AECMA PREN 6122-2005 Aerospace series Blind bolt 130 degrees flush head high strength preferable in composite application Edition P 1《航空航天系列.螺丝钉130度埋头钉高强度混合物应用.P1版》.pdf

1、ASD STANDARD NORME ASD ASD NORM prEN 6122 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, 130 flush head, high strength, preferable in composite application Srie arospatiale Boulon aveugle, tte fraise 130, haute rsistance, utilisation prfrable pour matriaux composites Luft- und Raumfahrt Blindbolzen, 130 Senkkopf, hochfest, Anwendung vorzugsweise in Verbundwerkstoff This

3、“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 Industry. It has been technically approved by the experts of the concerned Domain

4、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-identification of the standard. After examination and review by users and formal agreemen

5、t 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 to implement the EN at national level by giving the EN the status of a nationa

6、l 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 Domain Copyright 2005 by ASD-STAN Copyright Association Europeene des Constru

7、cteurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 2 prEN 6122:2005Contents Page 1 Scope 3 2 Normative references3 3 Requirements.3 3.1 Configuration, dimensions and tolerances.3 3.2 Grip rang

8、e and mass.3 3.3 Material, finish and lubrication.3 4 Designation 12 5 Marking .12 6 Technical specification .12 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license fro

9、m IHS-,-,-Page 3 prEN 6122:20051 Scope This standard specifies the configuration, dimension, tolerances and mass of a stainless steel and titanium blind bolt with protruding head for aerospace application. 2 Normative references This European Standard incorporates by dated or undated reference provi

10、sions from other publications. These normative references are cited at the appropriate places in the text and the publications 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 b

11、y amendment or revision. For undated references the latest edition of the publication referred to applies (including amendments). ISO 8080, Aerospace Anodic treatment of titanium and titanium alloys sulfuric acid process EN 2424, Aerospace series Marking of aerospace products EN 4473, Aerospace seri

12、es Aluminium pigmented coatings Technical specification 1)AS 5272, Lubricant, solid film, heat cured, corrosion inhibiting procurement 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

13、-2,5Mo (SAE 30316) solution heat treated 2)AMS 5737, Steel, corrosion and heat-resistant, bars, wire, forgings, and tubing 15Cr-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-resi

14、stant steel 2)MIL-PRF-46010, Lubricant, solid film, heat cured, corrosion inhibiting 3)MIL-L-87132, Lubricant, cetyl alcohol, 1-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, ins

15、tallation formed corrosion resistant steel, heat resistant steel and titanium General specification for 3)DOD-L-85645, Lubricant, dry film, molecular bonded 3)3 Requirements 3.1 Configuration, dimensions and tolerances The configuration, dimensions, tolerances, static and dynamic values shall confor

16、m 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 Tables 5 and 6. 3.4 First oversize See Tables 7, 8 and 9. 1) Published as AECMA Prestandard at the date of publication of this standard2) Published by: Society of Automotive

17、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 by: American Society for Testing and Materials (ASTM), 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959, USA Copyright Associ

18、ation Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 4 prEN 6122:2005Detail of serrated pin geometry: Detail A Detail A Optional configuration Key 1 Marking see clause

19、 5 5 Crown Height 2 Serrated pin 6 Locking collar 3 Sleeve 7 Shifting Anvil 4 Grip 8 Drive washer a Diameter of pin head shall not exceed “ D” max. b Fasteners are supplied with shifting anvil/drive washer of manufacturers option. The shifting anvil/drive washer is not part of the installed fastener

20、. Figure 1 Configuration Dimensions 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 5 prEN 6122:2005Key 1 Marking see clause 5 a Blind side head m

21、ay be installed on 7 max slope. Figure 2 Typical installation Table 1 Dimensions and tolerances for Cres and Titanium Dimensions in mm (inch) A1A2B H W D J aN Q D1 D2P b P2Theor. Diameter code Ref. min. Ref. Gage HT GageDia. 0,03( .001) 0,13( .005) 1,52( .060) 0,13( .005) max. max. max. min. 05 8,43

