ASD-STAN PREN 2590-1992 Aerospace Series Steel Sheets and Plates Hot Rolled Dimensions (Issue P 1)《航空航天系列 热轧钢薄板材和厚板材 尺寸 第P1版》.pdf

《ASD-STAN PREN 2590-1992 Aerospace Series Steel Sheets and Plates Hot Rolled Dimensions (Issue P 1)《航空航天系列 热轧钢薄板材和厚板材 尺寸 第P1版》.pdf》由会员分享，可在线阅读，更多相关《ASD-STAN PREN 2590-1992 Aerospace Series Steel Sheets and Plates Hot Rolled Dimensions (Issue P 1)《航空航天系列 热轧钢薄板材和厚板材 尺寸 第P1版》.pdf（7页珍藏版）》请在麦多课文档分享上搜索。

1、CEN PREN*2590 92 = 3404589 0033350 T39 = A. E.C. M .A. STAN DARD prEN 2590 NORME A.E.C.M.A. Issue P 1 A.E.C.M.A. NORM August 1992 Edition approved for publication 1992-08-31 EDITE PAR LASSOCIATION EUROPEENNE DES CONSTRUCTEURS DE MATERIEL AFFCSPATl41 Technopolis - 175. rue Jean-Jacques Rousseau - F-9

2、2138 Issy-les-Moulineaux Cedex - TF 1 I 47 36 98 76 Comments should be sent within six months C6 Chairman Mr GREGOIRE after the date of publication decision AECMA 92138 Issy-les Moiilineaux Cdex - FRANCE Teclinopolis - 175 rue Jean-Jacques Rousseau UDC Kev words ENGLISH VERSION Aerospace series Stee

3、l Sheets and plates, hot rolled Dimensions Srie arospatiale Acier Tles et plaques lamines chaud Dimensions Luft- und Raumfahrt Stahl Bleche und Platten, warmgewalzt Mae This .Aerospace Series. pre-standard has been drawn up under the responsibility of AECMA (Association Europenne des Constructeurs d

4、e 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 following comment by the Member countries. Subsequent to the publication of this pre-standard, the technical content shall not be changed

5、to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. 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 submitted as a draft E

6、uropean Standard to CEN (European Committee for Standardization) for final vote. - CEN PREN*2590 92 m 3484589 0033353 975 m prEN 2590 Page 3 1 This standard defines the dimensions and tolerances of sheets and plates, hot rolled, in steel, used in aerospace constructions. 2 References Scope and field

7、 of application EN 2209 EN 2212 EN 2215 EN 2216 EN 2217 EN 2228 EN 2246 EN 2250 EN 2273 EN 2276 EN 2280 EN 2467 EN 2538 EN 2540 EN 2543 EN 2600 EN 2770 EN 2773 EN 2776 Steel FE-PL43S - 900 MPa 4 Rm 4 1100 MPa - Sheets, strips and plates 0,5 rnm S a 4 20 mm - Aerospace series 11 Steel FE-PL43S - 670

8、MPa 4 Rm 4 870 MPa - Sheets, strips and plates 0.5 rnm L a 4 20 mm - Aerospace series 11 Steel FE-PL52S - 980 MPa S Rm 5 1180 MPa - Sheets 0,5 mm 4 a 4 6 mm - Aerospace series 1) Steel FE-PL52S - 1050 MPa 4 Rm 4 1250 MPa - Sheets a 4 2 mm - Aerospace series 1) Steel FE-PL52S - 1080 MPa 4 Rm 4 1250 M

9、Pa - Sheets and plates 2 mm S a 5; 20 mm - Aerospace series 1) Steel FE-PA12 - 500 MPa 4 Rm 4 700 MPa - Sheets 0,5 mm 4 a 4 6 mm - Aerospace series 1) Aerospace series - Steel FE-PL43S - 11 50 MPa 4 Rm i; 1300 MPa - Sheet, strip and plate 0,5 rnrn I a 4 20 mm 21 Aerospace series - Steel FE-PL52S - R

10、m S 700 MPa - Sheets, strips and plates 0,3 rnm I a 5 12 mm 2) Steel FE-PM13S - 1800 MPa 4 Rm 4 2000 MPa - Sheet and plate a 5 30 mm - Aerospace series 1) Steel FE-PA95 - 1750 MPa 4 Rm 4 2000 MPa - Sheet and plate a 4 40 mm - Aerospace series 1) Steel FE-PM37 - 900 MPa 4 Rm 4 11 O0 MPa - Sheet a S 6

