The concept of generating electric power from flying windmills
originated with Prof. Bryan Roberts from the University of
Technology in Sydney, Australia. These devices were to be tethered
to the earth and fly at altitudes of between 15,000-feet and
30,000-ft where winds were strong, consistent and reliable. At its
inception, the concept generated little interest from investors as
it flew at the same altitude as commercial aircraft. If it were to
be flown at lower altitudes, it would be restricted to operating
in regions that have strong and steady winds year round. The
flying windmill concept has the advantage of offering cost
reductions with regard to the high cost of building towers to
support wind turbines. New types of cost-competitive and powerful
flying windmills could be developed using recent advances and
developments that have occurred in kite technology, in model
airplane technology and other areas of unpowered flight.
Kite Developments
Since its inception, the idea of the flying windmill has had
several spin-offs that include a wind-powered toy helicopter that
featured a spinning rotor while it flew like a kite. Hobbyists
developed a method whereby multiple wind-powered toy helicopters
could be flown in a line up of progressively higher altitudes when
attached to a single control line. Kite builders in China
developed a similar method of simultaneously flying multiple kites
at progressively higher altitudes using a single control line.
Over a century ago, telephone pioneer Alexander Graham Bell
built a kite able lift a grown man. Bell's precedent indicated
that if the height and width of a kite were increased
arithmetically, its lifting capacity could increase geometrically.
In more recent years, kite hobbyists have used computer technology
to design super kites that fly while controlled by multiple
control lines. They have developed a method of using a single set
of control lines to fly a line-up of several such kites at
progressively higher altitudes.
Model Airplane Development
A model airplane hobbyist in the UK recently built a scale
model aircraft that uses a "paddle wheel" that rotates on a
transverse axis and is mounted within the upper side of the wings.
The rapidly rotating paddle wheel accelerates a stream of air over
the upper surface of the sharply curved wing and generates
substantial lift at very low flight speeds. The wing curvature
(angle of attack) is adjustable to over 45-degrees and that the
aircraft can be made to hover like a helicopter.
This technology can be adapted for stationary flight using wind
power and control lines and where the paddle-wheel would be
replaced by a magnus rotor that would use the boundary layer
effect to re-direct a fast-flowing wind stream over the sharply
curved upper surface of the wing to generate lift. When built to a
large scale (wingspan of over 200-feet), the concept may be able
to carry a light windmill and electrical generation equipment.
Unpowered Flight developments
During the 1970's a popular disc-shaped flying toy called a
Frisbee appeared on the market. When thrown by hand in a way that
produced a spin, a spinning Frisbee could remain aloft for up to a
minute. A machine-launched, fast-spinning Frisbee could remain
aloft for several minutes. The spinning motion of the Frisbee
induced a boundary layer effect in the air on its curved upper
surface while centrifugal forces pushed air outward and over the
sharply curved outer rim of the Frisbee to produced lift. When the
centre of a Frisbee-shaped disc is mounted on a powered axle
(e.g.: a toy flying saucer held by a tether), the spinning disc
could remain aloft for extended periods of time.
Over the past 30-years, numerous aeronautical hobbyists have
designed, built and tested a variety of unpowered flying
ultra-lights, paraplanes, parasails and kites that can carry a
person. These technological developments can be adapted for
stationary flight using multiple control cables in perpetually
windy locations. A battery of such units would then be able to
carry the weight of wind-powered electrical generation equipment
at high altitude over extended periods of time. The main drawback
of such designs is that they are restricted in the weight carrying
capacity because they only use the lower surface of the
paraplanes, parasails and kites to maintain lift.
Applying the Precedents
The aforementioned advances that have occurred in kite and
model aircraft technology can be combined into a revised flying
windmill concept. One such concept could involve a series of up to
12-airborne windmills being flown at progressively higher
altitudes from 3000-feet to 5000-feet (below the altitude of
propeller-driven commercial aircraft). This battery of flying
windmills would all be controlled by one common set of cables that
are well secured to the ground and controlled from a ground-based
control station. The control station may be computer controlled
and also have a degree of rotational freedom. The control cables
may be made from a lightweight high-tensile strength metallic
alloy or a modern composite fibre. The design of the flying
windmill could incorporate kites as well as lightweight rotating
machinery.
