Facial noninvasive propeller assembly structure
By optimizing the structural design of the non-invasive facial propulsion device, the built-in micro air pump and air storage chamber are integrated, solving the problems of inaccurate pressure control and dependence on external air tanks in existing technologies. This achieves safe, precise, and portable gas propulsion, suitable for different skin depths and injection medium viscosities, and reduces the risk of tissue damage.
Patent Information
- Application Number
- CN202520797995.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-04-25
- Publication Date
- 2026-07-24
- Estimated Expiration
- 2035-04-25
AI Technical Summary
The existing non-invasive facial pusher assembly structure cannot achieve precise pressure control, cannot adapt to different skin depths and injection medium viscosities, and requires an external air tank, making operation inconvenient.
A structure including a cylinder back cover, cylinder body and push rod was designed, with a built-in micro air pump and air storage chamber integrated, eliminating the need for an external air tank. By optimizing pressure control and gun structure, precise and portable gas propulsion is achieved, adaptable to different skin depths and injection medium viscosities, with a pressure fluctuation range of ≤±2%, and conforming to ergonomic design.
It achieves safe and precise gas propulsion, reduces operational complexity, minimizes the risk of tissue damage, is suitable for delicate facial procedures, has minimal pressure fluctuations, is ergonomically designed, is applicable to different skin depths and injection medium viscosities, and eliminates the need for external gas cylinders.