# US 10,870,472 B2 · Deployable wingsail for container ships > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 10,870,472 B2 - Document ID: US10870472B2 - Status: Granted - Kind: B2 - Application number: 16/392,459 - Filed: 2019-04-23 - Published: 2019-08-15 - Granted: 2020-12-22 - Earliest claimed: 2016-05-13 - Assignees: Wind + Wing Technologies, Inc. - Applicants: Wind + Wing Technologies, Inc. - Inventors: Jay Michael Gardner; George Reginald Seyfang - Web page: https://patentgrep.com/patent/US10870472B2 ## CPC - B63H 9/061: Rigid sails; Aerofoil sails - B63H 9/071: for use in combination with other propulsion means, e.g. for improved fuel economy - Y02T 70/5236: Renewable or hybrid-electric solutions - B63H: MARINE PROPULSION OR STEERING (propulsion of air-cushion vehicles B60V1/14; specially adapted for submarines, other than nuclear propulsion, B63G; specially adapted for torpedoes F42B19/00) - Y02T: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION ## Abstract A wingsail includes a wing body, a wing axle having an axis, and at least one trim plate supported on a side surface of the wing body, the trim plate to control a rotational movement of the wing body about an axis of the wing axle. ## Claims ### Claim 1 A wingsail comprising: a wing body configured to be supported for rotation about a first axis; and at least one trim plate supported on at least one side of the wing body, the trim plate configured to control a rotational movement of the wing body about the first axis; wherein the at least one trim plate is configured to rotate or pivot about a second axis between at least a first position and a second position to adjust an amount of wind force applied to the trim plate, the second axis being transverse to the first axis. ### Claim 2 (depends on 1) The wingsail of claim 1, wherein the at least one trim plate is configured to rotate or pivot between at least a first position and a second position to adjust the amount of wind force applied to the trim plate. ### Claim 3 (depends on 2) The wingsail of claim 2, wherein the trim plate comprises: a hinge; and a wind opposing surface configured to pivot about the hinge to transition between the first position and the second position. ### Claim 4 (depends on 1) The wingsail of claim 1, wherein the wing body has two sides with one or more surfaces configured to provide a lift force in wind, the wingsail further comprising a support structure extending from at least one of the sides of the wing body to support the trim plate on the at least one side of the wing body. ### Claim 5 (depends on 4) The wingsail of claim 4, wherein the support structure extends from the at least one side surface of the wing body and positions each trim plate a distance away from the side surface of the wing body. ### Claim 6 A wingsail comprising: a wing body; a wing axle having an axis; at least one trim plate supported on a side surface of the wing body, the trim plate configured to control a rotational movement of the wing body about the axis of the wing axle; and a shaft to support the trim plat on the side surface of the wing body; wherein the shaft extends the trim plate away from the side surface of the wing body; and wherein the shaft extends perpendicularly from the side surface of the wing body. ### Claim 7 A wingsail comprising: a wing body; a wing axle having an axis; at least one trim plate supported on a side surface of the wing body, the trim plate configured to control a rotational movement of the wing body about the axis of the wing axle; and a shaft to support the trim plat on the side surface of the wing body; wherein the shaft is configured to telescopically extend to control a distance between the trim plate and the side surface of the wing body. ### Claim 8 A wingsail comprising: a wing body; a wing axle having an axis; at least one trim plate supported on a side surface of the wing body, the trim plate configured to control a rotational movement of the wing body about the axis of the wing axle; and a shaft to support the trim plat on the side surface of the wing body; wherein the shaft includes a length, and the trim plate is configured to slide along the length of the shaft to control a distance between the trim plate and the side surface of the wing body. ### Claim 9 (depends on 1) The wingsail of claim 1, wherein the at least one trim plate comprises a first trim plate supported by the support structure on one side of the wing body and a second trim plate supported on an opposite side of the wing body. ### Claim 10 (depends on 9) The wingsail of claim 9, wherein each of the first trim plate and the second trim plate is configured to rotate or pivot between at least a first position and a second position to control a steering force of the wing body about the first axis. ### Claim 11 (depends on 10) The wingsail of claim 10, wherein the steering force trims a lift force to provide thrust in the direction of the lift force. ### Claim 12 A method of steering a wingsail, the method comprising: installing a wingsail on a surface of a container or vessel, the wingsail comprising: a wing body; a wing axle