[go: up one dir, main page]

WO2019109622A1 - Optimizing propeller direction in drone design using onboard network of sensors - Google Patents

Optimizing propeller direction in drone design using onboard network of sensors Download PDF

Info

Publication number
WO2019109622A1
WO2019109622A1 PCT/CN2018/091592 CN2018091592W WO2019109622A1 WO 2019109622 A1 WO2019109622 A1 WO 2019109622A1 CN 2018091592 W CN2018091592 W CN 2018091592W WO 2019109622 A1 WO2019109622 A1 WO 2019109622A1
Authority
WO
WIPO (PCT)
Prior art keywords
drone
rotatable
propellers
sensors
movement
Prior art date
Application number
PCT/CN2018/091592
Other languages
French (fr)
Inventor
Seng Fook LEE
Original Assignee
Guangdong Kang Yun Technologies Limited
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Guangdong Kang Yun Technologies Limited filed Critical Guangdong Kang Yun Technologies Limited
Publication of WO2019109622A1 publication Critical patent/WO2019109622A1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/22Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B64C27/26Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/22Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B64C27/28Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with forward-propulsion propellers pivotable to act as lifting rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/20Vertical take-off and landing [VTOL] aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/25Fixed-wing aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports
    • B64U30/29Constructional aspects of rotors or rotor supports; Arrangements thereof
    • B64U30/296Rotors with variable spatial positions relative to the UAV body
    • B64U30/297Tilting rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/13Propulsion using external fans or propellers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B64C2027/8236Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft including pusher propellers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/30UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00UAVs characterised by their flight controls
    • B64U2201/20Remote controls
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports
    • B64U30/29Constructional aspects of rotors or rotor supports; Arrangements thereof
    • B64U30/296Rotors with variable spatial positions relative to the UAV body

