AECMA PREN 6057-2007 Aerospace series Rod-ends with bearing per EN4265 in corrosion resisting steel internal threaded shank Dimensions and loads Inch series Edition P 1《航空航天系列.内螺纹柄.pdf

1、ASD STANDARD NORME ASD ASD NORM prEN 6057 Edition P 1 October 2007 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONAvenue de Tervuren, 270 - B-1150 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: Descriptors: ENGLISH VERSION Aero

2、space series Rod-ends, with bearing per EN4265 in corrosion resisting steel, internal threaded shank Dimensions and loads Inch series Srie arospatiale Embouts rotules lisses EN4265 en acier rsistant la corrosion avec filetage intrieur Dimensions et charges Sries en inches Luft- und Raumfahrt senkpfe

3、, mit Gelenklager nach EN4265 aus korrosionsbestndigem Stahl mit Innengewinde Mae und Belastungen Inch Reihe This “Aerospace 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

4、the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically

5、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 a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (E

6、N). 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 national standards conflicting with the EN. Edition approved for publication 31 October 2007 Comments should be sent within six months after the date

7、 of publication to ASD-STAN Mechanical Domain Copyright 2007 by ASD-STAN Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 6057:20072 Contents Page Foreword2 1 Scope

8、3 2 Normative references 3 3 Terms and definitions .4 4 Symbols and abbreviations 4 5 Requirements.4 6 Designation 9 7 Marking .9 8 Technical specification .9 Annex A (normative) Verification of fatigue loads 10 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Mec

9、hanical 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. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for Res

10、aleNo reproduction or networking permitted without license from IHS-,-,-prEN 6057:20073 1 Scope This standard specifies the characteristics of adjustable rod-ends consisting of: a spherical plain bearing, metal to metal, in corrosion resisting steel, wide series (EN 4265), a rod-end with internal th

11、readed shank. They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms. They shall be used in the temperature range 54 C to 150 C. As they are lubricated by means of the following greases: Code A: Grease as per MIL-PRF-23827, operating temperature ran

12、ge 73 C to 121 C, Code B: Grease as per MIL-PRF-81322, operating temperature range 54 C to 177 C. The range of application for bearings lubricated with grease per code A is limited to 121 C. In both cases the spherical surfaces of the outer or inner ring have to be provided with a dry-film lubricant

13、 as per MIL-PRF-46010 or equivalent (anti-seizing protection). 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document

14、 (including any amendments) applies. ISO 1132-1, Rolling bearings Tolerances Part 1: Terms and definitions. ISO 3161, Aerospace UNJ threads General requirements and limit dimensions. ISO 8074, Aerospace Surface treatment of austenitic stainless steel parts. EN 2133, Aerospace series Cadmium plating

15、of steels with specified tensile strength 1 450 MPa, copper, copper alloys and nickel alloys. EN 2424, Aerospace series Marking of aerospace products. EN 4265, Aerospace series Bearings, spherical plain, in corrosion resisting steel Wide series Dimensions and loads Inch series. 1)EN 6099, Aerospace

16、series Rod-ends with plain bearing Technical specification. 2)MIL-PRF-23827, Grease, aircraft and instrument, gear and actuator screw, NATO Code G-354, metric. 3)MIL-PRF-81322, Grease, aircraft, general purpose, wide temperature range, NATO code G-395. 3)MIL-PRF-46010, Lubricant, solid film, heat cu

17、red, corrosion-inhibiting. 3)1) Published as ASD Prestandard at the date of publication of this standard. 2) In preparation at the date of publication of this standard. 3) Published by: Department of Defense (DoD), the Pentagon, Washington, D.C., 20307, USA. Copyright European Association of Aerospa

18、ce Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 6057:20074 AMS 5643, Steel, corrosion resistant, bars, wire, forgings, tubing, and rings 16Cr - 4.0Ni - 0.30Cb - 4.0Cu solution heat treated, precipitation h

19、ardenable. 4)TR 4475, Aerospace series Bearings and mechanical transmissions for airframe applications Vocabulary. 5)3 Terms and definitions For the purposes of this document, the terms and definitions given in ISO 1132-1 and TR 4475 apply. 4 Symbols and abbreviations = maximum angle of tilt of the

20、outer ring with respect to the inner ring, the spherical surface of the outer ring being completely in contact with the inner ring Cp = push out loads Cs = permissible static radial load dmp = single plane mean bore diameter deviation ds = deviation of a single bore diameter Cf= fatigue loads 5 Requ