11、 mm - Aerospace series Steel FE-PA1 1 - Softened - Sheets or plates 0,5 mm S a S 20 mm - Aerospace series 11 Aerospace series - Steel FE-PM61 - Solution annealed and precipitation hardened - 1240 MPa 4 Rm 4 1310 MPa - Sheet - a 4 10 mm 3) Aerospace series - Steel FE-PM62 - 1200 MPa S Rm 4 1450 MPa -

12、 Sheets Aerospace series - Steel FE-PL43S - Annealed - Sheet and strip 0,3 mm 4 a 4 2 mm - For prevailing torque nuts 3) Aerospace series - Designation of metallic semi-finished products - Rules 31 Aerospace series - Steel FE-PL53S - Hardened and tempered - 1050 MPa 4 Rm 4 1220 MPa - Sheet and plate

13、 - 0,5 mm 4 a I; 12 mm 3) Aerospace series - Steel FE-PM61 - Rm 2 131 O MPa - Sheet and plate - a 4 12 mm Aerospace series - Steel FE-PI 1 - Rrn L 340 MPa - Sheet and strip - a 4 2 mm 31 11 2) 3) 1) Published as AECMA standard at the date of publication of this standard. 21 In preparation at the dat

14、e of publication of this standard. 3) Published as AECMA pre-standard at the date of publication of this standard. Previous page ic hlanlt -_ CEN PREN*E590 92 m 3404589 0031352 BOL a It2 1.4 prEN 2590 Page 4 kg/m2 9,4 11 3 Required characteristics 1 i6 1,8 2 2.5 3.1 Materials 12,6 14,1 15,7 19.6 Ste

15、els EN 2209, EN 2212, EN 2215, EN 2216, EN 2217, EN 2228, EN 2246, EN 2250, EN 2273, EN 2276, EN 2280, EN 2467, EN 2538, EN 2540, EN 2543, EN 2770, EN 2773, EN 2776. 3 4. 5 3.2 Form 23,6 31,4 39.3 In accordance with figure 1. A D i_ii Figure 1 3.3 Dimensions 3.3.1 Thicknesses and masses 3.3.1.1 Shee

16、ts In accordance with table 1. Table 1 Dimensions in millimetres 1 Thickness I Mass per unit area 1) I For information, calculated with a density I I 7.85 ka/dm3 - _- -_ _ CEN PRENx2590 72 3404589 0033353 748 a prEN 2590 Page 5 kg/m2 3.3.1.2 Plates 8 In accordance with table 2. Table 2 63 Dimensions

17、 in millimetres I Thickness I Mass per unit area 1) 1 I 10 I 78.5 -1 15 I 118 1) For information, calculated with a density : 7, a 5 kg /d m3 I 3.3.2 Widths Widths are not defined. 3.3.3 Lengths Lengths are not defined. 3.4 Dimensional tolerances 3.4.1 Thicknesses In accordance with table 3. Measure

18、ments shall be taken at least 20 mm from the edge. CEN PREN*:2590 9iJ m prEN 2590 Page 6 2 a C Y -0 I- I 3404589 0031354 684 = I CEN PRENr2590 92 3404589 0031355 510 = prEN 2590 Page 7 3.4.2 Widths In accordance with table 4. Table 4 Dimensions in millimetres Widths b 5 1200 +4 O I +6 I O 1 1200 250

19、0 0,004 x I O 3.5.2 Local straightness In accordance with figure 2. References Figure 2 CEN PREN*ZiO 92 W 3404589 003135b 457 W prEN 2590 Page 0 3.5.3 Flatness 3.5.3.1 Method of measurement The sheet or plate shall be placed on a flat surface, under its own mass. The raised surface is given by the m

20、easurement of the max. distance between the sheet or plate and a reference line which coincides in two points with the sheet or plate, see figure 3. -I lorb P- W I-=- -i I W = Length of local amplitude XI = Raised surface for measuring length I or b X2 = Raised surface for measuring length W. Figure 3 3.5.3.2 Tolerances In accordance with table 7. Table 7 Dimensions in millimetres X1 for : X2 for : Thickness I orb S 1200 1200 Iorb 5 1500 W 2 300 1 %ofW max. X1 as15 10 15 4 Designation In accordance with EN 2600.