一种提升高速进气道流量的复合涡流发生器及设计方法
By designing a composite vortex generator, combining a reverse-mounted ramp-type vortex generator with a streamlined vortex generator, the problem of insufficient airflow capture in the air intake of high-speed aircraft was solved, achieving a wider range of airflow control and stronger airflow capture capability, thereby improving engine performance.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- BEIJING INST OF TECH
- Filing Date
- 2025-06-03
- Publication Date
- 2026-07-17
AI Technical Summary
Traditional vortex generators cannot effectively improve flow capture capability in the air intake of high-speed aircraft, especially in integrated designs where boundary layer thickening leads to flow blockage, affecting engine performance.
A composite vortex generator is designed by combining a ramp-type vortex generator installed in reverse with a streamlined vortex generator to form opposing and flowing vortex pairs, thereby enhancing the transport of high-energy fluid to the boundary layer and improving flow capture capability.
Under high-speed incoming flow conditions, the composite vortex generator significantly improves the intake flow capture, enhances the control range and stability of the vortex generator, reduces the number of vortex generators, reduces parasitic drag, and improves engine performance.
Smart Images
Figure CN120819436B_ABST