1、ASD STANDARD NORME ASD ASD NORM prEN 6100 Edition P 2 December 2006 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONGulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: Supersedes edition P 1 February 2001 Descr
2、iptors: ENGLISH VERSION Aerospace series Pins, close tolerance, swage locking, 100 countersunk head, shear type, in aluminium alloy 7050, chemical film Inch series Srie arospatiale Rivets de prcision, boulon serti, tte fraise 100, cisaillement-type, en alliage daluminium 7050, film sec Srie en inche
3、s Luft- und Raumfahrt Paniete fr Quetschverriegelung mit Senkkopf 100 fr Scherbeanspruchung, aus Aluminiumlegierung 7050, Schmierfilm behandelt Inch-Reihe This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of E
4、urope - 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 Prestandard, the technical content shall not be changed to an extent th
5、at 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 formal vote a
6、nd 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 31 December 2006 Comments
7、should be sent within six months after the date of publication to ASD-STAN Mechanical Domain Copyright 2006 by ASD-STAN Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-p
8、rEN 6100:20062 Contents Page Foreword2 1 Scope 3 2 Normative references 3 3 Requirements.3 4 Designation 6 5 Marking .6 6 Technical specification .6 7 Example of installation7 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Mechanical Domain. After inquiries and
9、votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Process Manual, this standard has received approval for Publication. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking per
10、mitted without license from IHS-,-,-prEN 6100:20063 1 Scope This standard specifies the characteristics of close tolerance pins, swage locking, 100 countersunk head, shear type, in aluminium alloy 7050-T73 with chemical film, inch series, with a maximum operating temperature of 80 C for aerospace ap
11、plication. Pins with diameter code 040 shall be used in combination with collars as per EN 6051 only. Pins with diameter code 050, 060 or 080 shall be used in combination with collars as per EN 6054 only. 2 Normative references The following referenced documents are indispensable for the application
12、 of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2424, Aerospace series Marking of aerospace products. EN 6051, Aerospace series Collars, swage locking, shear type, in
13、 aluminium alloy 3003, chemical film Inch series. 1)EN 6052, Aerospace series Rivets Collar System in aluminium alloy shear type inch series Technical specification. 1)EN 6054, Aerospace series Collars, swage locking, shear type, in aluminium alloy 6061, chemical film Inch series. 1)MIL-C-5541, Chem
14、ical conversion coatings on aluminium and aluminium alloys. 2)MIL-L-87132, Lubricant, cetyl alcohol, 1-hexadecanol, application to fasteners. 2)QQ-A-430, Aluminium alloy rod and wire, for rivets and cold heading. 3)3 Requirements 3.1 Configuration, dimensions, tolerances and mass The configuration,
15、dimensions, tolerances and mass shall conform to Figure 1 and Tables 1, 2 and 5. Dimensions and tolerances are expressed in millimetres. 1) Published as ASD Prestandard at the date of publication of this standard. 2) Published by: Department of Defense (DoD), the Pentagon, Washington, D.C., 20301, U
16、SA 3) Published by: Superintendent of Documents, U.S. Government Printing Office, Washington, D.C., 20402, USA Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 6100:
17、2006 4 Values apply before lubrication Key 2 Predetermined breaking point 1 Sealant escape groove: Code letter G. Form of sealant escape groove straight or diagonal at manufacturers option 3 Marking, see Clause 5. aTheoretical intersection of head face and head angle Figure 1 Configuration, dimensio