22、 (.332) 7,52 (.296) 0,99 (.039) 0,48 0,38 (.0188) (.0148) 7,1937,188(.2832)(.2830)4,14 (.163) 9,53 (.375) 3,56 (.140) 1,70 (.067) 3,05 (.120) 2,16 (.085) 7,63(.300)5,66(.223)06 9,80 (.386) 8,81 (.347) 1,09 (.043) 0,49 0,39 (.0192) (.0152) 8,3118,306(.3272)(.3270)5,03 (.198) 9,53 (.375) 4,06 (.160) 2

23、,21 (.087) 3,81 (.150) 2,79 (.110) 8,13(.320)6,86(.270)08 12,88 (.507) 11,76 (.463) 1,45 (.057) 0,60 0,50 (.0237) (.0197) 10,97310,968(.4320)(.4318)6,58 (.259) 9,53 (.375) 4,83 (.190) 2,79 (.110) 4,83 (.190) 3,66 (.144) 9,50(.370)9,01(.355)R S J1 J2 X E C1 C2 F G min. Hole limits Diameter code max.

24、Ref. 0,76 ( .030) Number of serrations 0,76( .030) min. Ref. 0,05 ( .002) 5 5 min. max. 05 0,64 (.025) 5,89 (.232) 20,32 (.800) 18 1,52 (.060) 0,13(.005) 0,33(.013) 0,81 (.032) 45 30 4,17(.164) 4,24(.167)06 0,64 (.025) 7,42 (.292) 21,08 (.830) 19 1,78 (.070) 0,13(.005) 0,33(.013) 0,81 (.032) 45 30 5

25、,06(.199) 5,13(.202)08 0,76 (.030) 9,17 (.361) 24,77 (.975) 20 2,29 (.090) 0,13(.005) 0,33(.013) 0,81 (.032) 45 30 6,60(.260) 6,68(.263)aDiameter code 05 is also available with reduced diameter shifting anvil/drive washer (7,90,13 /.312.005). See part number examplesbIn the length P of D may be 0,05

26、1 mm (.002) undersize 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 6 prEN 6122:2005Table 2 Static values (installed strength) for Cres and Tita

27、nium Dimensions in kN (lbf) Installed strength Single shear min. Tensile strength min. Tensile preload min. Spindle retention min. Diameter code Cres Titan. Cres Titan. Cres Titan. Cres Titan. 05 8,807 (1 980) 8,807 (1 980) 4,671 (1 050) 3,603 (810) 0,467 (105) 0,544 (121) 2,335 (525) 1,826 (410) 06

28、 13,011 (2 925) 13,011 (2 925) 6,673 (1 500) 5,605 (1 260) 0,667 (150) 0,841 (189) 3,336 (750) 2,804 (630) 08 22,242 (5 000) 22,242 (5 000) 11,566 (2 600) 8,407 (1 890) 1,157 (260) 1,261 (284) 5,783 (1 300) 4,205 (945) Table 3 Grip range Dimensions in mm (inch) Diameter code Under lap Grip range Ove

29、r lap 05 06 08 L K L K L K Grip length code min. only 05 dia. min. 06 dia. to 08 dia. min. max. max. 05 dia. to 08 dia. Ref. max. Ref. max. Ref. max. 02 2,39 a(.094) 3,99 (.157) 4,39 (.173) 8,53 (.336) 12,09(.476) 9,02 (.355) 13,23 (.521) 03 3,71 (.146) 3,56 b(.140) 3,96 (.156) 5,59 (.220) 5,99 (.23

30、6) 10,11(.398) 13,69(.539) 10,59(.417) 14,81 (.583) 12,17 (.479) 16,38(.645) 04 5,31 (.209) 5,16 (.203) 5,56 (.219) 7,16 (.282) 7,57 (.298) 11,68(.460) 15,29(.602) 12,19(.480) 16,41 (.646) 13,74 (.541) 17,96(.707) 05 6,89 (.271) 6,73 (.265) 7,14 (.281) 8,76 (.345) 9,17 (.361) 13,28(.523) 16,87(.664)

31、 13,77(.542) 17,98 (.708) 15,34 (.604) 19,56(.770) 06 8,48 (.334) 8.33 (.328) 8,74 (.344) 10,34 (.407) 10,74 (.423) 14,86(.585) 18,47(.727) 15,37(.605) 19,58 (.771) 16,92 (.666) 21,13(.832) 07 10,06 (.396) 9,91 (.39) 10,31 (.406) 11,94 (.470) 12,34 (.486) 16,46(.648) 20,04(.789) 16,94(.667) 21,16 (.

