Patent Application
20230023286
The present application relates generally to a type of watercraft known as unmanned trans-surface vehicles (UTVs) and, more particularly, to UTVs for fleet protection decoys and stand-in intelligence, surveillance, and reconnaissance (ISR), electronic warfare (EW), and operational support.
The Navy has long wished to leverage advances in low-cost commercial technology to support the Navy's mission and our national defense generally. In the maritime context, systems can generally be broken down into two parts: the platform and the payload. Payloads, such as radios, radars, sonars, and other systems, perform the desired mission. Platforms, such as submarines, ships, and aircraft transport payload and provide power and survivability. The cost of performing a mission includes the cost of the platform and the cost of the payload.
Until now, commercial technology has largely been seen as a way to decrease the cost of payloads. Decreases to the cost of platforms has proven elusive. Without the ability to decrease the cost of both the payload and the platform, it is difficult to generate a step change in either cost or operational strategy. For example, if it were possible to decrease the cost of a radar from $10M to $10 k (a 100× decrease), but the cost of the ship to place it on still cost $20M, the overall cost savings is only 30%. When combined with operation and maintenance costs, the cost delta becomes even less.
The primary challenge in decreasing the platform cost is the need to maintain speed, power, endurance, and survivability. These features scale poorly with decreasing vehicle size. For example, the maximum speed of standard vessels (displacement hull) in knots is given by 1.32*Sqrt (length), where the length is in feet. Thus, to go 20 knots, a vessel must be approximately 230′ long. Since vessel cost scales roughly with the cube of vehicle length, creating fast, low-cost platforms is challenging. Similarly, survivability, endurance, and availability of power all scale with vessel length.
The present application discloses a new vessel concept that addresses the need for speed, power, endurance, and survivability using a combination of new technologies and conops (concept of operations) that, together, provide a viable low-cost platform that breaks the standard scaling laws and provides useful capability in a small and inexpensive platform.
In accordance with one or more embodiments, a watercraft is disclosed that is selectively operable in one of a submerged mode and a foiling mode. The watercraft comprises a vehicle payload bay; a sail connected to the payload bay for propelling the watercraft in the foiling mode; and three or more hydrofoils connected to the payload bay. The hydrofoils are configured to provide control of the roll, pitch, and yaw of the watercraft and to elevate the vehicle payload by above a water surface when the watercraft is in the foiling mode.
In accordance with one or more further embodiments, a watercraft is disclosed that is selectively operable in one of a prone mode and a foiling mode. The watercraft comprises a vehicle payload bay; a sail connected to the payload bay for propelling the watercraft in the foiling mode; three or more hydrofoils connected to the vehicle payload bay configured to provide control of roll, pitch, yaw, and elevation of the watercraft during the transition from the prone mode to the foiling mode; and a mechanical propulsive system for propelling the watercraft at least during transition from the prone mode to the foiling mode. The watercraft does not include a hull such that during the transition from the prone mode to the foiling mode, pitch and roll control are not substantially provided through the actions of gravity and buoyancy.
Like or identical reference numbers are used to identify common or similar elements.
Various embodiments disclosed herein relate to a hybrid-sail/mechanical hydro-foil trans-surface vehicle.
The vehicle payload bay 12 contains vehicle control electronics, batteries, the payload, and other systems required for vehicle operation. In an exemplary embodiment, the payload bay 12 is sized to fit within a standard Mark 48 torpedo tube.
The sail and electronics platform 14 includes a rigid sail 24, which provides the vehicle primary propulsion, and also provides space aloft to house antennas and other sensors and EW packages. In this embodiment, the sail 24 is a rigid carbon-fiber composite airfoil comprised of four vertical sections that nest when stowed. Thus, by nesting the vertical sections and rotating the mast 16 forward the sail 14 can be stowed within the form-factor of a Mark 38 torpedo. In the exemplary embodiment depicted, the sail area is approximately 5 square meters, which is comparable to a sail for a windsurfer.
In one or more alternate embodiments, the sail 24 comprises a furling sail.
The mast 16 can be a carbon fiber composite tube. The mast 16 is stepped in the main payload bay 12. In this embodiment, the mast 16 is actuated at the vehicle payload bay 12 to adjust the angle of attack of the sail 24. Alternately, the sail 24 can rotate freely, and the angle of attack can be adjusted with control surfaces, using methods known to those skilled in the art. In this exemplary embodiment, the mast 16 is shown at mounted to the sail 24 at approximately the %-chord point to minimize rotational (yaw) moments.
The forward hydrofoils 18 are control surfaces comprising two largely vertical foils (‘pylons’ or centerboards) 26 and two horizontal foils (ailerons) 28. In this exemplary embodiment, when stowed the hydrofoil pylons 26 rotate forward and the foils 28 rotate parallel to the pylons 26, enabling the assembly to be contained within the form factor of a tube, e.g., a Mark 28 torpedo tube. This assembly provides services, including windward lift, vertical lift, and windward roll.
