AECMA PREN 2338-1983 Sheets Titanium and Titanium Alloys Hot Rolled Thickness 0 8 mm Less Than or Equal to a Less Than or Equal to 5 mm Dimensions Aerospace Series Edition 1《航空航天系列.pdf
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1、AECMA PREN2338 83 m 10L23LL 0002357 2 m . - - A.E .C.M.A. STANDARD prEN2338 NORME A.E.C.M.A. Edition 1 A.E.C.M.A. NORM January 1983 Approved by COMITE DE NORMALISATION of A.ECMA. 1982-07-26 ENGLISH VERSION The equivalent versions in French and German languages can be supplied by B.NA.E., 8, rue More
2、au-Vauthier - - 92100 BOULOGNE-BILLANCOURT -FRANCE. SHEETS, TITANIUM AND TITANIUM ALLOYS HOT ROLLED THICKNESS 0,8 mm 1000 I. i ,i3 I agreed Tobe i 0,15 _-_ between manufacturer t 0,18 t 0.40 I Width b I * Calculated on the basis of density of 4,5 g/cm3. r6 O l I f 10 O I 18,O r I-%,-; I l Copyright
3、Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN2338 Page 4 AECMA PREN2338 i33 W 1012311 0002962 2 W 4.2 Geometrical tolerances 4.2.1 Squareness See table 2.
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