AECMA PREN 6101-2005 Aerospace series Rivet 100 medium flush head close tolerance Inch series Edition P 2 Corrigendum 06 30 2006 2001 Edition P 1《航空航天系列.铆钉100度中度埋头钉紧公差英尺系列.P2版 2001.pdf

《AECMA PREN 6101-2005 Aerospace series Rivet 100 medium flush head close tolerance Inch series Edition P 2 Corrigendum 06 30 2006 2001 Edition P 1《航空航天系列.铆钉100度中度埋头钉紧公差英尺系列.P2版 2001.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 6101-2005 Aerospace series Rivet 100 medium flush head close tolerance Inch series Edition P 2 Corrigendum 06 30 2006 2001 Edition P 1《航空航天系列.铆钉100度中度埋头钉紧公差英尺系列.P2版 2001.pdf（14页珍藏版）》请在麦多课文档分享上搜索。

1、ASD STANDARD NORME ASD ASD NORM prEN 6101 Edition P2 November 2005 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Gulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: Supersedes Edition P1 February 2001 CORRIG

2、ENDUM 30-06-2006 ENGLISH VERSION Aerospace series Rivet, 100 medium flush head, close tolerance Inch series Srie arospatiale Rivets de prcision, 100 tte fraise mdium Sries en inches Luft- und Raumfahrt Vollniet, 100 Medium Senkkopf, enge Toleranz Zoll-Reihe Replace Page 4 of the previous edition by

3、the attached page 4 modified as follows : - Figure 1 : “ in front “0,254 max. rad.“ Replace page 5 of the previous edition by the attached page 5 modified as follows : - Tables 1 and 2 : “Ref.“ for diameter code E is deleted in both tables. Edition approved for publication 30 June 2006 Comments shou

4、ld be sent within six months after the date of publication to ASD-STAN Mechanical Domain Copyright 2006 by ASD-STAN Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license

5、 from IHS-,-,-Page 4 prEN 6101:2005 (E) 1 Requirements 1.1 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

6、 only) shall conform with Figure 1 and Tables 2 and 3. Dimensions and tolerances are expressed in millimetres. 1.2 Material and surface treatment See Table 4. Key 1 Angular misalignment of rivet head to rivet shank axis 0,5 max. 2 Marking (see clause 5) a0,025 mm increase of shank diameter is permis

7、sible within 2,54 mm of the base of the head. bChamfered ends with radius to the R1dimensions or a 20 chamfer to dimension “S”. cMaximum head diameters are to theoretical sharp corners as measured by projection. dMeasurement method for inspection of head characteristics in accordance with NAS9800. F

8、igure 1 Configuration Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 5 prEN 6101:2005 (E) Table 1 Dimensions and tolerances Diameter code D Nomi

9、nal diameter A A1B C E F P R1S W + 0,03 0,03 max. min. min. Ref. + 0,050 - 0,13 max. min. 0,25 0,25 max. min. 2 1,58 2,90 2,80 2,44 0,53 2,07 0,287 0,238 0,48 0,41 2,228 2,223 3 2,38 4,55 4,45 4,09 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 4,41

10、8 4,413 5 3,97 7,18 7,10 6,74 1,330,08 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 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 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 1

11、3,29 2,42 10,15 1,471 1,402 2,49 1,98 10,279 10,27412 9,53 16,42 16,32 15,96 2,870,10 0,08 to 0,1512,15 1,734 1,660 2,97 2,39 12,329 12,324Table 2 Dimensions and tolerances for oversize rivets Diameter code D Nominal diameter A A1B C E F P R1S W + 0,03 0,03 max. min. min. Ref. + 0,050 - 0,13 max. mi

12、n. 0,25 0,25 max. min. 3X 2,78 4,55 4,45 4,09 0,72 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 1,160,08 5,25 0,861 0,810 1,24 0,99 5,151 5,146 6X 5,16 8,43 8,35 7,99 1,36 6,20 0,946 0,894 1,50 1,19 6,200 6,195 7X 5,

13、96 9,67 9,59 9,23 1,540,10 0,08 to 0,157,15 1,001 0,948 1,75 1,37 7,310 7,305 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,- White page - (separatio

