AECMA PREN 6080-2005 Aerospace Series Rivet 100 Degrees Normal Flush Head Close Tolerance Inch Series Edition P 3 2001 Edition P 1《航空航天系列.铆钉100度普通埋头钉紧公差英尺系列 P3版 2001.P1版》.pdf

《AECMA PREN 6080-2005 Aerospace Series Rivet 100 Degrees Normal Flush Head Close Tolerance Inch Series Edition P 3 2001 Edition P 1《航空航天系列.铆钉100度普通埋头钉紧公差英尺系列 P3版 2001.P1版》.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 6080-2005 Aerospace Series Rivet 100 Degrees Normal Flush Head Close Tolerance Inch Series Edition P 3 2001 Edition P 1《航空航天系列.铆钉100度普通埋头钉紧公差英尺系列 P3版 2001.P1版》.pdf（10页珍藏版）》请在麦多课文档分享上搜索。

1、ASD STANDARD NORME ASD ASD NORM prEN 6080 Edition P3 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 + 32 2 763 3565 - www.asd-stan.orgICS: See foreword for superseded versions Descr

2、iptors: ENGLISH VERSION Aerospace series Rivet, 100 normal flush head, close tolerance Inch series Srie arospatiale Rivets de prcision, 100 tte fraise normale Srie en inches Luft- und Raumfahrt Vollniet, 100 normaler Senkkopf, enge Toleranz Zoll-Reihe This “Aerospace Series“ Prestandard has been dra

3、wn 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. Subsequent to th

4、e 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 submitted as a dr

5、aft 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 any national

6、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 Provided by

7、IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 2 prEN 6080:2005Foreword Due to a communication problem between the sponsor/responsible project team and ASD-STAN there was a confusion regarding the edition numbering of the recent ve

8、rsion of this standard. In order to solve the situation the ASD-STAN Board agreed to publish this version as Edition P3 and it is superseding any version of prEN6080 with a lower edition numbering (P1, P2). Contents Page 1 Scope 3 2 Normative references3 3 Requirements.4 3.1 Configuration, dimension

9、s, tolerances and mass .4 3.2 Material and surface treatment.4 4 Designation 8 5 Marking .9 5.1 Material identification9 5.2 Manufacturers identification.9 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

10、Titanium alloy rivet 10 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 3 prEN 6080:2005 1 Scope This standard specifies the dimensions, tolerance

11、s and mass of rivets with 100 normal flush head, close 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, th

12、e latest edition of the referenced document (including any amendments) applies. ISO 8080, Aerospace Anodic treatment of titanium and titanium alloys Sulfuric acid process. EN 2115, Aerospace series Aluminium alloy 2117-T4 Wire for solid rivets D 10 mm. 1)EN 2116, Aerospace series Aluminium alloy 201

13、7A-H13 Wire for solid rivets D 10 mm. 2)EN 2117, Aerospace series Aluminium alloy 5056A-H32 Wire for solid rivets D 10 mm. 2)EN 2424, Aerospace series Marking of aerospace products. EN 2941, Aerospace series Nickel alloy rivets - Technical specification 3)EN 3115, Aerospace series Aluminium alloy AL

14、-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 6101, Aerospace series Aerospace series - Rivets, 100 medium flush head, close tolerance - Inch series. 3)EN 6104, Aerospace series Rivets, so

15、lid, in aluminium or aluminium alloy Inch series Technical specification. 3)EN 6118, Process specification Aluminium base protection for fasteners. 1)AMS 4982, Titanium alloy wire 44.5 Cb. 4)MIL-A-8625, Anodic coatings for aluminum and aluminum alloys. 5)MIL-C-5541, Chemical conversion coatings on a

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

17、2) Published as AECMA standard 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

18、(DoD), the Pentagon, Washington, 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 AECMANot for Res

19、aleNo reproduction or networking permitted without license from IHS-,-,-Page 4 prEN 6080:20053 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 dimens

20、ions and tolerances 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. Dimensions and tolerances are expressed in millimetres. 0,051Marking ( see chapter 5 ) D

21、1)AS2)2) F A3)100 0,5EC WPB3)L 0,254Angular misalignmentof rivet head to rivet shank axis 0,5max.0,254 max radA A1R14)1 2 c a R1b c d b Key 1 Angular misalignment of rivet head to rivet shank axis 0,5 max. 2 Marking (see clause5) a0,025mm shank diameter increase is permissible within 2,54 mm of the

22、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. Figure 1 Configuration Copyri

23、ght Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 5 prEN 6080:2005 Table 1 Dimensions and tolerances Diameter code D A A1B C E F P R1S W + 0,03 0,03 max.

24、min. min. Ref.+ 0,050 0,13 max. min. 0,25 0,25 max. min. 2 3 4 Use rivets according to EN 6101 5 3,97 7,25 7,15 6,79 1,350,085,29 0,706 0,650 1,24 0,99 5,588 5,583 6 4,76 8,95 8,85 8,49 1,74 6,55 0,899 0,839 1,50 1,19 6,833 6,827 7 5,56 10,55 10,45 10,09 2,07 7,73 1,068 1,005 1,75 1,37 8,033 8,027 8

25、 6,36 12,10 12,00 11,64 2,39 8,88 1,227 1,161 1,98 1,57 9,208 9,202 10 7,93 14,35 14,25 13,89 2,67 10,54 1,371 1,302 2,49 1,98 11,119 11,11112 9,53 17,65 17,55 17,19 3,390,100,08to 0,1513,05 1,682 1,608 2,97 2,39 13,684 13,676Table 2 Dimensions and tolerances for oversize rivets Diameter code D A A1

