常用图纸中英文对照

holes should be punched in final step point A,point B and point C are located on surface A BLANK STEEL ROLLING DIRECTION VALID ONLY FOR EUROPE metal marking:format E-DD-MM-valid only for europe. E-EUROPE,D-DAY,M-MONTH,MARKING.MARKING HIGHT:3-5MM ROUND THE EDGES WITH R1-R3MM MTERIAL THICKNESS BEFORE STAMPING:2.5±0.15MM (MATERIAL THICKNESS AFTER STAMPING 2.2MM MINIMUM-NOT APPLICABLE TOAREA D) THICKNESS TO BE CONTROLLED IN CRITICAL SECTION BY CUTTING THE PART(SECTION A-A)AND CHECKING THETHICKNESS ON EVERY RADIUS AND IN THE MIDDLE OF STRAIGHT EDGES TO BE FREE FROM BRUUS ACCORDING TO DIN ISO 13715

孔应在最后一步冲 A点，B点和C点位于表面A 坯轧制有效方向仅适用于欧洲 金属打标：格式e-dd-mm 仅适用于欧洲有效。 E-欧洲，D-日期，M-月份，标记.标记高度：3-5mm 圆边r1-r3mm 材料厚度：2.5冲压前±0.15mm (材料厚度2.2mm冲压后的最小不适用领域D) 厚度被切割的部分控制在临界截面(剖面)检查 在每一个半径和直边中间的厚度 根据DIN ISO 13715应无毛刺

FOR OTHER DIMESIONS USE 3D MODEL ESTIMATED MASS:0.526kg ALL ENGINEERING CHANGES MUST BE APPROVED AND IN ACCORDANCE

在其他部位使用3D数模 重量：0.526kg估计 所有工程变更必须按照批准的

no cracks or other defects permitted here resistance weld accoring to Φ 54.9/Φ 54.7 fressfitting force test fressfitting force to introduce one cylinder Φ 54.9mm into this dia must reach a load of 350 daN min one cylinder of dia Φ 54.9 introduced into the dia "Z" will have as a minimum one generatratrix of contact on each quadant of the outer and inner bracket

在这里不允许有裂纹或其它缺陷 电阻焊按Φ 54.9 / Φ 54.7 压装力测试 压装力引入气缸直径Φ 54.9m 必须达到不小于350 daN(相关资料显示约等于kg) 一个气缸直径54.9Φ 引入直径“Z 会有一个最低母线接触 外及内支架的每个象限

Φ54.7

Φ54.9m

引入直径“Z

heignt of wings difference MAX.0.5mm welding spots may not fail at inner-outer bracket surface for welding test specification 18A00119 tumble and wash before assembly to be free from burrs for significant spec.18000010 MTERIAL THICKNESS:2.5±0.1 MTERIAL:Q/BQB310-2003 QSTE 380 TM for measure dim.after tooling Φ 54.8±0.1 has to put into and fixed for measure dim.after trapezoidal tooling has to put into and fixed tooling dim.(35.55±0.1&36.25±0.2)*34*150 plug gage of dim.30.29/30.302*50mm hans to pass through radius not specified:R=2.5MM REDUCTION RATE OF THICKNESS MUST BE LESS THAN 12% MTERIAL THICKNESS:2.3MM for other views see sheet 2.3 and 4 OF 4 for other notes and views see sheet 1.3 anf 4 OF 4 EUROPEAN/FIRST ANGLE PORJECTION this document was frinted on 24 October 07-13:12

翅膀最大高度差 0.5mm 焊接点在内表面外表面不能失效 焊接试验规范18a00119 装配前清洗 应无毛刺 重要规格.18000010 材料厚度：2.5±0.1 材料执行标准：Q / BQB310-2003 QSTE 380 TM 模具完成后测量统计Φ 54.8±0.1 必须

投入和固定 梯形模具完成后测量统计 必须投入和固定 模具测量统计(35.55±0.1 & 36.25±0.2)* 34 * 150 通过塞规测量统计30.29 / 30.302×50mm 未指定半径：r=2.5mm 减薄率必须小于12% 材料厚度：2.3mm 对于其他意见，见表2.3和4的4 和其他笔记的看法见表1.3和4 4 欧洲/第一角投射 本文件于十月24 07-13:12印刷

Φ54.8±0.1

在最后一步冲

和C点位于表面A

方向仅适用于欧洲

d-mm 仅适用于欧洲有效。 月份，标记.标记高度：3-5mm

边r1-r3mm 2.5冲压前±0.15mm 压后的最小不适用领域D) 制在临界截面(剖面)检查 径和直边中间的厚度 SO 13715应无毛刺

部位使用3D数模 ：0.526kg估计 更必须按照批准的

许有裂纹或其它缺陷

Φ 54.9 / Φ 54.7

装力测试 入气缸直径Φ 54.9m aN(相关资料显示约等于kg)

径54.9Φ 引入直径“Z 个最低母线接触 支架的每个象限

Φ

大高度差 0.5mm 表面外表面不能失效 验规范18a00119 配前清洗 应无毛刺 规格.18000010

度：2.5±0.1 BQB310-2003 QSTE 380 TM

测量统计Φ 54.8±0.1 投入和固定

完成后测量统计 投入和固定 0.1 & 36.25±0.2)* 34 * 150

计30.29 / 30.302×50mm

半径：r=2.5mm

率必须小于12%

厚度：2.3mm

见，见表2.3和4的4

的看法见表1.3和4 4

/第一角投射

月24 07-13:12印刷