ASD-STAN PREN 4693-2015 Aerospace series Tie rod with integrated bolts Assembly code A B and C (Edition P 2).pdf
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1、ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM prEN 4693 Edition P 2 April 2015 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.org ICS: Supersedes edition P 1 of Octobe
2、r 2012 Descriptors: ENGLISH VERSION Aerospace series Tie rod with integrated bolts Assembly code A, B and C Srie arospatiale Bielle avec axes intgrs Code assemblage A, B et C Luft- und Raumfahrt Tie Rod mit integriertem Bolzen Zusammenbaucode A, B und C This “Aerospace Series“ Prestandard has been d
3、rawn 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 approved by the experts of the concerned Domain following member comments. Subsequent
4、 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 examination and review by users and formal agreement of ASD-STAN, it will be submitted as
5、 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 national level by giving the EN the status of a national standard and by withdrawing any nati
6、onal standards conflicting with the EN. Edition approved for publication 1st April 2015 Comments should be sent within six months after the date of publication to ASD-STAN Mechanical Domain Copyright 2015 by ASD-STAN prEN 4693:2015 (E) 2 Contents Page Foreword 2 Introduction .3 1 Scope 4 2 Normative
7、 references 4 3 Requirements .5 4 Assembly code definitions .5 5 Materials .7 6 Locking clips 8 7 Fork and eye ends .9 8 Mass calculation of tie rods . 17 9 Marking 19 10 Dimensions 20 11 Designation . 20 12 Technical specification 20 Annex A (informative) Standard evolution form . 21 Foreword This
8、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 standard has received approval for Publication. prEN 4693:2015 (E) 3 Introduction
9、 Aerospace and Defence Standardization (ASD-STAN) draws attention to the fact that it is claimed that compliance with this document may involve the use of a patent. USA: US 8371767 China: CN 10104431 Japan: JP 4885140 Russia: RU 2389914 South Africa: ZA 2007/03913 Canada: 2584387 South Korea: 701155
10、9 ASD-STAN takes no position concerning the evidence, validity and scope of this patent right. The holder of this patent right has assured ASD-STAN that he/she is willing to negotiate licences under reasonable and non-discriminatory terms and conditions with applicants throughout the world. In this
11、respect, the statement of the holder of this patent right is registered with ASD-STAN. Information may be obtained from: GMT Gummi-Metall-Technik GmbH Liechtersmatten 5 D-77815 Bhl TRIGUM Engineering GmbH Brunskamp 4 D-21220 Seevetal/Maschen Attention is drawn to the possibility that some of the ele
12、ments of this document may be the subject of patent rights other than those identified above. ASD-STAN shall not be held responsible for identifying any or all such patent rights. prEN 4693:2015 (E) 4 1 Scope This standard specifies the dimensions and tolerances of rod assemblies for aerospace appli
13、cations with two adjustable ends with integrated bolts for interior and sub structure in the temperature range 55 C to 85 C. The rod ends should not be screwed completely apart. 2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are i
14、ndispensable for its application. 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 3311, Aerospace series Titanium alloy TI-P64001
15、 (Ti-6Al-4V) Annealed Bar for machining D 110 mm EN 4614, Aerospace series Spherical plain bearings in corrosion resisting steel with self-lubricating liner wide series Dimensions and loads Inch series EN 4691-1, Aerospace series Tie rod with integrated bolts Part 1: Technical specification 1) EN 46
16、92, Aerospace series Tie rod with integrated bolts Locking clip 1) EN 10088-3, Stainless steel Part 3: Technical delivery conditions for semi finished products, bars, rods, wire, sections and bright products of corrosion resisting steels for general purposes ISO 2768-1, General tolerances Part 1: To
17、lerances for linear and angular dimensions without individual tolerance indications ISO 2768-2, General tolerances Part 2: Geometrical Tolerances for Features without individual tolerance indications ISO 8075, Aerospace series Surface treatment of hardenable stainless steel parts DIN 6799, Retaining
18、 washers for shafts 2) DIN 65038-1, Aerospace Steel, nickel-and cobalt-alloy bars Technical specification 2) LN 9368-4, Aerospace Designation of surface treatments Identification numbers for methods of anodic treatment 2) LN 9368-7, Aerospace Designation of surface treatments Identification numbers
19、for methods of organic coating 2) WL 1.4548 (all parts), Aerospace Precipitation-hardening stainless chromium-nickel-copper steel with approx. 0,05C-16Cr-4Cu-4Ni 2) WL 3.1354 (all parts), Aerospace Wrought aluminium alloy with approx. 4,4Cu-1,5Mg-0,6Mn 2) FAR/JAR/CS 25.853, Compartment Interiors 3)
20、1) Published as ASD-STAN Prestandard at the date of publication of this standard. http:/www.asd-stan.org/ 2) Published by: Beuth Verlag GmbH. www.beuth.de 3) European Aviation Safety Agency, Postfach 101253, D-50452 Koeln, Germany. prEN 4693:2015 (E) 5 3 Requirements 3.1 Configuration, dimensions, t
21、olerances and masses 3.1.1 Configuration The configuration shall be in accordance with Figure 1, Figure 2 and Figure 3. 3.1.2 Dimensions, tolerances and masses Dimensions are in millimetres, tolerances and masses in accordance to Table 4, Table 5, Table 6, Table 7 and Table 8. General tolerances sha
22、ll be in accordance to ISO 2768-mK. Missing dimensions are manufacturing options. 4 Assembly code definitions Assembly code A, B and C are shown in Figure 1, Figure 2 and Figure 3. For assembly code A, B and C: d1 20 mm and adjustable range for L1 12,7 mm. Key 1 2 4 5 6 7 and 8 The position numbers
23、and the materials are shown in Table 1 and Table 2. Figure 1 Assembly code A prEN 4693:2015 (E) 6 Key 1 2 3 4 5 6 7 8 and 9 The position numbers and the materials are shown in Table 1 and Table 2. Figure 2 Assembly code B Key 1 3 5 6 8 and 9 The position numbers and the materials are shown in Table
24、1 and Table 2. Figure 3 Assembly code C prEN 4693:2015 (E) 7 5 Materials See Table 1 and Table 2. Table 1 Material code A Position Description Material Surface treatment 1 Rod body Aluminium alloy according to WL 3.1354 T351 Anodized according to LN 9368-4-2000 and coating according to LN 9368-7-502
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