Definitions

  • the present disclosure relates generally to drone based systems, and more specifically to optimizing propeller direction in drone design using an onboard network of sensors.
  • a drone corresponds to a flying object of a shape such as a plane or a helicopter flying by a control signal of a radio wave while not carrying a human. They may carry various items such as cameras, sensors, and communications equipment. Drones can vary greatly in terms of size and complexity.
  • a drone includes a propulsion system, a power source for powering the propulsion system, a steering mechanism, a controller including a remote communication system, and a frame maintaining all other components.
  • the small-sized drones include multiple propellers or rotors to reduce an overall footprint of the drone while increasing lift, each propeller provided with an electric motor.
  • rotors include, but are not limited to banana-type twin-rotors, counter-rotating coaxial rotors, quadcopter and quadrotors.
  • a drone that includes a set of rotatable and fixed propellers powered by one or more battery powered electric motor for providing upward/forward thrust to the drone during upward/forward movement of the drone respectively.
  • the rotatable propellers are rotatable from 0-90 degrees according to the direction of movement of the drone.
  • the rotatable propellers when the rotatable propellers are disposed in a plane parallel to the wings of the drone, during the upward movement of the drone, they provide an upward thrust to the drone, facilitating the drone to lift higher and remain in the air for a longer duration, thereby increasing the flying time of the drone, and optimizing the battery usage.
  • first and second rotatable propellers when they and are in a plane perpendicular to the wings during the forward movement of the drone, they provide a forward thrust to the drone, facilitating the drone to remain in the air for a longer duration, thereby increasing the flying time of the drone, and optimizing the battery usage.
  • FIG. 1 illustrates a drone moving in an upward direction, in accordance with an embodiment of the present invention
  • FIG.2 illustrates a drone moving in a forward direction, in accordance with an embodiment of the present invention.
  • FIG. 3 illustrates a camera of the drone, in accordance with an embodiment of the present invention.
  • FIG. 1 illustrates a drone 100 moving in an upward direction, in accordance with an embodiment of the present invention.
  • the drone 100 is a shape of an aircraft with wings 102, first and second rotatable propellers 104a and 104b, and first, second and third fixed propellers 104c, 104d (not shown) and 104e (hereinafter collectively referred to as propellers 104). It will be apparent to a person skilled in the art that further propellers 104 may be added to the drone 100, without limiting the scope of the disclosure.
  • the propellers 104 may be powered by one or more battery powered electric motors (not shown) and provide necessary upward/forward thrust to the drone 100 during upward/forward movement of the drone 100 respectively.
  • the drone 100 may be remotely controlled by a remote control device using RF technology.
  • the drone 100 includes a processor so that it can be remotely controlled using an application executing on a smart phone of the user.
  • the first rotatable propeller 104a is fixedly attached to a first attachment 108a that is rotatably attached to a front end of a first hanger 110a.
  • the second rotatable propeller 104b is fixedly attached to a second attachment 108b that is rotatably attached to a front end of a second hanger 110a.
  • the first and second attachments 108a and 108b are rotatable so as to rotate the first and second rotatable propellers 104a and 104b from 0-90 degrees according to the direction of movement of the drone 100.
  • the first and second attachments 108a and 108b may be rotated either manually or automatically so as to set the first and second rotatable propellers 104a and 104b in a plane parallel to the wings 102.
  • the first and second rotatable propellers 104a and 104b are disposed in a plane parallel to the wings 102 during the upward movement of the drone 100, they provide an upward thrust to the drone 100, facilitating the drone 100 to lift higher and remain in the air for a longer duration, thereby increasing the flying time of the drone 100, and optimizing the battery usage.
  • the drone 100 includes one or more on-board sensors (not shown) such as wind direction sensor, speed sensor, thermos sensor, drone direction sensor, so as to automatically/manually align the first and second rotatable propellers 104a and 104b in the direction of the movement of the drone 100.
  • sensors such as wind direction sensor, speed sensor, thermos sensor, drone direction sensor, so as to automatically/manually align the first and second rotatable propellers 104a and 104b in the direction of the movement of the drone 100.
  • the drone 100 carries a camera 112 that may be used to do aerial scanning of the outdoor environment, wherein the aerial scanning results in two-dimensional/three dimensional view of the outdoor environment. It will be apparent to a person skilled in the art that further cameras, RGB cameras, sensors may be added to the drone 100, without limiting the scope of the disclosure.
  • FIG.2 illustrates the drone 100 moving in a forward direction, in accordance with an embodiment of the present invention.
  • the first and second attachments 108a and 108b may be rotated either manually or automatically so as to set the first and second rotatable propellers 104a and 104b in a plane perpendicular to the wings 102.
  • the first and second rotatable propellers 104a and 104b are in a plane perpendicular to the wings 102 during the forward movement of the drone 100, they provide a forward thrust to the drone 100, facilitating the drone 100 to remain in the air for a longer duration, thereby increasing the flying time of the drone 100, and optimizing the battery usage.
  • FIG.3 illustrates an inbuilt camera 114 embedded in the drone 100 for performing an aerial scanning of the outdoor environment, in accordance with an embodiment of the present invention.
  • the drone 100 may be used for applications other than capturing videos/images, without limiting the scope of the disclosure.
  • the drone 100 may be used for remote sensing applications, delivery applications, commercial aerial surveillance, commercial and motion picture filmmaking, oil, gas and mineral exploration, disaster relief, real estate and construction, and recreational use.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Toys (AREA)

Abstract

A drone (100) includes one or more rotatable propellers (104a, 104b) and one or more fixed propellers (104c, 104d, 104e) powered by one or more battery powered electric motors for providing upward and forward thrust to the drone (100) during upward and forward movement of the drone (100) respectively. The drone (100) includes a set of sensors, so as to align the rotatable propellers (104a, 104b) in the direction of the movement of the drone (100) based on sensed data.

