It is desirable to transfer electrical energy from a source to a destination without the use of wires to guide the electromagnetic fields. A difficulty of previous attempts has been low efficiency together with an inadequate amount of delivered power.
Our previous applications and provisional applications, including, but not limited to, U.S. patent application Ser. No. 12/018,069, filed Jan. 22, 2008, entitled “Wireless Apparatus and Methods”, the entire contents of the disclosure of which is herewith incorporated by reference, describe wireless transfer of power.
The system can use transmit and receiving antennas that are preferably resonant antennas, which are substantially resonant, e.g., within 5%, 10% of resonance, 15% of resonance, or 20% of resonance. The antenna(s) are preferably of a small size to allow it to fit into a mobile, handheld device where the available space for the antenna may be limited, and the cost may be a factor. An efficient power transfer may be carried out between two antennas by storing energy in the near field of the transmitting antenna, rather than sending the energy into free space in the form of a travelling electromagnetic wave. Antennas with high quality factors can be used. Two high-Q antennas are placed such that they react similarly to a loosely coupled transformer, with one antenna inducing power into the other. The antennas preferably have Qs that are greater than 1000.
The present application describes transfer of energy from a power source to a power destination via electromagnetic field coupling. Embodiments describe techniques for maximizing the energy transfer.
These and other aspects will now be described in detail with reference to the accompanying drawings, wherein:
A basic embodiment is shown in
The frequency generator 104 can be preferably tuned to the antenna 110, and also selected for FCC compliance.
This embodiment uses a multidirectional antenna 115 shows the energy as output in all directions. The antenna 100 is non-radiative, in the sense that much of the output of the antenna is not electromagnetic radiating energy, but is rather a magnetic field which is more stationary. Of course, part of the output from the antenna will in fact radiate.
Another embodiment may use a radiative antenna.
A receiver 150 includes a receiving antenna 155 placed a distance D away from the transmitting antenna 110. The receiving antenna is similarly a high Q resonant coil antenna 151 having a coil part and capacitor, coupled to an inductive coupling loop 152. The output of the coupling loop 152 is rectified in a rectifier 160, and applied to a load. That load can be any type of load, for example a resistive load such as a light bulb, or an electronic device load such as an electrical appliance, a computer, a rechargeable battery, a music player or an automobile.
The energy can be transferred through either electrical field coupling or magnetic field coupling, although magnetic field coupling is predominantly described herein as an embodiment.
Electrical field coupling provides an inductively loaded electrical dipole that is an open capacitor or dielectric disk. Extraneous objects may provide a relatively strong influence on electric field coupling. Magnetic field coupling may be preferred, since extraneous objects in a magnetic field have the same magnetic properties as “empty” space.
The embodiment describes a magnetic field coupling using a capacitively loaded magnetic dipole. Such a dipole is formed of a wire loop forming at least one loop or turn of a coil, in series with a capacitor that electrically loads the antenna into a resonant state.
Wireless energy transfer, however, requires an analysis of the efficiency. The efficiency data can be expressed as
where Pr is power output at the receive antenna and Pt is power input at the transmit antenna.
The inventors considered both electrical field coupling and magnetic field coupling, and have decided that magnetic field coupling may be more promising for wireless power transfer. While electrical field coupling may be promising for proximity power transmission, a significant problem from electrical field coupling is that it shows a relatively strong influence from extraneous objects. Electrical field coupling uses an inductively loaded electrical dipole e.g. an open capacitor or dielectric disc.
Magnetic field coupling, as used according to embodiments, uses a capacitively loaded magnetic dipole antenna as described in the embodiments. This antenna can include a conductive single loop or series of loops with a capacitor attached across the inductance. Magnetic field coupling may have the advantage of relatively weak influence from extraneous objects.
A desirable feature of this technique is to use resonant coil antennas, with an inductance coil 300 in the series with a capacitance 305.
A receiving coil 320 has a capacitance 321 connected in series therewith, in the area of the magnetic field, located a transfer distance d away from the transmit antenna. The received energy from the receiving antenna 320, 321 is coupled to coupling loop 325, and sent to a load 330. The load may include, for example, power rectification circuitry therein.
The loss resistance within the circuit is dependent on radiation resistance, eddy current losses, skin and proximity effect, and dielectric losses.
The transfer efficiency can be derived according to the equations:
Three specific coil geometry forms are shown in
The coil characteristics are as follows:
The transfer efficiency can therefore be calculated as
So, given a Q-factor, efficiency is no longer a function of frequency.
Efficiency decreases with d6.
Doubling transmitter coil radius increases range by sqrt (2)=(41%)
Doubling transmitter Q-factor doubles efficiency
Doubling Q-factor increases distance only by sixth root of 2(12%).
Conclusion:
Based on these characteristics, the coupling factor can be considered primarily a function of geometric parameters and distance. The distance cannot be controlled, but of course the geometric parameters can be. The mutual inductance, overall loss resistances of the antennas and operating frequencies may also relate to the efficiency. Lower frequencies may require lower loss resistances or higher mutual inductance to get the same transfer efficiency as at higher frequencies.
