1、ASD STANDARD NORME ASD ASD NORM prEN 6120 Edition P 1 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: Descriptors: ENGLISH VERSION Aerospace ser
2、ies Pins, close tolerance, swage locking, protruding head, shear type, in aluminium alloy 7050, chemical film Inch series Srie arospatiale Rivets de prcision, boulon serti, tte protubrante, cisaillement-type, en alliage daluminium 7050, film sec Srie en inches Luft- und Raumfahrt Paniete fr Quetschv
3、erriegelung mit Universalkopf 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 Europe - Standardization). It is publishe
4、d 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 that interchangeability is affected, physi
5、cally 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 and transformation to full European Stand
6、ard (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 2006Comments should be sent within six months after th
7、e 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-,-,-prEN 6120:2006 2 Contents Page Foreword2 1
8、 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 votes carried out in accordance with the
9、 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 permitted without license from IHS-,-,-prEN
10、 6120:2006 3 1 Scope This standard specifies the characteristics of close tolerance pins, swage locking, protruding head, shear type, in aluminium alloy 7050-T73 with chemical film, inch series, with a maximum operating temperature of 80 C for aerospace application. Pins with diameter code 040 shall
11、 be used in combination with collars as per EN 6051 only. Pins with diameter code 050, 060 and 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 of this document. For dated references, on
12、ly 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 aluminium alloy 3003, chemical film Inch s
13、eries. 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, Chemical conversion coatings on aluminium and a
14、luminium 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, dimensions, tolerances and mass shall confo
15、rm 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, USA 3) Published by: Superintendent of Docum
16、ents, 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 6120:2006 4 Values apply before lubrication Key
17、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. Figure 1 Configuration, dimensions and tolerances Table 1 Dimensions and tolerances d1a b d2 d3 r l4 Diameter code min. max. 0,13
18、 max. 0,13 min. max. 040 4,140 4,153 6,35 3,96 0,97 1,22 050 4,801 4,813 7,47 4,67 1,19 1,45 060 5,530 5,542 8,51 5,41 1,37 1,63 080 6,325 6,337 9,55 6,20 0,51 1,55 1,80 aUnderfill permissible, but must be within d1when measured with a standard 6,35 mm diameter micrometer. bRequirement for shank str
19、aightness: Maximum 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 6120:2006 5 Table 2 Dimensions, tolerances and ma
20、ss Grip length 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
21、0,363 26,54 7,54 0,526 030 3,18 4,78 4,78 26,29 9,09 0,423 28,65 9,14 0,607 30,73 10,62 0,904 30,73 10,62 1,207 040 4,78 6,35 6,35 29,46 10,67 0,484 31,83 10,72 0,689 33,91 12,19 1,012 33,91 12,19 1,348 050 6,35 7,92 7,92 32,64 12,24 0,544 35,00 12,29 0,770 37,08 13,77 1,120 37,08 13,77 1,489 060 7,
22、92 9,53 9,53 35,81 13,84 0,605 38,18 13,89 0,851 40,26 15,37 1,228 40,26 15,37 1,630 070 9,53 11,13 11,13 38,99 15,44 0,665 41,35 15,49 0,933 43,43 16,97 1,335 43,43 16,97 1,771 080 11,13 12,70 12,70 42,16 17,02 0,726 44,53 17,07 1,014 46,61 18,54 1,443 46,61 18,54 1,912 090 12,70 14,27 14,27 45,34
23、18,59 0,786 47,70 18,64 1,095 49,78 20,12 1,551 49,78 20,12 2,053 100 14,27 15,88 15,88 48,51 20,19 0,847 50,88 20,24 1,177 52,96 21,72 1,659 52,96 21,72 2,194 110 15,88 17,46 17,46 56,13 23,29 1,767 56,13 23,29 2,335 120 17,46 19,05 19,05 59,31 24,89 1,875 59,31 24,89 2,476 130 19,05 20,64 20,64 62
24、,48 26,47 1,983 62,48 26,47 2,617 aDimension l1is 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 all
25、oy 7050-T73 as 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
26、with listed collar 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 net
27、working permitted without license from IHS-,-,-prEN 6120:2006 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 EN6120P04
28、0A040G Number of 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
29、 2424, style F 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 6120:2006 7 7 Example of install
30、ation See Figure 2. Key 1 Pin EN 6120 (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-,-,-
