Damage tolerance optimization method for rib integral panel
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
- Publication Date
- 2021-07-30
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Abstract
Description
technical field
[0001] The invention belongs to the field of damage tolerance design of aircraft structures, and in particular relates to a method for optimizing the damage tolerance of rib overall wall plates. Background technique
[0002] Due to the advantages of good fatigue performance, simple manufacture and light structure weight, the integral panel has been applied in many medium and large aircraft structures. However, compared with the traditional riveted siding, the integral siding lacks the natural crack arresting element—the rivet connecting the stringer and the skin, which makes the damage tolerance performance poor. The damage tolerance characteristics of the panels are an important design point for integral panels used in aircraft structures. In the past few years, when the structural design of the integral wall panel generally focused on the static strength performance, if the requirements were met, only a passive check was performed on whether the wall panel...