[특허]Rotocraft

Marcus, Robert

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특허 상세정보

MyON담기

내보내기 페이스북 공유 트위터 공유 카카오톡 공유

Rotocraft

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64C-027/08
미국특허분류(USC)	244/017.23; 244/023B; 244/001R
출원번호	US-0712094 (2010-02-24)
등록번호	US-8590828 (2013-11-26)
발명자 / 주소	Marcus, Robert
출원인 / 주소	Marcus, Robert
대리인 / 주소	Weaver Austin Villeneuve & Sampson, LLP
인용정보	피인용 횟수 : 16 인용 특허 : 21

초록
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An aerial vehicle includes independently controlled horizontal thrusters and vertical lifters to provide design and operational simplicity while allowing precision flying with six degrees of freedom and use of mounted devices such as tools, sensors, and instruments. Each horizontal thruster and vertical lifter can be mounted as constant-pitch, fixed-axis rotors while still allowing for precise control of yaw, pitch, roll, horizontal movement, and vertical elevation. Gyroscopes and inclinometers can be used to further enhance flying precision. A controlle...

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1. An aerial vehicle comprising: a frame;a plurality of horizontal thrusters attached to the frame, the plurality of horizontal thrusters configured to provide yaw rotation and horizontal translation of the aerial vehicle;a plurality of vertical lifters attached to the frame;a device attached to the frame, wherein the device comprises one or more items selected from the group consisting of a mechanical tool, a sensor, and a weapon; anda controller attached to the frame and configured to control the plurality of horizontal thrusters and/or the plurality of vertical lifters, wherein the aerial vehicle is: capable of maneuvering in all directions and axes by independently controlling the thrust applied by the plurality of horizontal thrusters and the plurality of vertical lifters, andconfigured to open, using a mechanical claw, one or more items from the group consisting of an internal door, an external door, and a window. 2. The aerial vehicle of claim 1, wherein the aerial vehicle is capable of changing yaw, pitch, and roll independently from each other while maintaining the device on a target. 3. The aerial vehicle of claim 1, wherein a portion of the device is configured to move relative to the frame. 4. The aerial vehicle of claim 1, wherein the aerial vehicle is an unmanned aerial vehicle (UAV). 5. The aerial vehicle of claim 1, wherein an external force is exerted by moving the device relative to the frame. 6. The aerial vehicle of claim 1, wherein an external torque is exerted by moving the device relative to the frame. 7. The aerial vehicle of claim 1, wherein the plurality of horizontal thrusters comprises two independently controlled horizontal thrusters, wherein the thrust applied by each of the independently controlled horizontal thrusters is varied by changing rotational speeds associated with each of the independently controlled horizontal thrusters. 8. The aerial vehicle of claim 7, further comprising a battery, wherein the aerial vehicle is configured to establish an electrical connection with a stationary external power source to recharge the battery while the aerial vehicle is under remote operation. 9. The aerial vehicle of claim 8, wherein the stationary external power source is a wall-mounted electrical outlet. 10. The aerial vehicle of claim 1 further comprising a gyroscope for controlling the plurality of vertical lifters. 11. The aerial vehicle of claim 1, further comprising a proximity sensor, wherein the controller is communicatively connected with the proximity sensor and the controller controls one or more of the vertical lifters from the plurality of vertical lifters and/or one or more of the horizontal thrusters from the plurality of horizontal thrusters to maintain substantially constant distance from an external object detected by the proximity sensor based on data received by the controller from the proximity sensor. 12. The aerial vehicle of claim 1, wherein the device comprises a mechanical claw that is substantially fixed in space with respect to the frame. 13. The aerial vehicle of claim 12, wherein the mechanical claw is configured to turn a door knob. 14. The aerial vehicle of claim 13, wherein the mechanical claw comprises a plurality of mechanical fingers and at least one mechanical finger is movable. 15. The aerial vehicle of claim 14, wherein at least one mechanical finger in the plurality comprises a roller. 16. The aerial vehicle of claim 14, wherein the only movement that the mechanical claw is configured to make relative to the frame is to move the at least one movable mechanical finger to open and close the mechanical claw. 17. The aerial vehicle of claim 16, wherein the controller is configured to: control the vertical lifters to cause the aerial vehicle to rotate about a wrist axis substantially centered between the mechanical fingers when the mechanical claw is used to grasp a doorknob of a door, thereby rotating the doorknob and unlatching the door; andcontrol the horizontal thrusters to cause the aerial vehicle to move in a direction substantially parallel to the wrist axis while the aerial vehicle is rotated about the wrist axis and while the door is unlatched. 