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A high speed ship configuration for achieving a plane state efficiently, with threshold power available in fully loaded cargo ship. The system may include a boost phase assist structure to assist in the achievement of a plane state. The boost assist may be external or internal to the ship. The boost

A high speed ship configuration for achieving a plane state efficiently, with threshold power available in fully loaded cargo ship. The system may include a boost phase assist structure to assist in the achievement of a plane state. The boost assist may be external or internal to the ship. The boost assist may provide power and/or lift assist. In one embodiment, the configuration includes a retractable lateral wing structure disposed toward the stern of the vessel and containing auxiliary power providing thrust for the vessel. The wing structure is deployed during an initial boost phase acceleration and may be stowed in the vessel once the vessel achieves full plane operation. In one embodiment, the boost power structure may include propeller drive, paddle drive, or waterjet drive. The boost power structure may provide buoyancy and/or hydrodynamic trim to assist in achieving plane state operation.

대표청구항 ▼

1. A method for assisting a vessel to achieve a plane operation state, the method comprising: providing a cruise power source insufficient to achieve said plane operation state from a stationary state using a fixed configuration of weight and trim;providing a boost power source separate from said cr

1. A method for assisting a vessel to achieve a plane operation state, the method comprising: providing a cruise power source insufficient to achieve said plane operation state from a stationary state using a fixed configuration of weight and trim;providing a boost power source separate from said cruise power source;deploying a boost thrust mechanism coupled to said boost power source for a speed less than a minimum planing speed; andretracting said boost thrust mechanism for a speed greater than said minimum planing speed;wherein said boost power source and said boost thrust mechanism are deployed extending from a side of the vessel, longitudinally between amidships and the stern of the vessel. 2. The method in accordance with claim 1, wherein said boost power source has a separate thrust mechanism from the cruise power source. 3. The method in accordance with claim 1, further including the step: adjusting a variable trim in conjunction with deploying said boost thrust mechanism to lower a pitch angle of said vessel to achieve said plane operation state. 4. A method for achieving a plane state in a vessel having insufficient cruise power to achieve the plane state from a fixed configuration, the method comprising the steps: establishing the vessel initially at rest;deploying a retractable power boost system; applying cruise power to establish the vessel underway; setting a variable trim to achieve a relatively higher pitch angle when underway;shifting a load aft to further increase the pitch angle;applying said boost power to accelerate the vessel; said boost power separate from said cruise power;upon achieving a first speed at the increased pitch angle, shifting the load to a forward position, and adjusting the variable trim to achieve a lower pitch angle than said increased pitch angle and to bring the vessel into a plane operational state;disengaging the power boost system and configuring the power boost system for minimum drag when the vessel attains said plane state; andthe vessel maintains a cruise speed in said plane operational state. 5. The method according to claim 4, further including step: upon achieving said full plane state, reducing power, shifting the load to a neutral position, and setting the trim for plane operation. 6. The method according to claim 4, further including steps: upon achieving the first speed, the load is shifted further forward and the trim is adjusted to achieve a further lower pitch angle; andadditional load and trim adjustments are applied to incrementally transition from a pitch up configuration to the plane configuration. 7. The method according to claim 4, wherein the vessel is equal or greater than 10,000 tons maximum gross weight. 8. The method according to claim 4, wherein the vessel is equal or greater than 100,000 tons maximum gross weight.