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公开(公告)号：US20170259914A1
公开(公告)日：2017-09-14
申请号：US15386344
申请日：2016-12-21
Applicant: JoeBen Bevirt , Andy Clark
Inventor： JoeBen Bevirt , Andy Clark
CPC classification number: B64C27/52 , B64C1/30 , B64C27/08 , B64C27/20 , B64C27/50 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/141 , B64C2201/162 , B64C2201/165 , B64D27/24 , B64D47/08 , Y02T50/62
Abstract: A system for video imaging and photographing using an autonomous aerial platform. The system may be a quad rotor system using electrically powered propellers. The aerial platform may be commanded by the user to follow an object of interest. The aerial platform may have multiple configurations for its thrust units such that they are clear of the field of view of the imaging device in a first configuration, such that they protect the imaging device during landing in a second configuration, and that allows for efficient storage in a stowed configuration.
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公开(公告)号：US09751619B1
公开(公告)日：2017-09-05
申请号：US15377300
申请日：2016-12-13
Applicant: John V. Howard
Inventor： John V. Howard
CPC classification number: B64C27/12 , B64C1/0009 , B64C25/02 , B64C25/04 , B64C27/04 , B64C27/10 , B64C39/024 , B64C2025/325 , B64C2201/024 , B64C2201/108 , B64C2201/12 , B64C2201/128 , B64C2211/00 , B64D1/22 , Y02T50/12
Abstract: An unmanned rotorcraft has a lift module having a propulsion system and coaxial rotors driven in rotation by the propulsion system. The rotorcraft includes a payload support system adapted to couple an external payload directly to the lift module. The rotorcraft is devoid of provisions for human passengers.
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公开(公告)号：US09745050B2
公开(公告)日：2017-08-29
申请号：US14975563
申请日：2015-12-18
Applicant: Amazon Technologies, Inc.
Inventor： Brian C. Beckman , Allan Ko
IPC: G05D1/00 , G05D1/06 , G05D3/00 , G06F7/00 , G06F17/00 , B64C11/00 , B64C39/02 , G01C21/00 , G05D13/00 , B64C27/32 , B64C27/08 , G05D1/10
CPC classification number: B64C11/00 , B64C11/20 , B64C27/08 , B64C27/32 , B64C27/473 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/108 , B64C2201/128 , B64C2201/141 , B64C2230/14 , G01C21/00 , G05D1/101 , G05D13/00 , Y02T50/166
Abstract: Aerial vehicles may be operated with discrete sets of propellers, which may be selected for a specific purpose or on a specific basis. The discrete sets of propellers may be operated separately or in tandem with one another, and at varying power levels. For example, a set of propellers may be selected to optimize the thrust, lift, maneuverability or efficiency of an aerial vehicle based on a position or other operational characteristic of the aerial vehicle, or an environmental condition encountered by the aerial vehicle. At least one of the propellers may be statically or dynamically imbalanced, such that the propeller emits a predetermined sound during operation. A balanced propeller may be specifically modified to cause the aerial vehicle to emit the predetermined sound by changing one or more parameters of the balanced propeller and causing the balanced propeller to be statically or dynamically imbalanced.
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公开(公告)号：US20170244270A1
公开(公告)日：2017-08-24
申请号：US15438718
申请日：2017-02-21
Applicant: WiBotic Inc.
Inventor： Benjamin Waters
CPC classification number: B64C39/024 , B60L53/12 , B60L53/36 , B60L53/38 , B64C2201/024 , B64C2201/027 , B64C2201/042 , H02J7/0047 , H02J7/025 , H02J50/10 , H02J50/80 , H02J50/90 , H02J2007/0001 , H02J2007/005
Abstract: A smart battery includes a battery and a measurement module coupled to measure electrical characteristics of the battery. The smart battery also includes processing logic and a communication interface configured to receive the electrical characteristics and transmit the electrical characteristics to a receiver.
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公开(公告)号：US20170227963A1
公开(公告)日：2017-08-10
申请号：US15206222
申请日：2016-07-09
Applicant: Proxy Technologies, Inc.
