1、Aerospace series - Tie rod with integrated bolts Part 1: Technical specification BS EN 4691-1:2017 BSI Standards Publication WB11885_BSI_StandardCovs_2013_AW.indd 1 15/05/2013 15:06 EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4691-1 October 2017 ICS 49.035 English Version Aerospace series -
2、 Tie rod with integrated bolts - Part 1: Technical specification Srie arospatiale - Bielle avec axes intgrs - Partie 1 : Spcification technique Luft- und Raumfahrt - Zug-Druck-Stange mit integrierten Bolzen - Teil 1: Technische Lieferbedingungen This European Standard was approved by CEN on 25 June
3、2016. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtaine
4、d on application to the CEN-CENELEC Management Centre or to any CEN member. This European Standard exists in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the CEN-C
5、ENELEC Management Centre has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, I
6、taly, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG CEN-CENELEC Management C
7、entre: Avenue Marnix 17, B-1000 Brussels 2017 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4691-1:2017 E National foreword This British Standard is the UK implementation of EN 4691-1:2017. The UK participation in its preparation
8、 was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems. A list of organizations represented on this committee can be obtained on request to its secretary. This publication does not purport to include all the necessary provisions of a contract. Users are responsible f
9、or its correct application. The British Standards Institution 2017 Published by BSI Standards Limited 2017 ISBN 978 0 580 94025 5 ICS 49.035Compliance with a British Standard cannot confer immunity from legal obligations. This British Standard was published under the authority of the Standards Polic
10、y and Strategy Committee on 31 October 2017. Amendments/corrigenda issued since publication Date Text affected BRITISH STANDARD BS EN 4691-1:2017 EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4691-1 October 2017 ICS 49.035 English Version Aerospace series - Tie rod with integrated bolts - Par
11、t 1: Technical specification Srie arospatiale - Bielle avec axes intgrs - Partie 1 : Spcification technique Luft- und Raumfahrt - Zug-Druck-Stange mit integrierten Bolzen - Teil 1: Technische Lieferbedingungen This European Standard was approved by CEN on 25 June 2016. CEN members are bound to compl
12、y with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN-CENELEC
13、Management Centre or to any CEN member. This European Standard exists in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the CEN-CENELEC Management Centre has the sam
14、e status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg,
15、 Malta, Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG CEN-CENELEC Management Centre: Avenue Marnix 17, B-1000 Brus
16、sels 2017 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4691-1:2017 E BS EN 4691-1:2017EN 4691-1:2017 (E) 2 Contents Page European foreword . 3 Introduction 4 1 Scope 5 2 Normative references 5 3 Terms and definitions . 7 4 Symbo
17、ls and abbreviations . 8 5 Required characteristics, inspections and test methods 9 6 Allowable static loads . 10 7 Allowable dynamic loads . 17 8 Assembly load locking clip EN 4692 22 9 Adjustment-torque 23 10 Technical requirements. 24 11 Qualification . 30 12 Condition on delivery . 31 13 Materia
18、l 31 Annex A (normative) Sampling 37 A.1 Acceptance test samples 37 A.2 Qualification test samples . 38 Annex B (informative) Standard evolution form . 54 BS EN 4691-1:2017EN 4691-1:2017 (E) 3 European foreword This document (EN 4691-1:2017) has been prepared by the Aerospace and Defence Industries
19、Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member countries of ASD, prior to its presentation to CEN.
20、 This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by April 2018, and conflicting national standards shall be withdrawn at the latest by April 2018. Attention is drawn to the possibility that some of t
21、he elements of this document may be the subject of patent rights. CEN shall not be held responsible for identifying any or all such patent rights. According to the CEN-CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European S
22、tandard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, S
23、lovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. BS EN 4691-1:2017EN 4691-1:2017 (E) 4 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 C
24、hina: CN 10104431 Japan: JP 4885140 Russia: RU 2389914 South Africa: ZA 2007/03913 Canada: 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 negotiat
25、e licences under reasonable and non-discriminatory terms and conditions with applicants 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 T
26、RIGUM Engineering GmbH Brunskamp 4 D-21220 Seevetal/Maschen Attention is drawn to the 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. BS
27、 EN 4691-1:2017EN 4691-1:2017 (E) 5 1 Scope This standard specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for rod assemblies with two adjustable ends with integrated bolts, designed to withstand static and dynamic loads possible for interi
28、or and substructure in the temperature range from 55 C to 85 C. It is applicable whenever referenced. For a complete overview see EN 4691-2. 2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For
29、 dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. DIN 53504, Testing of rubber Determination of tensile strength at break, tensile stress at yield, elongation at break and stress values in a te
30、nsile test DIN 65271, Aerospace series Elastomeric semi-finished products and parts Technical specification EN 571-1, Non-destructive testing Penetrant testing Part 1: General principles EN 2004-1, Aerospace series Test methods for aluminium and aluminium alloy products Part 1: Determination of elec
