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The following is an outline of an idea that I have been working on for
some time, for the sake of brevity I have omitted details at this stage, they will follow. The primary purpose of this post is to publish this idea, for the usual reasons, though discussion, debate, criticism and advice would be appreciated, it should be a simple concept for most people to grasp. It is my intention to write a paper on this in a few months time. Space related applications might be far better air launch platforms and vehicle recovery systems, even planes for Mars. Energy related applications include the possibility of far more effective and efficient wind turbines and aircraft. Introduction The ongoing development of traction kites and unmanned air vehicles has raised the possibility of some alternate solutions to some of the most basic of aerodynamic design problems. Possible advantage lies in the separation of wing from body via a load carrying tether, this allows the wing to otherwise fly, and generate lift, independently of the body. It also enables loads to be distributed in tension, avoiding much of the need for heavy structure and the weight and cost so incurred. Powered free flying wings of this kind will likely have sufficient thrust to weight ratios to take off and land vertically, and by circling, take off and land their payloads vertically. The following is a outline of some of the possible applications of such free flying tethered wings to aircraft, wind turbines, kite sailing, and other technologies, and some of the potential advantages there of. Aircraft An airplane utilising the free flying wing concept might consist of a streamlined body, in which payload and fuel are stored, with retractable landing gear sufficient for VTOL and taxiing purposes, and perhaps landing pads on the top of the body suitable for holding free flying wings when not in use. Likely multiple wings will be used so as to balance rotating tether loads and for the purposes of redundancy. Fuel, electrical power, and control, will likely be transmitted within the line fairing with the wing capable of a degree of autonomy in case of emergency, numerous safety features could be added. Such aircraft could be built with payloads ranging from a few grams, to a few thousands of tons. Compared to a standard air plane such aircraft would have VTOL and a significantly lower mass fraction, resulting in much greater range, payload, efficiency, and much lower cost. Primarily this is due to the elimination of a large part of the aircrafts structure and weight, which no longer serves any purpose. Such an aircraft would have similar advantages over a helicopter with additional advantages in the elimination of the heavy gear box and the additional capacity for high speed flight. For a given amount of lift a free flying wing is far lighter than a rotor, and by being far less constrained by effective rotor diameter greatly improved hover performance, and much higher efficiency is possible. In effect, such an aircraft might even hover more efficiently than it could fly horizontally, due to the reduction in body drag. The heavy lift capacity, perhaps into the thousands of tons, of such a large helicopter might be particularly useful. Wind turbines The free flying wing approach might offer especially great advantage with regard to power generation from the wind. With VTOL, such a wing could be developed to launch and land autonomously and due to the high flying speed should be able to survive extreme wind strengths without even needing to land. In comparison to a standard wind turbine, the tower is replaced by a line with the free flying wing replacing the rotor tip, eliminating most of the blade. The large low speed generator and gearbox are replaced by a small high speed generator/motor direct coupled to a small propeller or ducted fan. This is sufficient for VTOL, electrical power is transmitted via a cable within the line fairing. Even with the much higher speed operation the generator is the dominant cost, there is significant advantage in using lower performance generator designs of far lower cost. The dominant generator cost also favours the use of a larger wing that can generate in much lower wind speeds, further, such a system is able to operate at much higher altitude where the wind is generally stronger. Wind turbines typically have a utility of around 25%, with the capacity to generate in much lighter winds, this system would operate far more of the time. A further advantage is the capacity to scale up to very large sizes, units in the hundreds of megawatts at least, should be possible, this is not possible with current wind turbines. A comparative analysis would tend to infer that this system should be able to generate electricity for about a tenth the cost of standard wind turbines, direct cost analysis would tend to confer with this. It has the potential to be significantly less expensive than other mainstream electricity production. This does not, however, account for the cost of a site, power transmission, and social and environmental costs. Parachutes An interesting application for an unpowered free flying wing is as a parachute or even paraglider. While structurally similar such a wing can be made much smaller than a parachute due to the much higher flight speeds, and can be made of high performance materials. For these reasons an arch style wing system especially, can be made much lighter than a comparable parachute. By using such a free flying wing as a gyrocopter reasonable glide rates are possible, in effect the gyrocopter mode trades glide rate, or lift to drag ratio, for lift. With this system it is possible to combine a flared landing, as per a paraglider, with pitch control and energy storage in the wing's speed, for highly effective and controlled vertical landings. Kite sailing In recent times high performance kite development has been greatly pushed by kite traction and kitesurfing in particular. Considerable effort is now going into the development of kite sailing, this is in many ways driving the development of the free flying wing concept. Traditional problems for kite sailing are launching, landing, power control and light wind operation. Light wind operation is particularly difficult because it necessitates extremely light weight construction. One possibility is to use the wind turbine type solution, this enables launching and landing, and the capacity to motor the wing in light winds. It also enables power generation for use on board and if used in conjunction with a diesel electric type ship, the capacity to sail directly into the wind, avoiding the need to tack. The free flying wing enables a comprehensive solution to power control and lends itself to control by autopilot. Aerostats Another possible application for free flying wings is as aerostats. For example, a wing might be flown high over a city providing everything from communications to surveillance services. Power might be transmitted up the line, enabling it to generate power when the wind blows, and to be powered when it does not. Water application It would seem possible to use free flying wings to generate power from water currents, rivers, tides, even ocean currents, in much the same way as a wind power generation system would work. While the free flying wing approach is very effective at extracting energy from such flows the available energy is not as great as one would think. While water is far more dense than air it is the speed of the flow and available area that is really important. The power available is proportional to the speed of the flow cubed, this makes wind power more attractive, especially as the available areas are much greater. There are also issues with regard to impacting submerged objects, even so, this could be a significant application for free flying wings. This system might also be used in place of water propellers, they would be particularly useful in applications requiring high thrust at low speed, they might also be useful with regard to manoeuvring. Pitch, yaw and roll mitigation might also be possible, this can actually use the energy of waves to power forward motion. In this way wave energy power schemes could also be developed. Pete |
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