Inventor： John KLINGER , Bruce ANDREWS , Patrick C. CESARANO
CPC classification number: G05D1/0214 , B64C39/024 , B64C2201/021 , B64C2201/024 , B64C2201/141 , B64C2201/143 , B64C2201/146 , G01B9/021 , G01B11/00 , G01C21/165 , G01N21/8851 , G01N27/20 , G01N2201/12 , G01S7/006 , G01S13/02 , G01S13/06 , G01S13/42 , G01S15/02 , G01S19/13 , G01S2013/0254 , G05B11/42 , G05B13/024 , G05B13/042 , G05D1/0022 , G05D1/0027 , G05D1/0088 , G05D1/0094 , G05D1/02 , G05D1/0202 , G05D1/0204 , G05D1/0206 , G05D1/021 , G05D1/0246 , G05D1/0278 , G05D1/104 , G05D2201/0207 , G06K9/00637 , G06K9/00677 , G08G5/0039 , G08G5/045 , G08G9/02 , H01Q3/26 , H01Q3/2617 , H01Q3/28 , H01Q3/36 , H04B7/0617 , H04B7/18506 , H04N5/225 , H04N7/183 , H04N2005/2255
Abstract: Some embodiments are directed to a system for use with a vehicle, the system including control circuits for controlling an operation of the vehicle, each of the control circuits implementing autopilot coefficients. The system further includes a sensor that is configured to detect control circuits operating in an untuned or incorrectly tuned state from the control circuits; an electronic switch that is configured to isolate the control circuits in the untuned or incorrectly tuned state from other control circuits; a tuning circuit that is configured to determine tuned values of the autopilot coefficients corresponding to the control circuits in the untuned or incorrectly tuned state; the tuned values of the autopilot coefficients enabling the control circuits to operate in a tuned state; and a memory to store the tuned values of the autopilot coefficients, wherein the electronic switch is further configured to connect the control circuits in the tuned state to the other control circuits.
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Patent Agency Ranking
公开(公告)号：US20170227956A1
公开(公告)日：2017-08-10
申请号：US15092576
申请日：2016-04-06
Applicant: PROXY TECHNOLOGIES, INC.
Inventor： Patrick C. CESARANO
CPC classification number: G05D1/0214 , B64C39/024 , B64C2201/021 , B64C2201/024 , B64C2201/141 , B64C2201/143 , B64C2201/146 , G01B9/021 , G01B11/00 , G01C21/165 , G01N21/8851 , G01N27/20 , G01N2201/12 , G01S7/006 , G01S13/02 , G01S13/06 , G01S13/42 , G01S15/02 , G01S19/13 , G01S2013/0254 , G05B11/42 , G05B13/024 , G05B13/042 , G05D1/0022 , G05D1/0027 , G05D1/0088 , G05D1/0094 , G05D1/02 , G05D1/0202 , G05D1/0204 , G05D1/0206 , G05D1/021 , G05D1/0246 , G05D1/0278 , G05D1/104 , G05D2201/0207 , G06K9/00637 , G06K9/00677 , G08G5/0039 , G08G5/045 , G08G9/02 , H01Q3/26 , H01Q3/2617 , H01Q3/28 , H01Q3/36 , H04B7/0617 , H04B7/18506 , H04N5/225 , H04N7/183 , H04N2005/2255
Abstract: Some embodiments are directed to an unmanned vehicle for transmitting signals. The unmanned vehicle includes a transmitting unit that is configured to transmit a signal towards an object. The unmanned vehicle also includes a control unit that is in communication with at least one companion unmanned vehicle. The control unit is configured to determine a position of the at least one companion unmanned vehicle relative to the unmanned vehicle. The control unit is further configured to control the transmitting element based on at least the position of the at least one unmanned vehicle such that the transmitting element forms a phased-array transmitter with a transmitting element of the at least one companion unnamed vehicle, the phased-array transmitter emitting a transmission beam in a predetermined direction.
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公开(公告)号：US20170217578A1
公开(公告)日：2017-08-03
申请号：US15494251
申请日：2017-04-21
Applicant: SZ DJI TECHNOLOGY Co., LTD.