31、trical conductivity of wrought aluminium alloys EN 2424, Aerospace series Marking of aerospace products EN 2825, Aerospace series Burning behaviour of non metallic materials under the influence of radiating heat and flames Determination of smoke density EN 2826, Aerospace series Burning behaviour of
32、 non metallic materials under the influence of radiating heat and flames Determination of gas components in the smoke EN 3844 (all parts), Aerospace series Flammability of non metallic materials EN 4691-2, Aerospace series Tie rod with integrated bolts Part 2: Overview construction kit EN 4692, Aero
33、space series Tie rod with integrated bolts Locking clip EN 4693, Aerospace series Tie rod with integrated bolts Assembly Code A, B and C EN 4694, Aerospace series Tie rod with integrated bolts Assembly Code D, E and F EN 4695, Aerospace series Tie rod with integrated bolts Assembly Code G, H and K E
34、N 9100, Quality Management Systems Requirements for Aviation, Space and Defense Organizations EN 9133, Aerospace series Quality management systems Qualification procedure for aerospace standard parts EN 10204, Metallic products Types of inspection documents EN ISO 75-2, Plastics Determination of tem
35、perature of deflection under load Part 2: Plastics and ebonite (ISO 75-2) EN ISO 175, Plastics Methods of test for the determination of the effects of immersion in liquid chemicals (ISO 175) BS EN 4691-1:2017EN 4691-1:2017 (E) 6 EN ISO 178, Plastics Determination of flexural properties (ISO 178 EN I
36、SO 179-1, Plastics Determination of Charpy impact properties Part 1: Non-instrumented impact test (ISO 179-1) EN ISO 291, Plastics Standard atmospheres for conditioning and testing (ISO 291) EN ISO 527-2, Plastics Determination of tensile properties Part 2: Test conditions for moulding and extrusion
37、 plastics (ISO 527-2) EN ISO 1172, Textile-glass-reinforced plastics Prepregs, moulding compounds and laminates Determination of the textile-glass and mineral-filler content Calcination methods (ISO 1172) EN ISO 1183-1, Plastics Methods for determining the density of non-cellular plastics Part 1: Im
38、mersion method, liquid pyknometer method and titration method (ISO 1183-1) EN ISO 9001, Quality management systems Requirements (ISO 9001) EN ISO 9227, Corrosion tests in artificial atmospheres Salt spray tests (ISO 9227) ISO 34-1, Rubber, vulcanized or thermoplastic Determination of tear strength P
39、art 1: Trouser, angle and crescent test pieces ISO 37, Rubber, vulcanized or thermoplastic Determination of tensile stress-strain properties ISO 1817, Rubber, vulcanized or thermoplastic Determination of the effect of liquids ISO 2781, Rubber, vulcanized or thermoplastic Determination of density ISO
40、 5855-1, Aerospace MJ threads Part 1: General requirements ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts ISO 10123, Adhesives Determination of shear strength of anaerobic adhesives using pin-and-collar specimens ISO 10964, Adhesives Determination of torque strength of
41、anaerobic adhesives on threaded fasteners ASTM E112, Standard Test Methods for Determining Average Grain Size 1)ASTM C177, Standard Test Method for Steady-State Heat Flux Measurements and Thermal Transmission Properties by Means of the Guarded-Hot-Plate Apparatus 2)ASTM D696, Standard Test Method fo
42、r Coefficient of Linear Thermal Expansion of Plastics Between 30 C and 30 C with a Vitreous Silica Dilatometer 2)FAR/JAR/CS 25.853, Compartment Interiors 2)1) Published by: American Society for Testing and Materials (ASTM), 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959, USA. http:/www.astm
43、.org/ 2) Published by: European Aviation Safety Agency, Postfach 101253, D-50452 Koeln, Germany. BS EN 4691-1:2017EN 4691-1:2017 (E) 7 RTCA-DO 160E, Environmental Conditions and Test Procedures for Airborne Equipment 3)UL 746B version 1.3 date 29.11.2000, Plastics Polymeric Materials Long Term Prope
44、rty Evaluations 4)3 Terms and definitions For the purposes of this document, the following terms and definitions apply. 3.1 standard part completed rod assembly, which consists of a rod body, two end fittings (adjustable) and their associated locking or blocking system 3.2 assembly See EN 4693; See
45、EN 4694; See EN 4695. 3.3 traceability ability to trace the history, application or location of an entity by means of recorded identifications Note 1 to entry: Traceability of raw materials and manufacturing processes of each individual component of every tie rod refers to EN 9100. Every tie rod is
46、marked for traceability with a serial number. 3.4 Batch definition 3.4.1 manufacturing batch composed of rod bodies made of same material (same material batch), with same diameter and same thickness and belonging to the same manufacturing campaign and equipped with rod body ends and rods ends of sam
47、e design 3.4.2 artificial batch consists of different manufacturing batches and are limited to a maximum of 100 rods 3.5 qualification test is a test or series of tests to demonstrate that the products comply with the requirements stipulated in this specification and/or in a product standard and are
48、 accomplished according to documented parameters and under reproducible conditions 3.6 acceptance test demonstrates that the characteristics of manufactured products comply with the requirements 3) Published by: Radio Technical Commission for Aeronautics (RTCA), 1140 Connecticut Ave., N.W. Suite 102
49、0, Washington, D.C. 20036, USA. 4) Published as UL Standard, http:/. BS EN 4691-1:2017EN 4691-1:2017 (E) 8 4 Symbols and abbreviations L 1 = tie rod length Pin to Pin mm a = amplitude D = outer diameter rod body d = transformed diameter rod body D a = total damage D ai = partial damage R = border stress rate n = lifetime R a = roughness s 1 = factor ultimate, limit load s 2 = fitting factor QTP = Qualification Tes