21、irements 5.1 Configuration, dimensions, tolerances and mass See Figure 1 and Table 1. Dimensions and tolerances are expressed in millimetres (inches). 5.2 Surface roughness In accordance with Figure 1. 5.3 Material Inner ring : see product standard EN 4265 Outer ring : see product standard EN 4265 R

22、od-end body : see AMS 5643, hardness 35 HRC 42 5.4 Surface 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) Except: threads, 5 m to 15 m (200 in to 600 in). Bearing : See EN 4265, without c

23、ode for passivated 4) Published by: Society of Automotive Engineers Inc., 400 Commonwealth Drive, Warrendale, PA 15096-0001 USA. 5) Published as ASD Technical Report at the date of publication of this standard. Copyright European Association of Aerospace Industries Provided by IHS under license with

24、 AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 6057:20075 5.5 Loads and clearance See Tables 3 and 4. 0,8(32)0,8(32)45aInspectionhole(0.25)l1,6(63)ADR= 3,012ld4m6,35BCU D2 dqd3Ts3,2(125)0,8(32)1,6(63)X0,25(0.010)XX0,127 to 0,381(0.005 to 0.015)radius o

25、r chamfer at 45Xl3max.0,8(32)(0.12)min.YrUYoptionald2a)UKey 1 Inspection hole 2 0,127 to 0,381 (0.005 to 0.015) radius or chamfer at 45 aThread Pitch diameter Figure 1 Configuration 2 1 Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo r

26、eproduction or networking permitted without license from IHS-,-,-prEN 6057:20076 Table 1 Dimensions, tolerances and mass d3d2bd D D2d4B C q Limit deviation Dia-meter codeaType of thread UNJF-38 nominal max. dmpdsBearing diametermin. Drill 0,050(0.0020) 00,25+(00.010+) 0,38 ( 0.015) 03 4,826 (0.1900)

27、 04 6,350 (0.2500) 15,875(0.6250)7,62 (0.300)8,56 (0.337) 05 0.3125-24 7,249 (0.2854) 7,937 (0.3125) 17,463(0.6880)9,14 (0.360)11,10 (0.437) 8,31 (0.327) 9,65 (0.380)06 0.3750-24 8,837 (0.3479) 9,525 (0.3750) 20,638(0.8130)11,84(0.466)12,70 (0.500) 10,57 (0.416) 11,18(0.440)07 0.4375-20 10,287 (0.40

28、50) 11,113 (0.4375) 23,017(0.9060)13,64(0.537)14,27 (0.562) 11,48 (0.570) 12,70(0.500)08 0.5000-20 11,875 (0.4675) 12,700 (0.5000) 25,400(1.0000)15,42(0.607)15,88 (0.625) 13,08 (0.515) 14,22(0.560)10 0.6250-18 14,958 (0.5889) 15,875 (0.6250) 30,163(1.1880)18,97(0.747)19,05 (0.750) 14,66 (0.577) 17,5

29、3(0.690)12 0.7500-16 18,019 (0.7094) 19,050 (0.7500) 34,925(1.3750)21,64(0.845)16,26 (0.640) 20,83(0.820)14 0.8750-14 21,046 (0.8286) 22,225 (0.8750) 0,0130(0.00050)41,275(1.6250)25,27(0.995)22,23 (0.875) 19,43 (0.765) 23,88(0.940)16 1.0000-12 24,026 (0.9459) 25,400 (1.0000) 0,0130(0.00050) 0,0150,0

30、03+(0.00060.0001+)53,975(2.1250)32,23(1.269)1,77 (0.070)34,93 (1.375) 25,78 (1.015) 27,18(1.070)continued Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 6057:20077

31、 Table 1 Dimensions and mass (concluded) m l1l2l3 U A S T r cMass Dia-meter code a 0,25 ( 0.010) 0,25 ( 0.010) 0,761,52+(0.0300.060+) max. 0,25 ( 0.010) 0,13 ( 0.005) 0.25 ( 0.010) min. g/piece 03 12,70 (0.500) 34,93 (1.375) 04 12,95 (0.510) 37,31 (1.469) 22,03(0.867) 9,30 (0.366) 20,50(0.807) 11,10

