This application is based on and claims priority to Japanese Patent Application No. 2004-081930, filed Mar. 22, 2004, the entire content of which is hereby expressly incorporated by reference.
1. Field of the Invention
The present invention generally relates to a control system for controlling a marine engine, and more particularly relates to an improved control system that controls a marine engine using a security system that has various modes of operation and that includes a transmitter and a receiver.
2. Description of the Related Art
Watercraft have been provided with an automatic control system using a transmitter that can remotely communicate with a receiver on the watercraft to allow an engine of the watercraft to start. Typically, an ID code is applied to identify whether a transmitter is the true key that is accessible to an associated receiver. Unless the system determines that the ID code is true, the person who has tried to use the key is not allowed to start the engine. Japanese Patent Publication No. 2001-254549 discloses examples of such watercraft systems.
Small watercraft employ an engine to power the vehicle. For example, in a personal watercraft (PWC), a hull of the watercraft typically defines a rider's area above an engine compartment. An internal combustion engine powers a jet propulsion unit that propels the watercraft by discharging water rearward. The engine lies within the engine compartment in front of a tunnel, which is formed on an underside of the hull. At least part of the jet propulsion unit is placed within the tunnel and includes an impeller that is driven by the engine.
One aspect of embodiments described herein is a watercraft that includes a hull, a seat, a control mast, and an engine disposed within the hull. The watercraft includes a controller that communicates with at least one engine parameter and that is configured to control engine operation. A security system in the watercraft is configured to communicate with the engine controller. A receiver communicates with the security system. A portable transmitter transmits at least one signal to the receiver. The portable transmitter comprises at least one sealed airtight cavity that maintains a density of the portable transmitter below the density of water. The security system determines how the engine controller controls the engine in response to a signal received from the receiver. The receiver is located in a remote location above the water level of the watercraft and adjacent to an access opening.
In certain embodiments, the signal sent by the transmitter is a signal that prohibits engine operation. In other embodiments, the signal sent by the transmitter is a signal that permits engine operation. In other embodiments, the signal sent by the transmitter is a signal that limits engine operation.
Preferably, the transmitter is removably mounted to the watercraft and the transmitter communicates by radio waves with the receiver. In particular embodiments, the transmitter is rectangular. The transmitter preferable includes a transmitter housing that is at least partially transparent.
Preferably, the receiver has an antenna that extends from the receiver. In certain embodiments, the antenna is formed in a substantially closed loop configuration. Also preferably, the antenna includes a connector to extend the antenna.
Another aspect in accordance with embodiments disclosed herein is a watercraft that includes a hull, a seat, a control mast, and an engine disposed within the hull. The watercraft includes a controller that communicates with at least one engine parameter and that is configured to control engine operation. A security system in the watercraft is configured to communicate with the engine controller. A receiver in the watercraft communicates with the security system. A portable transmitter transmits at least one signal to the receiver. The portable transmitter comprises a housing that it is at least partially transparent. The security system determines how the engine controller controls the engine in response to a signal received from the receiver. The receiver is located in a remote location above the water level of the watercraft and adjacent to an access opening.
In one preferred embodiment, the signal sent by the transmitter is a signal that prohibits engine operation. In another preferred embodiment, the signal sent by the transmitter is a signal that permits engine operation. In another preferred embodiment, the signal sent by the transmitter is a signal that limits engine operation.
Preferably, the transmitter is rectangular. Also preferably, the transmitter is buoyant. In certain preferred embodiments, the transmitter is removably mounted to the watercraft, and the transmitter communicates by radio waves with the receiver.
Further aspects, features and advantages of this invention will become apparent from the detailed description of the preferred embodiments which follow.
The foregoing features, aspects, and advantages of the present invention are described below with reference to the drawings of several preferred embodiments that are intended to illustrate and not to limit the invention, in which:
An overall configuration of an embodiment of a personal watercraft 10 is described below in connection with
As shown in
The illustrated upper hull section 18 preferably comprises a hatch cover 24, a control mast 26, a smaller hatch cover 27, and a seat 28, which are arranged generally in series from fore to aft. In the illustrated arrangement, a forward portion of the upper hull section 18 defines a bow portion 30 that slopes upwardly.
A forward bulkhead 33 is formed within the hull. Preferably, a storage compartment 31 is positioned proximate the forward bulkhead 33. In the illustrated arrangement, a lower surface 35 of the storage compartment 31 rests on a generally horizontal surface 37 of the forward bulkhead 33. A downwardly sloping surface preferably is located rearward of the surface 37. A lower hull cavity 39 is positioned generally beneath the forward bulkhead 33 and, more particularly, generally beneath the generally horizontal surface 37.