The transfer efficiency for a rectangular loop is as follows, for the loop with characteristics shown in
Optimization of the number of turns can be considered as follows:
for a coil of length lA, radius rA, and pitch to wire diameter ratio of θ=2c/2b.
If resonance frequency is used as the optimization parameter, then
From these equations, we can draw the conclusion that for given coil form factor the Q factor is independent to some extent of the number of turns. Coils formed of thicker wires and less windings may perform as well as coils with a higher number of turns. However, the Q factor is highly dependent on the frequency. At low frequencies the Q factor increases according to f1/2. This is dependent primarily on the skin effect. At higher frequencies, the key factor increases as f−7/2. This is dependent on the skin effect plus the radiation resistance.
There exists an optimum frequency where the Q is maximized. For any given coil this depends on the coil's form factor. The maximum Q, however, almost always occurs above the self resonance for frequency of the coil. Near self resonance, the coil resonator is extremely sensitive to its surroundings.
This produced a result shown in
The magnetic power transmission according to this disclosure may rely on high-Q for improved efficiency. A lossy environment can have a deleterious effect on high Q resonators. Using the antenna 1005 near a lossy material such as a dielectric material 1010 such as a table or a conductive material such as a metal part 1000 is shown in
In order to reducing the effects of the environment, various measures can be taken. First, consider the Q factor
This is three variables and two equations, leaving 1 degree of freedom for the resonator design.
Resonators with low inductance to capacitance ratios tend to be more stable in an environment where dielectric losses are predominant. Conversely, high inductance to capacitance ratio resonators tend to be more stable in environments where eddy current losses are predominant. Most of the time, the dielectric losses are predominant, and hence most of the time it is good to have a low L/C ratio.
Note that there is a strong effect from lossy dielectrics.
Exemplary resonators for environments with lossy dielectrics can include 13.56 MHz plus coupling loop may using a seven turn, 6 mm silver plated copper wire with a 17 cm coil diameter and an air capacitor of 10 pF. Conversely, a low L/C ratio resonator for this frequency can operate without a coupling loop, using a 3 cm silver plated copper tube, 40 cm diameter loop and high-voltage vacuum capacitor of 200 pf.
For the low L/C resonant antennas, a vacuum capacitor may produce significant advantages. These might be available in capacitance value of the several nanofarads, and provide Q values greater than 5000 with very low series resistance. Moreover, these capacitors can sustain RF voltages up to several kilovolts and RF currents up to 100 A.
To conclude from the above, high L/C ratio resonator antennas e.g. multi-turn loops are more sensitive to lossy dielectrics. Low L/C ratio resonator antennas e.g. single turn loops are more sensitive to a lossy conductive or ferromagnetic environment. Q factors of the described antennas, however, may vary between 1500-2600. A single turn transmit loop of 40 cm in diameter may have a Q value larger than 2000.
The wireless power may be integrated into portable devices and a number of different ways as shown in
Given a specified magnetic field strength at a specified receiver position, at an operating frequency, receive power may be expressed as:
where:
Note according to this equation, that the value of N, the number of turns, appears both in the numerator and denominator, (appearing as a squared term in the numerator).
The power is also inversely proportional to Aw; the cross-sectional area of the winding. Increasing the cross-sectional area may improve power yield. However, this may become too heavy and bulky for practical integration.
The value δ represents the electrical conductivity of the wire material. Increasing this may increase the power yield proportional to δk, with the exponent K. in the range of 0.5 to 1. Copper and silver are the best conductors, with silver being much more expensive than copper. Room temperature superconductivity could improve this value.
RA represents the physical or equivalent radius.
However, this physical radius is limited by the form factor of the device into which the antenna will be integrated. The equivalent radius of a wire loop of this type may be increased through use of materials or devices that locally increase alternating magnetic flux to generate electromotive force in the wire loop. Increasing this equivalent radius may be a very effective antenna parameter, since the received power is proportional to this radius to the fourth power. Moreover, increasing the equivalent radius also increases the Q factor by R2. This produces a double benefit.
An embodiment discloses increasing the equivalent radius of a wire loop antenna without increasing its actual radius. A first technique uses materials with ferromagnetic properties such as ferrite. It is also possible to exploit the gyromagnetic effect of ferrites. In addition, the use of magneto MEMS systems can be used for this. Each of these techniques will be separately discussed.
Materials that have ferromagnetic properties (susceptibility Xm greater than zero) can magnify magnetic flux density inside a coil.
B=μ
0(1+Xm)H=μ0(H+M)=μ0μrH
where M is the magnetization of the material and ur is the relative permeability of the material. The ferromagnetic material in essence adds additional magnetic flux to the already existing flux. This additional flux originates from the microscopic magnets or magnetic dipoles that are inside the material.
The magnetic dipole moment results from electron spin and orbital angular momentum in atoms. The moment mostly comes from atoms that have partially filled electron shells and unimpaired/non-compensated spins. These atoms may exhibit a useful magnetic dipole moment.