Description

OPTIMIZING PROPELLER DIRECTION IN DRONE DESIGN USING ONBOARD NETWORK OF SENSORS
TECHNICAL FIELD
The present disclosure relates generally to drone based systems, and more specifically to optimizing propeller direction in drone design using an onboard network of sensors.
BACKGROUND
A drone corresponds to a flying object of a shape such as a plane or a helicopter flying by a control signal of a radio wave while not carrying a human. They may carry various items such as cameras, sensors, and communications equipment. Drones can vary greatly in terms of size and complexity. Typically, a drone includes a propulsion system, a power source for powering the propulsion system, a steering mechanism, a controller including a remote communication system, and a frame maintaining all other components.
The small-sized drones include multiple propellers or rotors to reduce an overall footprint of the drone while increasing lift, each propeller provided with an electric motor. Examples of rotors include, but are not limited to banana-type twin-rotors, counter-rotating coaxial rotors, quadcopter and quadrotors.
However, existing drones are not able to achieve very high flying heights and also not able to stay in air for a long time, because of limited battery available. Small drones typically employ battery-powered electric motors, and it is not possible to increase the size of battery as it may affect the overall weight of the drone.
In light of the above, a need exists for increasing the flying time of a drone without increasing the size of the battery.
SUMMARY
In accordance with an embodiment of the present disclosure, there is provided a drone that includes a set of rotatable and fixed propellers powered by one or more battery powered electric motor for providing upward/forward thrust to the drone during upward/forward movement of the drone respectively.
In accordance with an embodiment of the present disclosure, the rotatable propellers are rotatable from 0-90 degrees according to the direction of movement of the drone.
In accordance with an embodiment of the present disclosure, when the rotatable propellers are disposed in a plane parallel to the wings of the drone, during the upward movement of the drone, they provide an upward thrust to the drone, facilitating the drone to lift higher and remain in the air for a longer duration, thereby increasing the flying time of the drone, and optimizing the battery usage.
In accordance with an embodiment of the present disclosure, when the first and second rotatable propellers and are in a plane perpendicular to the wings during the forward movement of the drone, they provide a forward thrust to the drone, facilitating the drone to remain in the air for a longer duration, thereby increasing the flying time of the drone, and optimizing the battery usage.
It will be appreciated that features of the present disclosure are susceptible to being combined in various combinations without departing from the scope of the present disclosure as defined by the appended claims.
BRIEF DESCRIPTION OF THE DRAWINGS
In the following description, for purposes of explanation, numerous specific details are set forth in order to provide a thorough understanding of the invention. It will be apparent, however, to one skilled in the art that the invention can be practiced without these specific details. In other instances, structures and devices are shown in block diagram form only in order to avoid obscuring the invention.
The present invention, in accordance with one or more various embodiments, is described in detail with reference to the following figures. The drawings are provided for purposes of illustration only and merely depict exemplary embodiments of the invention. These drawings are provided to facilitate the reader’s understanding of the invention and shall not be considered limiting of the breadth, scope, or applicability of the invention. It should be noted that for clarity and ease of illustration these drawings are not necessarily made to scale.
FIG. 1 illustrates a drone moving in an upward direction, in accordance with an embodiment of the present invention;
FIG.2 illustrates a drone moving in a forward direction, in accordance with an embodiment of the present invention; and
FIG. 3 illustrates a camera of the drone, in accordance with an embodiment of the present invention.
DETAILED DESCRIPTION
In the following description, for purposes of explanation, numerous specific details are set forth in order to provide a thorough understanding of the invention. It will be apparent, however, to one skilled in the art that the invention can be practiced without these specific details. In other instances, structures and devices are shown in block diagram form only in order to avoid obscuring the invention.
Reference in this specification to “one embodiment” or “an embodiment” means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one embodiment of the invention. The appearance of the phrase “in one embodiment” in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments. Moreover, various features are described which may be exhibited by some embodiments and not by others. Similarly, various requirements are described which may be requirements for some embodiments but not other embodiments.
Moreover, although the following description contains many specifics for the purposes of illustration, anyone skilled in the art will appreciate that many variations and/or alterations to said details are within the scope of the present invention. Similarly, although many of the features of the present invention are described in terms of each other, or in conjunction with each other, one skilled in the art will appreciate that many of these features can be provided independently of other features. Accordingly, this description of the invention is set forth without any loss of generality to, and without imposing limitations upon, the invention.
FIG. 1 illustrates a drone 100 moving in an upward direction, in accordance with an embodiment of the present invention.
The drone 100 is a shape of an aircraft with wings 102, first and second rotatable propellers 104a and 104b, and first, second and third fixed propellers 104c, 104d (not shown) and 104e (hereinafter collectively referred to as propellers 104). It will be apparent to a person skilled in the art that further propellers 104 may be added to the drone 100, without limiting the scope of the disclosure.
The propellers 104 may be powered by one or more battery powered electric motors (not shown) and provide necessary upward/forward thrust to the drone 100 during upward/forward movement of the drone 100 respectively.
