Wingless Electromagnetic Air Vehicle

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The Wingless Electromagnetic Air Vehicle (WEAV) is a heavier-than-air flight system which can self-lift, hover, and fly reliably with no moving components Schematic of WEAV.png
The Wingless Electromagnetic Air Vehicle (WEAV) is a heavier-than-air flight system which can self-lift, hover, and fly reliably with no moving components

The Wingless Electromagnetic Air Vehicle (WEAV) is a heavier than air flight system developed at the University of Florida, funded by the Air Force Office of Scientific Research. [1] [2] [3] The WEAV was invented in 2006 by Dr. Subrata Roy, [4] plasma physicist, aerospace engineering professor at the University of Florida, and has been a subject of several patents. [5] [6] [7] [8] [9] [10] The WEAV employs no moving parts, and combines the aircraft structure, propulsion, energy production and storage, and control subsystems into one integrated system.

Contents

Operating mechanism

The WEAV uses a multitude of small electrodes covering the whole wetted area of the aircraft, in a multi-barrier plasma actuator (MBPA) arrangement, an enhancement over dual-electrode dielectric barrier discharge (DBD) systems using multiple layers of dielectric materials and powered electrodes. [11] These electrodes are very close to one another so surrounding air can be ionized using RF AC high voltage of a few tens of kilovolts even at the standard pressure of one atmosphere. The resultant plasma contains ions that are accelerated by the Coulomb force using electrohydrodynamics (EHD) at low altitude and small velocity. The surface of the vehicle acts as an electrostatic fluid accelerator pumping surrounding air as ion wind, radially then downward, so the lower pressure zone on the upper surface and the higher pressure zone underneath the aircraft produces lift and thrust for propulsion and stability. [1] At a higher altitude and to reach greater speeds, a magnetic field is also applied to enhance collisions between electrons and heavy species in the plasma and use the more powerful Lorentz body force to accelerate all charge carriers in the same direction along a radial high speed jet. [2] A very early version of this documented by Jean-Louis Naudin used wire originally from a hard disk drive cable (aka 80/40 wire) with alternate HV on each pair and this works but is very inefficient compared to newer approaches as discussed above.[ citation needed ]

Novel technologies

To achieve its mission, the WEAV-related research introduced a number of plasma actuator designs. This section highlights the main technologies.

Multi-barrier plasma actuators

Schematic of a tri-layer multi-barrier plasma actuator (MBPA) design. Though a tri-layer MBPA design is shown, other configurations are possible. MBPA schematic.png
Schematic of a tri-layer multi-barrier plasma actuator (MBPA) design. Though a tri-layer MBPA design is shown, other configurations are possible.
Comparison of force and effectiveness among various single, bi-layer, and tri-layer MBPA designs. MBPA Design Comparison.png
Comparison of force and effectiveness among various single, bi-layer, and tri-layer MBPA designs.

The conventional single dielectric barrier discharge (DBD) actuator design is composed of two electrodes separated by a single dielectric material. Much work has gone into optimizing the design and performance of the single DBD design, [12] however research work continues to improve the performance of these actuators. The MBPA design is an extension of the single DBD actuator design which introduces additional dielectric barriers and electrodes, and thus additional design parameters. Research indicates that MBPA designs may achieve higher resultant thrust and improved thrust-to-power ratios than the single DBD actuator design. [11] [13] [14] Sample trials of a bi-layer MBPA design demonstrated an approximately 40% increase in effectiveness over the conventional single layer design. [2] [13]

Serpentine actuators

The WEAV employed serpentine geometry plasma actuators for fully three-dimensional flow control which combine the effects of a linear actuator and plasma synthetic jet. [15] [16] [17] Due to the periodic geometry of the serpentine design, there is pinching and spreading of the surrounding air along the actuator. [18] Consequently, serpentine actuators generate both spanwise and streamwise vorticity, resulting in unique flow structures that are not reproduced by conventional linear geometry plasma actuators.[ citation needed ]

Micro-scale actuators

Top and cross-sectional schematic of microscale dielectric barrier discharge plasma actuator. Micro-scale actuator schematic.png
Top and cross-sectional schematic of microscale dielectric barrier discharge plasma actuator.

