ASD-STAN PREN 3278-2018 ENGLISH VERSION Aerospace series - Sleeves tubular protruding head in corrosion resisting steel passivated (0 25 mm wall thickness) (Edition P 2).pdf

1、 ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM ASD-STAN prEN 3278 Edition P2 June 2018 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Rue Montoyer 10 - 1000 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 775 8131 - www.asd-stan.orgICS: Descriptors: ENGLISH

2、VERSION Aerospace series Sleeves, tubular, protruding head, in corrosion resisting steel, passivated (0,25 mm wall thickness) Luft- und Raumfahrt Hlsen, berstehender Kopf, aus korrosionsbestndigem Stahl (Wanddicke 0,25 mm) Srie arospatiale Douilles tubulaires, tte saillante en acier rsistant la corr

3、osion (paisser de paroi 0,25 mm) 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 technically approv

4、ed 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. After examinatio

5、n and review by users and formal agreement of ASD-STAN, the ASD-STAN prEN 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

6、 national level by giving the EN the status of a national standard and by withdrawing any national standards conflicting with the EN. ASD-STAN Technical Committee approves that: “This document is published by ASD-STAN for the needs of the European Aerospace Industry. The use of this standard is enti

7、rely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.” ASD-STAN reviews each standard and technical report at least every five years at which time it may be revised, reaffirmed, stabi

8、lized or cancelled. ASD-STAN invites you to send your written comments or any suggestions that may arise. All rights reserved. No parts of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or

9、 otherwise, without prior written permission of ASD-STAN. Order details: E-mail: salesasd-stan.org Web address: http:/www.asd-stan.org/ Edition approved for publication 1stJune 2018 Comments should be sent within six months after the date of publication to ASD-STAN Mechanical Domain prEN 3278:2018 (

10、E) 2 Contents Page 1 Scope 3 2 Normative references 3 3 Terms and definitions . 3 4 Required characteristics 4 5 Designation 7 6 Marking . 7 7 Technical requirements 7 8 Quality assurance 8 prEN 3278:2018 (E) 3 1 Scope This European standard specifies the characteristics and technical requirements f

11、or protruding head tubular sleeves, in corrosion resisting steel, which may be plain or provided with a series of annular grooves. Passivated sleeves are for use in aerospace assemblies whose maximum operating temperature does not exceed 650 C. The operating temperatures for aluminium pigmented slee

12、ves should not exceed 230 C. 2 Normative references The following documents are referred to in the text in such a way that some or all of their content constitutes requirements of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the r

13、eferenced document (including any amendments) applies. EN 2175, Aerospace series Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) Solution treated and precipitation treated Sheet, strip and plate 0,5 mm a 10 mm, Rm 850 MPa1)EN 2424, Aerospace series Marking of aerospace products EN 2516, Aerospace

14、series Passivation of corrosion resisting steels and decontamination of nickel base alloys EN 4473, Aerospace series Aluminium pigmented coatings for fasteners Technical specification ISO 2859, Sampling procedures and tables for inspection by attributes 3 Terms and definitions For the purposes of th

15、is document, the following terms and definitions apply. ISO and IEC maintain terminological databases for use in standardization at the following addresses: IEC Electropedia: available at http:/www.electropedia.org/ ISO Online browsing platform: available at http:/www.iso.org/obp 3.1 crack rupture i

16、n the material which may extend in any direction and which may be intercrystalline or transcrystalline in character 3.2 seam open surface defect which is the result of the extrusion of the material 1) Published as ASD-STAN Prestandard at the date of publication of this European standard (www.asd-sta

17、n.org/). prEN 3278:2018 (E) 4 3.3 lap surface defect caused by folding over metal fins or sharp corners and then rolling or forging them into the surface 4 Required characteristics 4.1 Configuration Dimensions Tolerances The configuration shall be in accordance with Figure 1; the dimensions and tole

