Invention Grant
- Patent Title: Solid state supersonic flow actuator and method of use
- Patent Title (中): 固态超音速流动执行器及其使用方法
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Application No.: US12015142Application Date: 2008-01-16
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Publication No.: US07988103B2Publication Date: 2011-08-02
- Inventor: H. Bruce Land, III , Kenneth R. Grossman , Bohdan Z. Cybyk , David M. VanWie
- Applicant: H. Bruce Land, III , Kenneth R. Grossman , Bohdan Z. Cybyk , David M. VanWie
- Applicant Address: US MD Baltimore
- Assignee: John Hopkins University
- Current Assignee: John Hopkins University
- Current Assignee Address: US MD Baltimore
- Agent Aisha Ahmad
- Main IPC: B64C21/08
- IPC: B64C21/08

Abstract:
A method and device are provided for manipulating high-speed flows without moving aerodynamic structures. More particularly, a flow control actuator device is provided that is capable of producing a pulsating synthetic jet with high exhaust velocities for manipulating high-speed flows without moving aerodynamic structures. The high exhaust velocities of the actuator device may reach sonic levels of Mach 1 or greater. In one embodiment, the device may be constructed as an array of devices. In such an embodiment, each individual device is preferably reduced to a very small size. In such an embodiment, each individual device can then be fired in temporal patterns to create high-speed synthetic jets of air extending above the surface of the each device.
Public/Granted literature
- US20100284825A1 Solid State Supersonic Flow Actuator and Method of Use Public/Granted day:2010-11-11
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