ASD-STAN PREN 4613-2007 Spherical plain bearings in corrosion resisting steel with self-lubricating liner narrow series Dimensions and loads Inch series (Edition 1)《窄系列带自润滑衬套的耐蚀钢制普.pdf

上传人:amazingpat195 文档编号:453333 上传时间:2018-11-23 格式:PDF 页数:11 大小:159.23KB
下载 相关 举报
ASD-STAN PREN 4613-2007 Spherical plain bearings in corrosion resisting steel with self-lubricating liner narrow series Dimensions and loads Inch series (Edition 1)《窄系列带自润滑衬套的耐蚀钢制普.pdf_第1页
第1页 / 共11页
ASD-STAN PREN 4613-2007 Spherical plain bearings in corrosion resisting steel with self-lubricating liner narrow series Dimensions and loads Inch series (Edition 1)《窄系列带自润滑衬套的耐蚀钢制普.pdf_第2页
第2页 / 共11页
ASD-STAN PREN 4613-2007 Spherical plain bearings in corrosion resisting steel with self-lubricating liner narrow series Dimensions and loads Inch series (Edition 1)《窄系列带自润滑衬套的耐蚀钢制普.pdf_第3页
第3页 / 共11页
ASD-STAN PREN 4613-2007 Spherical plain bearings in corrosion resisting steel with self-lubricating liner narrow series Dimensions and loads Inch series (Edition 1)《窄系列带自润滑衬套的耐蚀钢制普.pdf_第4页
第4页 / 共11页
ASD-STAN PREN 4613-2007 Spherical plain bearings in corrosion resisting steel with self-lubricating liner narrow series Dimensions and loads Inch series (Edition 1)《窄系列带自润滑衬套的耐蚀钢制普.pdf_第5页
第5页 / 共11页
亲,该文档总共11页,到这儿已超出免费预览范围,如果喜欢就下载吧!
资源描述

1、ASD STANDARD NORME ASD ASD NORM prEN 4613 Edition P 1 October 2007 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONGulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: Descriptors: ENGLISH VERSION Aerospace seri

2、es Spherical plain bearings in corrosion resisting steel with self-lubricating liner, narrow series Dimensions and loads Inch series Srie arospatiale Rotules lisses rsistant la corrosion garniture autolubrifiante, srie troite Dimensions et charges Sries en inches Luft- und Raumfahrt Gelenklager aus

3、korrosionsbestndigem Stahl mit selbstschmierender Beschichtung, schmale Reihe 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 prEN 4613:20072 Contents Page Foreword2 1 Scope 3 2 Normative references 3 3 Terms and definitions .3 4 Symbols and abbreviations 4 5 Requirements.4 6 Designation . 11 7 Marking 11 8 Technical specification 11 Foreword This sta

8、ndard 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 4613:20073 1 Scope This standar

9、d specifies the characteristics of bearings, spherical plain in corrosion resisting steel with self-lubricating liner, narrow series for aerospace applications. They are intended for use in fixed or moving parts of the aircraft structure and control mechanisms. They shall be used in the temperature

10、range 55 C to 163 C. 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 (including any amendments) applies. ISO 1

11、132-1, Rolling bearings Tolerances Part 1: Terms and definitions. ISO 8075, Aerospace Surface treatment of hardenable stainless steel parts. EN 2030, Steel FE-PM43 Hardened and tempered Bars D 150 mm Aerospace series. 1)EN 2133, Aerospace series Cadmium plating of steels with specified tensile stren

12、gth 1 450 MPa, copper, copper alloys and nickel alloys. EN 2424, Aerospace series Marking of aerospace products. EN 2755, Aerospace series Bearings spherical plain, in corrosion resisting steel with self-lubricating liner Elevated loads at ambient temperature Technical specification. 2)EN 3161, Aero

13、space series Steel FE-PM3801 (X5CrNiCu17-4) Air melted Solution treated and precipitation treated Bar a or D 200 mm Rm 930 MPa. 2)TR 4475, Aerospace series Bearings and mechanical transmissions for airframe applications Vocabulary. 3)3 Terms and definitions For the purposes of this document, the ter

14、ms and definitions given in TR 4475 apply. 1) Published as ASD Standard at the date of publication of this standard. 2) Published as ASD Prestandard at the date of publication of this standard. 3) Published as ASD Technical Report at the date of publication of this standard. prEN 4613:20074 4 Symbol

