# US 7,607,615 B2 · Brake for a kite > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 7,607,615 B2 - Document ID: US7607615B2 - Status: Granted - Kind: B2 - Application number: 11/327,300 - Filed: 2006-01-06 - Published: 2007-07-26 - Granted: 2009-10-27 - Earliest claimed: 2006-01-06 - Assignees: Revolution Enterprises, Inc. - Inventors: Joseph Hadzicki - Web page: https://patentgrep.com/patent/US7607615B2 ## CPC - B64C 31/06: Kites (toy aspects A63H27/08; airborne towed targets, e.g. kites F41J9/10) - B64C: AEROPLANES; HELICOPTERS ## Abstract A kite brake and a kite that uses a brake are disclosed. The brake includes a spring-loaded standoff that is biased to push a top surface of a sail of the kite away from a strut of the kite when an air pressure on the bottom surface of the sail is less than a bias force of the spring. The brake can be deployed by operation of the kite, or simply based on a removal of the air pressure. ## Claims ### Claim 1 A kite brake for a kite, the kite brake comprising: a spring-loaded standoff connected to a strut of the kite between opposite ends of the strut, the spring-loaded standoff biased to push a top surface of a sail of the kite away from the strut of the kite when an air pressure on the bottom surface of the sail is less than a bias force of the spring, to form the sail into a concave-up shape that removes lift from the kite. ### Claim 2 (depends on 1) The kite brake in accordance with claim 1, wherein the spring includes a coil configured for being wound around the strut. ### Claim 3 (depends on 2) The kite brake in accordance with claim 2, wherein the standoff further includes a rod having a first end configured to be coupled to the coil and a second end configured to abut the top surface of the sail. ### Claim 4 (depends on 1) The kite brake in accordance with claim 1, wherein when the standoff pushes the top surface of the sail away from the strut, the sail is formed into a concave airfoil relative to the top surface of the sail. ### Claim 5 (depends on 4) The kite brake in accordance with claim 4, wherein when the air pressure is greater than the bias force of the spring, the sail is formed into a concave airfoil relative to the bottom surface of the sail. ### Claim 6 A kite comprising: a sail having a top surface and a bottom surface; at least one strut supporting the sail along the top surface of the sail; a spring-loaded standoff connected to the at least one strut between opposite ends of the strut, the spring-loaded standoff biased to push a top surface of the sail away from the at least one strut when an air pressure on the bottom surface of the sail is less than a bias force of the spring, to form the sail into a concave-up shape that removes lift from the kite. ### Claim 7 (depends on 6) The kite in accordance with claim 6, wherein the spring includes a coil that is wound around the strut. ### Claim 8 (depends on 7) The kite in accordance with claim 7, wherein the standoff further includes a rod having a first end coupled to the coil and a second end to abut the top surface of the sail. ### Claim 9 (depends on 6) The kite in accordance with claim 6, wherein when the standoff pushes the top surface of the sail away from the strut, the sail is formed into a concave airfoil relative to the top surface of the sail. ### Claim 10 (depends on 9) The kite in accordance with claim 9, wherein when the air pressure is greater than the bias force of the spring, the sail is formed into a concave airfoil relative to the bottom surface of the sail. ### Claim 11 A kite comprising: a sail having a top surface and a bottom surface, the sail being responsive to an air pressure on the bottom surface to form a concave airfoil relative to the bottom surface of the sail; a strut traversing the top surface of the sail; a spring-loaded standoff connected to the strut between opposite ends of the strut, the spring-loaded standoff biased to push the top surface of the sail away from the strut when the air pressure on the bottom surface of the sail is less than a bias force of the spring to form a convex airfoil for the whole sail relative to the bottom surface of the sail, to remove lift from the kite. ### Claim 12 (depends on 11) The kite in accordance with claim 11, further comprising at least two struts, each strut including a spring-loaded standoff. ### Claim 13 (depends on 11) The kite in accordance with claim 11, wherein the spring includes a coil that is wound around the strut. ### Claim 14 (depends on 11) The kite in accordance with claim 11, wherein the standoff further includes a rod having a first end coupled to the coil and a second end to abut the top surface of the sail. ### Claim 15 (depends on 11) The kite in accordance with claim 11, further comprising a leading edge pole coupled with the at least one strut at a leading edge of the sail. ### Claim 16 (depends on 15) The kite in accordance with claim 15, wherein the standoff is configured to rotate the leading edge pole in orientation with the convex airfoil relative to the bottom surface of the sail. ### Claim 17 A kite comprising: a leading edge pole defining a nose of the kite; a sail having a top surface and a bottom surface; at least one strut traversing the top surface of the sail; one or more control lines connected with the kite, and configured to be maintained under tension when an air pressure is applied to the bottom surface of the sail; a spring-loaded standoff connected to the at least one strut between opposite ends of the strut, the spring-loaded standoff biased to push against the top surface of the sail from the at least one strut when the air pressure on the bottom surface of the sail is less than a bias force of the spring, the at least one strut configured to rotate the leading edge pole to turn up the nose of the kite when the standoff is pushed against the top surface of the sail, to form the sail into a concave-up shape that removes lift from the kite. ### Claim 18 (depends on 17) The kite in accordance with claim 17, wherein rotation of the leading edge pole to turn up the nose of the kite causes at least one of the one or more control lines to be momentarily loose before being re-maintained under tension. ### Claim 19 A kite, comprising: a spring-loaded sail biased to a concave-up shape, the spring-loaded sail configured to switch entirely to a concave-down shape when an air pressure on a bottom surface of the spring-loaded sail exceeds a bias force of the spring-loaded sail, to form the sail into a concave-up shape that removes lift from the kite, and further configured to return to the concave-up shape when the air pressure drops below the bias force of the spring-loaded sail. ### Claim 20 (depends on 19) The kite in accordance with claim 19, further comprising one or more control lines coupled with the kite, the control lines being controllable to adjust the air pressure on the bottom surface of the spring-loaded sail.