With reference to
The present invention is directed towards a control system for operating a remotely operated winged underwater vehicle (ROV). The winged ROV has a propulsion system and directional controls that allow an operator to control the speed and direction of the winged ROV through a body of water. The winged ROV can also have sensors and feedback devices that can provide information that is transmitted back to the operator or any other receiver.
A ship can be coupled to the winged ROV with an optical tether. A remotely located controller can be coupled to an optical transceiver so the operator can transmit and receive data from the winged ROV. For example, the controller transmits control signals through the tether to the winged ROV and the winged ROV performs the actions of the control signals. The sensors and feedback signals produced by the winged ROV are transmitted back through the tether to the controller on the ship.
The diving depth of the winged ROV can be limited by the length of the tether. The tether can have various lengths and diameters. A larger diameter tether will be stronger but will also result in more drag forces as the winged ROV moves through the water. A ⅜ inch tether cable can have sufficient room for a conductive wire cable and may be suitable for tether lengths up to 500 feet. A ⅛ inch diameter cable can have a length of up to about 1,000 feet and can have sufficient room in the cable cross section for an optical data fiber. The system solves the problem of remotely controlling winged ROVs in a manner that allows the winged ROV to travel through any body of water while being in full high speed data communications with a controller.
In order to drive the winged ROV, an alternate means for power is required. Various energy systems can be employed to provide on board power for the ROV. In a preferred embodiment, the invention's power is provided by lithium ion batteries as used on Hawkes designed manned submersibles. In addition to the power supply, an optical communications system is also required. The data transfer rate for high bandwidth communications sufficient to support a closed circuit television may require data transfer rate of about 1-12 Mega Bytes per second (MBps).
With reference to
As the ROV 201 moves, the communications tether 205 is pulled in tension and the surface buoy 211 is towed across the surface of the water 219. As the ROV 201 moves horizontally away from the support ship 221, the tether 205 will be tensioned and additional tether 205 can be released from the support ship 221 or the support ship 221 will follow the ROV 205. Thus, the ROV 201 is free to move anywhere horizontally through the water and the depth of the ROV 201 movement will only be restricted by the fully extended length of the tether 205.
In some cases, the described system can be used with other communications systems that would like to receive data from the ROV 201 or transmit data to the support ship 221 or the ROV 201. For example, a land based control station 215 can transmit data to a support ship 221 which then transmits the data through the tether 205 coupled to the ROV 201. Similarly, the ROV 201 can transmit signals through the tether 205 to the support ship 221 and then the support ship 221 can transmit information to the land based control station 215. Since the support ship 221 will always remain on the water surface, the ROV 201 can travel anywhere.
In an embodiment the maximum length of the cable tether will depend upon the type of cable being used and the drag generated by the tether. The ROV will have to have sufficient power to overcome the buoyant forces of the ROV and the forces applied to the ROV by the tether. A wider cross section tether will cause more drag as it moves through the water and therefore a wider tether may need to be shorter in length for the ROV to overcome the drag forces than a thinner cross section tether. As discussed, the tether can contain an electrical conductor or an optical fiber. The tether containing a conductive wire cable will tend to be wider in diameter. For example, a ⅜ inch diameter cable may be required to contain a copper wire can only have a maximum length of approximately 500 feet. In contrast a ⅛ inch diameter armored cable that contains a thin optical fiber can be up to about 1,000 ft in length.
In some embodiments, the system can use different cables depending upon the dive that can be connected to the control ship and the ROV by optical fiber connectors. An optical fiber connector terminates the end of an optical fiber, and enables quicker connection and disconnection than splicing. The connectors mechanically couple and align the cores of fibers so that light can pass. Most optical fiber connectors are spring-loaded so the fiber endfaces of the two connectors are pressed together, resulting in a direct glass to glass or plastic to plastic contact, avoiding any glass to air or plastic to air interfaces, which would result in higher connector losses. A variety of optical fiber connectors are available. The main differences among types of connectors are dimensions and methods of mechanical coupling.