having a first axis; and at least one trim plate supported on a side surface of the wing body; extending the at least one trim plate into relative wind forces; and adjusting a position of the at least one trim plate by rotating or pivoting the at least one trim plate about a second axis to control a rotational movement of the wing body about the first axis of the wing axle; wherein the at least one trim plate is configured to rotate or pivot about a second axis between at least a first position and a second position to adjust an amount of wind forces applied to the trim plate, the second axis being transverse to the first axis. ### Claim 13 (depends on 12) The method of claim 12, wherein the adjusting of the position of the at least one trim plate comprises rotating the at least one trim plate between at least a first position and a second position to control an amount of the wind forces applied to a wind opposing surface of the trim plate. ### Claim 14 (depends on 12) The method of claim 12, wherein the adjusting of the position of the trim plate comprises pivoting a wind opposing surface of the trim plate about a hinge to open or close the wind opposing surface to the relative wind forces. ### Claim 15 (depends on 12) The method of claim 12, further comprising: providing a shaft on the side surface of the wing body; and attaching the trim plate to the shaft. ### Claim 16 A method of steering a wingsail, the method comprising: installing a wingsail on a surface of a container or vessel, the wingsail comprising: a wing body; a wing axle having an axis; and at least one trim plate supported on a side surface of the wing body; extending the at least one trim plate into relative wind forces; adjusting a position of the at least one trim plate to control a rotational movement of the wing body about the axis of the wing axle; providing a shaft on the side surface of the wing body; and attaching the trim plate to the shaft; wherein the extending of the at least one trim plate into relative wind forces comprises: attaching the at least one trim plate to an end of the shaft; and telescopically extending the shaft from the side surface of the wing body. ### Claim 17 A method of steering a wingsail, the method comprising: installing a wingsail on a surface of a container or vessel, the wingsail comprising: a wing body; a wing axle having an axis; and at least one trim plate supported on a side surface of the wing body; extending the at least one trim plate into relative wind forces; adjusting a position of the at least one trim plate to control a rotational movement of the wing body about the axis of the wing axle; providing a shaft on the side surface of the wing body; and attaching the trim plate to the shaft; wherein the extending of the at least one trim plate into relative wind forces comprises: sliding the at least one trim plate along a length of the shaft. ### Claim 18 (depends on 12) The method of claim 12, wherein the trim plate includes a first trim plate supported on the side surface of the wing body, and a second trim plate supported on an opposite side surface of the wing body, and the method further includes: adjusting a position of each of the first and second trim plates such that the first trim plate generates drag relative to the relative wind forces and the second trim plate does not generate drag relative to the relative wind forces, wherein, in response, a steering force is generated to rotate the wingsail about the wing axle. ### Claim 19 (depends on 18) The method of claim 18, wherein the steering force trims a corresponding lift force to provide thrust in the direction of the lift force. ### Claim 20 A wingsail comprising: a wing body; a wing axle having an axis; and at least one trim plate supported on a side surface of the wing body, the trim plate configured to control a rotational movement of the wing body about the axis of the wing axle; wherein the at least one trim plate is secured to the support structure and movable to adjust its distance from the at least one side of the wing body. ### Claim 21 A wingsail comprising: a wing body; a wing axle having an axis; and at least one trim plate supported on a side surface of the wing body, the trim plate configured to control a rotational movement of the wing body about the axis of the wing axle; wherein the wing body has a front end and a tail end that generally align with a wind direction when the wing body provides the lift force, and wherein the trim plate is located between the front end and the tail end of the wing body and laterally spaced from a side surface of the wing body. ### Claim 22 (depends on 1) The wingsail of claim 1, wherein the wing body has two sides with one or more surfaces configured to provide a lift force in wind wherein the two sides of the wing body extend from a front end to a tail end of the wing body, and wherein each trim plate is located between the front end and the tail end of the wing body and laterally spaced from one of the side surfaces of the wing body. ### Claim 23 (depends on 1) The wingsail of claim 1, wherein the second axis is perpendicular to the first axis.