a. Field of the Invention
The present invention relates generally to thrusters that provide motive power for watercraft, and, more particularly, to a thruster assembly that performs both propulsion and ballasting/dewatering functions onboard a vessel.
b. Related Art
Thrusters, as relate to waterborne vessels, are propulsive devices that are generally employed to propel and/or maneuver the vessel. As compared with shaft drives and other forms of propulsion that employ a remote power plant, thruster units commonly include an electric or hydraulic motor mounted in close association with the propeller itself in a submerged location, with electrical power or hydraulic pressure being supplied to the motor from a remote location within the hull. The propeller is frequently enclosed within a circular shroud. The motor may be reversible, and in some instances the assembly is pivotable so as to change the direction of thrust, e.g., to provide a steering effect.
Thruster units provide significant advantages in many applications, but like all propulsion systems they consume a degree of power. Power consumption is virtually always a concern in vessel design and operation, but it even more so in the case of watercraft and other vessels that are small in size and/or are intended to operate for long periods of time without refueling. Exemplary of this type of vessel are craft intended for autonomous operation such as for observation and surveillance purposes, for example. Such craft—referred to from time-to-time as unmanned autonomous vessels (UAVs)—frequently rely on wind, waves and/or sunlight as sources of energy to satisfy their power requirements in whole or in part. Typically, power requirements include not only propulsion, but steering and guidance systems, sensors onboard computing systems, and other electrical or mechanical loads as well. Moreover, some such vessels are designed for submersible operation, which necessitates pumping equipment to ballast and deballast in order to submerge and surface the craft. The low energy density of environmental sources (wind, solar, wave) means that comparatively small amounts of power can be obtained, with the result that the power budget is generally very tight. A related factor is that any added weight requires more power to propel, thus increasing energy consumption.
Much weight is the result of multiple components required to perform the above and additional functions. Furthermore, complexity and multiple components tend to both increase cost and reduce reliability, the latter again being a particularly significant consideration in the context of UAVs that must operate for extended periods with little or no human intervention. Weight and complexity also negatively impact the ability to transport, launch/retrieve and handle the craft. For example, many UAVs must be transported to distant operating areas (e.g., for military operations, ocean surveying, meteorological observations, and so on), often onboard an aircraft where weight and space are at a premium. Furthermore, after arriving at the operating area the craft must frequently be handled and launched from/recovered to a ship or other mother vessel, where excess weight can be a significant detriment. Still further, excess weight can compromise the vessel's maneuverability and responsiveness during operation.
Accordingly, there exists a need for an apparatus that enables a waterborn vessel to employ a thruster for propulsion while taking advantage of the thruster for other functions, so as to consolidate systems and reduce overall complexity and weight of the vessel. Furthermore, there exists a need for such an apparatus that can be economically constructed and that is robust and able to perform reliably without excessive maintenance.
The present invention addresses the problems cited above, and provides a thruster assembly having multiple functions, including the functions of providing propulsion for a vessel and of supplying and withdrawing flows of water to an interior volume, system or other location onboard the vessel.
In a broad aspect, the invention provides an assembly comprising: (a) a thruster that generates a flow of water generally along an axis of the thruster; (b) a passage into the vessel, the passage having an opening generally at an exterior of the vessel; and (c) a mechanism that pivots the thruster between a first position in which the axis of the thruster is directed to produce a flow that provides propulsion to the vessel, and a second position in which the axis of the thruster is directed into the end opening of the passage to produce a flow that enters or exits the vessel.
The passage into the vessel may comprise a chamber having the opening of the passage formed therein. The passage may further comprise at least one conduit extending from the chamber to an interior of the vessel. The at least one conduit may comprise an input conduit through which water flows from the chamber to on board the vessel in response to operation of the thruster in a first direction. The at least one conduit may comprise an outlet conduit through which water is withdrawn from the vessel in response to operation of the thruster in an opposite direction. The at least one conduit may comprise a first, inlet conduit in fluid communication with the chamber, and a second, outlet conduit in a fluid communication with the chamber. The conduits may comprise check valves that prevent backflow of water therethrough.
The opening of the conduit may be located generally at a side of the vessel, with the chamber extending into an interior of the vessel. The side of the vessel at which the opening is located may be a bottom side of the vessel. The mechanism that pivots the thruster may comprise a mechanism that pivots the thruster from a first position in which the axis of the thruster extends generally parallel to an axis of the vessel, to a second position in which the axis of the thruster extends generally perpendicular to the axis of the vessel so as to be directed into the opening of the chamber. The pivot mechanism may be operable to pivot the thruster to a third position in which the thruster is received in an interior of the chamber in a position inverted from the propulsion position.