The hydrodynamic drag can also be reduced by using a fairing around the tether. If a hydrodynamic fairing is used, the drag is significantly reduced in comparison to a circular cross section tether. The drag coefficient Cd used to predict the drag forces can be reduced from about 1.2 for a circular cross section to about 0.3 for a tether with fairing having a minimum thickness that is equal to the diameter of cross section. Thus, an ⅛ inch wide armored cable that has a fairing can be up to about 2,000 feet in length and produce less drag than a much shorter circular cross section cable. With reference to
The optical fiber cable includes an optical fiber that that is surrounded by a cladding of plastic layers that are coated around the outer diameter of the optical fiber. The cladding can be coated with a tough resin buffer layer, which may be further surrounded by a jacket layer which can be made of a plastic material. These layers add strength to the fiber but do not contribute to its optical wave guide properties. The jacketed fiber can be enclosed, with a bundle of high strength flexible fibrous polymer members like aramid materials. Each end of the cable may be terminated with a specialized optical fiber connector to allow it to be easily connected and disconnected from the ROV and communications equipment on the ship.
In an embodiment, the operator can select the most appropriate tether length. Since the operator will typically know the required dive depth prior to releasing the ROV, a suitable length communications cable can be attached between the ROV and buoy. During the dive, the operator can control the ROV so that it does not exceed the maximum depth. The system may also contain warning mechanisms that inform the operator when ROV is reaching the maximum depth for the cable being used.
In other embodiments, the tether can be retracted into the support ship 221 or a spool module that is placed in the water adjacent to the support ship 221. With reference to
With reference to
The forces acting on the ROV also include vertical forces. The wings of the ROV must be able to provide sufficient vertical forces to overcome both the buoyant forces of the ROV and the lift forces from the tension on the cable. Hence in order for the vehicle to move as commanded, it will need to at all times be able to generate the counter forces and vector to the tension, direction and rotational moments inflicted by the tension in the tow cable and its angle and place of action(s) on the vehicle.
The ability of the ROV to physically move as commanded and remain under control and counter all tether forces and moments coupled to a support ship with a cable has been impractical to date, even using a minimum diameter and streamlined drag armored fiber optic link. As the ROV moves, the cable tension pulls the ROV up and prevents accurate movement control. In order to overcome this problem, a winged submersible is required, such as the Hawkes Ocean Technologies (HOT), US Pat. No. 7,131,389 which is hereby incorporated by reference. The wings, rudders and elevators of the ROV produce strong directional forces that are able to resist the uncontrolled disruptive physical vertical pull and turning moments caused by the tow cable. The cable and buoy forces that result from movement of the ROV are instantly controlled by controllable winged surfaces of the ROV. In order to minimize the effects of the buoy, the connection point can be at the center of hydrodynamic effort of the winged submersible ROV. Alternatively, the connection point can be slightly forward of the center of hydrodynamic effort of the winged submersible ROV. Thus, any vertical forces applied to the ROV by the tether will not alter the pitch of the ROV. The tether can also be connected to an elevated surface such as a fin, so that it is kept away from any moving components such as the propellers to avoid entanglement. When the tension on the tether pulls the ROV sideways, the ROV can roll so that the tether is vertically aligned with the ROV. This allows the wings to provide both a down ward vertical force and a horizontal side force to resist the tension in the cable.
The remotely controlled ROV uses winged surfaces with single or multiple thrusters providing forward thrust and speed. The winged ROV uses the movement or flow of the water over the wings to provide forces perpendicular to the wings. Thus, a winged ROV that is traveling horizontally through the water will produce a substantial vertical force that is substantially greater than any vertical forces caused by the cable drag or buoy buoyancy. The relationship between thrust and lift can by estimated and quantified by the lift/drag ratio. In an embodiment the lift to drag ratio of the winged ROV may be about 10:1. Thus, an upward pull of the tow cable of say 100 lbs can be resisted by a downward lift from a wing of 100 lbs for a forward thrust penalty of only 10 lbs. In contrast, a non-winged ROV will require a downward thrust of 100 lbs. just to counteract the cable drag.
