1、ASD STANDARD NORME ASD ASD NORM prEN 6054 Edition P 4 May 2007 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONAvenue de Tervuren, 270 - B-1150 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: Supersedes edition P 3 October 2006 D
2、escriptors: ENGLISH VERSION Aerospace series Collars, swage locking, shear type, in aluminium alloy 6061, chemical film Inch series Srie arospatiale Bagues, cisaillement-type, en alliage daluminium 6061, film sec Srie en inches Luft- und Raumfahrt Schlieringe fr Scherbeanspruchung, aus Aluminiumlegi
3、erung 6061, 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 published for the needs of the European Aerospace Industry. It has been techni
4、cally 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, physically or functionally, without re-identification of the standard. Afte
5、r 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 Standard (EN). The CEN national members have then to implement the EN at na
6、tional 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 May 2007 Comments should be sent within six months after the date of publication to ASD-STAN Mechanical Domain Copyright 2007 by ASD-
7、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 6054:20072 Contents Page Foreword2 1 Scope 3 2 Normative references 3 3 Requirements.4 4 Designation 5 5 Markin
8、g .5 6 Technical specification .5 7 Example of installation6 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 rules of ASD-STAN defined in ASD-STANs General Process Manual, this standa
9、rd 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 6054:20073 1 Scope This standard specifies the characteristics of a collar
10、, swage locking, shear type, in aluminium alloy 6061-T7, with a maximum operating temperature of 80 C for aerospace application. This collar shall be used with pins as per EN 6050, EN 6100 or EN 6120. 2 Normative references The following referenced documents are indispensable for the application of
11、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 6050, Aerospace series Pins, close tolerance, swage locking, 100
12、countersunk head reduced, shear type, in aluminium alloy 7050, chemical film Inch series. 1)EN 6052, Aerospace series Rivets Collar System in aluminium alloy shear type inch series Technical specification. 1)EN 6100, Aerospace series Pins, close tolerance, swage locking, 100 countersunk head, shear
13、type, in aluminium alloy 7050, chemical film Inch series. 1)EN 6120, Aerospace series Pins, close tolerance, swage locking, protruding head, shear type, in aluminium alloy 7050, chemical film Inch series. 1)AS87132, Lubricant, cetyl alcohol, 1-hexadecanol, application to fasteners.2)MIL-DTL-5541F, C
14、hemical conversion coatings on aluminium and aluminium alloys. 3)QQ-A-430, Aluminium alloy rod and wire, for rivets and cold heading. 4)1) Published as ASD Prestandard at the date of publication of this standard. 2) Published by: Society of Automotive Engineers, Inc. (SAE), 400 Commonwealth Drive, W
15、arendale, PA15096-001 USA. 3) Published by: Department of Defense (DoD), the Pentagon, Washington, D.C., 20301, USA. 4) Published by: Superintendent of Documents, U.S. Government Printing Office, Washington, D.C., 20402, USA. Copyright European Association of Aerospace Industries Provided by IHS und
16、er license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 6054:20074 3 Requirements 3.1 Configuration, dimensions, tolerances and mass The configuration, dimensions, tolerances and mass shall conform with Figure 1 and Tables 1 and 2. Dimensions and
17、 tolerances are expressed in millimetres. Values apply before lubrification 0,8Values apply before lubricationMarking (see clause 5)1)2)3)h1h2h3 d5 d3 d2 d1 d4 0,251) r 1,0 max. or underfill2) Punchout burr permitted within limits of d4 and h2 (one end only)3) Permissible circular burr or offset d5
18、max. (one end only)20RefFigure 1 Configuration, dimensions and tolerances 3.2 Material and surface treatment See Table 1. Table 1 Material and surface treatment Code Material Heat treatment Hardness Surface treatment Lubricant A Aluminium alloy 6061T7 in accordance with chemical composition of QQ-A-
19、430 521 C - 532 C for 35 - 45 minutes Aging treatment: 210 C - 221 C for 115 - 125 minutes 47 to 57 Rockwell 30T (86 to 111 Vickers 15 KgF) Chemical film per MIL-DTL-5541F class 1A (gold chromate) plus green dye Cetyl alcohol lubrication per AS87132, grade B 0,82 b 1 c a Key 1 20 Ref. 2 Marking (see
20、 Clause 5) ar 1,0 max. or underfill bPunchout burr permitted within limits of d4and h2(one end only) cPermissible circular burr or offset d5max. (one end only) Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking
21、permitted without license from IHS-,-,-prEN 6054:20075 Table 2 Dimensions, tolerances and mass d1d2d3d4d5h1h2h3Diameter code 0,05 max. min. max. min. max. 0,25 max. Ref. Mass kg/1 000 pieces 050 4,83 5,38 6,76 6,80 4,70 6,88 5,72 0,41 1,65 0,26 060 5,51 6,02 7,88 7,97 5,38 8,07 7,19 0,41 1,78 0,46 0
22、80 6,32 7,11 8,84 8,94 6,22 9,19 7,19 0,41 1,78 0,56 4 Designation EXAMPLE Description block COLLAR Identity block EN6054-050A Number of this standard Diameter code (see Table 2) Surface treatment code (see Table 1) NOTE If necessary, the code I9005 shall be placed between the description block and
23、the identity block. 5 Marking EN 2424, style F, depressed 0,25 mm max. Marking position at manufacturers discretion. 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
24、 without license from IHS-,-,-prEN 6054:20076 7 Example of installation See Figure 2. Key 1 Pin EN 6050, EN 6100 or EN 6120 2 Collar 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-,-,-