32、833) 18,52 (.729) 22,73(.895) 08 11,66 (.459) 11,51 (.453) 11,91 (.469) 13,51 (.532) 13,92 (.548) 18,03(.710) 21,64(.852) 18,54(.730) 22,76 (.896) 20,09 (.791) 24,31(.957) 09 13,23 (.521) 13,08 (.515) 13,49 (.531) 15,11 (.595) 15,51 (.611) 19,63(.773) 23,22(.914) 20,12(.792) 24,33 (.958) 21,69 (.854

33、) 25,91(1.020) 10 14,83 (.584) 14,68 (.578) 15,09 (.594) 16,69 (.657) 17,09 (.673) 21,21(.835) 24,82(.977) 21,72(.855) 25,93 (1.021) 23,27 (.916) 27,48(1.082) 11 16,41 (.646) 16,26 (.64) 16,66 (.656) 18,29 (.720) 18,69 (.736) 22,81(.898) 26,39(1.039) 23,29(.917) 27,51 (1.083) 24,87 (.979) 29,08(1.14

34、5) 12 18,01 (.709) 17,86 (.703) 18,26 (.719) 19,86 (.782) 20,27 (.798) 24,38(.960) 27,99(1.102) 24,89(.980) 29,11 (1.146) 26,44 (1.041) 30,658(1.207) 13 19,58 (.771) 19,43 (.765) 19,84 (.781) 21,46 (.845) 21,86 (.861) 25,98(1.023) 29,57(1.164) 26,47(1.042) 30,68 (1.208) 28,04 (1.104) 32,26(1.270) 14

35、 21,18 (.834) 21,03 (.828) 21,44 (.844) 23,04 (.907) 23,44 (.923) 27,56(1.085) 32,44(1.227) 28,07(1.105) 32,28 (1.271) 29,62 (1.166) 33,83(1.332) 15 22,76 (.896) 22,61 (.890) 23,01 (.906) 24,64 (.970) 25,04 (.986) 29,16(1.148) 32,74(1.289) 29,64(1.167) 33,86 (1.333) 31,22 (1.229) 35,43(1.395) 16 24,

36、36 (.959) 24,21 (.953) 24,61 (.969) 26,21 (1.032) 26,62 (1.048) 30,73(1.210) 34,34(1.352) 31,24(1.230) 35,46 (1.396) 32,79 (1.291) 37,01(1.457) 17 25,78 (1.015) 26,19 (1.031 27,81 (1.095) 28,22 (1.111) 34,39 (1.354) 38,61(1.520) 18 27,38 (1.078) 27,79 (1.094) 29,39 (1.157) 29,79 (1.173) 35,97 (1.416

37、) 40,18(1.582) 19 28,96 (1.14) 29,36 (1.156) 30,99 (1.22) 31,39 (1.236) 37,57 (1.479) 41,78(1.645) 20 30,56 (1.203) 30,96 (1.219) 32,56 (1.282) 32,97 (1.298) 39,14 (1.541) 43,36(1.707) aMinimum grip for 06 dia is 3,048 (.120). bUnderlap grip for 06 dia. is 3,556 (.140) and for 08 dia. is none. Copyr

38、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 7 prEN 6122:2005 Table 4 Mass Mass in kg (lbs)/1 000 pieces Diameter code 05 06 08 Grip length code Tit

39、anium Cres Titanium Cres Titanium Cres 02 0,63 (1.39) 1,04 (2.29) 1,02 (2.25) 1,67 (3.69) 03 0,72 (1.59) 1,20 (2.64) 1,13 (2.48) 1,86 (4.09) 2,31 (5.10) 3,79 (8.36) 04 0,83 (1.82) 1,37 (3.01) 1,28 (2.81) 2,11 (4.64) 2,36 (5.65) 4,21 (9.28) 05 0,93 (2.04) 1,53 (3.38) 1,42 (3.13) 2,35 (5.18) 2,81 (6.2