A maintenance opening 40 is advantageously defined through a wall of the storage compartment 31. In one arrangement, the maintenance opening 40 is defined through a rear wall of the storage compartment. The opening 40 preferably is sufficiently large to allow maintenance of portions of the security system 11, which is described in greater detail below. More preferably, the opening 40 is sufficiently large to allow the serviced components to be removed from the watercraft through the opening 40.
An opening is advantageously provided through the bow portion 30 so the rider can access the internal storage compartment 31. An access lid 41 is securely attached through fasteners 43 to an upper support 45 of the storage compartment 31. The lid 41 is designed to close the opening 40. Preferably, the lid 41 seals or substantially seals the opening 40. More preferably, when the lid 41 is closed, a substantially watertight seal is formed over the opening 40. As discussed above, removal of the lid 41 allows access to a front portion of the internal cavity 20.
The hatch cover 24 is detachably affixed or hinged to the bow portion 30 to cover the opening in the hull that provides access to the storage compartment 31 or the corresponding region of the watercraft. The smaller hatch cover 27 allows access to a second, smaller storage compartment 29 that lies generally between the control mast 26 and the seat 28.
The control mast 26 extends upwardly and supports a handle bar 32 through a steering bracket 34. The handle bar 32 is provided primarily for controlling the direction of the watercraft 10. The handle bar 32 preferably carries other mechanisms, such as, for example, a throttle lever (not shown) that is used to control the engine output (i.e., to vary the engine speed) and a starter switch 47 that is used to initiate a starter motor 49 (
The seat 28 extends rearwardly from a portion just rearward of the bow portion 30. In the illustrated arrangement, the seat 28 has a saddle shape. Hence, a rider can sit on the seat 28 in a straddle fashion.
Foot areas 36 are defined on both sides of the seat 28 along a portion of the top surface of the upper hull section 18. The foot areas 36 are formed generally flat but may be inclined toward a suitable drain configuration.
A fuel tank 42 is positioned in the cavity 20 under the bow portion 30 of the upper hull section 18 in the illustrated arrangement. A duct 43 preferably couples the fuel tank 42 with a fuel inlet port positioned at a top surface of the bow 30 of the upper hull section 18. A closure cap 44 (
An engine 12 is disposed in an engine compartment that is defined, for example, within the cavity 20. The engine compartment preferably is located under the seat 28, but other locations are also possible (e.g., beneath the control mast or in the bow). In the illustrated configuration, the engine compartment is defined within the cavity 20 by the forward bulkhead 33 and a rearward bulkhead 46.
A jet pump unit 48 propels the illustrated watercraft 10. Other types of marine drives can be used depending upon the application. The jet pump unit 48 preferably is disposed within a tunnel 50 formed on the underside of the lower hull section 16. The tunnel 50 has a downward facing inlet port 52 opening toward the body of water. A jet pump housing 54 is disposed within a portion of the tunnel 50. Preferably, an impeller 55 is supported within the jet pump housing 54.
An impeller shaft 56 extends forwardly from the impeller and is coupled with a crankshaft 58 of the engine 12 by a suitable coupling device 60. The crankshaft 58 of the engine 12 thus drives the impeller shaft 56. The rear end of the housing 54 defines a discharge nozzle 61. A steering nozzle 62 is affixed proximate the discharge nozzle 61. The steering nozzle 62 is pivotally movable about a generally vertical steering axis. The steering nozzle 62 is connected to the handle bar 32 by a cable or other suitable arrangement so that the rider can pivot the nozzle 62 for steering the watercraft.
The engine 12 in the illustrated arrangement operates on a four-stroke cycle combustion principal. The engine 12 is an inclined L4 (in-line four cylinder) type. The illustrated engine, however, merely exemplifies one type of engine on which various aspects and features of the present invention can be used. Engines having a different number of cylinders, other cylinder arrangements, other cylinder orientations (e.g., upright cylinder banks, V-type, W-type, and opposing), and operating on other combustion principles (e.g., crankcase compression two-stroke, diesel, and rotary) are all practicable. Many orientations of the engine are also possible (e.g., with a transversely or vertically oriented crankshaft).
The engine 12 preferably includes an air induction system 78 to guide air to the engine 12. The illustrated air induction system includes an air intake box 84 for smoothing intake airflow and acting as an intake silencer. The intake box 84 in the illustrated embodiment is generally rectangular. Other shapes of the intake box of course are possible.
One advantageous arrangement includes an electronic control unit 98 (ECU), such as, for example, a microcomputer. The ECU 98 preferably comprises a microcontroller having a central processing unit (CPU), a timer, and memory storage. The memory storage comprises at least an electrically erasable programmable read only
Number | Date | Country | Kind |
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2004-081930 | Mar 2004 | JP | national |