As shown in
When in wind-powered foiling mode, the ‘lift’ generated by the sail 24 acts substantially horizontally to leeward and either forward or aft depending on the relationship between the vehicle's motion and the surrounding airmass (the ‘point of sail’). This ‘lift’ pulls the vehicle to leeward. Further, because the sail 24 is above both the center of mass and the center of drag of the vehicle 10, this horizontal lift generates both a leeward roll moment, and either forward or aft pitching moment on the vehicle 10.
To enable the vehicle 10 to track in a substantially forward direction, the leeward horizontal force generated by the sail 24 is offset by a windward horizontal force generated by the vertical pylons 26 that are designed to operate like the centerboard or keel on a sailboat. Using the rudder 32, the angle of attack between the oncoming water and the vertical pylons 26 is adjusted, thereby controlling the windward lift.
With respect to vertical lift and the control of vehicle elevation, during foiling operation, the ailerons 28 work in concert with the elevators 34 to lift the vehicle payload bay 12 out of the water to a substantially constant elevation above the water surface. This is achieved by a combination of (1) adjusting the overall vehicle angle of attack using the elevators 34, or (2) operating left and right ailerons 28 and elevator 34 in tandem to adjust their individual angles of attack. Though the individual lift generated by each surface may be varied (or even be in opposition), the net lift must be sufficient to counteract vehicle weight (adjusted for any potential buoyancy) so as to hold the vehicle 10 at the desired elevation.
Roll control is provided using one or more of the ailerons 28. As noted, the ailerons 28 and elevator 34 must provide, in combination, sufficient net lift to counteract weight and hold the vehicle 10 at the desired elevation. As the ailerons 28 are offset from the vehicle center of mass, the ailerons 28 can be operated differentially to provide vehicle roll control. As discussed above, during wind-power foiling operation, the lift generated by the wing 24 pulls the wing to leeward, thereby inducing a leeward rolling moment. As the leeward aileron is leeward of the center of mass of the vehicle 10, the leeward aileron can induce a windward rolling moment counteracting the leeward moment of the wing 24. Similarly, the windward aileron can provide a windward rolling moment by generating a downward force. However, in this case, the net lift generated by the ailerons 28 and elevators 34 would still need to be sufficient to overcome the weight of the vehicle 10. One skilled in the art will appreciate that if one side of the vehicle 10 is always the leeward side then only one aileron 28 is technically required to provide both sufficient lift (along with the elevator 34) and to provide windward rolling moment. However, two ailerons 28 are generally required to enable operation on both starboard tack (wind to starboard) and port tack (wind to port).
Pitch control is provided using the combined action of the ailerons 28 and the elevator 34. As noted, the ailerons 28 and elevator 34 must provide, in combination, sufficient total lift to counteract weight and hold the vehicle 10 at the desired elevation. Through differential control of the ailerons 28 and elevator 34, the pitch of the vehicle 10 can be controlled. During wind-powered foiling operation, the lift generated by the wing 24 will pull the vehicle 10 either forward or aft depending upon the point of sail 24. As the wing 24 is above the center of mass and drag of the vehicle 10, this will induce a pitching moment in the vehicle 10. This pitching moment is offset as described using the ailerons 28 and elevators 34.
With respect to yaw control, the rudder 32 is positioned aft of the center of mass and drag of the vehicle 10. Action of the rudder 32 thereby generates a yawing motion on the vehicle 10.
Many embodiments will also include a propulsion system 22. This propulsion system 22 may optionally comprise an electromotive system, or a hybrid electric propulsion and generation system. Activation of the propulsion system 22 uses energy from the batteries to propel the vehicle 10. When in generation mode, motion of the vehicle 10 through the water (for example, from sail power) results in generation of electricity to charge batteries and provide payload power.
The design and operation of the sail and various hydrofoils will be understood by one skilled in the art.
UTVs 10 in accordance with various embodiments can operate in one of several modes, as depicted in
In the foiling mode shown in
The vehicle 10 is designed to have its first neutral buoyancy point with approximately one meter of sail protruding from the water. At this point, the weight of the vehicle 10 above the waterline is offset by the positive buoyancy of the portion of the vehicle 10 below the waterline. Stability in this configuration is achieved by loading buoyancy in the mast 16 and leaving the vehicle payload bay 12 negatively buoyant. This so-called ‘prone’ operating mode depicted in
The UTV 10 may also operate in a fully submerged mode as depicted in
In design of the vehicle 10, consideration must be given to the performance of the vehicle 10 as it transitions from one mode to another.
