Multi-shock wave focusing ignition promotion experimental device and experimental method
By designing a multi-shock focus ignition promotion experimental device, the shock wave collision chamber and double-membrane shock tube are used to achieve the collection and focus of multi-angle shock waves, solving the problem of fast and reliable ignition in the detonation engine, and improving the ignition efficiency and system reliability.
Patent Information
- Application Number
- CN202510348642.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-03-24
- Publication Date
- 2025-04-22
- Estimated Expiration
- 2045-03-24
AI Technical Summary
The prior art is difficult to achieve fast and reliable fuel ignition in detonation engines, especially when the aircraft is at a high speed. Traditional methods have problems of insufficient energy, high system complexity and poor stability.
A multi-shock focus ignition promotion experimental device is designed, including a shock wave collision chamber, a shock tube unit and a data acquisition unit. Multi-angle shock waves are generated through a double-membrane shock tube and a gas distribution assembly, and the multiple connection ports in the shock wave collision chamber are used to achieve the collection and focus of shock waves.
It has realized the disclosure of the shock focus rules and mechanisms under dual shock wave or even multi-shock coupling, which has improved the ignition efficiency, simple structure, good operability and strong repeatability, making up for the shortcomings of the traditional single shock focus ignition method.