Civil aircraft door pressurization prevention mechanism
By designing the trajectories of the front guide groove, rear guide groove, and drive groove, and the arrangement of the upper crank, connecting rod, and lower crank, the difficulties in opening the aircraft cabin door pressurization prevention mechanism under icing conditions and the problem of sealing strip compression were solved, thus improving opening efficiency and safety.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- AVIC SAC COMML AIRCRAFT
- Filing Date
- 2026-04-17
- Publication Date
- 2026-06-02
AI Technical Summary
Existing aircraft door pressurization prevention mechanisms are difficult to open under icing conditions, and the sealing strip is easily jammed or compressed too much, resulting in increased operating force and reduced safety.
The design incorporates the trajectories of the front guide groove, rear guide groove, and drive groove. Through the arrangement of the upper crank, connecting rod, and lower crank, the designable motion trajectory of the pressurized prevention door is realized, preventing reverse drive and improving ice-breaking efficiency and safety.
It enables the pressurized anti-icing door to open quickly under icing conditions, reduces the compression rate of the sealing strip, and improves operating force and safety.
Smart Images

Figure CN122126436A_ABST