Submerged to Prone Transition. The vehicle 10 is designed to have positive buoyancy in the prone configuration, which is balanced by the weight of the portion of the mast 16 above the waterline. Further, the vehicle 10 is designed to have neutral (negatively stable) buoyancy a short distance below the water surface, and neutral (positively stable) buoyancy at its target submerged depth (e.g., 200′). This is accomplished through use of both collapsible and rigid buoyancy devices 36, which can be housed in the vehicle payload bay 12, in appropriate combination. Rigid devices exhibit positive stability, in that if they are put in water they will naturally ascend or descend until they achieve neutral buoyancy. On the other hand, collapsible devices exhibit a negative buoyancy stability characteristic. If above their neutrally buoyant point, collapsible devices become more buoyant as they ascend. Similarly, collapsible devices become less buoyant as they descend past their neutrally buoyant point. Thus, once they begin to move, collapsible devices will either rise or sink from their neutral buoyancy point until they either burst, become rigid, or are fully collapsed. In the prone configuration, the vehicle 10 is designed so that both rigid and collapsible devices are inflated, and the vehicle 10 exhibits positive buoyancy, thereby holding a portion of the sail 24 out of the water. Thus, while positively buoyant, the vehicle 10 is stable in this configuration. Next, the vehicle 10 is designed so that the neutral buoyancy point is a short distance below the surface, such that the vehicle 10 is able to propel itself down past the neutral buoyancy point. Once below the neutral buoyancy point, the vehicle 10 will descend without power until the collapsible devices are fully collapsed. At that point the vehicle 10 will find its second neutrally buoyant point. When ascending, the vehicle 10 propels itself electrically upwards until it reaches the neutral buoyancy point. At that point the vehicle 10 will rise on its own to the surface of the water.
Prone to Foiling Transition. Transition from prone (e.g., stationary) to foiling modes can be caused by action of the wind acting on the sail 24, or by the forward motion generated by the propulsion system 22. If the wind is used, then, as noted, the force generated by the wind on the sail 24 induce pitch and roll moments. A vessel with one or more hulls can use the buoyant force generated by the hull (offset from the center of mass) to offset these moments until such time as the vehicle has sufficient forward speed that the ailerons 28, elevators 34, and rudder 32 become effective. Once effective these control surfaces can provide pitch, roll and yaw control. In place of a hull, the vehicle 10 can include weights, floats, or other to provide roll and pitch control. In place of a hull, a vehicle can achieve the same effect through a combination of weights and floats, some of which are offset from the center of mass of the vehicle.
A vehicle without a hull or offset weights or floats cannot utilize buoyancy to maintain pitch and roll control during the prone to foiling transition. Such vehicles, such as the current embodiment, utilize a propulsion system generate the initial forward motion required to render the ailerons 28, elevators 34, and rudder 32 effective. Once these control surfaces become effective they can provide roll, pitch and yaw control, the vehicle 10 can be caused to rise out of the water, and the sail 24 can be brought online and used to drive further acceleration of the watercraft. Either before or during this transition, the rear elevator assembly 20 is rotated into the aft/down configuration.
The transition from foiling to prone is more straight forward. The vehicle 10 is brought down towards the water. Water drag over the vehicle payload bay 12 slows the vehicle 10 and it sinks into the prone configuration. The elevator assembly 20 is moved into the up configuration if desired to facilitate motion in the prone state.
The vehicle 10 can also be designed with a stowed configuration. A partially stowed vehicle 10 is shown in
As outlined above, the primary challenge in creating a useful, low-cost platform is achieving sufficient vehicle speed in a small platform. The commercial vehicles shown in
Further, the integration of a hybrid-electric system enables the vehicle 10 considerable residual mobility in no-wind conditions, and significant power availability, and endurance, when wind is present. Finally, the ability to submerge provides a critical ability to evade capture and ride out adverse weather conditions. A submerged depth of 100′ to 200′ is sufficient to evade capture and ride out storms, while also being consistent with depth conditions experienced by technical SCUBA divers, and thus accessible using equipment manufactured with commercial manufacturing practices.
Having thus described several illustrative embodiments, it is to be appreciated that various alterations, modifications, and improvements will readily occur to those skilled in the art. Such alterations, modifications, and improvements are intended to form a part of this disclosure, and are intended to be within the spirit and scope of this disclosure. While some examples presented herein involve specific combinations of functions or structural elements, it should be understood that those functions and elements may be combined in other ways according to the present disclosure to accomplish the same or different objectives. In particular, acts, elements, and features discussed in connection with one embodiment are not intended to be excluded from similar or other roles in other embodiments. Additionally, elements and components described herein may be further divided into additional components or joined together to form fewer components for performing the same functions. Accordingly, the foregoing description and attached drawings are by way of example only, and are not intended to be limiting.
This application claims priority from U.S. Provisional Patent Application No. 62/951335 filed on Dec. 20, 2019 entitled UNMANNED TRANS-SURFACE VEHICLE, which is hereby incorporated by reference.
This invention was made with Government support under Agreement No. N00014-19-9-0019 awarded by Office of Naval Research (ONR). The Government has certain rights in the invention.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/US20/66353 | 12/21/2020 | WO |
| Number | Date | Country | |
|---|---|---|---|
| 62951335 | Dec 2019 | US |
