ASD-STAN PREN 6133 CORR 1-2018 Aerospace series - Rod-end with bearing per EN 6096 with self-lubricating liner in corrosion resisting steel extra wide inner ring external threaded .pdf

1、 ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM Corrigendum 1 ASD-STAN prEN 6133 Edition P2 April 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: Descri

2、ptors: ENGLISH VERSION Aerospace series Rod-end, with bearing per EN 6096, with self-lubricating liner in corrosion resisting steel, extra wide inner ring, external threaded shank Dimensions and loads Inch series Luft- und Raumfahrt senkopf mit Gelenklager nach EN 6096 mit selbstschmierender Beschic

3、htung aus korrosionsbestndigen Stahl, extra breiter Innenring, mit Auengewinde Mae und Belastungen Inch Reihe Srie arospatiale Embout rotule lisse par EN 6096 en acier inoxydable et garniture autolubrifiante Bague interne extra large filetage extrieur Dimensions et charges Srie en inches This “Aeros

4、pace 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 approved by the experts of the concerned Domain fo

5、llowing 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 examination and review by users and formal agreement o

6、f 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 national level by giving the EN the status

7、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 entirely voluntary, and its applicability and su

8、itability 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, stabilized or cancelled. ASD-STAN invites you to

9、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 otherwise, without prior written permission

10、 of ASD-STAN. Order details: E-mail: salesasd-stan.org Web address: http:/www.asd-stan.org/ Edition approved for publication 1stFebruary 2018 Comments should be sent within six months after the date of publication to ASD-STAN Mechanical Domain prEN 6133:2018 (E) 2 Contents Page Foreword 3 Introducti

11、on 4 1 Scope 5 2 Normative references 5 3 Symbols and abbreviations . 6 4 Requirements . 6 4.1 Configuration, dimensions, tolerances and mass 6 4.2 Surface roughness . 6 4.3 Right or left hand thread . 10 4.4 With or without longitudinal groove 10 4.5 Materials 10 4.6 Surface treatment 10 4.7 Loads

12、. 11 4.8 Starting torque values 12 4.9 Temperature range . 12 5 Designation. 13 6 Marking 13 7 Technical specification . 13 8 Quality management system 13 (normative) Verification of fatigue loads 14 Annex AA.1 Standard rod end fatigue spectrum . 14 A.2 Method . 14 (informative) Standard evolution f

13、orm . 15 Annex BBibliography . 16 prEN 6133:2018 (E) 3 Foreword This document (prEN 6133:2018) has been prepared by the Aerospace and Defence Industries Association of Europe Standardization (ASD-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Stan

14、dard has received the approval of the National Associations and the Official Services of the member of ASD, prior to its presentation to CEN. prEN 6133:2018 (E) 4 Introduction This document is published at edition P2. Former P1 and drafts may exist of Airbus development only but without any ASD-STAN

15、 official publication. In consequence configuration management discrepancies with these unofficial documents are under Airbus responsibility. prEN 6133:2018 (E) 5 1 Scope This European standard specifies the characteristics of adjustable rod ends consisting of: a self-aligning spherical plain bearin

16、g with self-lubricating liner per EN 6096; a rod-end with threaded shank with an optional longitudinal groove for locking purposes. They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms. 2 Normative references The following documents are referred t

17、o 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 referenced document (including any amendments) applies. EN 2068, Aerospace series Rod-ends

18、with self-lubricating, self-aligning bearings Technical specification1) EN 2133, Aerospace series Cadmium plating of steels with specified tensile strength 1 450 Mpa, copper, copper alloys and nickel alloys1)EN 2424, Aerospace series Marking of aerospace products EN 6096, Aerospace series Bearings s

19、pherical plain with self-lubricating liner extra wide inner ring in corrosion resisting steel Dimensions and loads Inch seriesISO 1132-1, Rolling bearings Tolerances Part 1: Terms and definitions ISO 3161, Aerospace UNJ threads General requirements and limit dimensions ISO 3353-1, Aerospace Lead and

20、 runout threads Part 1: Rolled external threads ISO 3353-2, Aerospace Lead and runout threads Part 2: Internal threads ISO 8074, Aerospace Surface treatment of austenitic stainless steel parts NAS 559, Lock-rod end (key type)2)SAE AMS 5643, Steel, corrosion resistant, bars wire, forgings, tubing and

21、 rings 16Cr-4.0Ni-0.30(Cb+Ta)-4.0Cu solution heat treated, precipitation hardenable TR 4475, Aerospace series Bearings and mechanical transmissions for airframe applications Vocabulary 1) Published as ASD-STAN Standard at the date of publication of this European standard (www.asd-stan.org). 2) Publi

22、shed by: Aerospace Industries Association of America, Inc. (AIA), 1250 Eye Street, N.W., Washington, D.C. 20005-3924, USA. prEN 6133:2018 (E) 6 3 Symbols and abbreviations Symbols of limit deviations are in accordance with definitions of ISO 1132-1. maximum angle of tilt of the outer ring with respe

