AECMA PREN 6127-2006 Aerospace series Blind bolt 100 degrees reduced flush head high strength Edition P 2《航空航天系列.螺丝钉100度埋头钉高强度.P2版》.pdf

《AECMA PREN 6127-2006 Aerospace series Blind bolt 100 degrees reduced flush head high strength Edition P 2《航空航天系列.螺丝钉100度埋头钉高强度.P2版》.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 6127-2006 Aerospace series Blind bolt 100 degrees reduced flush head high strength Edition P 2《航空航天系列.螺丝钉100度埋头钉高强度.P2版》.pdf（12页珍藏版）》请在麦多课文档分享上搜索。

1、ASD STANDARD NORME ASD ASD NORM prEN 6127 Edition P 1 February 2006 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 + 32 2 763 3565 - www.asd-stan.orgICS: See foreword for superseded version Descr

2、iptors: ENGLISH VERSION Aerospace series Blind bolt, 100 reduced flush head, high strength Srie arospatiale Boulon aveugle tte fraise rduite 100 haute rsistance Luft- und Raumfahrt Blindniet 100 reduzierter Senkkopf, hochfest This “Aerospace Series“ Prestandard has been drawn up under the responsibi

3、lity 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 the publication of this pre-

4、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 draft European Standard (prE

5、N) 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 standards conflicting with

6、 the EN. Edition approved for publication 28 February 2006 Comments should 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 AEC

7、MA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 2 prEN 6127:2006Foreword 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 version of this standard. I

8、n order to solve the situation the ASD-STAN Board agreed to publish this version as Edition P2 and it is superseding the P1 version of prEN6127. Contents Page 1 Scope 3 2 Normative references. 3 3 Requirements 3 3.1 Configuration, dimensions and tolerances. 3 3.2 Grip range and weight. 3 3.3 Materia

9、l, finish and lubrication 3 4 Designation 8 5 Marking. 8 6 Technical specification 12 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 3 prEN 6127

10、:20061 Scope This standard specifies the configuration, dimension, tolerance and mass of a stainless steel blind bolt with 100 reduced flush head for aerospace application. 2 Normative references This European Standard incorporates by dated or undated reference provisions from other publications. Th

11、ese 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 by amendment or revision. For unda

12、ted references the latest edition of the publication referred to applies (including amendments). 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 p

13、rocurement 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 1

14、5Cr-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

15、, 1-hexadecanol, application to fasteners 3)NASM 8975, Fastener, blind, high strength, installation 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 to

16、lerances 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 Tables 5 and 6. 3.4 First oversize See Tables 7, 8 and 9. 1) Published as ASD Presta

17、ndard 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 Copyright Association Europeene des Constructeurs de Mate

18、riel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 4 prEN 6127:2006 Detail of serrated pin geometry: Detail A Detail A Optional configuration Key 1 Marking see clause 5 5 Locking collar 2 Serrated pin 6 Sh

19、ifting Anvil 3 Sleeve 7 Drive washer 4 Grip 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. Figure 1 Configuration - Dimensions Copyright Associ

20、ation 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 6127:2006 Key 1 Grip a Blind side head may be installed on 7 max slope Figure 2 Typical installation Table

21、 1 Dimensions and tolerances Dimensions in mm (inch) A B C H W D J aN Q D1 D2P b P2Theor. Ref. Diameter code Ref. max. Gage HT GageDia. 0,03( .001) 0,13( .005) 1,52( .060) 0,13( .005) max. max. max. min. 05 7,37 (.290) 1,32 (.052) 0,25 (.010) 0,58 0,51 (.023) (.020) 5,9465,941(.2341)(.2339)4,14 (.16

22、3) 9,53 (.375) 3,56 (.140) 1,70 (.067) 3,05 (.120) 2,16 (.085) 7,62(.300)5,66(.223)06 9,07 (.357) 1,65 (.065) 0,25 (.010) 0,76 0,69 (.030) (.027) 7,2167,210(.2841)(.2839)5,03 (.198) 9,53 (.375) 4,06 (.175) 2,21 (.087) 3,81 (.150) 2,79 (.110) 8,13(.320)6,86(.270)08 12,19 (.480) 2,31 (.091) 0,31 (.012

23、) 1,02 0,91 (.040) (.036) 9,7869,792(.3855)(.3853)6,58 (.259) 9,53 (.375) 4,83 (.190) 2,79 (.110) 4,83 (.190) 3,66 (.144) 9,4(.370)9,01(.355)R S J1J2X E C1C2F G min. Hole limits Diameter code max. max. 0,76( .030)Number ofserrations max. min. Ref. 0,05 ( .002) 5 5 min. max. 05 0,25 (.010) 5,89 (.232

24、) 20,32(.800) 18 1,52(.060)0,13(.005)0,33(0.013)0,81 (.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(0.013)0,81 (.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(0.013)0,81 (.032) 45 30 6,60(.260)6,

