1、ASD STANDARD NORME ASD ASD NORM prEN 6129 Edition P1 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: Descriptors: ENGLISH VERSION Aerospace ser
2、ies Blind bolt, Protruding head, high strength Srie arospatiale Boulon aveugle, tte protubrante, haute rsistance Luft- und Raumfahrt Blindbolzen Universalkopf, hochfest This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (AeroSpace and Defence Industries Associ
3、ation 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 the publication of this pre-standard, the technical content shall not be changed to a
4、n 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 draft European Standard (prEN) to CEN (European Committee for Standardization) for fo
5、rmal 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 standards conflicting with the EN. Edition approved for publication 30 November 200
6、5 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 IHS under license with AECMANot for ResaleNo reproduction or networking permitted w
7、ithout license from IHS-,-,-Page 2 prEN 6129:2005Contents Page 1 Scope 3 2 Normative references3 3 Requirements.3 3.1 Configuration, dimensions and tolerances.3 3.2 Grip range and mass.3 3.3 Material, finish and lubrication.3 4 Designation 9 5 Marking .10 6 Technical specification .10 Copyright Asso
8、ciation 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 6129:20051 Scope This standard specifies the configuration, dimension, tolerances and mass of a stainless
9、 steel and titanium blind bolt with protruding head for aerospace application. 2 Normative references This European Standard incorporates by dated or undated reference provisions from other publications. These normative references are cited at the appropriate places in the text and the publications
10、are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies (including amendments
11、). ISO 8080, Aerospace Anodic treatment of titanium and titanium alloys sulfuric acid process EN 2424, Aerospace series Marking of aerospace products EN 4473, Aerospace series Aluminium pigmented coatings Technical specification 1)AS 5272, Lubricant, solid film, heat cured, corrosion inhibiting proc
12、urement specification 2)AMS 5687, Nickel alloy, corrosion and heat-resistant, wire 74Ni-15,5Cr-8,0Fe annealed 2)AMS 5690, Steel, corrosion and heat resistant, wire 17Cr-12Ni-2,5Mo (SAE 30316) solution heat treated 2)AMS 5737, Steel, corrosion and heat-resistant, bars, wire, forgings, and tubing 15Cr
13、-25,5Ni-1,2Mo-2,1Ti-0,006B-0,30V consumable electrode melted 1 650 F (899 C) solution and precipitation heat treated 2)AMS-QQ-P-35, Passivation treatments for corrosion-resistant steel 2)MIL-PRF-46010, Lubricant, solid film, heat cured, corrosion inhibiting 3)MIL-L-87132, Lubricant, cetyl alcohol, 1
14、-hexadecanol, application to fasteners 3)ASTM B 348, Standard specification for titanium and titanium alloy bars and billets 4)NASM 8975, Fastener, blind, high strength, installation formed corrosion resistant steel, heat resistant steel and titanium General specification for 3)DOD-L-85645, Lubrican
15、t, dry film, molecular bonded 3)3 Requirements 3.1 Configuration, dimensions and tolerances The configuration, dimensions, tolerances, static and dynamic values shall conform to Figures 1 and 2 and Tables 1 and 2. 3.2 Grip range and mass See Tables 3 and 4. 3.3 Material, finish and lubrication See T
16、ables 5 and 6. 1) Published as AECMA Prestandard at the date of publication of this standard2) Published by: Society of Automotive Engineers (SAE), 400 Commonwealth drive, Warrendale, PA 15096-0001, USA 3) Published by: Department of Defense (DOD), the Pentagon, Washington, D.C. 20301 4) Published b
17、y: American Society for Testing and Materials (ASTM), 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959, USA Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license f
18、rom IHS-,-,-Page 4 prEN 6129:2005Detail of serrated pin geometry: Detail A Detail A Optional configuration Key 1 Marking see clause 5 5 Locking collar 2 Serrated pin 6 Shifting Anvil 3 Sleeve 7 Drive washer 4 Grip a Diameter of pin head shall not exceed “ D” max. b Fasteners are supplied with shifti
19、ng anvil/drive washer of manufacturers option. The shifting anvil/drive washer is not part of the installed fastener. Figure 1 Configuration Dimensions Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or n
20、etworking permitted without license from IHS-,-,-Page 5 prEN 6129:2005Key 1 Marking see clause 5 aBlind side head may be installed on 7 max slope. Figure 2 Typical installation Table 1 Dimensions and tolerances Dimensions in mm (inch) A Theor. B Ref. D JaN Q D1 D2 P b P2Diameter code min. max. min.