In an embodiment, the drone 100 may be remotely controlled by a remote control device using RF technology. In another embodiment, the drone 100 includes a processor so that it can be remotely controlled using an application executing on a smart phone of the user.
In an embodiment of the present invention, the first rotatable propeller 104a is fixedly attached to a first attachment 108a that is rotatably attached to a front end of a first hanger 110a. Similarly, the second rotatable propeller 104b is fixedly attached to a second attachment 108b that is rotatably attached to a front end of a second hanger 110a. The first and second attachments 108a and 108b are rotatable so as to rotate the first and second rotatable propellers 104a and 104b from 0-90 degrees according to the direction of movement of the drone 100.
As illustrated in FIG.1, during the upward movement of the drone 100, the first and second attachments 108a and 108b may be rotated either manually or automatically so as to set the first and second rotatable propellers 104a and 104b in a plane parallel to the wings 102. When the first and second rotatable propellers 104a and 104b are disposed in a plane parallel to the wings 102 during the upward movement of the drone 100, they provide an upward thrust to the drone 100, facilitating the drone 100 to lift higher and remain in the air for a longer duration, thereby increasing the flying time of the drone 100, and optimizing the battery usage.
In an embodiment of the present invention, the drone 100 includes one or more on-board sensors (not shown) such as wind direction sensor, speed sensor, thermos sensor, drone direction sensor, so as to automatically/manually align the first and second rotatable propellers 104a and 104b in the direction of the movement of the drone 100.
In an embodiment, the drone 100 carries a camera 112 that may be used to do aerial scanning of the outdoor environment, wherein the aerial scanning results in two-dimensional/three dimensional view of the outdoor environment. It will be apparent to a person skilled in the art that further cameras, RGB cameras, sensors may be added to the drone 100, without limiting the scope of the disclosure.
FIG.2 illustrates the drone 100 moving in a forward direction, in accordance with an embodiment of the present invention.
During the forward movement of the drone 100, the first and second attachments 108a and 108b may be rotated either manually or automatically so as to set the first and second rotatable propellers 104a and 104b in a plane perpendicular to the wings 102. When the first and second rotatable propellers 104a and 104b are in a plane perpendicular to the wings 102 during the forward movement of the drone 100, they provide a forward thrust to the drone 100, facilitating the drone 100 to remain in the air for a longer duration, thereby increasing the flying time of the drone 100, and optimizing the battery usage.
FIG.3 illustrates an inbuilt camera 114 embedded in the drone 100 for performing an aerial scanning of the outdoor environment, in accordance with an embodiment of the present invention.
It will be further apparent to a person skilled in the art that the drone 100 may be used for applications other than capturing videos/images, without limiting the scope of the disclosure. For example, the drone 100 may be used for remote sensing applications, delivery applications, commercial aerial surveillance, commercial and motion picture filmmaking, oil, gas and mineral exploration, disaster relief, real estate and construction, and recreational use.
Numerous specific details may be set forth herein to provide a thorough understanding of a number of possible embodiments of a drone incorporating the present disclosure. It will be understood by those skilled in the art, however, that the embodiments may be practiced without these specific details. In other instances, well-known methods, procedures, components and circuits have not been described in detail so as not to obscure the embodiments. It can be appreciated that the specific structural and functional details disclosed herein may be representative and do not necessarily limit the scope of the embodiments.
Although the invention is described above in terms of various exemplary embodiments and implementations, it should be understood that the various features, aspects and functionality described in one or more of the individual embodiments are not limited in their applicability to the particular embodiment with which they are described, but instead can be applied, alone or in various combinations, to one or more of the other embodiments of the invention, whether or not such embodiments are described and whether or not such features are presented as being a part of a described embodiment. Thus, the breadth and scope of the present invention should not be limited by any of the above-described exemplary embodiments.
Terms and phrases used in this document, and variations thereof, unless otherwise expressly stated, should be construed as open ended as opposed to limiting. As examples of the foregoing: the term “including” should be read as meaning “including, without limitation” or the like; the term “example” is used to provide exemplary instances of the item in discussion, not an exhaustive or limiting list thereof; the terms “a” or “an” should be read as meaning “at least one,” “one or more” or the like; and adjectives such as “conventional,” “traditional,” “normal,” “standard,” “known” and terms of similar meaning should not be construed as limiting the item described to a given time period or to an item available as of a given time, but instead should be read to encompass conventional, traditional, normal, or standard technologies that may be available or known now or at any time in the future. Likewise, where this document refers to technologies that would be apparent or known to one of ordinary skill in the art, such technologies encompass those apparent or known to the skilled artisan now or at any time in the future.
Although the invention is described above in terms of various exemplary embodiments and implementations, it should be understood that the various features, aspects and functionality described in one or more of the individual embodiments are not limited in their applicability to the particular embodiment with which they are described, but instead can be applied, alone or in various combinations, to one or more of the other embodiments of the invention, whether or not such embodiments are described and whether or not such features are presented as being a part of a described embodiment. Thus, the breadth and scope of the present invention should not be limited by any of the above-described exemplary embodiments.

