AECMA PREN 2590-1992 Aerospace Series Steel Sheets and Plates Hot Rolled Dimensions Issue P 1《航空航天系列钢片和版热轧尺寸.P1版》.pdf

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. 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-,-,- CEN PREN*2590 92 m 34

7、84589 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 of application EN 2209 EN 2212 EN 2215 EN 2216 EN 2217 EN 2228 EN 2246 EN 2250 EN 2273 EN 2276 EN 2280

8、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 MPa 4 Rm 4 870 MPa - Sheets, strips and plates 0.5 rnm L a 4 20 mm - Aerospace series 11 Steel FE-PL52S

9、- 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 MPa - Sheets and plates 2 mm S a 5; 20 mm - Aerospace series 1) Steel FE-PA12 - 500 MPa 4 Rm 4 700 MPa -

10、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 - Rm 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

11、 - 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 mm - Aerospace series Steel FE-PA1 1 - Softened - Sheets or plates 0,5 mm S a S 20 mm - Aerospace serie

12、s 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 - Sheets Aerospace series - Steel FE-PL43S - Annealed - Sheet and strip 0,3 mm 4 a 4 2 mm - For prevailin

13、g 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 - 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 m

14、m 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 date of publication of this standard. 3) Published as AECMA pre-standard at the date of publication of this

15、 standard. Previous page ic hlanlt 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-,-,-_ CEN PREN*E590 92 m 3404589 0031352 BOL a It2 1.4 prEN 2590 Page 4

16、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 Steels 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 accordan

17、ce with figure 1. A D i_ii Figure 1 3.3 Dimensions 3.3.1 Thicknesses and masses 3.3.1.1 Sheets 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 Copyright Association Europeene des Constructe

18、urs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,- _- -_ _ 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 in millimet

19、res 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. Measurements shall

20、be taken at least 20 mm from the edge. 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-,-,-CEN PREN*:2590 9iJ m prEN 2590 Page 6 2 a C Y -0 I- I 3404589 00

21、31354 684 = 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-,-,-I CEN PRENr2590 92 3404589 0031355 510 = prEN 2590 Page 7 3.4.2 Widths In accordance with t

22、able 4. Table 4 Dimensions in millimetres Widths b 5 1200 +4 O I +6 I O 1 1200 2500 0,004 x I O 3.5.2 Local straightness In accordance with figure 2. References Figure 2 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo

23、 reproduction or networking permitted without license from IHS-,-,-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 measurement of the max

24、. 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

25、 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. 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-,-,-