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 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 con
5、form with Figure 1 and Tables 1 and 3. The dimensions 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. 1.2 Material and surface treatment See Table 4. Key 1 Angular misalignment of rivet hea
6、d 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 a 20 chamfer to dimension “S”. cMaximum head diameters are to theoretical sharp corners as measured b
7、y projection. dMeasurement method for inspection of head characteristics in accordance with NAS9800. Figure 1 Configuration 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. + 0,050 - 0,13 max. min. 0,25 0
8、,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 8,35 7
9、,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 0,
10、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. 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 4X 3,5
11、8 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 - White page - (se
12、paration between the modified pages above and the initial version of prEN 6101 below) not to be inserted into the final text 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-
13、1200 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: Supersedes Edition P1 February 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 Luf
14、t- und Raumfahrt Vollniet, 100 Medium Senkkopf, enge Toleranz Zoll-Reihe This “Aerospace Series“ Prestandard 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 Indu
15、stry. It has been technically approved by the experts of the concerned Domain following member comments. Subsequent 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-identificat
16、ion of the standard. After examination and review by users and formal agreement of ASD-STAN, it will be submitted 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
17、to implement the EN at national level by giving the EN the status of a national standard and by withdrawing any 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
18、 Domain Copyright 2005 by ASD-STAN 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 treatment.4 4 Designation 8 5 Marking .9 5.1 Material identification9 5.2 Manufacturers identif
19、ication.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 Page 3 prEN 6101:2005 (E) 1 Scope This standard specifies the dimensions, tolerances and mass of rivets with 100 medium f
20、lush 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, the latest edition of the referenced doc
21、ument (including 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)
22、EN 2116, Aerospace 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
23、)EN 3115, Aerospace 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 speci
24、fication. 3)EN 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 a
25、nd aluminium 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 standar
26、d.2) In preparation 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
27、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 Page 4 prEN 6101:2005 (E) 3 Requirements 3.1 Configuration, dimensions, tolerances and mass The configuration shall conform with Figure
28、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 Figure 1 and Tables 2 and 3. Dimensions and tolerances are expressed in millimetres. 3.2 Material and surface treatment See
29、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 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
30、diameter is permissible 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 accordan
31、ce with NAS9800. Figure 1 Configuration 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. 0,25 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
32、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 8,35 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
33、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 0,1512,15 1,734 1,660 2,97 2,39 12,329 12,324Table 2 Dimensions and tolerances for
34、 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 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,
35、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 Page 6 prEN 6101:2005 (E) Table 3 Length code and masses Diameter code Lengtha b2 3 4 5 6 7 8
36、10 12 codeL 0,254 Mass 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 -
37、 10 15,88 0,09 0,21 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
38、1,25 1,71 2,25 3,57 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
39、 1,36 1,96 2,68 3,52 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
40、to: 6/16 inch (9,53 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. 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 treatmen
41、t (code see clause 4) Density kg/dm Multiplicator of mass (see Table 3)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 2,75 0,98 D Aluminium alloy 2017A-T4 per EN2116 2,79 1 B aAluminium alloy 5056A-H32 per EN2117 2,64
42、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 Heat resisting alloy NiCu31 per EN4372, annealed IVD per EN6118 8,85 3,17 T Anodized per ISO8
43、080 V Titanium alloy 44.5 Cb, annealed per AMS4982 IVD per EN6118 5,8 2,08 a Not for new design b Not for oversize rivets Page 8 prEN 6101:2005 (E) 4 Designation EXAMPLE Description block RIVET Identity block EN6101D6X-06A-5 Number of this standard Material code (see Table 4) Diameter code (see Tabl
44、e 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, - Code “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, s
45、ee footnote aand bin Table 3. NOTE If necessary, the code I9005 shall be placed between the description block and the identity block. Page 9 prEN 6101:2005 (E) 5 Marking 5.1 Material identification Symbol on the rivet head see Figure 2. EN2114 EN2115 EN2116 No head marking Indented 0,2 mm max. Embos
46、sed 0,2 mm max. EN2117 EN3115 EN4372 Embossed 0,2 mm max. Embossed 0,2 mm max. Embossed 0,2 mm max. AMS4982 Indented 0,25 mm max. Figure 2 Material identification 0,8 max. 0,8 max. 0,8 max. 0,8 max. 0,8 max. 1,020 min. 1,780 max. 0,762 min. 1,270 max. Page 10 prEN 6101:2005 (E) 5.2 Manufacturers ide
47、ntification 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 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. Figur
48、e 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 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 NASM 5674 except for the finish as stated.
