GB202008363D0 - A coaxial double-propeller vertical take-off and landing aircraft using moving mass control and a control method thereof - Google Patents

A coaxial double-propeller vertical take-off and landing aircraft using moving mass control and a control method thereof

Info

Publication number
GB202008363D0
GB202008363D0 GBGB2008363.0A GB202008363A GB202008363D0 GB 202008363 D0 GB202008363 D0 GB 202008363D0 GB 202008363 A GB202008363 A GB 202008363A GB 202008363 D0 GB202008363 D0 GB 202008363D0
Authority
GB
United Kingdom
Prior art keywords
control
moving mass
vertical take
landing aircraft
coaxial double
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
GBGB2008363.0A
Other versions
GB2588478A (en
GB2588478B (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Northwestern Polytechnical University
Original Assignee
Northwestern Polytechnical University
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 Northwestern Polytechnical University filed Critical Northwestern Polytechnical University
Publication of GB202008363D0 publication Critical patent/GB202008363D0/en
Publication of GB2588478A publication Critical patent/GB2588478A/en
Application granted granted Critical
Publication of GB2588478B publication Critical patent/GB2588478B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16Blades
    • B64C11/20Constructional features
    • B64C11/28Collapsible or foldable blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C17/00Aircraft stabilisation not otherwise provided for
    • B64C17/02Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus
    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/24Aircraft characterised by the type or position of power plants using steam or spring force
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D35/00Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • B64D35/04Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D35/00Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • B64D35/04Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors
    • B64D35/06Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors the propellers or rotors being counter-rotating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports
    • B64U30/24Coaxial rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U40/00On-board mechanical arrangements for adjusting control surfaces or rotors; On-board mechanical arrangements for in-flight adjustment of the base configuration
    • B64U40/20On-board mechanical arrangements for adjusting control surfaces or rotors; On-board mechanical arrangements for in-flight adjustment of the base configuration for in-flight adjustment of the base configuration
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/19Propulsion using electrically powered motors
    • 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
    • B64U30/293Foldable or collapsible rotors or rotor supports
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/30Supply or distribution of electrical power

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
GB2008363.0A 2019-06-09 2020-06-03 A coaxial double-propeller vertical take-off and landing aircraft using moving mass control and a control method thereof Active GB2588478B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910494371.2A CN110155316A (en) 2019-06-09 2019-06-09 A kind of coaxial twin screw vertically taking off and landing flyer of Moving mass control and its control method

Publications (3)

Publication Number Publication Date
GB202008363D0 true GB202008363D0 (en) 2020-07-15
GB2588478A GB2588478A (en) 2021-04-28
GB2588478B GB2588478B (en) 2022-02-23

Family

ID=67628148

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2008363.0A Active GB2588478B (en) 2019-06-09 2020-06-03 A coaxial double-propeller vertical take-off and landing aircraft using moving mass control and a control method thereof

Country Status (2)

Country Link
CN (1) CN110155316A (en)
GB (1) GB2588478B (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108298064B (en) * 2017-11-09 2024-04-26 青岛兰道尔空气动力工程有限公司 Unconventional yaw control system
CN110427043B (en) * 2019-09-04 2021-09-28 福州大学 Pose controller design method based on gravity center offset of operation flying robot
US11524766B2 (en) 2020-06-01 2022-12-13 Textron Innovations Inc. Single motor single actuator rotorcraft
CN112277551B (en) * 2020-10-28 2022-04-15 北京航空航天大学 Variable structure multi-mode mobile robot
CN113200145B (en) * 2021-07-05 2021-10-01 南京傲宁数据科技有限责任公司 Portable micro coaxial double-propeller unmanned aerial vehicle and control method thereof
CN113656920B (en) * 2021-10-20 2021-12-21 中国空气动力研究与发展中心计算空气动力研究所 Missile rudder surface hinge moment design method capable of reducing power redundancy of steering engine
CN114180056B (en) * 2021-12-06 2023-04-07 南京航空航天大学 Cross-medium unmanned aerial vehicle variant device
CN114291254A (en) * 2021-12-28 2022-04-08 中南大学 A barycenter control system and stamp rotor craft for stamp rotor craft
CN114348237A (en) * 2021-12-31 2022-04-15 洛阳瑞极光电科技有限公司 Closing and locking mechanism for ejection port of folding wing surface of small aircraft
CN114476045B (en) * 2022-04-07 2022-08-02 西安工业大学 Variable-centroid coaxial dual-rotor aircraft and control method thereof

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3722830A (en) * 1971-02-12 1973-03-27 G Barber Helicopter type vehicle
US10054939B1 (en) * 2012-09-22 2018-08-21 Paul G. Applewhite Unmanned aerial vehicle systems and methods of use
EP4053016A1 (en) * 2014-11-10 2022-09-07 Ascent Aerosystems Inc. Unmanned flying device
CN105197249B (en) * 2015-11-02 2018-10-16 首都师范大学 Displacement adjustment device, battery holder and unmanned plane for unmanned plane
KR101874080B1 (en) * 2016-12-05 2018-07-03 이충열 Quad copter with switchable camcorder handle
CN106828886A (en) * 2017-01-16 2017-06-13 北京猎鹰无人机科技有限公司 A kind of aircraft center of gravity dynamically balancing device
CN107117300B (en) * 2017-04-26 2019-04-16 哈尔滨工业大学 Unmanned vehicle based on coaxial more rotor pose adjustments
US11027840B2 (en) * 2017-08-29 2021-06-08 Hangzhou Zero Zero Technology Co., Ltd. Autonomous self-stabilizing aerial system and method
CN108557070B (en) * 2018-04-12 2019-05-03 北京理工大学 A kind of small-sized coaxial dual-rotor helicopter
CN108545178B (en) * 2018-06-12 2023-05-16 西北工业大学 Coaxial double-rotor unmanned aerial vehicle based on vector mechanism
CN109533310B (en) * 2018-10-18 2022-05-06 沈阳理工大学 Miniature coaxial double-rotor suspension device of maneuvering launching foldable type
CN109733597B (en) * 2019-03-06 2020-12-08 杭州电子科技大学 Remote-controllable coaxial double-oar single-shaft aircraft

Also Published As

Publication number Publication date
CN110155316A (en) 2019-08-23
GB2588478A (en) 2021-04-28
GB2588478B (en) 2022-02-23

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