14、n between the modified pages above and the initial version of prEN 6101 below) not to be inserted into the final text Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without licen

15、se from IHS-,-,-ASD STANDARD NORME ASD ASD NORM prEN 6101 Edition P2 November 2005 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Gulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: Supersedes Edition P1 Febr

16、uary 2001 Descriptors: ENGLISH VERSION Aerospace series Rivet, 100 medium flush head, close tolerance Inch series Srie arospatiale Rivets de prcision, 100 tte fraise mdium Sries en inches Luft- und Raumfahrt Vollniet, 100 Medium Senkkopf, enge Toleranz Zoll-Reihe This “Aerospace Series“ Prestandard

17、has been drawn up under the responsibility of ASD-STAN (AeroSpace and Defence Industries Association of Europe - Standardization). It is published for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments. Subs

18、equent to the publication of this pre-standard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and review by users and formal agreement of ASD-STAN, it will be submi

19、tted as a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN national members have then to implement the EN at national level by giving the EN the status of a national standard and by withdrawing a

20、ny national standards conflicting with the EN. Edition approved for publication 30 November 2005 Comments should be sent within six months after the date of publication to ASD-STAN Mechanical Domain Copyright 2005 by ASD-STAN Copyright Association Europeene des Constructeurs de Materiel Aerospatial

21、Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 2 prEN 6101:2005 (E) Contents Page 1 Scope 3 2 Normative references3 3 Requirements.4 3.1 Configuration, dimensions, tolerances and mass .4 3.2 Material and surface treatm

22、ent.4 4 Designation 8 5 Marking .9 5.1 Material identification9 5.2 Manufacturers identification.10 5.3 Identification of oversize rivets10 6 Technical specification .10 6.1 Aluminium alloy rivet 10 6.2 Heat resisting alloy NiCu31 rivets10 6.3 Titanium alloy rivet 10 Copyright Association Europeene

23、des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 3 prEN 6101:2005 (E) 1 Scope This standard specifies the dimensions, tolerances and mass of rivets with 100 medium flush head, cl

24、ose tolerance, inch series, for aerospace application. 2 Normative references The following referenced 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 (includ

25、ing any amendments) applies. ISO 8080, Aerospace Anodic treatment of titanium and titanium alloys Sulfuric acid process. EN 2114, Aerospace series Aluminium 1050A-H14 - Wire for solid rivets - D 10 mm. 1)EN 2115, Aerospace series Aluminium alloy 2117-T4 Wire for solid rivets D 10 mm. 2)EN 2116, Aero

26、space series Aluminium alloy 2017A-H13 Wire for solid rivets D 10 mm. 1)EN 2117, Aerospace series Aluminium alloy 5056A-H32 Wire for solid rivets D 10 mm. 1)EN 2424, Aerospace series Marking of aerospace products. EN 2941, Aerospace series Nickel alloy rivets - Technical specification 3)EN 3115, Aer

27、ospace series Aluminium alloy AL-P7050- Wire for solid rivets D 10 mm. 3)EN 4372, Aerospace series Heat resisting alloy NI-PD9001 (NiCu31) - Non heat treated - Wire for rivets -D 10mm. 3)EN 6104, Aerospace series Rivets, solid, in aluminium or aluminium alloy Inch series Technical specification. 3)E

28、N 6118, Process specification Aluminium base protection for fasteners. 2)AMS 4982, Titanium alloy wire 44.5 Cb. 4)AMS-QQ-P-416, , Plating, cadmium (electrodeposited) 2)MIL-A-8625, Anodic coatings for aluminum and aluminum alloys. 5)MIL-C-5541, Chemical conversion coatings on aluminium and aluminium

29、alloys. 5)NAS 9800, Head protrusion gaging, 100 flush head fasteners, gage block, gage diameters and stylus.)6NASM 5674, Rivets, structural, aluminium alloy, titanium columbium alloy, general specification for. 6) 1) Published as AECMA standard at the date of publication of this standard.2) In prepa