26、B 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. 5X 4,37 7,25 7,15 6,79 1,190,085,29 0,706 0,650 1,24 0,99 5,588 5,583 6X 5,16 8,95 8,85 8,49 1,57 6,55 0,899 0,839 1,50 1,19 6,833 6,827 6Y 5,56 8,95 8,85 8,49 1,40 6,55 0,899 0,839 1,50 1,19 6,833 6,827 7X 5,9

27、6 10,55 10,45 10,09 1,91 7,73 1,068 1,005 1,75 1,37 8,033 8,027 8Y 7,14 12,10 12,00 11,64 2,060,100,08to 0,158,88 1,227 1,161 1,98 1,57 9,208 9,202 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or netwo

28、rking permitted without license from IHS-,-,-Page 6 prEN 6080:2005Table 3 Length code and masses Diameter code Lengtha b2 3 4 5 6 7 8 10 12 codeL 0,254 Mass c kg/ 1 000 parts 03 4,76 - - - - - - 04 6,35 0,26 - - - - - 05 7,94 0,32 0,48 - - - - 06 9,53 0,37 0,56 0,80 - - - 07 11,11 0,43 0,64 0,90 1,2

29、2 - - 08 12,70 0,48 0,72 1,01 1,36 - - 09 14,29 0,54 0,80 1,12 1,50 2,33 - 10 15,88 0,59 0,88 1,23 1,64 2,54 3,86 12 19,05 0,70 1,04 1,44 1,92 2,98 4,50 14 22,23 0,81 1,19 1,66 2,20 3,42 5,13 16 25,40 0,92 1,35 1,87 2,48 3,86 5,76 18 28,58 1,03 1,51 2,09 2,76 4,29 6,39 20 31,75 1,14 1,67 2,30 3,05 4

30、,73 7,02 22 34,93 1,25 1,82 2,52 3,30 5,17 7,65 24 38,10 1,36 1,98 2,73 3,61 5,61 8,28 28 44,45 1,58 2,30 3,16 4,17 6,48 9,55 32 50,80 1,80 2,61 3,59 4,73 7,35 10,81 40 63,50 Use rivets according to EN 6101 - - 4,457 5,86 9,10 13,34 aLengths missing in table can be created in 1/16 inch (1,59 mm) ste

31、ps, 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 mm) + 1/32 inch (0,79 mm) = 13/32 inch (10,32 mm). dMass based on aluminium al

32、loy 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 AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 7 prEN 6080:2005Table 4

33、 Material code Diameter code Material code 2 3 4 5 5X 6 6X 6Y a7 7X 8 8Y 10 12 Surface treatment (code see clause 4) Density kg/dm Multiplicator of mass (see Table 3)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

34、,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 N None R Heat resisting alloy NiCu31 per EN4372, annealed IVD per EN6118 8,85 3,17 T Anodized per ISO8080 V Use rivets according to EN6101 Titanium all

35、oy 44.5 Cb, annealed per AMS4982 IVD per EN6118 5,8 2,08 a Not for new design Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 8 prEN 6080:20054 De

36、signation EXAMPLE Description block RIVET Identity block EN6080D6X-06A-5 Number of this standard Material code (see Table 4) Diameter code (see Table 1 and 2) Length code (see Table 3) (1/16 of an inch)* Surface treatment for Aluminium alloy (see Table 4): - No code indicates yellow chromated, - Cod

37、e “A” indicates anodised (not for new design) Additional length code (see Table 3) (1/16 of an inch plus 1/32 inch)* * For supplying purpose only, see footnote aand bin Table 3. NOTE If necessary, the code I9005 shall be placed between the description block and the identity block. Copyright Associat

38、ion Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 9 prEN 6080:20055 Marking 5.1 Material identification Symbol on the rivet head see Figure 2. EN2115 EN2116 EN2117 In

39、dented 0,2 mm max. Embossed 0,2 mm max. Embossed 0,2 mm max. EN3115 EN4372 AMS4982 Embossed 0,2 mm max. Embossed 0,2 mm max. Indented 0,25 mm max. Figure 2 Material identification 5.2 Manufacturers identification EN 2424, style F to be embossed or indented on rivet head. Manufacturers identification

40、 is required on rivet heads for diameter code 4 and larger. 0,8 max. 0,8 max. 0,8 max. 1,020 min. 1,780 max. 0,762 min. 1,270 max. 0,8 max. 0,8 max. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or netw

41、orking permitted without license from IHS-,-,-Page 10 prEN 6080:20055.3 Identification of oversize rivets Symbol on rivet shank end see Figure 3. Max. 0,5 D 0,8 max. Triangular shape indented 0,2 mm max. Figure 3 Identification of oversize rivets 6 Technical specification 6.1 Aluminium alloy rivet A

42、luminium alloy rivets shall conform with the requirements of EN 6104. 6.2 Heat resisting alloy NiCu31 rivets NiCu31 rivets shall conform with the requirements of EN2941. Shear strength Rc = 340 MPa to 407 MPa. NOTE Rivets manufactured prior to August 1st 2005 with a max. shear strength of 450 Mpa ma

43、y be procured and used until stocks are depleted. 6.3 Titanium alloy rivet TiCb rivets shall conform with the requirements of NASM 5674 except for the finish as stated. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-