Patent Application
20140103165
The present disclosure relates to a control system that provides improved maneuverability and stability of jet-packs that propel a passenger by means of a pressurized fluid expelled through one or more nozzles. In one embodiment, it is directed to such a jet-pack that is supplied with the pressurized fluid through a remote compressor station.
In general, a jet-pack is a device that is designed to be strapped to the torso of a passenger, and propels the passenger, e.g. through the air, by means of a thrust that is generated by expelling a pressurized fluid through one or more nozzles on the jet-pack. Typically, the jet-pack has two nozzles respectively located on its right and left sides. The source of the thrust can be mounted on the jet-pack, for example a tank of pressurized gas, or it can be provided at a remote station. For example, the remote station can be located on a floating body that supplies pressurized water to the jet-pack via a conduit, and travels with the passenger suspended over the water by the thrust of the jet-pack.
The maneuverability of the jet-pack is controlled by adjusting the orientation of the nozzles. For example, the nozzles might be normally oriented to provide a downwardly vertical thrust, and thereby obtain maximum lifting force. Once the passenger has been lifted to a desired height, he or she can move forward by adjusting the nozzles to an inclined position that induces a component of rearwardly facing thrust. To turn, the passenger might cause one of the nozzles to move to an inclined position, while keeping the other nozzle in the vertical position. For example, to turn to the left, the passenger might cause the nozzle on the right side of the jet-pack to move to an inclined position that provides rearward thrust on the right side, thus inducing rotation to the left. However, this action reduces some of the downward thrust on the right side. With the left side maintaining full downward thrust, the resulting forces cause the passenger to tilt to the right, which is counterintuitive when turning to the left, and may cause instability. Consequently, it may be difficult for the passenger to learn how to properly maneuver the jet-pack.
To improve the maneuverability and stability of a jet-pack, in one embodiment according to the invention, the thrust of the nozzles can be varied, relative to one another, through a suitable valve arrangement. In one example, the valves can be flap valves that open and close to increase or decrease the amount of pressurized fluid flowing through each nozzle. The ability to reduce the pressure on one side or the other side of the jet-pack enables much more flexible turns to be accomplished, and requires much less effort on the part of the passenger.
In another aspect, the invention employs actuators, such as piston-cylinder arrangements, to control the positioning of the nozzles and thereby assist the passenger in the piloting of the jet-pack.
To further increase maneuverability, additional nozzles can be incorporated into the jet-pack to control the forward and backward tilt of the device, to more easily accomplish hovering, forward movement and backward movement.
In accordance with another aspect of the invention, a control system for actuating the valves and pistons can utilize position and/or acceleration sensors to assist in the maneuvering of the jet-pack. For instance, in the absence of a positive indication from the passenger to move in a particular direction, the sensors can cause the jet-pack to assume a default position, e.g. stationary hovering. Such a feature is particularly helpful for a novice passenger.
The foregoing features and advantages of the invention are explained in detail hereinafter with reference to exemplary embodiments illustrated in the accompanying figures.
To facilitate an understanding of the principles that underlie the disclosed invention, various embodiments are described with reference to a jet-pack that is supplied with a pressurized liquid from a remote source. Examples of this type of jet-pack are described in U.S. Pat. Nos. 3,277,858 and 7,258,301. It will be appreciated, however, that the applications of the invention are not limited to this particular type of jet-pack. Rather, it can be implemented in jet-packs having on-board sources of pressurized fluid, as well as those which receive a pressurized fluid from a remote source.
A valve is located in the flow path of each nozzle 2, at the juncture of the nozzle with the manifold 3, to regulate the amount of pressurized fluid entering each nozzle. In one embodiment, the valve is implemented as a pivotable flap 5, similar in operation to the choke plate on a carburetor. In a normal position, the plane of the flap can be parallel to the direction of flow of the fluid from the manifold into the nozzle, to thereby obtain maximum thrust. An actuator 6 associated with each flap 5 causes the flap to pivot about an axis that is transverse to the direction of fluid flow, to partially close the valve and thereby reduce the amount of fluid flowing into the nozzle. In the illustrated embodiment, the flaps 5 pivot about a vertical axis, and the regulators 6 are positioned at the top of the juncture between the manifold and the nozzles. It will be appreciated that other arrangements, e.g. a horizontal pivot axis, are also feasible. By selectively activating one of the two actuators 6, the thrust on one side of the jet-pack can be reduced, relative to the thrust coming from the nozzle on the other side, to thereby cause the jet-pack to tilt to the right or left.
