AECMA PREN 3136-1990 Aerospace Series Rivets Solid Universal Head in Corrosion Resisting Steel FE-PA92HT Passivated Issue P 1《航空航天系列实心平头柳钉防腐蚀钢l FE-PA92HT钝化处理》.pdf

《AECMA PREN 3136-1990 Aerospace Series Rivets Solid Universal Head in Corrosion Resisting Steel FE-PA92HT Passivated Issue P 1《航空航天系列实心平头柳钉防腐蚀钢l FE-PA92HT钝化处理》.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 3136-1990 Aerospace Series Rivets Solid Universal Head in Corrosion Resisting Steel FE-PA92HT Passivated Issue P 1《航空航天系列实心平头柳钉防腐蚀钢l FE-PA92HT钝化处理》.pdf（5页珍藏版）》请在麦多课文档分享上搜索。

1、 AECMA PREN3L31r 70 LOL23Ll 0004874 T W , -_ A.E.C.M.A. STANDARD NORME A.E.C.M.A. A.E.C.M.A. NORM prEN 3136 - Issue P 1 5 v: r April 1990 DIT PAR LASSOCIATION EUROPEENNE DES CONSTRUCTEURS DE MATRIEL AROSPATIAL 88, boulevard Malesherbes, 75008 PARIS -TL. 45-63-82-85 UDC : Key words : ENGLISH VERSION

2、Aerospace series Rivets, solid, universal head, in ,rrosion resisting steel FE-PA92HT. passivated Srie arospatiale Luft- und Raumfahrt Rivets ordinaires, tte ronde aplatie, en acier rsistant la corrosion FE-PA92HT, Vollniete, mit Universalkopf, aus korrosionsbestndigem Stahl FE-PA92HT. passvs passiv

3、iert This .Aerospace Series. pre-standard has been drawn up under the responsibility of AECMA (Association Europenne des Constructeurs de Matriel Arospatial). It is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Commission fo

4、llowing comment by the Member countries. Subsequent to the publication of this pre-standard, 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 signature of the AECM

5、A Standard Checking Centre (NPS) and formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CEN (European Committee for Standardization) for final vote. Nota - Extra copies can be supplied by B.N.A.E. - 8, rue Moreau-Vauthier - 92100 BO

6、ULOGNE-BILLANCOURT C3 Chairman I Comments should be sent within six months after the date of publication decision I Edition approved for publication Mr. ARENA I A.E.C.M.A. I 88, Bd. Malesherbes 25th April 1990 75008 PARIS - FRANCE aecma 1990 Copyright Association Europeene des Constructeurs de Mater

7、iel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AECMA PREN3L3b 90 - m LOL23LL 0004895 L m . prEN 3136 Page 3 i Scope and field d application This standard specifies the characteristics of solid rivets, with un

8、iversal head, in corrosion resictinq steel, passivated, for maximiim operating temperature 750 OC., ? References IS0 10399, Aerospace - Identificatim marking of solid rivets 1) EN 21 19, tleat resistina steel FE-PA.q?t!T - Solution treated and,precipitation FN 2024, Aerospace series - Identification

9、 marking of standard fastaners FN 2516, Aerospace series - Passivat.ion of corrosion rssistant steels treated - Wires for rivets D I Ir) mm - Aerospace series ?I 11 FN 2898, Aerospace series - Corrosion and heat resisting steel rivets - Techni- cal specification . 3 3 Req!uFred charac terist ics 3.1

10、 Sonfigiiratirzn - Dimensions - Masses See figiire and tables 1 and ?. 3.? %teriai EN 2119. The riwt shall be delivet*ed in solution treated and precipitation treated condi tion Shear strenclth of the rivets shall be : !?!in MPa 12 65tl MPa, 3.3 Surface treatment FFI ?516, Cl, - c- 11 In preparation

11、 at the date QF publication of the present standard. 71 Piihiished as AECMA standard at the date of publication of the present standard. 31 Puhlstied as AECMR pro-standard at the date of piihlication of the present standard. Copyright Association Europeene des Constructeurs de Materiel Aerospatial P

12、rovided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AECMA PREN3L3b 90 W LOl123Ll 000489b 3 W j Diameter code 024 03 2 040 04 8 056 064 prEN 3136 Page 4 D 6) E F GH J +8J2 max. min. max. min. max. min. 2,45 2,35 5 3,25 3,15 6,7 6 3

13、,2 2,4 1 ,4 4,s 2,4 1,8 1 2 s9 3 89 4,05 3,94 8,3 7,s 4 3 Is7 196 4,9 4,85 4,73 10 9 4,8 3,6 2 5 99 5,65 5,53 11,7 10,s 5,6 4,2 2,4 2 6,8 6,45 6,33 13,3 12,l 6,4 4,8 2,7 7J8 drill start (code 1) opt ional Radiused tail end (code IRtt) 1) 2) Non-radiueed tail end ( code INH) Figure Table 1 5) Dimensi

14、ons in miiiimetres 1) The length range is limited (see table 2). 2) Chamfer or convex radius, at manufacturers option. 3) Rounded edge permissible within limiting E dimension, 4) Or (L-H)/2 if (L-H) 0. 5) Values applicable after passivation, 6) Over length H, D max. may increase by 0,03. Copyright A

15、ssociation Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Di ameter code I= o1 2 12 Dl4 1 14 01 6 16 O1 7 17 O1 8 18 o1 9 19 020 2 022 22 b2 4 24 02G 26 02 8 2 030 30 03 2

16、32 03 5 35 040 I 40 I 03 2 02 4 I Mass kp/1000 Mass kg/l O00 pieces 3) 0,426 0,492 O ,555 0,G21 O ,684 o ,750 0,813 0,879 0,942 1,007 1,071 1,135 1,199 1,263 1,331 1,396 1,460 1,589 1,717 1) Values applicable after passivation. 2) Tail end code (see figure). prEN 3136 Page S Table 2 1 Dimensions in

17、millimetres 04 0 O4 8 Of 6 3,140 3,343 3,544 2,107 X X 3,028 2,256 X X 3,226 2,399 X X 3,422 2,542 X X 3,618 2,688 X X 3,816 2,834 X X 4,016 2,979 X X 4,217 II I I XI X I 4,829 3,412 4,860 X X 6,772 5,149 X X 7,164 5,613 X 7,757 6,394 X 8,742 064 2) I pass kg/ 1 000 - picces N R 3) x x 3,773 X X 4,0

18、32 X X 4,291 x x 4,55 31 Approximative values, calculated on the basis of 7,9 kg/dm3, given for information purpose only. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without li

19、cense from IHS-,-,-I i ! AECMA PREN313b 90 L0123LL 0004898 7 : prEN 3136 Page 6 4 Designa tion Example : Description block RIVET Identity block EN3136-O T Number of EN standard I Diameter code (see table 1) IO .- DR1 Tail end code (see figure) Drill start code (see figure) J Length code (see table 2

20、) Note - If necessary, the originator code 19005 may be introduced between the description block and identity block. 5 Marking 5.1 Rivets identification. EN 2424, style G. 5.2 Material identification IS0 10299, 6 Technical specification EN 2898. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-