18、ns and tolerances Table 1 Dimensions and tolerances d1a bd2d3d4d5c1 c2 k r Diameter code f7 min. max. theor. 0,003 min. max. max. theor. min. max. 4,140 040 4,153 6,604 3,962 7,049 5,149 0,757 0,838 0,254 1,219 0,381 0,635 4,801 050 4,813 7,442 4,674 8,189 6,198 0,795 0,876 0,381 1,420 0,508 0,762 5
19、,530 060 5,542 8,687 5,410 9,436 7,572 0,742 0,823 0,381 1,636 0,508 0,762 6,325 080 6,337 10,008 6,198 10,754 8,418 0,940 1,021 0,381 1,857 0,508 0,762 aUnderfill permissible, but must be within d1when measured with a standard 6,35 mm diameter micrometer. bRequirement for shank straightness: Maximu
20、m deviation of 0,004 mm / mm of pin length. 3,2 0,8 Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 6100:2006 5 Table 2 Dimensions, tolerances and mass Grip length
21、Diameter code 040 Diameter code 050 Diameter code 060 Diameter code 080 l1 al2l3Massbl2l3Massbl2l3Massbl2l3MassbGrip length code min. max. 0,127 + 1,5 0 0,254kg/1000 pieces + 1,50 0,254kg/1000 pieces + 1,50 0,254 kg/1000 pieces + 1,50 0,254kg/1000 pieces 020 1,60 3,18 3,18 24,69 7,49 0,281 26,54 7,5
22、4 0,373 030 3,18 4,78 4,78 26,29 9,09 0,320 28,65 9,14 0,484 30,73 10,62 0,777 30,73 10,62 1,035 040 4,78 6,35 6,35 29,46 10,67 0,377 31,83 10,72 0,564 33,91 12,19 0,885 33,91 12,19 1,176 050 6,35 7,92 7,92 32,64 12,24 0,441 35,00 12,29 0,643 37,08 13,77 0,993 37,08 13,77 1,317 060 7,92 9,53 9,53 35
23、,81 13,84 0,503 38,18 13,89 0,723 40,26 15,37 1,101 40,26 15,37 1,458 070 9,53 11,13 11,13 38,99 15,44 0,565 41,35 15,49 0,803 43,43 16,97 1,209 43,43 16,97 1,599 080 11,13 12,70 12,70 42,16 17,02 0,627 44,53 17,07 0,883 46,61 18,54 1,316 46,61 18,54 1,740 090 12,70 14,27 14,27 45,34 18,59 0,689 47,
24、70 18,64 0,963 49,78 20,12 1,424 49,78 20,12 1,881 100 14,27 15,88 15,88 48,51 20,19 0,751 50,88 20,24 1,043 52,96 21,72 1,532 52,96 21,72 2,022 110 15,88 17,46 17,46 56,13 23,29 1,640 56,13 23,29 2,163 120 17,46 19,05 19,05 59,31 24,89 1,748 59,31 24,89 2,305 130 19,05 20,64 20,64 62,48 26,47 1,856
25、 62,48 26,47 2,446 aDimension I1is measured up to the end of full cylindrical portion of shank bInstalled mass without collar 3.2 Material and surface treatment See Table 3. Table 3 Material and surface treatment Code Material Shear strength Surface treatment Lubricant A Aluminium alloy 7050-T73 as
26、per QQ-A-430 283 MPa 324 MPa Chemical film per MlL-C-5541 class 1A (gold chromate) Cetyl alcohol lubrication per MIL-L-87132, grade B 3.3 Mechanical properties See Table 4. Table 4 Mechanical properties Diameter code Min. double shear Collar part number Min. ultimate tensile strength with listed col
27、lar Min. preload kN kN kN 040 7,62 EN 6051040A 2,20 1,00 050 10,23 EN 6054050A 3,34 1,45 060 13,58 EN 6054060A 5,50 2,75 080 17,77 EN 6054080A 6,68 3,34 Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitt
28、ed without license from IHS-,-,-prEN 6100:2006 6 3.4 Pin version See Table 5. Table 5 Pin version Code Pin version G With sealant escape groove (see Figure 1) P With pintail, “Pull-type” (see Figure 1) 4 Designation EXAMPLE Description block PIN, SWAGE LOCKING Identity block EN6100P040A040G Number o
29、f this standard Pin version (see Table 5) Diameter code (see Table 1) Surface treatment (see Table 3) Grip length code (see Table 2) Sealant escape groove (see Table 5) NOTE If necessary, the code I9005 shall be placed between the description block and the identity block. 5 Marking EN 2424, style F
30、or P, depressed 0,15 mm max. depth. 6 Technical specification EN 6052 Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 6100:20067 7 Example of installation See Figur
31、e 2. Key 1 Pin EN 6100 (installed condition) 2 Collar EN 6051 or EN 6054 (installed condition) Figure 2 Example of installation 1 2 Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-
