Hinge for luggage compartment
By using a stop pawl and ratchet in the hinge structure, assembly is simplified and stable torque adjustment is provided. This solves the problems of inconvenient operation and insufficient safety of baggage compartment hinges under high loads, achieving smooth buffering and power assistance, and improving the ease of use and safety of baggage compartments in vehicles and aircraft.
Patent Information
- Application Number
- CN202510688792.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Priority Date
- 2024-05-27
- Filing Date
- 2025-05-27
- Publication Date
- 2025-11-28
AI Technical Summary
In the existing technology, the hinges of the luggage compartment are difficult to provide smooth cushioning and assistance under high load and complex load conditions, resulting in inconvenient opening and closing operation and insufficient safety.
A hinge structure is designed, including first and second hinge pages, a shaft tube, a torsion spring, a buffer element, and an adjustment element. The torsion spring is reliably stopped by the engagement of a stop pawl and a ratchet, avoiding axial preload, simplifying assembly, and providing stable torque adjustment. The opening speed of the flip cover is adjusted in conjunction with the buffer element.
The operation comfort and safety of the luggage compartment flap have been improved, ensuring that the flap opens stably under high-frequency opening and closing and complex loads, avoiding sudden pop-up, and improving ease of use and safety.