21、max. 0,03(.001)0,13(.005)1,52(.060)0,13(.005)max. max. max. min. 05 7,52 (.296) 8,33 (.328) 1,70 (.067) 1,96(.077)4,14(.163)9,53(.375)3,56(.140)1,70(.067)3,05 (.120) 2,16 (.085) 7,62(.300)5,66(.223)06 9,04 (.356) 10,01 (.394) 2,03 (.080) 2,29(.090)5,03(.198)9,53(.375)4,06(.160)2,21(.087)3,81 (.150)
22、2,79 (.110) 8,13(.320)6,86(.270)08 12,07 (.475) 13,34 (.525) 2,72 (.107) 2,97(.117)6,58(.259)9,53(.375)4,83(.190)2,79(.110)4,83 (.190) 3,66 (.144) 9,40(.370)9,01(.355)R S J1J2 min.X E C1 C2F G Hole limits Diameter code max. max. 0,76 (.030) Number ofserrations0,76(.030)min. Ref. 0,05(.002)5 5 min. m
23、ax. 05 0,25 (.010) 5,84 (.232) 20,32 (.800) 18 1,52(.060)0,13(.005)0,33(.013)0,80(.032) 45 30 4,17(.164) 4,24(.167) 06 0,38 (.015) 7,42 (.292) 21,08 (.830) 19 1,78(.070)0,13(.005)0,33(.130)0,80(.032) 45 30 5,06(.199) 5,13(.202) 08 0,51 (.020) 9,17 (.361) 24,77 (.975) 20 2,29(.090)0,13(.005)0,33(.130
24、)0,80(.032) 45 30 6,60(.260) 6,68(.263) aDiameter code 05 is also available reduced diameter drive anvil (7,90,13 / .312.005). See part number examples.bIn the length P of D may be 0,05 mm (.002) undersize. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS und
25、er license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 6 prEN 6129:2005Table 2 Static values (installed strength) for Cres Dimensions in kN (lbf) Installed strength Single shear min. Tensile strength min. Tensile preload min. Spindle retention mi
26、n. Diameter code Cres Cres Cres Cres 05 8,811 (1 980) 5,117 (1 150) 0,512 (115) 2,558 (575) 06 13,016 (2 925) 7,520 (1 690) 0,752 (169) 3,760 (845) 08 22,250 (5 000) 12,905 (2 900) 1,29 (290) 6,408 (1 440) Table 3 Grip range Dimensions in mm (inch) Under lap Grip range Over lap Diameter code 05 06 0
27、8 only 05 dia. only 06 to 08 dia. 05 to 08 dia. L K L K L K Grip length code min. min. min. max. max. Ref. max. Ref. max. Ref. max. 01 0,79 (.031) 2,41 (.095) 2,82 a (.111)a7,19 (.283) 11,35(.447) 02 2,13 (.084) 1,99 (.078) 2,39 (.094) 3,99 (.0157) 4,39 (.173) 8,79 (.346) 12,95(.510) 9,47 (.373) 14,
28、48 (.57) 10,49 (.413) 16,76(.66) 03 3,71 (.146) 3,56 (.140) 3,96 (.156) 5,59 (.220) 5,99 (.236) 10,37(.408) (14,53(.572) 11,05(.435) 16,05 (.632) 12,07 (.475) 18,34(.722) 04 5,31 (.209) 5,16 (.203) 5,56 (.219) 7,16 (.282) 7,57 (.298) 11,97(.471) 16,13(.635) 12,65(.498) 17,65 (.695) 13,67 (.538) 19,9
29、4(.785) 05 6,88 (.271) 6,73 (.265) 7,14 (.281) 8,76 (.345) 9,17 (.361) 13,54(.533) 17,70(.697) 14,22(.560) 19,23 (.757) 15,24 (.600) 21,51(.847) 06 8,48 (.334) 8,33 (.328) 8,74 (.344) 10,34 (.407) 10,74(.423) 15,14(.596) 19,30(.760) 15,82(.623) 20,83 (.820) 16,84 (.663) 23,11(.910) 07 10,06 (.396) 9
