王俊

【摘 要】多支點(diǎn)梁結(jié)構(gòu)廣泛應(yīng)用于客機(jī)及運(yùn)輸機(jī)的翼面類結(jié)構(gòu)。支點(diǎn)的位置選擇對(duì)翼面結(jié)構(gòu)的變形有較大影響。本文以某型飛機(jī)襟翼為例，研究了適用于翼面類結(jié)構(gòu)支撐位置選擇的計(jì)算過程，為翼面結(jié)構(gòu)后續(xù)剛度設(shè)計(jì)與變形控制提供基礎(chǔ)。

【關(guān)鍵詞】支點(diǎn)布置；翼面結(jié)構(gòu)；位置優(yōu)化

Supporting position design and optimization for flap structure based on Hyperstudy

WANG Jun

（Shanghai aircraft design and research institute，Shanghai 201210，China）

【Abstract】Many flap structures are designed as a beam with two or more supporting points，such as flap and aileron.The supporting position has a big effect to the deformation of the beam.This paper studies the position selection methods，for the flap structure of a particular aircraft type.The result can build the bases for the further design for the structure.

【Key words】Supporting position；Flap structure；Position optimization