根据辩证分析的方法,在保证使用技术条件下,力求所设计的襟翼重量达到最轻。在另构件安排的过程中,尽量使得各个另构件的受力,均较为合理。在设计过程中,着重地究研了襟翼的平面形状,襟翼翼梁的位置及其构造,襟翼翼肋的位置及其构造,和襟翼上的接头等问题。 According to the method of dialectical analysis, under the condition of ensuring the use of technology, strive to design the flaps to achieve the lightest weight. In the process of arranging the other components, it is more reasonable to try to make the stress of each other component as much as possible. In the process of design, the flaw shape, the position and structure of the wing spar, the position and structure of the wing, the joints on the flaps and so on are studied emphatically.