The original flying windmill concept that was envisioned by Dr
Roberts was designed to use one or two pairs of counter-rotating
rotors to simultaneously provide lift and drive lightweight
electrical generating equipment. The use of multiple control lines
would allow a battery of such windmills to fly "in formation" at
progressively higher altitudes of between 1000-feet and 2000-feet.
Rotors of 100-feet diameter may be mounted with their centres
105-feet apart on either side of a single upper cable and above
2-lower cables that will provide vertical and lateral control.
Lightweight vertical-axis wind turbines that feature helical
blades may be mounted below the rotors. These wind turbines could
drive the electrical generation gear and rotate independently of
the rotors that only provide lift.
A variation of this concept could use automotive-type Rzeppa
constant-velocity joints between the counter-rotating, helically
bladed wind turbines and the rotors. The wind turbines would drive
the rotors that in this case could be replaced by giant Frisbees
that will use the boundary layer effect to remain aloft. Birds
that bump into the giant spinning Frisbees may be none the worse
off after such an encounter. Large spinning Frisbees would produce
powerful gyroscopic effects that could strain bearings. A 4-cable
system may be used to control the tilt of the flight rotors, the
tilt of the vertical-axis bladed turbines, manage system torque
reactions and also provide lateral control to the system.
Transversely Mounted Wind Turbine
Large wind turbines that were designed to operate as
vertical-axis units may be transversely mounted as single units
below the flight rotors and operate in a horizontal-axis mode. The
helical blades of the turbine may be set so to produce power would
from below the horizontal rotational axis. Such operation may
produce some extra lift. An airfoil/kite may also be placed ahead
of the transverse mounted turbine and above its rotational axis to
produce additional lift and deflect a faster airstream over the
working surfaces of the turbine. Torque reactions from the
transversely mounted wind turbines would easily be restrained by
the upper and lower control-cables.
Take-off and Landing
Modern electrical multi-plexing technology could enable the
electric power cables to simultaneously perform multiple
functions. During take-off, the tilt of the rotor blades could be
adjusted (via solenoid) while power is provided to induction
motors that may be used during system take-off and landing. When
the system reaches an optimal altitude, the induction motors will
cut out while the rotor blades tilt (via spring pre-load) to
maintain wind-powered flight and spring-loaded clutch mechanisms
(previously dis-engaged by solenoid) would simultaneously engage
the electrical generation sub-system.
The landing sequence could follow standard helicopter practice
when after a mid-flight engine shutdown. Pilots are trained to
re-adjust the tilt of the rotors to accelerate them during
descent, then reverse the tilt of the rotor blades at low-altitude
so as to enable a gentle landing. Electrical signals sent along
the multi-plexed power cables could activate solenoids to
re-adjust the tilt of rotor blades and disengage power generation
during the descent and landing sequence of a flying windmill
battery.
Northern Winds
In parts of Alaska, Siberia and Northern Canada, the wind speed
is estimated at 45-feet/second at over 3000-feet above ground.
Remote communities in these regions could use flying windmills to
generate power during the winter months. Canada may have a
potential over of 30,000,000-Kw of wind power at altitudes between
3000-feet and 5000-feet above ground. During a typical Northern
Canadian or Alaskan winter, the air density at minus 40-degrees F
is 0.09447-lb/cu.ft. At a wind speed of 44-feet/second (~30-miles
per hour), an area that is 1000-feet wide by 3000-feet in height
would have a power generation potential of just over 1000-Mw in
wind energy. The potential would rise to over 8000-Mw in a wind
blowing at 60-miles/hour (88-feet/second). (Equation used for
power = 50% x air density x 1/gravity x cross section area x
velocity cubed).