15、s and abbreviations Symbols of limit deviations are in accordance with definitions of ISO 1132-1. = maximum angle of tilt of the outer ring with respect to the inner ring, with the spherical raceway of the outer ring being completely in contact with the inner ring. (see Figures 1 and 2) Ca = permiss

16、ible static axial load Cs = permissible static radial load C25 = permissible dynamic radial load by 25 000 cycles dmp = single plane mean bore diameter deviation Dmp = single plane mean outside diameter deviation ds = deviation of a single bore diameter Ds = deviation of a single outside diameter 5

17、Requirements 5.1 Configuration, dimensions, tolerances and mass According to Figures 1 and 2 and Table 1. Dimensions and tolerances are expressed in millimetres (inches). Values after passivating and/or cadmium plating. 5.2 Surface roughness In accordance with Figures 1 and 2. Values in micrometres

18、(micro inches), apply prior to surface treatment. 5.3 Material Inner ring: According to EN 2030, hardness 55 HRC 62 Outer ring: According to EN 3161, hardness 28 HRC 38 before swaging Liner: Self-lubricating liner according to EN 2755 5.4 Surface treatment Code T: Surface treatment according to ISO

19、8075 for inner ring before swaging. Code P: Without swaging groove code S: Surface treatment according to ISO 8075 for inner ring before swaging. Cadmium plating of outer ring: 5 m to 8 m (0.2 in to 0.3 in) according to EN 2133 (cylindrical surface area and chamfers and both end surfaces at manufact

20、urers option), followed by chromating. With swaging groove code R: Surface treatment according to ISO 8075 for inner ring before swaging. Cadmium plating of outer ring: 5 m to 8 m (0.2 in to 0.3 in) according to EN 2133 (cylindrical surface area, broken angles and radii, respectively, as well as bot

21、h end surfaces up to the swaging grooves), followed by chromating. prEN 4613:20075 5.5 Loads and starting torque values According to Tables 2 and 3. aSet back bSwaging groove cTFE liner dCadmium plated Figure 1 Code R with swaging grooves prEN 4613:20076 aSet back bTFE liner cCadmium plated Figure 2

22、 Code S without swaging grooves prEN 4613:20077 Table 1 Dimensions, tolerances and mass Diameter B C d1 d2P d D Limit deviation 00,05 0,13 00,2000,254Dia-meter code admpdsDmpDs(00.002) ( 0.005) min. (00.007)(00.0100)03 4,826 (0.1900) 14,287 (0.5625)7,14 (0.281) 5,54 (0.218) 7,44 (0.304) 12,70(0.500)

23、 04 6,350 (0.2500) 16,667 (0.6562)8,71 (0.343) 6,35 (0.250) 9,25 (0.364) 15,09(0.594) 0,635(0.0250)05 7,937 (0.3125) 19,050 (0.7500)00,008(00.0003)9,53 (0.375) 7,14 (0.281) 10,64 (0.419) 16,51(0.650) 06 9,525 (0.3750) 20,637 (0.8125)10,31(0.406) 7,93 (0.312) 12,06 (0.475) 18,08(0.712) 07 11,113 (0.4

24、375) 23,017 (0.9062)11,10(0.437) 8,71 (0.343) 13,46 (0.530) 20,47(0.806) 0,889(0.0350)08 12,700 (0.5000) 25,400 (1.0000)12,70(0.500) 9,91 (0.390) 15,24 (0.600) 22,25(0.876) 09 14,288 (0.5625) 27,780 (1.0937)14,28(0.562) 11,10 (0.437) 17,02 (0.670) 24,64(0.966) 10 15,875 (0.6250) 30,163 (1.1875)00,00

25、9(00.0004)15,88(0.625) 12,70 (0.500) 18,77 (0.739) 27,00(1.063) 12 19,050 (0.7500) 36,513 (1.4375)19,05(0.750) 15,06 (0.593) 23,37 (0.920) 33,35(1.313) 14 22,225 (0.8750) 39,688 (1.5625)00,013(00.0005)00,011(00.0004)00,013(00.0005)22,23(0.875) 17,86 (0.703) 24,89 (0.980) 36,52(1.438) 16 25,400 (1.00

26、00) 44,450 (1.7500)25,40(1.000) 20,24 (0.797) 28,40 (1.118) 41,30(1.626) 20 31,750 (1.2500) 50,800 (2.0000)27,76(1.093) 23,93 (0.942) 36,42 (1.434) 47,65(1.876) 24 38,100 (1.5000) 61,912 (2.4370)33,33(1.312) 28,70 (1.130) 46,43 (1.828) 58,75(2.313) 28 44,450 (1.7500) 71,437 (2.8120)38,89(1.531) 33,4