23、ct to the inner ring, with the spherical surface of the outer ring being completely in contact with the inner ring Cspermissible static radial load Cppush out loads dmpsingle plane mean bore diameter deviationdsdeviation of a single bore diameter Cffatigue loads For definitions and vocabulary, see T

24、R 4475. 4 Requirements 4.1 Configuration, dimensions, tolerances and mass See Figure 1 and Table 1. Table 1: Dimensions and tolerances are expressed in millimeters (inches). Figure 1: Dimensions and tolerances for Ra max. are expressed in m (in). Dimensions and tolerances are measured after surface

25、treatment. 4.2 Surface roughness In accordance with Figure 1. Surface roughness is measured before surface treatment. prEN 6133:2018 (E) 7 Key a) According to ISO 3353 d) Usable length for groove b) Thread, pitch diameter e) TFE linerc) Groove as per NAS 559 1 Marking2 Type code D 3 Type code EFigur

26、e 1 Configuration prEN 6133:2018 (E) 8 Table 1 Dimensions, tolerances and mass Dia-meter codeaD3 d2bd d3 B C D2 D b1 b2 l1 Type of thread UNIJF-3ALimit deviation 0 0 +0,254 0 0 +0,127 0,254 0,203 0,05 0 0,203 0,127 0nominal max. dmpds(0 (0 (+0.010 (0 Bearing diameter (0 (+0.005 (0.010) 0.008) 0.002)

27、 0) 0.008) 0.0050) 0)03 0.3125-24 7,249 (0.2854) 4,826 (0.1900) 5,232 (0.206) 12,700 (0.500) 5,588 (0.220)8,000 (0.315) 14,288 (0.5625) 6,604 (0.2600) 1,575 (0.062) 38,100 (1.500) 04 0.3750-24 8,837 (0.3479) 6,350 (0.2500) 6,756 (0.266) 15,062 (0.593) 6,731 (0.265) 9,700 (0.382) 18,796 (0.7400) 7,89

28、9 (0.3110) 2,362 (0.093) 49,225 (1.938) 05 0.4375-20 10,287 (0.4050) 7,938 (0.3125) 8,331 (0.328) 20,650 (0.813) 9,017 (0.355) 12,850 (0.506) 23,012 (0.9060) 9,398 (0.3700) 53,980 (2.125) 06 9,525 (0.3750) 9,931 (0.391) 13,250 (0.522) 0 07 0.5000-20 11,875 (0.4675) 11,113 (0.4375) 0,01311,506 (0.453

29、) 22,225 (0.875) 15,540 (0.612) 25,400 (1.0000) 11,074 (0.4360) 61,925 (2.438) 0 (0 08 0.6250-18 14,958 (0.5889) 12,700 (0.5000) 0,013 0.0005)13,106 (0.516) 23,800 (0.937) 10,439 (0.411) 18,290 (0.720) 28,575 (1.1250) 13,741 (0.5410) 3,175 (0.125) 66,675 (2.625) (0 10 0.7500-16 18,019 (0.7094) 15,87

30、5 (0.6250) 0.0005)16,281 (0.641) 30,480 (1.200) 14,656 (0.577) 21,540 (0.845) 34,925 (1.3750) 16,840 (0.6630) 73,025 (2.875) 12 0.8750-14 21,046 (0.8286) 19,050 (0.7500) 19,456 (0.766) 32,512 (1.280) 16,002 (0.630) 24,260 (0.955) 39,688 (1.5625) 19,736 (0.7770) 3,962 (0.156) 85,725 (3.375) 14 22,225

31、 (0.8750) 22,631 (0.891) 35,560 (1.400) 16,129 (0.635) 28,300 (1.114) 44,450 (1.7500) 95,250 (3.750) 16 1.2500-12 30,376 (1.1959) 25,400 (1.0000) 25,806 (1.016) 47,625 (1.875) 21,488 (0.846) 32,050 (1.262) 53,975 (2.1250) 28,854 (1.1360) 4,750 (0.187) 104,775 (4.125) +0,0030,01520 31,750 (1.2500) (+

32、0.000132,156 (1.266) 25,781 (1.015) 38,510 (1.516) 63,500 (2.5000) 127,000 (5.000) 0.0006)prEN 6133:2018 (E) 9 Diameter codeal2 l3 L1 E r1 cA Mass +1,524 +1,524 +0,203 +0,508 0,254 0,254 g/piece 0,762 0,762 0 0(+0.060 (+0.060 (+0.008 (+0.02 (0.010) min. (0.010) 0.030) 0.030) 0) 0)03 25,400 (1.000) 2

33、5,400 (1.000) 0,127 (0.005) 2,007 (0.079) 6,477 (0.255) 15 19,050 (0.750) 27 04 31,752 (1.250) 24 25,400 (1.000) 50 05 34,920 (1.375) 26,975 (1.062) 2,997 (0.118) 23 28,580 (1.125) 81 06 31,750 (1.250) 21,5 78 07 38,100 (1.500) 34,925 (1.375) 2,489 (0.098) 22 33,325 (1.312) 113 08 41,275 (1.625) 3,5