Experimental results and numerical simulation demonstrate that by shrinking the gap between electrodes to micron size, [19] [20] [21] the electric force density in the discharge region is increased by at least an order of magnitude and the power required for plasma discharge is decreased by an order of magnitude. Consequently, physically smaller and lighter power supplies can be used with these so-called micro-scale actuators. Investigations demonstrated that per actuator, induced velocities from the micro-scale plasma actuator are comparable to their standard, macro-scale counterparts, albeit with an order of magnitude less thrust. [2] However, due to the decreased power requirements of the micro-scale plasma actuators, experiments suggest effective macroscopic flow control via large arrays of micro-scale plasma actuators. [22] [23]

Novel materials

In addition to experimental plasma actuator designs and geometries, the WEAV investigated the performance of a large variety of insulating materials for use in the dielectric barrier layer, including flexible materials such as silicone rubber and ferroelectric modified lead zirconate-titanate (PZT) and silica aerogel. [24]

Successful dielectric materials investigated
MaterialThickness (μm)
Acrylic500, 1000, 3000
Cirlex254, 2540
PDMS (Polydimethylsiloxane)~1000
Silicone rubber (high-purity)127
Torlon250
PZT3000
Silica Aerogel6000

Liftoff

Demonstration of successful liftoff of WEAV prototype. Weav liftoff.png
Demonstration of successful liftoff of WEAV prototype.
Timeline demonstrating the accomplishments and progress of the WEAV. WEAV progress.png
Timeline demonstrating the accomplishments and progress of the WEAV.

An early prototype of the WEAV was able to sustain hovering flight a few millimeters above the ground for approximately 3 minutes. Prototypes of varying radii were also successfully tested, suggesting scalability of the design.[ citation needed ]

See also

Related Research Articles

In physics, the term dielectric strength has the following meanings:

<span class="mw-page-title-main">Electrical discharge machining</span> Metal fabrication process

Electrical discharge machining (EDM), also known as spark machining, spark eroding, die sinking, wire burning or wire erosion, is a metal fabrication process whereby a desired shape is obtained by using electrical discharges (sparks). Material is removed from the work piece by a series of rapidly recurring current discharges between two electrodes, separated by a dielectric liquid and subject to an electric voltage. One of the electrodes is called the tool-electrode, or simply the tool or electrode, while the other is called the workpiece-electrode, or work piece. The process depends upon the tool and work piece not making physical contact. Extremely hard materials like carbides, ceramics, titanium alloys and heat treated tool steels that are very difficult to machine using conventional machining can be precisely machined by EDM.

<span class="mw-page-title-main">Magnetohydrodynamic drive</span> Vehicle propulsion using electromagnetic fields

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<span class="mw-page-title-main">Dielectric barrier discharge</span> Electrical discharge between two electrodes separated by an insulating dielectric barrier

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<span class="mw-page-title-main">Plasma actuator</span> Type of actuator

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<span class="mw-page-title-main">Serpentine geometry plasma actuator</span>

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<span class="mw-page-title-main">Magnetohydrodynamic converter</span> Electromagnetic machine with no moving parts

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<span class="mw-page-title-main">Subrata Roy (scientist)</span> India-born American inventor, educator, and scientist

Subrata Roy is an Indian-born American inventor, educator, and scientist known for his work in plasma-based flow control and plasma-based self-sterilizing technology. He is a professor of Mechanical and Aerospace Engineering at the University of Florida and the founding director of the Applied Physics Research Group at the University of Florida.

References

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  3. "Department of Mechanical and Aerospace Engineering, University of Florida".
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  5. USpatent 8960595,Subrata Roy,"Wingless hovering of micro air vehicle",issued 2015-02-24, assigned to University of Florida Research Foundation Inc.
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