The nozzles 2 are connected to the manifold 3 by means of rotatable bearings 7, which enable the nozzles to independently pivot about a substantially horizontal axis 9, relative to the frame 1 and the manifold 3. The pivoting movement of the nozzles is effected by a pair of actuators 8 that are connected between the frame 1 and the nozzles. In the illustrated embodiment, the actuators comprise piston-cylinder mechanisms. When the pistons are contracted, the respective nozzles pivot in a counterclockwise direction, as viewed in
In one embodiment, the control of the actuators 6 for the valves 5 and the cylinders 8 can be manually performed by the passenger, for example by cables, pulleys and/or gears connected to a lifter. In an alternate embodiment, the actuation is implemented by means of a controller with associated sensors to receive input signals from the passenger, and generate control signals to activate the actuators 6 and cylinders 8. For example, the frame 1 can be provided with an arm rest 10 that houses a joystick 11 for input of maneuvering commands. The joystick has sensors to detect forward, back, left and right movement of the joystick. The sensed motions are input to the controller (not shown). In response, the controller sends signals to the actuator 6 and the cylinder 8 to perform associated movements. For example, if the passenger pushes the joystick forward, the two cylinders 8 can be actuated to extend the pistons and thereby rotate the nozzles in the clockwise direction, to produce rearward thrust. Pulling rearwardly on the joystick causes the opposite reaction.
In one implementation, a small portion of the pressurized fluid in the manifold 3 can be used to hydraulically or pneumatically actuate the cylinders 8. A small diversion valve can be employed to direct the pressurized fluid to one end or the other of the cylinder, to thereby cause the piston to contract or expand. This diversion valve can have a small electric motor that is controlled by a signal from the controller. Similarly, the actuators 6 for the flap valves 5 can be small electric motors.
Pulling the joystick to one side or the other induces a turning motion in that direction. For example, if the joystick is pulled to the left to initiate a turn in that direction, the actuator 6 for the valve 5 on the left nozzle causes that valve to close a certain amount, thereby reducing the pressure in the left nozzle and tilting the passenger to the left. At the same time, the cylinder 8 for the right nozzle is actuated to extend, and thereby rotate that nozzle to the rear, which induces the turning motion. By this coordinated action of the valve 5 on one side and the cylinder 8 on the other side, the passenger undergoes a more natural movement, in which he or she leans in the direction of the turn.
The controller can be a simple logic controller that receives the sensed positions of the joystick and outputs appropriate control signals to the right and left valve actuators 6 and the left and right cylinder actuators 8. One example of the logic implemented by the controller is provided in the following table, where 11 represents the position of the joystick, 6R and 6L represent the right and left valve actuators 6, and 8R and 8L represent the right and left cylinder actuators 8.
Thus, for instance, if the joystick is moved forward, the right and left cylinders 8 are actuated to extend the pistons, and thereby pivot the nozzles 2 rearwardly, to cause movement in a forward direction. If the joystick is pulled to the left, the left actuator 6 is activated to close the valve 5 and reduce the pressure in the left nozzle 2, while the right cylinder 8 is actuated to extend the piston and pivot the right nozzle 2 rearwardly, to effect a left turn. The symbol “C” indicating that a flap valve is to be closed does not necessarily mean that the valve is fully closed. In practice, the valve is only partially closed, to reduce the pressure in the associated nozzle to a desired level.
In an alternate embodiment, the jet-pack can be provided with left and right joysticks, one for each hand of the passenger. The two joysticks can independently control the pivoting of the respective nozzles 2. Pushing forward on one joystick while pulling backwards on the other causes the passenger to rotate in place.
The amount of thrust from the nozzles can be controlled by a throttle button or trigger (not shown) mounted on the joystick. Depression of the button or trigger sends a signal to the remote station, to increase the pressure of the fluid being supplied to the manifold 3, and thereby increase the thrust.
As a safety mechanism, the controller can be programmed with a default operation in the event that the passenger releases the joysticks. In such an event, each joystick returns to a center position, which causes the cylinders 8 to assume a neutral position in which the nozzles 2 are vertically oriented to provide a lifting thrust without forward or rearward movement. The controller can cause the actuators 6 to slowly close the valves 5, to thereby reduce the amount of thrust, and thereby provide a slow descent of the passenger to a safe landing. Alternatively, or in addition, the controller can send a signal to the remote station to gradually reduce the pressure of the fluid being supplied to the manifold 3.
As a further feature, the jet-pack can be equipped with one or more inflatable cushions to provide buoyancy in the case of a water landing. When the controller goes into the default operation, it can send a signal that causes the cushions to inflate, for example by opening compressed air cartridges.
The control of the actuators 15 for the valves 14 can be coordinated with the pivoting motion of the nozzles 2. For example, if the passenger pushes forward on the joystick 11 to induce forward movement, the main nozzles 2 are pivoted clockwise, to provide rearward thrust. At the same time, the flap valves 14 can be closed, to reduce the thrust provide by the nozzles 12, allowing the jet-pack frame and the passenger to tilt forward. Conversely, when the joystick is pulled backward, the flap valves 14 can be opened to provide greater thrust through the nozzles 12, thereby tilting the frame backwards in conjunction with the backward movement of the jet-pack.
In the foregoing embodiments, the controls for maneuvering the jet-pack are located on the jet-pack itself, for actuation by the passenger. Alternatively, the controls can be located on the remote compressor station, to enable a trained operator to control the movement of the jet-pack, for example in the case of a novice passenger or a young child. The commands from the remote control station can be relayed to the respective actuators by means of an electrical cable located within the conduit that supplies the pressurized fluid.
| Number | Date | Country | |
|---|---|---|---|
| 61711306 | Oct 2012 | US |