30、ration at the date of publication of this standard. 3) Published as AECMA Prestandard at the date of publication of this standard. 4) Published by: Society of Automotive Engineers (SAE), 400 Commonwealth Drive, Warrendale, PA 15096-0001. 5) Published by: Department of Defense(DoD), the Pentagon, Was

31、hington, D.C. 20301. 6) Published by: Aerospace Industries Association of America, Inc. (AIA), 1250 Eye Street, N.W., Washington, D.C. 20005-3924, USA Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or n

32、etworking permitted without license from IHS-,-,-Page 4 prEN 6101:2005 (E) 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 tolerance

33、s of oversizes (for repair purposes only) shall conform with Figure 1 and Tables 2 and 3. Dimensions and tolerances are expressed in millimetres. 3.2 Material and surface treatment See Table 4. Marking ( see 5 ) D1)AS2)2) F A3)10030EC WPB3)L 0,254Head-co gelrelative t isof rivet 1/ max.cking ano ax2

34、 0,254 max. rad. 0,127 A A14)b c d 2 1 100 0,5 R1a R1b c 0,051Key 1 Angular misalignment of rivet head to rivet shank axis 0,5 max. 2 Marking (see clause 5) a0,025 mm increase of shank diameter is permissible within 2,54 mm of the base of the head. bChamfered ends with radius to the R1dimensions or

35、a 20 chamfer to dimension “S”. cMaximum head diameters are to theoretical sharp corners as measured by projection. dMeasurement method for inspection of head characteristics in accordance with NAS9800. Figure 1 Configuration Copyright Association Europeene des Constructeurs de Materiel Aerospatial P

36、rovided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 5 prEN 6101:2005 (E) Table 1 Dimensions and tolerances Diameter code D Nominal diameter A A1B C E F P R1S W + 0,03 0,03 max. min. min. Ref. + 0,05 0 Ref. 0,13 max. min. 0,2

37、5 0,25 max. min. 2 1,58 2,90 2,80 2,44 0,53 2,07 0,287 0,238 0,48 0,41 2,228 2,223 3 2,38 4,55 4,45 4,09 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 1,330,08 5,25 0,861 0,810 1,24 0,99 5,151 5,146 6 4,76 8,43 8,3

38、5 7,99 1,52 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 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 10,27412 9,53 16,42 16,32 15,96 2,870,10 0,08 to

39、 0,1512,15 1,734 1,660 2,97 2,39 12,329 12,324Table 2 Dimensions and tolerances for oversize rivets Diameter code D Nominal diameter A A1B C E F P R1S W + 0,03 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 3,29 0,471 0,419 0,74 0,58 3,443 3,438

40、 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 1,160,08 5,25 0,861 0,810 1,24 0,99 5,151 5,146 6X 5,16 8,43 8,35 7,99 1,36 6,20 0,946 0,894 1,50 1,19 6,200 6,195 7X 5,96 9,67 9,59 9,23 1,540,10 0,08 to 0,157,15 1,001 0,948 1,75 1,37 7,310 7,305 Copyright A

41、ssociation Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 6 prEN 6101:2005 (E) Table 3 Length code and masses Diameter code Lengtha b2 3 4 5 6 7 8 10 12 codeL 0,254 M

42、ass 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

43、 0,37 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

44、 5,22 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 3,5

45、2 5,53 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

46、 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. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction o

47、r networking permitted without license from IHS-,-,-Page 7 prEN 6101:2005 (E) Table 4 Material code Diameter code Material code 2 3 3X 4 4X 5 5X 6 6X 7 7X 8 10 12 Surface treatment (code see clause 4) Density kg/dm Multiplicator of mass (see Table 3)H bAluminium alloy 1050A-H14 per EN2114 Yellow chr

48、omated per MIL-C-5541, class 1A 2,7 0,97 AD Aluminium alloy 2117-T4 per EN2115 2,75 0,98 D Aluminium 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 Yellow chromatedper MIL-C-5541, class 1A Anodized per MIL-A-8625, type II, class 1, clear a2,82 1,01 M Cadmiunm plated per AMS-QQ-P-416, type II, class 3 N None R