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Ducted Fans with Flow Control Synthetic Jet Actuators and Methods for Ducted Fan Force and Moment Control

机译:带流量控制合成射流执行器的风管风机以及风管力和力矩控制的方法

摘要

The present invention relates to the field of aerodynamics. More particularly, the present invention relates to manipulating air flow over a surface, such as the surface of a duct of a ducted fan vehicle. By controlling air flow over, at, or around the surface of a duct, the flight of the vehicle can be controlled. One embodiment of the invention provides a vertical take-off and landing (VTOL) ducted-fan vehicle comprising means for producing steady or unsteady blowing at a surface of a duct for producing control forces and moments for controlling flight. The means for unsteady blowing can be provided by synthetic jets and the means for steady blowing can be provided by a pressurized air supply. The synthetic jets can be integrated into the ducted-fan vehicles in numerous ways, including at the surface of the leading and/or trailing edge of the ducts. The synthetic jets can be independently operated to control the flight of the vehicle. A novel use of these inventive flow control concepts is to apply the control asymmetrically to the duct in order to produce an imbalance in forces, thus resulting in a moment or torque, which can be used to control flight.
机译:本发明涉及空气动力学领域。更具体地,本发明涉及操纵在表面上的空气流,该表面例如是管式风扇车辆的管道的表面。通过控制管道表面上方,周围或周围的气流,可​​以控制车辆的飞行。本发明的一个实施例提供了一种垂直起降(VTOL)管式风扇车辆,其包括用于在管道的表面处产生稳定或不稳定的吹气的装置,以产生用于控制飞行的控制力和力矩。用于不稳定吹气的装置可以由合成射流提供,并且用于稳定吹气的装置可以通过加压空气供应来提供。合成射流可以通过多种方式集成到风车中,包括在风道的前缘和/或后缘的表面。合成射流可以独立运行,以控制车辆的飞行。这些创造性的流量控制概念的新颖用途是将控制非对称地应用于管道,以产生力的不平衡,从而产生可用于控制飞行的力矩或扭矩。

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