ASD-STAN PREN 4695-2015 Aerospace series Tie rod with integrated bolts Assembly code G H and K (Edition P 2).pdf
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1、ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM prEN 4695 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 G, H and K Srie arospatiale Bielle avec axes intgrs Code assemblage G, H et K Luft- und Raumfahrt Zug-Druck Stange mit integrierten Bolzen Zusammenbaucode G, H und K 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 4695:2015 (E) 2 Contents Page Foreword . 2 Introduction 3 1 Scope . 4
7、 2 Normative references . 4 3 Requirements 5 4 Assembly code definitions 5 5 Materials 7 6 Locking clips . 7 7 Fork and eye ends 9 8 Mass calculation of tie rods . 15 9 Marking 16 10 Dimensions 17 11 Designation . 17 12 Technical specification 17 Annex A (informative) Standard evolution form 18 Fore
8、word 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. prEN 4695:2015 (E) 3 In
9、troduction 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 Kor
10、ea: 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 applicants throughout the world
11、. 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 possibility that some
12、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 4695:2015 (E) 4 1 Scope This standard specifies the dimensions and tolerances of rod assemblies for aeros
13、pace 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 referenced in this document
14、 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, Aerospace series Titanium alloy
15、 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: Technical specificatio
16、n 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 2768-1, General tolerances
17、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 stainless steel parts DIN 6799,
18、 Retaining 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 Identificatio
19、n numbers for methods of organic coating 2) LN 9499-1, Aerospace Inserts, helical coil threads, screw-locking Class: 1100 MPa/235 C/425 C 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), Aeros
20、pace Wrought aluminium alloy with approx. 4,4Cu-1,5Mg-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 Safe
21、ty Agency, Postfach 101253, D-50452 Koeln, Germany. prEN 4695:2015 (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 millim
22、etres, tolerances and masses in accordance to Table 4, Table 5, Table 6 and Table 7. General tolerances shall be in accordance to ISO 2768-mK. Missing dimensions are manufacturing options. 3.1.3 Technical requirements See EN 4691-1. 4 Assembly code definitions Assembly code G, H and K are shown in F
23、igure 1, Figure 2 and Figure 3. For assembly code G, H and K: d1 20,0 mm, SW 22,2 mm and adjustable range for L1 6,35 mm. 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 G prEN 4695:2015 (E) 6 Key 1 2 3 4 5 6 7 8 and 9 The positio
24、n numbers and the materials are shown in Table 1 and Table 2. Figure 2 Assembly code H Key 1 3 4 5 6 8 and 9 The position numbers and the materials are shown in Table 1 and Table 2. Figure 3 Assembly code K prEN 4695:2015 (E) 7 5 Materials See Table 1. Table 1 Material code C Position Description Ma
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