Claims (6)

  1. A drone, comprising:
    a plurality of fixed propellers;
    a plurality of rotatable propellers, wherein each rotatable propeller is configured to rotate in a range of 0 to 90 degrees in accordance with a direction of the movement of the drone; and
    a set of sensors for aligning the plurality of rotatable propellers in the direction of the movement of the drone based on sensed data.,
  2. The drone as claimed in claim 1, where the drone is remotely controlled by a remote control device using RF technology.
  3. The drone as claimed in claim 1, where the drone includes a processor so that it is remotely controlled using an application executing on a smart phone of a user.
  4. The drone as claimed in claim 1, wherein during the upward movement of the drone, each rotatable propeller may be rotated either manually or automatically so as to set each rotatable propeller parallel to wings of the drone.
  5. The drone as claimed in claim 1, wherein during the forward movement of the drone, each rotatable propeller may be rotated either manually or automatically so as to set each rotatable propeller perpendicular to wings of the drone.
  6. The drone as claimed in claim 1 further comprising a camera embedded therein for performing an aerial scanning of outdoor environment.
PCT/CN2018/091592 2017-12-06 2018-06-15 Optimizing propeller direction in drone design using onboard network of sensors WO2019109622A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201762595082P 2017-12-06 2017-12-06
US62/595,082 2017-12-06

Publications (1)

Publication Number Publication Date
WO2019109622A1 true WO2019109622A1 (en) 2019-06-13

Family

ID=62961019

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2018/091592 WO2019109622A1 (en) 2017-12-06 2018-06-15 Optimizing propeller direction in drone design using onboard network of sensors

Country Status (2)

Country Link
CN (1) CN108341050A (en)
WO (1) WO2019109622A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021010915A1 (en) * 2019-07-12 2021-01-21 Aselsan Elektroni̇k Sanayi̇ Ve Ti̇caret Anoni̇m Şi̇rketi̇ A multi-function unmanned aerial vehicle with tilting co-axial, counter-rotating, folding propeller system
WO2024263593A3 (en) * 2023-06-19 2025-04-10 Method Aeronautics, LLC Vertical take-off and landing aircraft

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5405105A (en) * 1993-05-28 1995-04-11 Hudson Valley V/Stol Aircraft, Inc. Tilt wing VTOL aircraft
CN204895859U (en) * 2015-08-28 2015-12-23 武汉捷特航空科技有限公司 Stationary vane aircraft with many rotors
CN105204514A (en) * 2015-09-18 2015-12-30 西北农林科技大学 Novel tilt-rotor unmanned aerial vehicle attitude control system
US20160122018A1 (en) * 2014-10-29 2016-05-05 Denso Corporation Observation Device
CN206125423U (en) * 2016-11-02 2017-04-26 北京航空航天大学 VTOL fixed wing uavs with power device verts
CN106956773A (en) * 2017-04-07 2017-07-18 南昌航空大学 Tilting rotor formula VUAV and its control method

