305 8 6,36 11,02 10,92 10,56 1,93 8,15 1,103 1,040 1,98 1,57 8,420 8,415 10 7,93 13,75 13,65 13,29 2,42 10,15 1,471 1,402 2,49 1,98 10,279 10,274 12 9,53 16,42 16,32 15,96 2,87 12,15 1,734 1,660 2,97 2,39 12,329 12,324 Table 2 Dimensions and tolerances for oversize rivets Diameter code D No

25、minal diameter A A1 B C E F P R1 S W +0,03 F 0,03 max. min. min. Ref. +0,05 0 Ref. 0,13 max. min. 0,25 0,25 max. min. 3X 2,78 4,55 4,45 4,09 0,72 0,08 0,08 to 0,15 3,29 0,471 0,419 0,74 0,58 3,443 3,438 4X 3,58 5,70 5,60 5,24 0,87 4,14 0,545 0,492 0,99 0,79 4,418 4,413 5X 4,37 7,18 7,10 6,74 1,16 5,

26、25 0,861 0,810 1,24 0,99 5,151 5,146 6X 5,16 8,43 8,35 7,99 1,36 0,10 6,20 0,946 0,894 1,50 1,19 6,200 6,195 7X 5,96 9,67 9,59 9,23 1,54 7,15 1,001 0,948 1,75 1,37 7,310 7,305 BS EN 6101:2016EN 6101:2016 (E) 7 Table 3 Length code and masses Lengtha bDiameter code 2 3 4 5 6 7 8 10 12 codeL 0,254 Mass

27、 c kg/ 1 000 parts 03 4,76 0,02 0,07 04 6,35 0,04 0,09 0,16 0,26 05 7,94 0,05 0,11 0,20 0,32 0,46 06 9,53 0,05 0,13 0,23 0,37 0,54 0,74 07 11,11 0,06 0,15 0,27 0,43 0,62 0,85 1,13 08 12,70 0,07 0,17 0,30 0,48 0,70 0,96 1,27 - - 09 14,29 0,08 0,19 0,34 0,54 0,78 1,07 1,41 2,26 - 10 15,88 0,09 0,21 0,

28、37 0,59 0,85 1,17 1,55 2,47 3,65 11 17,46 0,10 0,23 0,41 0,64 0,93 1,28 1,69 2,69 3,96 12 19,05 0,11 0,25 0,44 0,70 1,01 1,39 1,83 2,91 4,28 13 20,64 0,12 0,27 0,48 0,75 1,09 1,50 1,97 3,13 4,59 14 22,23 0,12 0,29 0,51 0,81 1,17 1,60 2,11 3,35 4,91 15 23,81 0,13 0,31 0,55 0,86 1,25 1,71 2,25 3,57 5,

29、22 16 25,40 0,14 0,33 0,58 0,92 1,33 1,82 2,40 3,79 5,54 17 26,99 - 0,35 0,62 0,97 1,41 1,93 2,54 4,00 5,86 18 28,58 - 0,37 0,65 1,03 1,49 2,03 2,68 4,22 6,17 20 31,75 - 0,41 0,72 1,14 1,64 2,25 2,96 4,66 6,80 22 34,93 - 0,45 0,79 1,25 1,80 2,46 3,24 5,10 7,44 24 38,10 - - 0,86 1,36 1,96 2,68 3,52 5

30、,53 8,07 aLengths missing in table can be created in 1/16 inch (1,59 mm) steps, e. g. length code 19 corresponds to: 19/16 inch (30,16 mm). b1/32 inch (0,79 mm) length increments may be obtained by adding code 5 after last digit of part number, e. g. length code 06-5 corresponds to: 6/16 inch (9,53

31、mm) + 1/32 inch (0,79 mm) = 13/32 inch (10,32 mm). cMass based on aluminium alloy with a density of 2,79 kg/dm, refer to Table 4 for conversion factors. BS EN 6101:2016EN 6101:2016 (E) 8 Table 4 Material code Material code Diameter code Surface treatment (code see clause 4) Density kg/dm Multiplicat

32、or of mass (see Table 3) 2 3 3X 4 4X 5 5X 6 6X 7 7X 8 10 12 H bAluminium alloy 1050A-H14 per EN2114 Yellow chromated per MIL-C-5541, class 1A 2,7 0,97 AD Aluminium alloy 2117-T4 per EN2115 Yellow chromated per MIL-C-5541, class 1A Anodized per MIL-A-8625, type II, class 1, clear a2,75 0,98 D Alumini

33、um alloy 2017A-T4 per EN2116 2,79 1 B aAluminium alloy 5056A-H32 per EN2117 2,64 0,95 KE Aluminium alloy 7050-T73 per EN3115 2,82 1,01 M Heat resisting alloy NiCu31 per EN4372, annealed Cadmiunm plated per AMS-QQ-P-416, type II, class 3 8,85 3,17 N None R IVD per EN 6118 T Titanium alloy 44.5 Cb, an

34、nealed per AMS4982 Anodized per ISO 8080 5,8 2,08 V IVD per EN 6118 a Not for new design b Not for oversize rivets BS EN 6101:2016EN 6101:2016 (E) 9 4 Designation EXAMPLE * For supplying purpose only, see footnote aand bin Table 3. NOTE If necessary, the code I9005 shall be placed between the descri

35、ption block and the identity block. BS EN 6101:2016EN 6101:2016 (E) 10 5 Marking 5.1 Material identification Symbol on the rivet head see Figure 2. EN 2114 EN 2115 EN 2116 No head marking Indented 0,2 mm max. Embossed 0,2 mm max. EN 2117 EN 3115 EN 4372 Embossed 0,2 mm max. Embossed 0,2 mm max. Embo

36、ssed 0,2 mm max. Indented 0,25 mm max. Figure 2 Material identification BS EN 6101:2016EN 6101:2016 (E) 11 5.2 Manufacturers identification EN 2424, style F to be embossed or indented on rivet head. Manufacturers identification is required on rivet heads for diameter code 4 and larger. 5.3 Identific

37、ation of oversize rivets Symbol on rivet shank end see Figure 3. Triangular shape indented 0,2 mm max. Figure 3 Identification of oversize rivets 6 Technical specification 6.1 Aluminium alloy rivet Aluminium alloy rivets shall conform with the requirements of EN 6104. 6.2 Heat resisting alloy NiCu31

38、 rivets NiCu31 rivets shall conform with the requirements of EN2941. Shear strength Rc = 340 MPa to 407 MPa. NOTE Rivets manufactured prior to August 1st2005 a max. shear strength of 450 MPa may be procured and used until stocks are depleted. 6.3 Titanium alloy rivet Titanium alloy 44.5 Cb rivets shall conform with the requirements of