The mechanism that pivots the thruster may comprise at least one pivot connection located proximate the external opening, about which the thruster is pivoted between its positions. The thruster may comprise a plate that is mounted to the thruster that closes off the exterior opening in response to the thruster being pivoted to the propulsion position, and that pivots upwardly together with an end of the thruster in response to the thruster being pivoted to the secondary position so as to permit the end of the thruster to enter the exterior opening. The closure plate may comprise an outer edge that conforms closely to an edge of the exterior opening when the thruster is in the drive position.
The mechanism that pivots the thruster between the primary and secondary positions, i.e., drive mechanism, may comprise a pinion gear that is mounted to the thruster, a drive gear that is in engagement with the pinion gear, and a mechanism that rotates the drive gear—i.e., actuator mechanism—so that in response the pinion gear rotates in an opposite direction so as to pivot the thruster. The drive gear may comprise a quadrant gear. The actuator mechanism that rotates the drive gear may comprise a linear actuator, and a linkage connecting an end of the linear actuator to the drive gear at a location spaced from an axis of the drive gear. The linear actuator may comprise a hydraulic cylinder, and the linkage may comprise a link rod having a first end mounted to the end of the hydraulic cylinder and a second end mounted to the drive gear. The hydraulic cylinder may comprise a second end that is mounted to the chamber via a swing arm that enables the linear actuator to pivot as the actuator is extended and retracted. The swing arm may comprise a first end that is pivotably mounted to the second end of the hydraulic cylinder, and a second end that is pivotably mounted to the chamber. The second end of the swing arm may be pivotably mounted to the pivot of the drive gear.
The assembly may further comprise a base that supports the pivot mechanism, chamber and thruster, and that is mountable in a cooperating opening in the vessel.
The conduits may comprise conduits leading into and out of a hull space of the vessel or a compartment of the vessel. The flows of water through the conduits may serve the functions of flooding and dewatering to submerge and surface the vessel or to ballast the vessel, or may serve other functions.
These and other features and advantages of the present invention will be more fully appreciated from a reading of the following detailed description with reference to the accompanying drawings.
Referring again to
As can be seen with further reference to
Rotation of the gears 36, 40, thus pivoting plate 28 and the thruster 12, is accomplished by operation of an actuator mechanism 49. In the illustrated embodiment, the actuator mechanism comprises a linear actuator, in the form of a hydraulic cylinder 50, and a link rod 52 that is connected to the quadrant gear 46. As can be seen in
As noted above, the plate 28 from which the thruster is suspended is located within opening 32 that leads upwardly into the assembly. As can be seen with further reference to
The discharge and intake lines 72, 74 include end openings 76, 78 that communicate with an interior volume or compartment of the vessel. The openings may be located directly within the compartment or volume into which water is discharged and from which it is drawn, or hoses, manifolds or other conduits may be connected to the openings so as to lead the flow to/from remote locations. Check valves 80, 82 are installed in lines 72, 74 so as to prevent backflow. Consequently, water may be supplied to an interior volume of the vessel from chamber 70 through line 72, and withdrawn back out via line 74. In the illustrated embodiment, the intake pipe and lower portion of the chamber are set within a tray-shaped coaming 84 extending upwardly from belly panel 34 that fits within a cooperating hull opening so as to locate the assembly in the bottom of the vessel and that also imparts strength and structural rigidity to the assembly, with drain parts 86 being formed in the coaming above the belly plate to permit water to pass therethrough during deballasting.
Mounted together on the belly plate, the assembly forms a compact, structurally self-contained unit that can be mounted in a corresponding opening in the hull of the vessel and that can be conveniently removed for servicing. In some embodiments, however, some the components may be mounted to the hull or other structure of the vessel while others may be mounted to the assembly base, or all of the components may be mounted to or built into the structure o the vessel itself.
Operation of the multifunction thruster assembly is illustrated in
Firstly,
In order to shift the thruster assembly to the ballasting position, hydraulic cylinder 50 is retracted in the direction indicated by arrow 110 in
It will be understood that the scope of the appended claims should not be limited by particular embodiments set forth herein, but should be construed in a manner consistent with the specification as a whole.
This application claims the benefit of Provisional Patent Application Ser. No. 62/231,163 filed Jun. 25, 2015.
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1011594 | Aug 1965 | GB |
Number | Date | Country | |
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20170137101 A1 | May 2017 | US |
Number | Date | Country | |
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62231163 | Jun 2015 | US |