Inventor： Tao Wang , Tao Zhao , Zhi Gang Ou
CPC classification number: B64C27/32 , A63H27/001 , A63H27/02 , B64C11/02 , B64C11/04 , B64C27/08 , B64C27/14 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/108 , F01D5/021 , F01D5/025
Abstract: Systems, methods, and devices for propelling self-propelled movable objects are provided. In one aspect, a rotor assembly for a self-propelled movable object comprises: a hub comprising a first fastening feature; a drive shaft comprising a second fastening feature and directly coupled to the hub by a mating connection of the first and second fastening features, wherein the drive shaft is configured to cause rotation of the hub such that the mating connection of the first and second fastening features is tightened by the rotation; and a plurality of rotor blades coupled to the hub and configured to rotate therewith to generate a propulsive force.
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公开(公告)号：US20170205827A1
公开(公告)日：2017-07-20
申请号：US15402312
申请日：2017-01-10
Applicant: Alarm.com Incorporated
Inventor： Babak Rezvani
IPC: G05D1/02 , G05D1/00 , G08B13/196
CPC classification number: G05D1/02 , B64C39/024 , B64C2201/021 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/127 , G05D1/0022 , G06Q10/00 , G08B13/196 , G08B13/1965 , G08B15/00 , G08B15/02 , G08B25/008 , G08B25/14
Abstract: In one general aspect, a drone control device includes a body, a motor that is configured to move the body, a network module, an input module, and a processor. The network module is configured to communicate with a security system that monitors a property and receive data associated with a location within the property. The input module is configured to receive user input. The processor is configured to perform operations that include: determine, from among the location within the property and other locations within the property, a target location within the property; move the body to the target location within the property by providing a signal to the motor; receive, from the input module, input data that is associated with an operation of the security system; and in response to receiving the input data, perform the operation of the security system.
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公开(公告)号：US20170197729A1
公开(公告)日：2017-07-13
申请号：US15321006
申请日：2015-06-18
Applicant: SIKORSKY AIRCRAFT CORPORATION
Inventor： Jason C. Derenick , Xuchu Ding , Igor Cherepinsky , Harshad S. Sane , Christopher Stathis
CPC classification number: B64D45/04 , B64C39/024 , B64C2201/024 , B64D45/08 , G01S13/89 , G01S13/913 , G01S17/89 , G01S17/933 , G06K9/0063 , G06K9/00637 , G06K9/4604 , G06K9/52 , G06K9/6201 , G06K9/6278 , G08G5/0013 , G08G5/0021 , G08G5/0039 , G08G5/0056 , G08G5/0086 , G08G5/025
Abstract: A method of performing a cooperative safe landing area determination includes receiving perception sensor data indicative of conditions at a plurality of potential landing areas. A processing subsystem of a vehicle updates a local safe landing area map based on the perception sensor data. The local safe landing area map defines safe landing area classifications and classification confidences associated with the potential landing areas. One or more remotely-generated safe landing area maps are received from one or more remote data sources. The one or more remotely-generated safe landing area maps correspond to one or more additional potential landing areas and non-landing areas. The local safe landing area map and the remotely-generated safe landing area maps are aggregated to form a fused safe landing area map. The fused safe landing area map is used to make a final safe landing area determination.
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公开(公告)号：US20170197703A1
公开(公告)日：2017-07-13
申请号：US14994080
申请日：2016-01-12
Applicant: Zenon Dragan
Inventor： Greg Wood
CPC classification number: B64C39/024 , B64C1/30 , B64C27/08 , B64C2201/024 , B64C2201/027
Abstract: A multi-rotor UAV comprises a body and a plurality of rotor arms extending radially from the body. A rotor assembly is connected to an outside end of each rotor arm. An attachment interface is connected to the body and provides rotor arm attachment points for attaching the rotor arms to the body and pivoting the rotor arms from an unfolded operating position, to a folded position wherein the rotor arms are pivoted such that an outer arm portion of each rotor arm is enabled to cross the pivot end and an inner arm portion of an adjacent or arm.
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