34、05 (0.138) 20 38,100 (1.500) 181 10 44,450 (1.750) 38,100 (1.500) 2,997 (0.118) 44,450 (1.750) 296 12 47,625 (1.875) 41,275 (1.625) 3,998 (0.157) 19 50,800 (2.000) 432 14 50,800 (2.000) 44,450 (1.750) 4,394 (0.173) 8,077 (0.318) 55,880 (2.200.) 513 16 53,975 (2.125) 47,625 (1.875) 6,198 (0.244) 9,70

35、3 (0.382) 21 69,850 (2.750) 1081 20 73,025 (2.875) 53,975 (2.125) 2,692 (0.106) 79,380 (3.125) 1480 aThe diameter code corresponds to nominal diameter d in 1/6 inch. b Rolled threads according to ISO 3161. c The acceptance value is the maximum value for the user. prEN 6133:2018 (E) 10 4.3 Right or l

36、eft hand thread Right or left hand thread should be according to Table 2. Table 2 Code letter for thread Code letter for thread L left hand thread R right hand thread 4.4 With or without longitudinal groove With or without longitudinal groove should be according to Table 3. Table 3 Code letter for g

37、roove Code letter for longitudinal groove K with longitudinal groove F without longitudinal groove 4.5 Materials Liner: PTFE liner (see product standard EN 6096). Inner ring: See product standard EN 6096. Outer ring: See product standard EN 6096. Rod end body: See AMS 5643, hardness 35 HRC 42. 4.6 S

38、urface treatment Rod end body: code T: Passivated according to ISO 8074; code P: Cadmium plating and chromating according to EN 2133, 10 m to 20 m (400 in to 800 in); exception: Threads, 5 m to 15 m (200 in to 600 in); bearing: see EN 6096, code T. prEN 6133:2018 (E) 11 4.7 Loads Loads should be acc

39、ording to Table 4. Table 4 Loads Diameter codeaRadial Axial static proof loadsc, eFatigue loaddPermissible static loadsbUltimate static loadb2 106cycles kN kN kN kN CsCpCf03 9,4f14,1f4,3 2,4 04 18,0f27,0f5,6 4,1 05 25,7f38,5f6,9 4,5 06 27,3 41,0 07 40,1 60,2 9,3 6,7 08 56,3 84,5 10,5 9,3 10 76,4 114

40、,7 12,8 12,6 12 97,2 145,8 16,3 16,0 14 101,8 152,6 18,3 16,8 16 189,8 284,8 22,2 31,3 20 224,0 335,6 26,1 36,9 aThe diameter code corresponds to nominal diameter d in 1/16 inch. bDefinition and testing according to EN 2068, Annex A. cDefinition and testing according to EN 2068, Annex B. dDefinition

41、 and testing according to Annex A. (permissible surface pressure: 100 MPa on smalest section). eAfter removing the load no permanent displacement of the bearing in the rodend greater thean 0,10 mm is permitted. fLimited by bolt bending (see EN 6096). prEN 6133:2018 (E) 12 4.8 Starting torque values

42、Starting torque values should be according to Table 5. Table 5 Starting torque values Diameter codeaStarting torque Nm normal reduced Code N Code R 03 0,06 0,34 0 - 0,11 04 0,11 0,56 05 06 07 0,03 0,15 08 10 12 14 0,23 0,90 0,04 0,25 16 20 0,23 1,50 0,05 0,32 aThe diameter code corresponds to nomina

43、l diameter d in 1/16 inch.4.9 Temperature range They shall be used in the temperature range 54 C to 150 C. prEN 6133:2018 (E) 13 5 Designation EXAMPLE NOTE If necessary, the code I9005 shall be placed between the description block and the identity block. 6 Marking EN 2424, style A. 7 Technical speci

44、fication According to EN 2068. 8 Quality management system 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 another in aero

45、space accepted and established quality management system). 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 ae

46、rospace accepted and established quality management system). The qualification procedure for aerospace standard products (e. g. according to EN 9133 or another in aerospace accepted and established qualification procedure) shall be used and documented according to the specified tests if not otherwis

47、e agreed between customer and supplier. The qualification procedure for aerospace standard products (e.g. according to EN 9133 or an equivalent aerospace accepted and established qualification procedure) shall be used and documented according to the specified tests if not otherwise agreed between cu

48、stomer and supplier. prEN 6133:2018 (E) 14 Annex A(normative) Verification of fatigue loads A.1 Standard rod end fatigue spectrum See Figure A.1. A.2 Method The loading shall be tensioned with the maximum load equal to the fatigue load given on applecable EN standard and with the minimum load equal

49、to 10% of the fatigue load see typical fatigue spectrum in Figure A.1. Loads shall be maintained within 2 % and testing speed shall not exceed 50 Hz. Rod ends shall be capable of with standing 2 milion cycles. Key X) time Y) charge-load a) cycle 1 b) cycle 2 c) cycle 3 Figure A.1 Verification of fatigue loads prEN 6133:2018 (E) 15 Annex B(informative) Standard evolution form Table B.1 Standard evolution form p