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160023755A1 (en) * 2014-05-05 2016-01-28 King Fahd University Of Petroleum And Minerals System and method for control of quadrotor air vehicles with tiltable rotors
CN205027951U (en) * 2015-09-16 2016-02-10 北京中科遥数信息技术有限公司 Oblique photography device of five dismountable camera lenses
CN205168881U (en) * 2015-10-30 2016-04-20 韩鹏飞 Multiaxial flying machine
CN205738117U (en) * 2016-06-27 2016-11-30 江苏冰城氢能科技有限公司 Fixed-wing unmanned plane
CN206515700U (en) * 2017-02-28 2017-09-22 上海拓攻机器人有限公司 A kind of UAV Flight Control System based on smart mobile phone
CN206704529U (en) * 2017-04-17 2017-12-05 深圳市九天创新科技有限责任公司 A kind of camera oblique photograph unmanned plane of four rotor five
CN107336833B (en) * 2017-07-05 2023-10-31 天津凤凰智能科技有限公司 Composite unmanned aerial vehicle and control method

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5405105A (en) * 1993-05-28 1995-04-11 Hudson Valley V/Stol Aircraft, Inc. Tilt wing VTOL aircraft
US20160122018A1 (en) * 2014-10-29 2016-05-05 Denso Corporation Observation Device
CN204895859U (en) * 2015-08-28 2015-12-23 武汉捷特航空科技有限公司 Stationary vane aircraft with many rotors
CN105204514A (en) * 2015-09-18 2015-12-30 西北农林科技大学 Novel tilt-rotor unmanned aerial vehicle attitude control system
CN206125423U (en) * 2016-11-02 2017-04-26 北京航空航天大学 VTOL fixed wing uavs with power device verts
CN106956773A (en) * 2017-04-07 2017-07-18 南昌航空大学 Tilting rotor formula VUAV and its control method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021010915A1 (en) * 2019-07-12 2021-01-21 Aselsan Elektroni̇k Sanayi̇ Ve Ti̇caret Anoni̇m Şi̇rketi̇ A multi-function unmanned aerial vehicle with tilting co-axial, counter-rotating, folding propeller system
WO2024263593A3 (en) * 2023-06-19 2025-04-10 Method Aeronautics, LLC Vertical take-off and landing aircraft

Also Published As

Publication number Publication date
CN108341050A (en) 2018-07-31

Similar Documents

Publication Publication Date Title
US11927877B2 (en) Interchangeable mounting platform
US20210223669A1 (en) Method and system for motion camera with embedded gimbal
US11423792B2 (en) System and method for obstacle avoidance in aerial systems
US20190291864A1 (en) Transformable apparatus
US10979651B2 (en) Imaging system
CN115412663A (en) System, method and non-transitory computer readable memory
CN104724286B (en) a spherical aircraft
CN108602555A (en) Unmanned vehicle with deformable arm
CN203747305U (en) Miniature quad-rotor unmanned aerial vehicle electric power line infrared patrol inspection system
US11530025B2 (en) Foldable rotor blade assembly and aerial vehicle with a foldable rotor blade assembly
CN104718509A (en) Remote control methods and systems
JP2017530302A (en) Support mechanism and system
CN108027492B (en) Imaging system
CN104058099A (en) Unmanned plane electro-optical pod
US11267568B2 (en) Aerial system including foldable frame architecture
CN110770123A (en) Portable integrated UAV
WO2017107275A1 (en) Multi-purpose unmanned aerial vehicle and unmanned aerial vehicle control system
CN207117778U (en) Image intake device, moveable platform and image capturing equipment
WO2019109622A1 (en) Optimizing propeller direction in drone design using onboard network of sensors
WO2019109621A1 (en) Optimizing propeller speed in drone design using onboard network of sensors
CN103345255A (en) Quad-rotor aerial photography positioning unmanned aerial vehicle
US11428362B2 (en) Two-axis gimbal system for supporting a camera
CN205396569U (en) Unmanned vehicles with battery formula counter weight device
CN205186523U (en) Meeting -place server based on four rotors
WO2020143029A1 (en) Two-axis gimbal system for supporting a camera

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 18885172

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

32PN Ep: public notification in the ep bulletin as address of the adressee cannot be established

Free format text: NOTING OF LOSS OF RIGHTS PURSUANT TO RULE 112(1) EPC (EPO FORM 1205A DATED 16/09/2020)

122 Ep: pct application non-entry in european phase

Ref document number: 18885172

Country of ref document: EP

Kind code of ref document: A1