ASD-STAN PREN 2911-1986 Aerospace Series Shank Nuts Self Locking Flange Restrained in Heat Resisting Steel FE-PA92HT (A286) Silver Plated Classification 1100 MPa 650 Degrees Celsiu.pdf

上传人:fuellot230 文档编号:451593 上传时间:2018-11-23 格式:PDF 页数:4 大小:148.58KB
下载 相关 举报
ASD-STAN PREN 2911-1986 Aerospace Series Shank Nuts Self Locking Flange Restrained in Heat Resisting Steel FE-PA92HT (A286) Silver Plated Classification 1100 MPa 650 Degrees Celsiu.pdf_第1页
第1页 / 共4页
ASD-STAN PREN 2911-1986 Aerospace Series Shank Nuts Self Locking Flange Restrained in Heat Resisting Steel FE-PA92HT (A286) Silver Plated Classification 1100 MPa 650 Degrees Celsiu.pdf_第2页
第2页 / 共4页
ASD-STAN PREN 2911-1986 Aerospace Series Shank Nuts Self Locking Flange Restrained in Heat Resisting Steel FE-PA92HT (A286) Silver Plated Classification 1100 MPa 650 Degrees Celsiu.pdf_第3页
第3页 / 共4页
ASD-STAN PREN 2911-1986 Aerospace Series Shank Nuts Self Locking Flange Restrained in Heat Resisting Steel FE-PA92HT (A286) Silver Plated Classification 1100 MPa 650 Degrees Celsiu.pdf_第4页
第4页 / 共4页
亲,该文档总共4页,全部预览完了,如果喜欢就下载吧!
资源描述

1、I I, -. . A.E,C.M.A. STANDARD NORM E A.E. C. M .A. A.E.C.M.A. NORM prEN2911 Issue P 1 May 1986 EDITE PAR LASSOCIATION EUROPENNE DES CONSTRUCTEURS DE MATRIEL AEROSPATIAL 88, boulevard Malesherbes, 75008 PARIS -TL. 45-63-82-85 UDC : Key words : ENGLISH VERSION Aerospace series Shank nuts, self locking

2、, flange restrained, in heat resisting steel FE-PA92HT (A286) silver plated Classification : 1 I O0 MPa/650 OC Srie arospatiale crou sertir, auto-freinant, en acier rsistant chaud FE-PA92HT (A286) argent Classification : 11 O0 MPa/650 OC Luft- und Raumfahrt Einnietmuttern, selbstsichernd, aus hochwa

3、rmfestem Stahl FE-PA92HT (A286) versilbert Klasse : 11 O0 MPa/650 OC This standard is initially published on green paper for the needs of AECMA-Members (Association Europenne des Constructeurs de Matriel Arospatial). It has been technically approved by the experts of the concerned AECMA Commission f

4、ollowing comment by the manufacturers of the Member countries. After examination and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of the Official Services of the Member countries it will be published in its final version on yellow paper as an AECMA Standard. Nota - Extr

5、a copies can be supplied by B.N.A.E. - 8, rue Moreau-Vauthier - 92100 BOULOGNE-BILLANCOURT I Comments should be sent within six months C8 Chairman I after the date of publication decision Edition approved for publication 15 May 1986 A.E.C.M.A. 88, Bd. Malesherbes Mr WILLIAMS 75008 PARIS - FRANCE aec

6、ma 1986 prEN2911 Page 3 Issue PI 1 Scope and field of application This standard specif ies the dimensions of self-locking, silver-coated shank nuts with MJ- thread, of heat resisting steel FE-PA92-HT, for aerospace applications at a maximum temperature of 650 OC. 2 References EN2399 Heat resisting s

7、teel FE-PA92-HT; Rm-900 MPa, bars for forged bolts DG25 mm - Aerospace series EN2424 Identification marking of standard fasteners - Aerospace series EN2786 Aerospace series - Electrolytic deposition of silver on metals (1) EN3004 Aerospace series - Nuts, self-locking, material FE-PA92-HT, classifica

8、tion 1100 MPa/650 OC; Technical specifications (1) IS05855/1 Aerospace construction - MJ threads - Part 1: Basic profile iSO5855/2 Aerospace construction - MJ threads - Part 2: Dimensions for bolts and nuts IS08788 Aerospace Fasteners - Tolerances of form and position for nuts (1) 3 Required charact

9、eristics 3.1 Material Heat resisting steel FE-PA92-HT according to EN2399 3.2 Configuration - Dimensions - Tolerances - Masses Configuration, dimensions, tolerances (2) and masses shall be in conformity with the values in the figure and in table. Dimensions are after coating. 3.3 Surface treatment S

10、ilver coat to EN2786, coating thickness 5 to 15 /um. On nuts MJ6 and larger, the coating thickness shall be not less than 5 /um, measured at the pitch diameter. Nuts MJ5 and smaller shall show complete coating coverage on the threads. i : - 3.4 Thread surface Thread surface will be achieved by norma

11、l methods of manufacture. Previous page is blank (i) in preparation (2) In conformity with IS08788 for tolerances of form and position I AE-C-NA PRENZILL Bb it032311 0004i.107 b M Thread CJ P E H L C T 2 t0,l o Diarne ter D %,i o -0,l h13 h14 TOI. + -0,l +0,25 rnax. code 050 fdJ 50, -4li6H 7 5,2 6,5

12、 13 7 1,8 t0,10 9,5 2,4 8,5 060 MJ 6x1 -4H5H O 6,2 7,5 14 8 1,8 t0,lO 10,5 2,4 9,5 070 MJ 7x1 -4H51-I 9 7,2 8,5 16 9 2,8 t0,lO 11,5 3,4 10,5 O80 MJ 8x1 -4H51-I 10 ,2 9,5 17 10 3,2 :0,15 12,5 3,9 11,5 prEN2911 Page 4 Issue PI Mass - kg/lUUU parts 2,70 3,35 4,16 5;40 o 13 A Bearing surface may be flat

13、 or concav, WnIbut shall not be convex. Figure - Configuration Table - Dimensions and masses AECMA PREN2911 Bb W LOI12311 OOL1408 B -2 Description block prEN2911 Page 5 Issue PI Identity block 4 Designation 5 Marking The shank nuts shall be marked according to EN2424, class A. 6 Technical specification The shank nuts shall conform with the requirements of EN3004 (1). (1) In preparation

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