27、5 (1.317) 50,71 (1.997) 68,27(2.688) 32 50,800 (2.0000) 80,962 (3.1875)00,013(00.0005) 0,0030,015+(0.00010.0006+)00,013(00.0005)0,0030,015+(0.00010.0006+)44,45(1.750) 38,23 (1.560) 61,98 (2.530) 77,83(3.064) 1,397(0.0550)continued prEN 4613:20078 Table 1 (concluded) r1 r2 r3 r4 b 1 2 N T 00,254or 0,

28、5 0,5 Mass g/piece Dia-meter code a(00.0100) max. r4 45 min. max. 03 7 04 20 10 05 0,508 (0.0200) 0,127 (0,0050) to 0,254 (0.0100) 10 0,08 (0.003) 14 06 9 18 07 23 08 0,5 (0.02) 32 09 41 10 0,762 (0.0300) 1,02 (0.040) 54 12 95 14 8 123 16 9 173 20 5,5 240 24 5 440 28 5,5 663 32 1,016 (0.0400) 0,254

29、(0.0100) to 0,432 (0.0170) 0,127 (0.0050) 0,127 (0.0050)to 0,381 (0.0150)5 30 30 1,14 (0.045) 0,13 (0.005) 980 aThe diameter code corresponds to bore diameter d in 1/16 inch. bThe acceptance value is the maximum value for the user. prEN 4613:20079 Table 2 Loads Permissible static load kN Ultimate st

30、atic load kN Dynamic load dkN Diameter code aRadial b eCsAxial b c fCaRadial bAxial bRadial gC2503 16,7h2,4 25,0 3,6 10,3 04 30,6 3,4 45,9 5,1 15,0 05 39,5 4,4 59,2 6,7 19,3 06 49,5 5,7 74,2 8,5 24,2 07 60,5 7,0 90,8 10,5 29,6 08 79,5 9,4 119,3 14,0 38,9 09 90,6 14,5 135,9 21,8 44,3 10 117,9 20,1 17

31、6,9 30,1 57,7 12 173,4 28,9 260,1 43,3 84,8 14 233,9 42,9 351,0 64,3 114,4 16 307,9 57,0 461,9 85,5 150,5 20 446,1 82,8 669,2 124,2 218,1 24 679,5 123,4 1 019,3 185,0 332,2 28 896,4 171,7 1 344,6 257,5 438,2 32 1 233,9 228,4 1 850,8 342,6 603,2 aThe diameter code corresponds to bore diameter d in 1/

32、16 inch. bDefinition and testing for permissible and ultimate static load according to EN 2755 and TR 4475. cThese values apply to loose spherical bearings. For installed bearings, the push-out loads may be smaller than these values. dDefinition and testing for dynamic radial load according to EN 27

33、55. ePermissible surface pressure 450 MPa, definition according to TR 4475. fPermissible surface pressure for diameter code 03 to 08: 150 MPa and for diameter code 09 to 32: 225 MPa. gSurface pressure 220 MPa, definition according to TR 4475. hLimit by bolt bending Definition: solid shaft rigid clam

34、ping on both sides uniform load permissible bending stress 1 350 MPa permissible shear stress 1 200 MPa prEN 4613:200710 Table 3 Starting torque values Starting torque bNm Diameter code aNormal Code N Reduced Code R 03 0,06 to 0,34 04 05 06 0 to 0,11 07 08 09 10 12 0,11 to 0,56 0,03 to 0,15 14 16 0,

35、23 to 0,90 0,04 to 0,25 20 24 28 32 0,23 to 1,50 0,05 to 0,32 aThe diameter code corresponds to bore diameter d in 1/16 inch. bDefinition and testing for starting torque according to EN 2755. prEN 4613:200711 6 Designation EXAMPLE Description block BEARING Identity block EN4613R03NTA Number of this

36、standard Swaging groove code (see Figures 1 and 2) Diameter code (see Table 1) Starting torque code (see Table 3) Surface treatment (see 5.4) Technology code Where the following technology codes are applied: code A, bonded liner technology; code B, injected or moulded liner technology; without code,

37、 both technologies can be used at users convenience. NOTE If necessary, the code I9005 shall be placed between the description block and the identity block. 7 Marking According to EN 2424, style A. The marking position is at the manufacturers option. Bearings ordered without technology code shall be delivered marked in accordance with its technology code. 8 Technical specification According to EN 2755.