30、,91 (.39) 10,31 (.406) 11,94 (.470) 12,34(.486) 16,71(.658) 20,88(.822) 17,40(.685) 22,40 (.882) 18,42 (.725) 24,69(.972) 08 11,66 (.459) 11,51 (.453) 11,91 (.469) 13,51 (.532) 13,92(.548) 18,29(.720) 22,45(.884) 19,00(.748) 24,00 (.945) 20,02 (.788) 26,29(1.035) 09 13,23 (.521) 13,08 (.515) 13,49 (
31、.531) 15,11 (.595) 15,52(.611) 19,86(.782) 24,03(.946) 20,57(.810) 25,58 (1.007) 21,59 (.850) 27,86(1.097) 10 14,83 (.584) 14.68 (.578) 15,09 (.594) 16,69 (.657) 17,09(.673) 21,46(.845) 25,63(1.009) 22,17(.873) 27,18 (1.070) 23,19 (.913) 29,46(1.16) 11 16,41 (.646) 16,26 (.640) 16,66 (.656) 18,29 (.
32、720) 18,69(.736) 23,06(.908) 27,23(1.072) 23,77(.936) 28,78 (1.133) 24,79 (.976) 31,06(1.223) 12 18,01 (.709) 17,86 (.703) 18,26 (.719) 19,86 (.782) 20,27(.798) 24,64(.970) 28,80(1.134) 25,35(.998) 30,35 (1.195) 26,37 (1.038) 32,64(1.285 13 19,58 (.771) 19,43 (.765) 19,84 (.781) 21,46 (.845) 21,87(.
33、861) 26,24(1.033) 30,40(1.197) 26,95(1.061) 31,95 (1.258) 27,97 (1.101) 34,24(1.348) continued 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 p
34、rEN 6129:2005 Table 3 Grip range (concluded) Dimensions in mm (inch) Under lap Grip range Over lap Diameter code 05 06 08 only 05 dia. only 06 to 08 dia. 05 to 08 dia. L K L K L K Grip length code min. min. min. max. max. Ref. max. Ref. max. Ref. max. 14 21,18 (.834) 21,03 (.828) 21,44 (.844) 23,04(
35、.907) 23,44(.923) 27,81(1.095) 31,98(1.259) 28,52 (1.123) 33,53 (1.32) 29,54(1.163) 35,81(1.410) 15 22,76 (.896) 22,61 (.89) 23,01 (.909) 24,64(.970) 25,04(.986) 29,41(1.158) 33,58(1.322) 30,12 (1.186) 35,13 (1.383) 31,14(1.226) 37,41(1.473) 16 24,36 (.959) 24,21 (.953) 24,61 (.969) 26,21(1.032) 26,
36、62(1.048) 30,991.220 35,151.384 31,70 (1.248) 36,70 (1.445) 32,72(1.288) 38,99(1.535) 17 25,81 (1.016) 26,19 (1.031) 27,81(1.095) 28,22(1.111) 33,30 (1.311) 38,30 (1.508) 34,32(1.351) 40,59(1.598) 18 27,38 (1.078) 27,79 (1.094) 29,39(1.157) 29,79(1.173) 34,87 (1.373) 39,88 (1.570) 35,89(1.413) 42,16
37、(1.660) 19 28,98 (1.141) 29,36 (1.156) 30,99(1.220) 31,39(1.236) 36,45 (1.435) 41,48 (1.633) 37,49(1.476) 43,76(1.723) 20 30,56 (1.203) 30,96 (1.219) 32,56(1.282) 32,97(1.298) 38,05 (1.498) 43,05 (1.695) 39,07(1.538) 45,34(1.785) 21 32,13 (1.265) 32,54 (1.281) 34,16(1.345) 34,54(1.360) 39,62 (1.560)
38、 44,65 (1.758) 40,67(1.601) 46,94(1.848) 22 33,73 (1.328) 34,14 (1.344) 35,74(1.407) 36,14(1.423) 41,22 (1.623) 46,23 (1.820) 42,24(1.663) 48,51(1.910) 23 35,31 (1.390) 35,71 (1.406) 37,34(1.470) 37,72(1.485) 42,80 (1.685) 47,83 (1.883) 43,84(1.726) 50,11(1.973) 24 36,91 (1.453) 37,31 (1.469) 38,91(
39、1.532) 39,32(1.548) 44,40 (1.748) 49,40 (1.945) 45,42(1.788) 51,69(2.035) 25 40,01 (1.575) 38,89 (1.531) 40,51(1.595) 40,89(1.610) 45,97 (1.810) 51,00 (2.008) 47,02(1.851) 53,29(2.098) aOnly for 05 dia. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under l