25、68(.263)aDiameter code 05 is also available with reduced diameter drive anvil/drive washer (7,92 0,13/.312 .005). See part number examples bThis length of D may be 0,05 mm (.002) undersize. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with A

26、ECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 6 prEN 6127:2006 Table 2 Static values Dimensions in kN (lbf) Installed strength Diameter code Single shear min. Tensile strength min. Tensile preload min. Spindle retention min. 05 8,807 (1 980) 4,671 (1 05

27、0) 0,467 (105) 2,335 (525) 06 13,011 (2 925) 6,673 (1 500) 0,667 (150) 3,336 (750) 08 22,242 (5 000) 11,566 (2 600) 1,157 (260) 5,783 (1 300) Table 3 Grip range Dimensions in mm (inch) Diameter code Under lap Grip range Over lap 05 06 08 L K L K L K Grip length code min. only 05 dia. min. 06 dia. to

28、 08 dia. min.max. max. 05 dia. to 08 dia. Ref. max. Ref. max. Ref. max. 02 - - a 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 (.236) 10,11(.398) 13,69(.539) 10,59(.417) 14,83 (.584) 12,17 (.479) 16,38(.645) 04 5,31

29、(.209) 5,16 (.203) 5,56 (.219) 7,16 (.282) 7,57 (.298) 11,68(.460) 15,29(.602) 12,19(.480) 16,43 (.647) 13,74 (.541) 17,98(.708) 05 6,88 (.271) 6,73 (.265) 7,14 (.281) 8,76 (.345) 9,17 (.361) 13,28(.523) 16,87(.664) 13,77(.542) 18,01 (.709) 15,34 (.604) 19,56(.770) 06 8,48 (.334) 8,33 (.328) 8,74 (.

30、344) 10,34 (.407) 10,74 (.423) 14,86(.585) 18,47(.727) 15,37(.605) 19,61 (.772) 16,92 (.666) 21,16(.833) 07 10,06 (.396) 9,91 (.390) 10,31 (.406) 11,94 (.470) 12,34 (.486) 16,46(.648) 20,04(.789) 16,94(.667) 21,18 (.834) 18,52 (.729) 22,73(.895) 08 11,66 (.459) 11,51 (.453) 11,91 (.469) 13,51 (.532)

31、 13,92 (.548) 18,03(.710) 21,64(.852) 18,54(.730) 22,78 (.897) 20,09 (.791) 24,33(.958) 09 13,23 (.521) 13,08 (.515) 13,49 (.531) 15,11 (.595) 15,52 (.611) 19,63(.773) 23,22(.914) 20,12(.792) 24,36 (.959) 21,69 (.854) 25,91(1.020) 10 14,83 (.584) 14.68 (.578) 15,09 (.594) 16,69 (.657) 17,09 (.673) 2

32、1,21(.835) 24,82(.977) 21,72(.855) 25,96 (1.022) 23,27 (.916) 27,51(1.083) 11 16,41 (.646) 16,26 (.640) 16,66 (.656) 18,29 (.720) 18,69 (.736) 22,81(.898) 26,391(1.039) 23,29(.917) 27,53 (1.084) 24,87 (.979) 29,08(1.145) 12 18,01 (.709) 17,86 (.703) 18,26 (.719) 19,86 (.782) 20,27 (.798) 24,38(.960)

33、 27,99(1.102) 24,89(.980) 29,13 (1.147) 26,44 (1.041) 30,68(1.208) 13 19,58 (.771) 19,43 (.765) 19,84 (.781) 21,46 (.845) 21,87 (.861) 25,98(1.023) 29,57(1.164) 26,47(1.042) 30,71 (1.209) 28,04 (1.104) 32,28(1.271) 14 21,18 (.834) 21,03 (.828) 21,44 (.844) 23,04 (.907) 23,44 (.923) 27,56(1.085) 31,1

34、7(1.227) 28,067(1.105) 32,31 (1.272) 29,62 (1.166) 33,86(1.333) 15 22,76 (.896) 22,61 (.89) 23,01 (.906) 24,64 (.970) 25,04 (.986) 29,16(1.148) 32,74(1.289) 29,64(1.167) 33,88 (1.334) 31,22 (1.229) 35,46(1.396) 16 24,36 (.959) 24,21 (.953) 24,61 (.969) 26,21 (1.032) 26,62 (1,048) 30,73(1.210) 34,34(

35、1.352) 31,24(1.230) 35,48 (1.397) 32,79 (1.291) 37,03(1.458) 17 25,86 (1.018) 26,19 (1.031) 27,81 (1.095) 28,22 (1.111) 32,82(1.292) 37,06 (1.459) 34,39 (1.354) 38,63(1.521) 18 27,38 (1.078) 27,79 (1.094) 29,39 (1.157) 29,79 (1.173) 34,42(1.355) 38,66 (1.522) 35,97 (1.416) 40,21(1.583) 19 28,98 (1.1