32、 (0.437) 16 27 05 14,75 (0.581) 34,93 (1.375) 19,05 (0.750) 25,40(1.000) 12,55(0.494) 22,90(0.902) 10,72(0.422) 12,70 (0.500) 15,5 31 06 16,51 (0.650) 41,28 (1.625) 23,80 (0.937) 28,58(1.125) 9,70 (0.382) 26,00(1.024) 14,40(0.567) 14,30 (0.563) 1,0 to 3,0 9,5 50 07 18,29 (0.720) 46,02 (1.812) 26,98

33、(1.062) 31,75(1.250) 15,00(0.591) 29,20(1.150) 15,49(0.610) 15,88 (0.625) 11,0 82 08 22,10 (0.870) 53,98 (2.125) 28,58 (1.125) 34,93(1.375) 16,70(0.657) 34,00(1.339) 18,67(0.735) 19,05 (0.750) 9,5 127 10 25,40 (1.000) 66,68 (2.625) 38,10 (1.500) 38,10(1.500) 17,40(0.685) 38,70(1.524) 21,84(0.860) 22

34、,23 (0.875) 12,0 190 12 26,92 (1.060) 73,03 (2.875) 41,15 (1.620) 44,45(1.750) 19,40(0.764) 45,10(1.776) 25,02(0.985) 25,40 (1.000) 14,0 231 14 30,15 (1.187) 85,73 (3.375) 47,63 (1.875) 52,38(2.062) 24,20(0.953) 51,40(2.024) 28,19(1.110) 28,58 (1.125) 6,0 426 16 33,33 (1.312) 104,78 (4.125) 53,98 (2

35、.125) 58,73(2.312) 36,50(1.437) 70,50(2.776) 31,37(1.235) 31,75 (1.250) 3,0 to 6,0 14,5 612 aThe diameter code corresponds to nominal diameter d in 1/16 inch. bThread as per ISO 3161. cThe acceptance value is the maximum value for user. Table 2 Code letter for thread Code letter for thread L Left ha

36、nd thread R Right hand thread Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 6057:20078 Table 3 Loads Radial Fatigue load f Permissible static loads Ultimate load

37、Axial static proof load e 2 106 cycles kNkN kN kN Diameter code a Cs b,c d CpCf03 04 20,6 30,9 4,7 3,3 05 21,4 32,0 5,2 3,4 06 29,1 43,6 7,6 4,8 07 31,6 47,3 8,4 6,1 08 60,8 91,2 9,3 9,7 10 66,9 100,4 11,1 11,0 12 88,8 133,1 14,4 14,5 14 102,8 154,2 17,0 17,0 16 154,2 231,2 22,2 38,1 aThe diameter c

38、ode corresponds to nominal diameter d in 1/16 inch bDefinition and testing according to EN 6099, Annex A cLimits by Csfrom rod-end dLimits by Csfrom spherical plain bearings EN 4265 eDefinition and testing according to EN 6099, Annex B fDefinition and testing according to EN 6099, Annex D Table 4 Cl

39、earance Clearance a radial axial normal reduced normal reduced Code N Code P Code N Code P Diameter code max. max. 03 04 05 06 07 0,01 to 0,03 (0.0004 to 0.0012) 0,12 (0.0047) 08 0,002 to 0,01 (0.0001 to 0.0004) 0,035 (0.0014) 10 0,003 to 0,012 (0.0001 to 0.0005) 0,04 (0.0016) 12 14 16 0,01 to 0,05

40、(0.0004 to 0.0020) 0,004 to 0,015 (0.0002 to 0.0006) 0,23 (0.0091) 0,05 (0.0020) aDefinition and testing according to EN 6099, Annex C Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license

41、 from IHS-,-,-prEN 6057:20079 6 Designation EXAMPLE Description block ROD-END Identity block EN6057R04NTA Number of this standard Thread code (see Table 2) Diameter code (see Table 1) Clearance code (see Table 4) Surface treatment (see 4.4) Grease code (see Clause 1) NOTE If necessary, the code I900

42、5 may be placed between the description block and the identity block. 7 Marking EN 2424, style A 8 Technical specification According to EN 6099 Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted withou

43、t license from IHS-,-,-prEN 6057:200710 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 tensiontension with the maximum load equal to the fatigue load given on applicable EN standard and with the minimum load equ

44、al to 10 % of the fatigue load see typical fatigue spectrum in Figure A.1 Loads shall be maintain within 2 % and testing speed shall not exceed 50 Hz Rod-ends shall be capable of with standing of 2 million cycles cycle 1Cf0,1 Cfcycle 2 cycle 30CHARGE-LOADFigure A.1 Verification of fatigue loads Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-