A small aircraft towing device
The design of the detachable aircraft wheel traction lock and traction bar solves the problem of existing technologies being unable to adapt to different aircraft wheel models, achieving the effect of rapid maintenance and reduced maintenance costs.
CN224448167UActive Publication Date: 2026-07-03HUBEI MOXING AVIATION IND CO LTD
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- HUBEI MOXING AVIATION IND CO LTD
- Filing Date
- 2025-07-31
- Publication Date
- 2026-07-03
AI Technical Summary
Technical Problem
In existing small aircraft towing devices, the towing rod and the locking assembly are fixedly connected, which cannot be flexibly disassembled or replaced. This makes them unsuitable for different aircraft wheel models, and requires complete disassembly for maintenance, which prolongs downtime and increases maintenance costs.
Method used
The aircraft wheel traction lock and traction rod are detachably connected. The connection mechanism enables quick disassembly and installation of the aircraft wheel traction lock. The cooperation of the limit block and the limit groove enhances the connection stability.
Benefits of technology
It enables flexible adaptation and rapid maintenance of wheels for different aircraft models, reducing maintenance costs and time.
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Smart Images
Figure CN224448167U_ABST
Abstract
This utility model discloses a small aircraft towing device, including a small aircraft wheel, an aircraft wheel towing lock, a towing rod body, a universal joint, a towing buffer, a towing head, and a towing handle. The aircraft wheel towing lock is detachably connected to the small aircraft wheel. One end of the towing buffer is connected to the towing handle via the towing head, and the other end is connected to the towing rod body via the universal joint. The end of the towing rod body away from the universal joint is connected to the aircraft wheel towing lock via a connecting mechanism. The connecting mechanism includes a connecting plate, a limiting block, a limiting groove, and a connecting block. The end of the aircraft wheel towing lock away from the small aircraft wheel is connected to the limiting block via the connecting plate. This utility model allows for the removal and installation of a usable aircraft wheel towing lock from damaged or different models, improving maintenance efficiency and reducing maintenance costs.
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