18、rances shall conform to the values shown in Figure 1 and in Table 1 and Table 2 after surface treatment. 4.2 Surface roughness See Figure 1. The values apply prior to application of aluminium pigmented coating respectively after passivation. 4.3 Material Steel EN 2175, received in the annealed condi

19、tion and cold worked during manufacture. 4.4 Surface treatment None: Passivation per EN 2516. Code “Z”: aluminium pigmented coating per EN 4473 type I or type III. Code “ZG”: aluminium pigmented coating per EN 4473 type II or type IV. Annotation: Coating required on sleeve outer surface only, coatin

20、g on inner surface depends on manufacturers option. 4.5 Form code See Figure 1 and Table 1. Values in micrometres apply prior to surface treatment. prEN 3278:2018 (E) 5 Plain form (code “P”) Grooved form (code “G”) Key 1 Unspecified dimensions: as plain form a Ref. b Pitch of grooves c Form of groov

21、e at manufacturers option d Detail enlarged Figure 1 Configuration prEN 3278:2018 (E) 6 Table 1 Dimensions Dimensions in millimetres Diameter code D E F H K max. min. max. min. 0,3 0,5 0,5 040 3,999 3,960 4,499 4,474 8,5 3 4 050 4,999 4,960 5,499 5,474 10 3 5,5 060 5,999 5,960 6,499 6,474 11,5 4,5 7

22、 080 7,994 7,955 8,494 8,470 14,5 6 7 100 9,994 9,955 10,494 10,470 17,5 7,5 10 Table 2 Lengths and masses Dimensions in millimetres Diameter code 040 050 060 080 100 Form Length Mass Code L+0,50kg/1 000 piecesa Plain 030 3 0,167 0,215 045 4,5 0,206 0,264 0,325 060 6 0,246 0,312 0,383 0,489 075 7,5

23、0,285 0,361 0,441 0,565 0,799 090 9 0,325 0,410 0,499 0,642 0,894 105 10,5 0,364 0,459 0,557 0,719 0,989 120 12 0,404 0,508 0,615 0,795 1,085 135 13,5 0,443 0,556 0,673 0,872 1,180 150 15 0,483 0,605 0,731 0,949 1,276 165 16,5 0,520 0,654 0,790 1,025 1,371 180 18 0,562 0,703 0,848 1,102 1,466 195 19

24、5 0,601 0,751 0,906 1,179 1,562 210 21 0,641 0,800 0,964 1,256 1,657 225 22,5 0,680 0,849 1,022 1,332 1,753 240 24 0,720 0,898 1,080 1,409 1,848 255 25,5 0,759 0,947 1,138 1,486 1,943 Grooved 25 0,747 0,931 1,119 1,460 1,912 aCalculated on basis of 7,95 kg/dm3. prEN 3278:2018 (E) 7 5 Designation Ea

25、ch sleeve shall only be designated as in the following example: Where the following codes apply: P = plain form G = grooved form NOTE If nessesary, the originator code S 9005 may be introduced between the description block and the identity block. 6 Marking EN 2424, style G. In addition, the quantity

26、 shall be stated on the package. 7 Technical requirements 7.1 Manufacture The sleeve shall be formed by a drawing process from sheet or strip stock to form a one piece tubular section and head. 7.2 Surface appearance The sleeves shall be free from cracks, seams and laps. Under visual examination, th

27、e sleeve may show axial flow lines in the tubular section typical of a drawn sleeve. The flow lines shall be continuous at the fillet radius. A slight visible orange peel effect is also permissible. 7.3 Sampling In conformity with ISO 2859, using normal or reduced inspection methods. The acceptable

28、quality level (AQL) is 1 %. prEN 3278:2018 (E) 8 8 Quality assurance 8.1 Product qualification The manufacturers operations shall be an approved production organisation for aerospace products and shall demonstrate that it has implemented and is able to maintain a quality management system (e.g. according to EN 9100 or an equivalent aerospace accepted and established quality management system). prEN 3278:2018 (E) 9 Bibliography EN 9100, Quality Management Systems Requirements for Aviation, Space and Defence Organizations