36、41) 29,36 (1.156) 30,99 (1.220) 31,39 (1.236) 35,99(1.417) 40,23 (1.584) 37,57 (1.479) 41,81(1.646) 20 30,56 (1.203) 30,96 (1.219) 32,56 (1.282) 32,97 (1.298) 37,59(1.480) 41,83 (1.647) 39,14 (1.541) 43,38(1.708) aMinimum grip length for diameter code 05 is 2,39 mm (.094) and for diameter code 06 is

37、 3,05 mm (.120). b No underlap for diameter code 08. 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 7 prEN 6127:2006 Table 4 Mass Weight in kg (

38、lbs)/1 000 pieces Diameter code Grip length code 05 06 08 02 1,01 (2.23) 1,66 (3.65) 03 1,16 (2.56) 1,85 (4.07) 3,91 (8.62) 04 1,33 (2.94) 2,10 (4.62) 4,33 (9.55) 05 1,50 (3.31) 2,35 (5.17) 4,75 (10.48) 06 1,67 (3.68) 2,59 (5.71) 5,18 (11.41) 07 1,84 (4.06) 2,84 (6.26) 5,60 (12.35) 08 2,01 (4.43) 3,

39、09 (6.81) 6,02 (13.28) 09 2,18 (4.80) 3,33 (7.35) 6,45 (14.21) 10 2,35 (5.18) 3,58 (7.90) 6,88 (15.14) 11 2,52 (5.55) 3,83 (8.44) 7,07 (16.07) 12 2,69 (5.93) 4,08 (8.99) 7,71 (17.00) 13 2,86 (6.31) 4,32 (9.54) 8,13 (17.93) 14 3,04 (6.69) 4,58 (10.09) 8,56 (18.86) 15 3,21 (7.07) 4,83 (10.64) 8,98 (19

40、.79) 16 3,38 (7.45) 5,08 (11.19) 9,40 (20.72) 17 5,33 (11.74) 9,82 (21.65) 18 5,58 (12.29) 10,24 (22.58) 19 5,82 (12.84) 10,66 (23.51) 20 6,07 (13.39) 11,09 (24.44) Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo rep

41、roduction or networking permitted without license from IHS-,-,-Page 8 prEN 6127:2006Table 5 Material, finish and lubrication Material Finish Material/Finish code Sleeve Stem Locking collar Sleeve Stem Locking collar LubricationA-286 Cres per AMS 5737, or 316 Cres per AMS 5690 Passivated per AMS-QQ-P

42、-35 C A-286 Cres per AMS 5737 A-286 Cres per AMS 5737 Inconel per AMS 5687 See Table 6. Passivated per AMS-QQ-P-35None aaIf lubricated pin and/or collar shall be lubricated per AS 5272 Type 1, MIL-PRF-46010 Type 1 or 3, MIL-L-87132 or DOD-L-85645, Manufacturers option. Table 6 Sleeve finish codes Co

43、de Material Finish P Passivated per AMS-QQ-P-35 H A-286 Cres Resin based aluminium pigment coating (Hi-Kote1) per EN 4473 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 Gage Dia. 0,03( .0

44、01) 0,13( .005) 1,52( .060) 0,13( .005) max. max. max. min. 05 7,37 (.290) 1,32 (.052) 0,25 (.010) 0,323 0,274 (.0127) (.0108) 6,500 (.2559) 4,55 (.179) 9,53 (.375) 3,56 (.140) 1,70 (.067) 3,05 (.120) 2,16 (.085) 8,00 (.315) 6,05(.238)06 9,07 (.357) 1,65 (.065) 0,25 (.010) 0,333 0,381 (.0131) (.0150

45、) 8,059 (.3173) 5,44 (.214) 9,53 (.375) 4,06 (.160) 2,21 (.087) 3,81 (.150) 2,79 (.110) 8,51 (.335) 7,24(.285)08 12,19 (.480) 2,31 (.091) 0,31 (.012) 0,498 0,447 (.0196) (.0176) 10,970 (.4319) 6,99 (.275) 9,53 (.375) 4,83 (.190) 2,79 (.110) 4,83 (.190) 3,66 (.144) 9,78 (.385) 9,27(.365)Copyright Ass

46、ociation 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 9 prEN 6127:2006 R S J1J2X E C1C2F G min. Hole limits Diameter code max. Ref. 0,76( .030)Number of serrations

47、0,76( .030)min. Ref. 0,05 ( .002) 5 5 min. max. 05 0,25 (.010) 6,27 (.247) 20,32(.800) 18 1,52 (.060) 0,13(.005)0,33(.013)0,81 (.032) 45 304,57(.180)4,65(.183)06 0,38 (.015) 7,80 (.307) 21,08(.830) 19 1,78 (.070) 0,13(.005)0,33(.013)0,81 (.032) 45 305,46(.215)5,54(.218)08 0,51 (.020) 9,55 (.376) 24,

48、77(.975) 20 2,29 (.090) 0,13(.005)0,33(.013)0,81 (.032) 45 307,01(.276)7,09(.279)aFirst oversize does not available with reduced diameter drive washer. bIn the length P of D may be 0,051 mm (.002) undersize 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 10 prEN 6127:2006Tab