When an external magnetic field is applied, magnetic dipoles organized in lattice domains align with the external field. See
Ferrite materials typically show a hysteresis effect between the applied magnetic field or H field and the resulting B field. The B field lags behind the H field. In an induction coil wound around the ferrite rod, this effect causes a non-90 degree phase shift between the AC current and the AC voltage against the inductor. At low-H field strength, the hysteresis effect is reduced, thereby reducing losses.
The flux magnification effect of the ferrite rod depends on both the relative permeability (ur) of the ferrite material used, and on the form factor of the rod, for example the diameter to length ratio. The effect of the ferrite rod and a coil antenna may be described by an equivalent relative permeability μe which is typically much smaller than μr. For an infinite diameter and length ratio μe approaches μr. The effect of the Ferrite rod is equivalent to an increase of antenna coil radius by √{square root over (μe)}. At frequencies below 1 MHz and a ratio the increase of the equivalent radius by the Ferrite will be in the order of 3 to 4. Nevertheless, depending on physical size constraints, the use of a Ferrite rod may be beneficial considering that power yield increases according to rA,e4.
The ferrite may need to be relatively long to increase the μe unless the coil radius is small. Ferrite antennas concentrate the magnetic flux inside the rod, which may also lower the sensitivity to the environment.
The Gyro magnetic effects of certain materials such as ferrite can also be used to increase the magnetic flux. When a static magnetic field is applied to a ferromagnetic material such that it saturates, the atomic magnetic dipole movement performs precession around the axis defined by the direction of the static magnetic field. This has an angular frequency of
ω0=γμ0H0
where
with
the gyromagnetic ratio
m: the magnitude of the magnetic dipole moment
J: the magnitude of the angular momentum
Its relative permeability can be described as a complex tensor
μr=μr′+jμr″
which shows a resonance at ω0. This gyromagnetic resonance effect can form resonators with very high Q factors as high as 10,000.
Properties that are similar to these Gyro magnetic materials can be reproduced with magnetomechanical systems formed using MEMS. These systems may have the potential to imitate the Gyromagnetic high Q resonance effect at lower frequency. Two different types of MEMS devices can be used: a compass type MEMS and a torsion type MEMS. The compass type MEMS uses a medium that is formed of micro-magnets that are saturated by applying a static magnetic field H0. The system exhibits resonance at the characteristic frequency defined by the magnetization and be inertial moment of the micro-magnets.
Similarly, a torsion type MEMS is formed of micro-magnets that can move along a torsion beam. The system exhibits ferromagnetic resonance based on the magnetization and inertial moment as well as the spring constant.
While the drawing shows mechano magneto oscillators that are bar-shaped, an embodiment may use disk or sphere shaped materials to improve their movability.
Another possible way of transforming magnetic energy into electrical energy is combined magnetoscriction and piezoelectricity, which can be thought of as reverse electrostriction. Magnetostriction is the changing of the material shape when the material is subjected to a magnetic field. This shape change can occur when the boundaries of Weiss domains within a material migrate or when the domains rotate through external field. Cobalt and Terfenol-D have very high magnetostrictions. The relation between the strain and applied magnetic field strength becomes nonlinear.
A ribbon of magnetostrictive material with a length of a few centimeters shows a resonance that is similar to piezo crystals and quartz in the low-frequency range e.g. around 100 kHz. This effect is also used in passive RFID systems to cause a resonance that can be detected by the RFID coil.
Although only a few embodiments have been disclosed in detail above, other embodiments are possible and the inventors intend these to be encompassed within this specification. The specification describes specific examples to accomplish˜more general goal that may be accomplished in another way. This disclosure is intended to be exemplary, and the claims are intended to cover any modification or alternative which might be predictable to a person having ordinary skill in the art. For example, other sizes, materials and connections can be used. Although the coupling part of the antenna in some embodiments is shown as a single loop of wire, it should be understood that this coupling part can have multiple wire loops. Other embodiments may use similar principles of the embodiments and are equally applicable to primarily electrostatic and/or electrodynamic field coupling as well. In general, an electric field can be used in place of the magnetic field, as the primary coupling mechanism. While MEMS is described in embodiments, more generally, any structure that can create small features could be used.
Any of the embodiments disclosed herein are usable with any other embodiment. For example, the antenna formation embodiments of
Also, the inventors intend that only those claims which use the-words “means for” are intended to be interpreted under USC 112, sixth paragraph. Moreover, no limitations from the specification are intended to be read into any claims, unless those limitations are expressly included in the claims.
Where a specific numerical value is mentioned herein, it should be considered that the value may be increased or decreased by 20%, while still staying within the teachings of the present application, unless some different range is specifically mentioned. Where a specified logical sense is used, the opposite logical sense is also intended to be encompassed.
This application claims priority from provisional application No. 60/973,100, filed Sep. 17, 2007, the entire contents of which disclosure is herewith incorporated by reference.
| Number | Date | Country | |
|---|---|---|---|
| 20090079268 A1 | Mar 2009 | US |
| Number | Date | Country | |
|---|---|---|---|
| 60973100 | Sep 2007 | US | |
| 60904628 | Mar 2007 | US |
| Number | Date | Country | |
|---|---|---|---|
| Parent | 12018069 | Jan 2008 | US |
| Child | 12211706 | US |