40、icense with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 8 prEN 6129:2005Table 4 Mass Mass in kg (lbs)/1 000 pieces Diameter code Grip length code 05 06 08 01 1,23 (2.72) 02 1,39 (3.06) 2,28 (5.02) 4,89 (10.78) 03 1,56 (3.43) 2,53 (5.57) 5,32 (11.73) 0
41、4 1,72 (3.80) 2,77 (6.11) 5,75 (12.68) 05 1,89 (4.17) 3,02 (6.66) 6,19 (13.64) 06 2,06 (4.55) 3,27 (7.21) 6,62 (14.59) 07 2,23 (4.92) 3,52 (7.75) 7,05 (15.54) 08 2,40 (5.29) 3,77 (8.30) 7,48 (16.49) 09 2,57 (5.67) 4,01 (8.85) 7,92 (17.45) 10 2,74 (6.04) 4,26 (9.39) 8,35 (18.40) 11 2,91 (6.41) 4,51 (
42、9.94) 8,78 (19.35) 12 3,08 (6.79) 4,75 (10.48) 9,21 (20.30) 13 3,25 (7.16) 5,00 (11.02) 9,64 (21.25) 14 3,42 (7.54) 5,25 (11.57) 10,07 (22.20) 15 3,59 (7.91) 5,49 (12.11) 10,50 (23.15) 16 5,74 (12,65) 10,93 (24.10) 17 5,98 (13.19) 11,36 (25.05) 18 6,23 (13.73) 11,79 (26.00) 19 6,47 (14.27) 12,22 (26
43、.95) 20 6,72 (14.81) 12,66 (27.90) 21 6,96 (15.35) 13,09 (28.85) 22 7,21 (15.89) 13,52 (29.80) 23 7,45 (16.43) 13,95 (30.75) 24 7,70 (16.97) 14,38 (31.70) 25 7,94 (17.51) 14,81 (32.65) Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMAN
44、ot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 9 prEN 6129:2005Table 5 Material, finish and lubrication Material Finish Material/Finish code Sleeve Serrated Pin Locking collar Sleeve Serrated Pin Locking collarLubricationA-286 Cres per AMS 5737 or 316 Cres per
45、 AMS 5690 Passivated per AMS-QQ-P-35C A-286 Cres per AMS 5737 A-286 Cres per AMS 5737 Inconel per AMS 5687 See Table 6. Passivated per AMS-QQ-P-35 None aaWhen lubricated, pin and/or collar shall be lubricated per AS 5272 Type 1, MIL-PRF-46010 Type 1 or 3, MIL-L-87132 orDOD-L-85645, Manufacturers opt
46、ion. Table 6 Sleeve finish codes Code Material Finish P Passivated per AMS-QQ-P-35 H A-286 Cres Resin based aluminum pigment coating (Hi-Kote1) per EN 4473 4 Designation EXAMPLE Description block BLIND BOLT Identity block EN6129C05-02H Number of this standard Material code (see Table 5) Diameter cod
47、e (see Table 1) On diameter 05 code only substitute “” with “R” for reduced diameter drive anvil. See dimension “J” in Table 1 Grip length code (see Table 3) Sleeve Finish code (see Table 6) NOTE If necessary, the code I9005 shall be placed between the description block and the identity block. Copyr
48、ight 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 10 prEN 6129:20055 Marking Marking as per EN 2424 style B on rivet head (EN standard number, grip length code and manufacturers identification required). Instead of the EN standard number, the manufacturers material code or part number shall be
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