分析了整体结构件加工变形的产生机理。
The mechanism of large integral structure machining distortions was analyzed.
概括分析了薄壁整体结构件切削加工的特点和难点。
This paper presents a brief analysis of the features specialties and problems of machining of integral parts with thin walls.
在现代飞机结构中，整体结构件的应用导致了飞机装配型架结构中大量使用接头和工艺孔定位器。
Single structural parts are widely used in the structure of modern aircraft, and this leads to mostly adopt components in aircraft assembly fixtures to locate product joints and process holes.
作为一种整体结构件，在实际应用中碳化钨硬质合金层的厚度对部件的内应力分布以及尺寸稳定性有着重要的影响。
Being a kind of integrated structural parts, different thickness of WC cemented carbide layer has great effect on distribution of internal stress and dimensional stability.
整体油箱，由机翼结构件梁、肋、蒙皮组成，用来在飞机上储存燃油的金属容器。
INTEGRAL TANK, a metal container formed by the wing structure (spars, ribs, skin) for storage of fuel on the airplane.
为了提高复合材料机翼的整体强度和刚度，降低制造成本，机翼的主要结构件采用缝编技术。
To increase the whole strength and stiffness of the composite wing and to lower the manufacturing cost, the main component of the wing is employed with stitched technique.
激光拼焊技术是将两块或多块具有相同或不同机械性能、不同表面状态的钢板使用激光焊接的方法连接成毛坯件，然后进行整体冲压成轿车结构件。
Tailor welded blanks are defined as two or more sheets of blanks with equal or different mechanical properties, or surface coatings welded together by laser before stamping.
激光拼焊技术是将两块或多块具有相同或不同机械性能、不同表面状态的钢板使用激光焊接的方法连接成毛坯件，然后进行整体冲压成轿车结构件。
Tailor welded blanks are defined as two or more sheets of blanks with equal or different mechanical properties, or surface coatings welded together by laser before stamping.
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