18. The aerial vehicle of claim 12, wherein the only movements that the mechanical claw is configured to make relative to the frame is to move the at least one movable mechanical finger to open and close the mechanical claw and to rotate the mechanical fingers of the mechanical claw about a wrist axis substantially centered between the mechanical fingers. 19. The aerial vehicle of claim 1, wherein the device comprises a mechanical claw and wherein the mechanical claw is configured to move in and out relative to the frame and to turn relative to the frame. 20. The aerial vehicle of claim 1, wherein the controller is configured to control one or more vertical lifters of the plurality of vertical lifters and one or more horizontal thrusters of the plurality of horizontal thrusters to counterbalance forces and torques exerted in the aerial vehicle during operation of the mechanical tool, sensor, or weapon. 21. The aerial vehicle of claim 1, wherein the controller is configured to: receive data collected from sensors mounted to the frame of the aerial vehicle,receive instructions over a wireless interface to operate the device attached to the frame; andindependently control power levels applied to each of the plurality of vertical lifters and each of the plurality of horizontal thrusters to compensate for feedback resulting from operating the device. 22. The aerial vehicle of claim 1, wherein the controller is configured to: receive data collected from sensors mounted to the frame;receive instructions over a wireless interface to guide the aerial vehicle; andcombine the data collected from the sensors and the instructions received over the wireless interface to independently control power levels applied to each of the plurality of vertical lifters and each of the plurality of horizontal thrusters to control a flying path of the aerial vehicle. 23. The aerial vehicle of claim 1, wherein the plurality of horizontal thrusters includes at least two horizontal thrusters that are offset from one another in a horizontal direction and that generate force in substantially parallel directions. 24. An aerial vehicle comprising: a frame;a plurality of horizontal thrusters attached to the frame, the plurality of horizontal thrusters configured to induce yaw rotation and horizontal translation of the aerial vehicle;a plurality of vertical lifters attached to the frame;a device attached to the frame, wherein the device comprises one or more items selected from the group consisting of a mechanical tool, a sensor, and a weapon; anda controller attached to the frame and configured to control the plurality of horizontal thrusters and the plurality of vertical lifters, wherein the aerial vehicle is configured to: maneuver in all directions and axes by independently controlling the thrust applied by the plurality of horizontal thrusters and the plurality of vertical lifters,ram through one or more of the items in the group consisting of an external door of a building, an internal door of the building, and a window of the building using a spring-loaded punch tool or a pneumatic punch tool,remain operational after ramming through the one or more items in the group consisting of the external door of the building, the internal door of the building, and the window of the building, andenter the building through a doorframe or a window frame, and wherein the aerial vehicle is sized to permit the aerial vehicle to navigate within the building. 25. An aerial vehicle comprising: a frame;a plurality of horizontal thrusters attached to the frame, the plurality of horizontal thrusters configured to provide yaw rotation and horizontal translation of the aerial vehicle;a plurality of vertical lifters attached to the frame;a device attached to the frame, wherein the device comprises one or more items selected from the group consisting of a mechanical tool, a sensor, and a weapon; anda controller attached to the frame and configured to control the plurality of horizontal thrusters and/or the plurality of vertical lifters, wherein the aerial vehicle is: capable of maneuvering in all directions and axes by independently controlling the thrust applied by the plurality of horizontal thrusters and the plurality of vertical lifters, andcapable of: opening one or more items from the group consisting of an internal door, an external door, and a window using a mechanical claw attachable to the aerial vehicle, andramming through one or more items from the group consisting of an internal door, an external door, and a window using a punch tool also attachable to the aerial vehicle.

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이 특허를 인용한 특허 피인용횟수: 16

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구성항목	관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표IPC 관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 공고번호, 공고일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표출원인, 출원인국적, 출원인주소, 발명자, 발명자E, 발명자코드, 발명자주소, 발명자 우편번호, 발명자국적, 대표IPC, IPC코드, 요약, 미국특허분류, 대리인주소, 대리인코드, 대리인(한글), 대리인(영문), 국제공개일자, 국제공개번호, 국제출원일자, 국제출원번호, 우선권, 우선권주장일, 우선권국가, 우선권출원번호, 원출원일자, 원출원번호, 지정국, Citing Patents, Cited Patents
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Rotocraft

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이 특허에 인용된 특허 (21)

이 특허를 인용한 특허 피인용횟수: 16

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