This negative lift of the ROV can be altered by changing the area of the wings. A larger wing will be able to produce more negative lift for a ROV velocity. Thus, if there is going to be a large tension force on the cable and the cable is positioned at a high vertical angle relative to the ROV and the ROV has a large buoyant force and must travel at slow horizontal speeds, larger wings may be necessary. A drawback of the larger wing is increased drag. Thus, more thrust is required to move an ROV having larger wings through the water. Conversely, if the tension is low and the ROV has a low buoyant force and must travel fast, smaller wings will reduce the drag and allow for more energy efficiency. In an embodiment, the ROV may have replaceable wings that allow for multiple negative lift forces. Alternatively, the ROV may have wings that are adjustable in size.
With reference to
Fv=T×SIN θ
Fh=T×COS θ+D/L×Fv
Fv=vertical force
Fh=horizontal force
T=tension
η=angle of cable to the ROV
L/D=lift/drag ratio
In addition to the tether forces, the buoyant force will lift the ROV. In order to overcome the buoyant vertical forces negative lift provided by the wings and must be greater than the Fv and buoyant force Fb. As discussed, the lift to drag ratio can be about 10:1, thus a thrust force Ft of 1 pound in the horizontal direction will result in 10 pounds of vertical force. The thrust must also overcome the horizontal forces. Thus, the required thrust of the ROV can be estimated based upon the equation:
Ft>D/L×(Fv+Fb)+Fh
Fb=buoyant force
Self-powered craft, especially battery-powered craft, are energy-limited. And thus the leverage and efficiency of a fully controllable (Pitch, Roll, yaw) winged body, able to hold large vertical loads and moments and able to manage the large tow forces with a smaller amount of additional forwards thrust, is a great advantage in making the concept work for a self-powered craft requiring minimum power.
The present invention has been described as having a rechargeable lithium battery which can limit the duration of the ROV operations. In an alternative embodiment, the support ship can have the energy source such as an electrical power supply, electrical generator, solar cells, fuel cells, etc. In this embodiment, the cable can include electrical conductors that provide a low resistance transmission of electrical power through tethered tow cable to the ROV. Since the power source is exposed to air, the source of power in the support ship can be an air-breathing gas powered electrical generator to provide longer duration operations.
The winged ROV can also have three axis sensors so the vehicle will be flown through the water manually with the wings level to a heading or have auto pilot controlling the ROV on three axis of movement. Because the wing surfaces of the ROV are substantially greater than the drag forces, the cable can move with the applied forces and the vehicle will stay on course.
In an embodiment, the system can estimate the position of the ROV by adding the length of the tether in the direction of the tether from the support ship. The system can then use a pressure transducer signal from the ROV to determine its depth. Based upon these calculations, the system can accurately determine the position of the ROV.
With reference to
While the invention has been described herein with reference to certain preferred embodiments, these embodiments have been presented by way of example only, and not to limit the scope of the invention. Accordingly, the scope of the invention should be defined only in accordance with the claims that follow.
This application is a continuation in part of U.S. patent application Ser. No. 12/712,082, REMOTELY OPERATED UNDERWATER VEHICLE filed Feb. 24, 2010 which claims priority to U.S. Provisional Patent Application No. 61/155,658, REMOTELY OPERATED UNDERWATER VEHICLE, filed on Feb. 26, 2009. U.S. patent application Ser. Nos. 12/712,082 and 61/155,658 are both hereby incorporated by reference in their entirety.
Number | Date | Country | |
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61155658 | Feb 2009 | US |
Number | Date | Country | |
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Parent | 12712082 | Feb 2010 | US |
Child | 12767984 | US |