If the total swept area for a flying windmill battery covered
1,000,000-square feet, its power output at 25% efficiency would be
42.2-Mw of power (wind speed at 30-miles per hour) for an
installation that could supply power to a community of some
8,500-homes. Some designs of wind turbines can operate at 35%
efficiency in high winds and raise power output to 59-Mw, enough
to supply power to a community of over 11,000-homes (5-kw per
home). During the cold northern winter months, winds frequently
exceed 30-miles per hour at elevations of over 3000-feet above
ground and can exceed 60-miles per hour for prolonged durations in
some regions. The power output could rise to 338-Mw at 25%
efficiency and to 473-Mw at 35% efficiency.
Magnus Rotors
As an alternative the bladed rotor, the flying windmill could
also use a Magnus rotor that is transversely mounted into the
upper control surface of a sharply curved wing. This approach
would be derived from the British "paddle wheel" propelled model
aircraft. Air that flows over the upper surface of the wing-kite
would spin the Magnus rotor and activate the boundary layer
effect. The boundary layer effect could re-direct the airstream on
the upper surface through an extreme "angle of attack". The moving
smooth surface of the spinning Magnus rotor would prevent the
separation of air from wing that would otherwise cause a stall on
the wing of conventional aircraft.
The combination of the Magnus rotors and specialized airfoils
could generate sufficient lift to carry the weight of power
generation equipment. In addition, the hollow spinning Magnus
rotors would produce a gyroscopic effect around the transverse
axis and provide a measure of stability. The electrical generation
equipment may be driven by a separate Magnus rotor that may also
be transversely mounted and near the rear of the under side of the
wing. There are a variety of arrangements as to how additional
Magnus rotors that spin on a transverse axis may be installed
below the wing. The main wing and additional kites mounted below
it may alternatively carry vertical-axis counter-rotating Magnus
rotors to generate power.
Lightweight, counter-rotating Magnus rotors that spin on a
vertical-axis could be designed to mimic the flying behavior of an
array of box kites so as to provide additional lift while
generating power. The main advantage of using Magnus rotors is
that they are quite harmless to birds. The helical-blade,
vertical-axis wind turbine can become more bird-friendly if the
surface that travels against the wind is shielded by a kite, an
airfoil or by a wind deflector that directs the airstream on to
the blades' working surfaces. Such turbines may be mounted under
the lift-enhanced wing that contains the Magnus rotor.
Suitable Locations
Suitable locations for batteries of flying windmills would be
perpetually windy areas that are fat away from population centres.
There are several suitable regions in Northern Canada that include
Nunavut, the mountainous regions of British Columbia, the
mountainous regions of Newfoundland and Labrador, the highland
regions of Northern Quebec, much of Northern Ontario, Northern
Manitoba and Northern Saskatchewan. There are many other suitable
regions around the world where flying windmills could be used and
where they would contribute to the amount of electric power that
may be generated there in the future.
The powerful Northeast Trade winds blow over the Lesser
Antilles in the Eastern Caribbean. Batteries of flying windmills
may have to land and take-off from the west coasts of the islands
of the Lesser Antilles. These island nations lack available space
on land. Powerful Southeast Trade winds blow on to Brazil's
sparsely populated coast between Natal and Salvador. Strong winds
called Westerlies blow over the high altitudes and sparsely
populated southern regions of Chile and Argentina. A range of
suitable locations exists around the world where batteries of
flying windmills could be installed to generate electric power.
Conclusions
Perhaps the main conclusion that can be drawn about batteries
of flying windmills is that it is a concept that is open to
further research and development. It does offer the promise of
reducing the cost of installing multiple wind turbines. It offers
the potential to economize on land area as far as generating large
amounts of power is concerned. The capital cost of wind power
generation is high when compared to the amount of power being
produced. These costs need to be reduced while the power output
needs to be raised. The flying windmill battery of multiple wind
turbines is one possibility in that direction in that it could be
developed further over the long-term future to improve the cost to
power ratio for wind power generation.
The main concern about flying windmills is the altitude at
which they can be flown (between 15,000-feet to 35,000-feet).
There are efficiency gains to be had from flying windmills at such
altitudes provided they fly well away from commercial flight
paths. When they are flown at lower altitudes, the risk of
collisions between large commercial passenger aircraft is greatly
reduced.
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