Quick-response direct force generating device

A technology of generating device and fast response, which is applied in the field of aerospace vehicle control, can solve the problems of increasing the complexity of cavity processing and packaging, difficult to adjust and control the working frequency and jet velocity of the exciter, etc. Responsive, controlled effects

Active Publication Date: 2013-02-27
NAT UNIV OF DEFENSE TECH
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  • Description
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Problems solved by technology

To this end, Cybyk, a researcher at the university, used a three-electrode cavity structure with added gates in the exciter design to reduce the required power supply, but this method increases the complexity of cavity processing and packaging. The input power circuit adopted is not easy to realize the adjustable and controllable operating frequency of the exciter and jet velocity

Method used

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  • Quick-response direct force generating device
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Embodiment Construction

[0025] See attached Figure 1~2 , an implementation example of a fast-response direct force generating device of the present invention, which is composed of a power supply system 1 and a spark discharge plasma synthetic jet actuator 2 . Wherein the spark discharge plasma synthetic jet actuator 2 such as figure 2 As shown, a cylindrical exciter body 24 is included, the section diameter of the exciter body 24 is Φ16mm, and the height is 20mm. The exciter body 24 and its cover plate 26 are made of commercially available glass ceramics or boron nitride ceramics with good insulation performance and machinability to reduce the processing difficulty of the exciter. The diameter of the cover plate 26 is the same as that of the exciter body 24. The diameter of the tube is matched, and the thickness is 3mm. The jet outlet hole 25 opened on the cover plate 26 is circular, and its diameter is Φ2mm. The jet outlet hole 25 can also choose different side inclination angles or pitch angles...

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Abstract

The invention discloses a quick-response direct force generating device. A power supply system (1) comprises a high-voltage pulse circuit (11), a high-voltage direct-current circuit (12) and a charging and discharging capacitor (13). A spark discharge plasma synthetic jet actuator (2) of the device comprises an actuator body (24) provided with a cover plate (26), and a main discharge electrode (21), an ignition positive electrode (22) and an ignition negative electrode (23) which are inserted in the actuator body (24) at intervals. A jet outlet (25) is opened in the cover plate (26). The main discharge electrode (21) is connected with the high-voltage direct-current circuit (12), and the ignition positive electrode (22) and the ignition negative electrode (23) are connected in parallel with the high-voltage pulse circuit (11). According to the device, the pulse jet frequency and the jet energy can be adjusted according to needs, a novel generating mode is provided for controlling quick-response direct force of a high-speed air vehicle, and the device can be used an actuator in active flow control in high-speed internal and external flow fields.

Description

technical field [0001] The invention belongs to the field of aerospace vehicle control, and in particular relates to a quick-response direct force generating device, which is suitable for the quick-response direct force control of the aircraft and the active control of the high-speed flow field inside and outside the aircraft. Background technique [0002] With the rapid development of supersonic / hypersonic aircraft technology, direct force control technology is becoming an effective means to improve the response speed of high-speed aircraft, improve the guidance accuracy, and increase the available overload and maneuverability. Compared with the aerodynamic control method based on the air rudder, the direct force control based on the lateral jet flow has the advantages of small time delay, fast response speed, and high control efficiency in high-altitude environments. [0003] At present, the reaction force control system based on side jet flow mainly generates side jet for...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F03H1/00
Inventor 王林罗振兵夏智勋邓雄刘冰
Owner NAT UNIV OF DEFENSE TECH
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