ASD-STAN PREN 4694-2015 Aerospace series Tie rod with integrated bolts Assembly code D E and F (Edition P 2).pdf
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1、ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM prEN 4694 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 D, E and F Srie arospatiale Bielle avec axes intgrs Code assemblage D, E et F Luft- und Raumfahrt Zug-Druck Stange mit integrierten Bolzen Zusammenbaucode D, E und F This “Aerospace Series“ Prestandard h
3、as 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 approved by the experts of the concerned Domain following member comments. S
4、ubsequent 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 sub
5、mitted 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 national level by giving the EN the status of a national standard and by withdrawing
6、 any national 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 4694:2015 (E) 2 Contents Page Foreword . 2 Introduction 3 1 Scope . 4
7、 2 Normative references Erreur ! Signet non dfini. 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
8、 evolution form 21 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 standard has received approval for Publication.
9、prEN 4694:2015 (E) 3 Introduction 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 Ca
10、nada: 2584387 South Korea: 7011559 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 applican
11、ts throughout the world. In this 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
12、 possibility that some of the elements 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 4694:2015 (E) 4 1 Scope This standard specifies the dimensions and tolerances of r
13、od assemblies for aerospace applications 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 refe
14、renced in this document and are indispensable 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, Aerospac
15、e series Titanium alloy TI-P64001 (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:
16、 Technical specification 1) EN 4692, 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
17、-1, General tolerances Part 1: Tolerances 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 stainles
18、s steel parts DIN 6799, Retaining washers for shafts 2) DIN 65038-1, Aerospace Steel, nickel-and cobalt-alloy bars Technical specification Erreur ! Signet non dfini.) LN 9368-4, Aerospace Designation of surface treatments Identification numbers for methods of anodic treatment 2) LN 9368-7, Aerospace
19、 Designation of surface treatments Identification numbers 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
20、,5Mg-0,6Mn 2) FAR/JAR/CS 25.853, Compartment Interiors 3) 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) Published by: European Aviation Safety Agency, Postfach 101253, D-50452 Koeln, Germa
21、ny prEN 4694:2015 (E) 5 3 Requirements 3.1 Configuration, dimensions, tolerances and mass 3.1.1 Configuration The configuration shall be in accordance with Figure 1, Figure 2 and Figure 3. 3.1.2 Dimensions, tolerances and mass Dimensions are in millimetres, tolerances and masses in accordance to Tab
22、le 4, Table 5, Table 6, Table 7 and Table 8. General tolerances shall be in accordance to ISO 2768-mK. Missing dimensions are manufacturing options. 4 Assembly code definitions Assembly code D, E and F are shown in Figure 1, Figure 2 and Figure 3. For assembly code D, E and F: d1 25,4 mm, d3 22,2 mm
23、 and adjustable range for L1 12,7 mm. For L1 less than 330 mm outer diameter of the rod body d3 22,2 mm (no swaging). Key 1 2 4 5 6 - 7 and 8 The position numbers and the materials are shown in Table 1 and Table 2. Figure 1 Assembly code D prEN 4694:2015 (E) 6 Key 1 2 3 4 5 6 7 8 and 9 The position
24、numbers and the materials are shown in Table 1 and Table 2. Figure 2 Assembly code E Key 1 3 5 6 8 and 9 The position numbers and the materials are shown in Table 1 and Table 2. Figure 3 Assembly code F prEN 4694:2015 (E) 7 5 Materials See Table 1 and Table 2. Table 1 Material code A Position Descri
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