展开阅读全文
相关资源
  • ASD-STAN PREN 4022-1994 Aerospace Series Pipe Coupling 8 Degrees 30 in Titanium Alloy Elbows 90 Degrees Bulkhead Welded (Edition P1)《航空航天系列 钛合金制830管接头 90焊接穿壁弯头 第P1版[替代 ASD-STAN.pdfASD-STAN PREN 4022-1994 Aerospace Series Pipe Coupling 8 Degrees 30 in Titanium Alloy Elbows 90 Degrees Bulkhead Welded (Edition P1)《航空航天系列 钛合金制830管接头 90焊接穿壁弯头 第P1版[替代 ASD-STAN.pdf
  • ASD-STAN PREN 4021-1994 Aerospace Series Pipe Coupling 8 Degrees 30 in Titanium Alloy Elbows 90 Degrees Bulkhead (Edition P1)《航空航天系列 钛合金制830管接头 90穿壁弯头 第P1版[替代 ASD-STAN PREN 325.pdfASD-STAN PREN 4021-1994 Aerospace Series Pipe Coupling 8 Degrees 30 in Titanium Alloy Elbows 90 Degrees Bulkhead (Edition P1)《航空航天系列 钛合金制830管接头 90穿壁弯头 第P1版[替代 ASD-STAN PREN 325.pdf
  • ASD-STAN PREN 4018-2007 Aerospace series Pipe coupling 8 degree 30 in titanium alloy Elbows 90 degree with thrust wire nut (Edition P2)《航空航天系列 钛合金制830管接头 旋转螺母、带止推金属丝帽的90弯头 第P2版.pdfASD-STAN PREN 4018-2007 Aerospace series Pipe coupling 8 degree 30 in titanium alloy Elbows 90 degree with thrust wire nut (Edition P2)《航空航天系列 钛合金制830管接头 旋转螺母、带止推金属丝帽的90弯头 第P2版.pdf
  • ASD-STAN PREN 3256-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 45 Degree Swivel Nut Welded (Edition P 2 )《航空航天系列 钛合金制830管接头 旋转螺母、焊接式45弯头 第P2版[替代为 AS.pdfASD-STAN PREN 3256-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 45 Degree Swivel Nut Welded (Edition P 2 )《航空航天系列 钛合金制830管接头 旋转螺母、焊接式45弯头 第P2版[替代为 AS.pdf
  • ASD-STAN PREN 3254-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 90 Degree Bulkhead Welded (Edition P 2)《航空航天系列 钛合金制830管接头 焊接式穿壁90弯头 第P2版[替代为 ASD-STAN.pdfASD-STAN PREN 3254-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 90 Degree Bulkhead Welded (Edition P 2)《航空航天系列 钛合金制830管接头 焊接式穿壁90弯头 第P2版[替代为 ASD-STAN.pdf
  • ASD-STAN PREN 3253-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 90 Degree Bulkhead (Edition P 2 )《航空航天系列 钛合金制830管接头 穿壁90弯头 第P2版[替代为 ASD-STAN PREN 402.pdfASD-STAN PREN 3253-1994 Aerospace Series Pipe Coupling 8 Degree 30 in Titanium Alloy Elbow 90 Degree Bulkhead (Edition P 2 )《航空航天系列 钛合金制830管接头 穿壁90弯头 第P2版[替代为 ASD-STAN PREN 402.pdf
  • ASD-STAN TR AMS2750-2009 《航空航天系列 航空航天材料规范 高温测定法》.pdfASD-STAN TR AMS2750-2009 《航空航天系列 航空航天材料规范 高温测定法》.pdf
  • ASD-STAN TR AMS2750 FRENCH-2009 《航空航天系列 航空航天材料规范 高温测定法》.pdfASD-STAN TR AMS2750 FRENCH-2009 《航空航天系列 航空航天材料规范 高温测定法》.pdf
  • ASD-STAN TR 9536-2008 Aerospace series Declarable Substances Recommended Practice《航空航天系列 需申报物质 建议做法》.pdfASD-STAN TR 9536-2008 Aerospace series Declarable Substances Recommended Practice《航空航天系列 需申报物质 建议做法》.pdf
  • ASD-STAN TR 9535-2008 Aerospace series Substance declaration (Edition 1)《航空航天系列 物质声明 第1版》.pdfASD-STAN TR 9535-2008 Aerospace series Substance declaration (Edition 1)《航空航天系列 物质声明 第1版》.pdf
  • 猜你喜欢
    相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > ASD

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1