The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefore.
Not applicable.
(1) Field of the Invention
The present invention relates in general to the powering of remote sensors, and more specifically to a wireless power transmission system for use with a network of sensing devices.
(2) Description of the Prior Art
Currently, underwater vehicles have on-hull sensor arrays connected to the inboard side of the underwater vehicles, particularly large submarines, by means of large, heavy expensive wiring harnesses. The sensors are embedded in an acoustic polymer material and are located several inches above the hull of the underwater vehicle. There is currently a need for a means of delivering power to the sensor arrays arranged over the exterior of the hull of an underwater vehicle without the use of wired connections in order to reduce costs and the overall weight of the system, and to improve reliability. What is needed is a displacement current method and apparatus for the remote powering of a sensor grid.
It is a general purpose and object of the present invention to provide a method and apparatus that efficiently delivers power to a large array of remote sensors in an on-hull sensor grid.
It is a further object to power the large array of remote sensors without the need of heavy expensive wired connections.
These objects are accomplished with the present invention by delivering electrical energy across the insulating gap that separates the sensor from the hull by means of a displacement current. The exterior hull of an underwater vehicle includes a conducting layer interposed between inner and outer decouplers and a ground plane interposed between a bonding layer and the inner decoupler. An application of alternating current to the ground plane will activate the conducting layer and provide power to the sensors at a location of the outer decoupler. The inner decoupler acts as a capacitor and the ground plane further provides an electrical path back to the hull.
A more complete understanding of the invention and many of the attendant advantages thereto will be readily appreciated as the same becomes better understood by reference to the following detailed description when considered in conjunction with the accompanying drawings wherein:
Referring now to
The sensors 24 are located directly above the boundary between the upper plate 14 and outer decoupler layer 12 and are in contact directly or indirectly with the upper plate 14. By stacking the layers in the manner illustrated in
In the preferred embodiment, it is assumed that a physical penetration of the inner decoupler 16 and the bonding layer 20 by structural members of the hull 22 exists. These sorts of penetrations are places of opportunity where a ground connection can be easily obtained either with or without a custom penetration. The hull 22 is assumed to be 0 volts at all times, making it the true ground of the system.
The sensor packages 24 are placed electrically in series with the upper plate 14. An alternating current voltage of sufficient frequency is induced on the upper plate 14 by the excitation of the lower plate 18. This voltage is rectified and filtered by the sensor packages 24, making a direct current voltage available for biasing of the RF payloads in the sensor packages 24. The rectifiers in the sensor packages 24 can be either half wave or full wave rectifiers. The ground connections of the sensors converge to the nearest available grounding point. In the preferred embodiment the sensors 24 tie into the nearest available grounding point through a bus connection to a ground distribution network 30 which connects electrically back to the hull 22 which serves as the ground. A bus connection is preferred to a ground plane, since the capacitance between the upper plate 14 and the lower plate 18 tend to create a voltage divider effect with the capacitance formed by the inner decoupler 16, reducing the efficiency of the powering scheme.
An equivalent circuit of a network operating on displacement current is shown in
The capacitance of CUBL, COD and CG are all parasitic to the network and should be minimized as much as possible. The voltage across ZL, the load impedance presented by the sensors, is determined in phasor notation using circuit theory according to equation (1) as set out below:
where
is the equivalent impedance formed by the parallel connection of the load impedance ZL and the two capacitors, COD and CG. The current flowing through the load ZL is:
and since the power delivered to the load ZL, then is:
using equations (1) and (4), the power can be expressed as:
For the case when the capacitive reactance of CG and COD are large compared with the load impedance ZL, these terms do not contribute appreciably to the overall expression in (2) and the equivalent impedance is approximately equal to ZL. Equation (5) then reduces to:
Equation (6) bears some closer scrutiny. The power delivered to the load ZL is seen to be a familiar V2/Z term representing the maximum power that can be delivered if the generator was connected directly to the load and a modifying term that depends on the frequency of operation. However, for situations where:
ωCIDZL>>1 (7)
this modifying term approaches unity. This indicates that nearly total power delivery to the load is possible, almost as if the inner decoupler is not there at all. Theoretically, at least, nearly perfect power delivery efficiency is possible under ideal conditions, and that is the appeal that this method has.
The overall efficiency of the power delivery includes generator mismatches and the efficiency of the rectifier and filter stage in the sensors 24 that follows in order to convert the alternating current energy into direct current power used to drive the electronics packages in the sensors.
The advantage of the present invention over the prior art is primarily its simplicity in implementation and function. From this simplicity flows a savings in costs of materials for prior art wiring harnesses, time in implementation of wiring harnesses and time in maintenance. The invention also has a minimal impact on the acoustic properties of the overall system.
In light of the above, it is therefore understood that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described.
Number | Name | Date | Kind |
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4201079 | Worcester | May 1980 | A |
4982385 | Eynck | Jan 1991 | A |
5267221 | Miller et al. | Nov 1993 | A |
5608692 | Toda | Mar 1997 | A |
5827198 | Kassal | Oct 1998 | A |
6127942 | Welle | Oct 2000 | A |
6490228 | Killam | Dec 2002 | B2 |