40、0) 4,63 (10.21) 06 1,03 (2.26) 1,71 (3.76) 1,57 (3.45) 2,60 (5.73) 3,06 (6.75) 5,05 (11.14) 07 1,13 (2.48) 1,87 (4.13) 1,72 (3.78) 2,84 (6.27) 3,31 (7.30) 5,48 (12.08) 08 1,23 (2.70) 2,04 (4.50) 1,86 (4.10) 3,09 (6.82) 3,56 (7.85) 5,90 (13.01) 09 1,33 (2.92) 2,21 (4.88) 2,01 (4.42) 3,34 (7.37) 3,82

41、(8.41) 6,32 (13.94) 10 1,42 (3.14) 2,38 (5.25) 2,16 (4.75) 3,59 (7.91) 4,06 (8.96) 6,75 (14.87) 11 1,52 (3.36) 2,55 (5.62) 2,30 (5.07) 3,83 (8.46) 4,31 (9.51) 7,17 (15.80) 12 1,62 (3.58) 2,72 (6.00) 2,45 (5.39) 4,09 (9.01) 4,56 (10.06) 7,59 (16.74) 13 2,89 (6.37) 2,59 (5.71) 4,33 (9.55) 4,81 (10.61)

42、 8,02 (17.67) 14 3,06 (6.74) 2,74 (6.03) 4,58 (10.10) 5,06 (11.16) 8,44 (18.60) 15 3,23 (7.12) 2,88 (6.35) 5,08 (11.19) 5,31 (11.71) 8,86 (19.53) 16 3,40 (7.49) 5,32 (11.73) 5,56 (12.26) 9,28 (20.76) 17 9,84 (21.69) 18 10,26 (22.62) 19 10,68 (23.55) 20 11,10 (24.48) Copyright Association Europeene d

43、es Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 8 prEN 6122:2005Table 5 Material, finish and lubrication Material Finish Material/Finish code Sleeve Stem Locking collar Sleeve Ste

44、m Locking collar LubricationA-286 Cres per AMS 5737 or 316 Cres per AMS 5690 Passivated per AMS-QQ-P-35 C A-286 Cres per AMS 5737 A-286 Cres per AMS 5737 Inconel per AMS 5687 Passivated per AMS-QQ-P-35None A-286 Cres per AMS 5737 or 316 Cres per AMS 5690 Passivated per AMS-QQ-P-35 T CP Titanium per

45、ASTM B 348Gr.138-6-44 Titanium per AMS 4957 Inconel per AMS 5687 See Table 6. None 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 option. Table 6 Sleeve finish codes Code Material Finish P A-286 Cr

46、es Passivated per AMS-QQ-P-35 CP Titanium None A CP Titanium Blue Anodize per ISO 8080 H CP Titanium or A-286 Cres Resin based aluminum pigment coating (Hi-Kote1) per EN 4473 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for Res

47、aleNo reproduction or networking permitted without license from IHS-,-,-Page 9 prEN 6122:2005 Table 7 First oversize “X“ Dimensions and tolerances for Cres Dimensions in mm (inch) A1A2B H W D J aN Q D1 D2P b P2Theor. Diameter code Ref. min. Ref. Gage HT GageDia. 0,03( .001) 0,13( .005) 1,52( .060) 0

48、,13( .005) max. max. max. min. 05 8,43 (.332) 7,52 (.296) 0,91 (.036) 0,478 0,376 (.0188) (.0148) 7,1937,188(.2832)(.2830)4,55 (.179) 9,53 (.375) 3,56 (.140) 1,70 (.067) 3,05 (.120) 2,16 (.085) 8,00(.315)6,15(.242)06 9,80 (.386) 8,81 (.347) 1,02 (.040) 0,488 0,386 (.0192) (.0152) 8,3118,306(.3272)(.3270)5,44 (.214) 9,53 (.375) 4,06 (.160) 2,21 (.087) 3,81 (.150) 2,79 (.110) 8,51(.335)7,34(.289)08