CN111874207A - 伸缩装置以及应用该伸缩装置的无人机 - Google Patents

伸缩装置以及应用该伸缩装置的无人机 Download PDF

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Publication number
CN111874207A
CN111874207A CN202010827633.5A CN202010827633A CN111874207A CN 111874207 A CN111874207 A CN 111874207A CN 202010827633 A CN202010827633 A CN 202010827633A CN 111874207 A CN111874207 A CN 111874207A
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China
Prior art keywords
hinge hole
hinged
straight
telescopic
hinge
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.)
Pending
Application number
CN202010827633.5A
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English (en)
Chinese (zh)
Inventor
杨陶
李鹏
刘云辉
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.)
Shenzhen Graduate School Harbin Institute of Technology
Original Assignee
Shenzhen Graduate School Harbin Institute of Technology
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 Shenzhen Graduate School Harbin Institute of Technology filed Critical Shenzhen Graduate School Harbin Institute of Technology
Priority to CN202010827633.5A priority Critical patent/CN111874207A/zh
Priority to PCT/CN2020/111107 priority patent/WO2022036732A1/fr
Publication of CN111874207A publication Critical patent/CN111874207A/zh
Pending legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/30Parts of fuselage relatively movable to reduce overall dimensions of aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061Frames
    • B64C1/063Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • B64U10/13Flying platforms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/19Propulsion using electrically powered motors

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Manipulator (AREA)
  • Forklifts And Lifting Vehicles (AREA)
CN202010827633.5A 2020-08-17 2020-08-17 伸缩装置以及应用该伸缩装置的无人机 Pending CN111874207A (zh)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN202010827633.5A CN111874207A (zh) 2020-08-17 2020-08-17 伸缩装置以及应用该伸缩装置的无人机
PCT/CN2020/111107 WO2022036732A1 (fr) 2020-08-17 2020-08-25 Dispositif télescopique et véhicule aérien sans pilote appliquant un dispositif télescopique

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010827633.5A CN111874207A (zh) 2020-08-17 2020-08-17 伸缩装置以及应用该伸缩装置的无人机

Publications (1)

Publication Number Publication Date
CN111874207A true CN111874207A (zh) 2020-11-03

Family

ID=73202837

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010827633.5A Pending CN111874207A (zh) 2020-08-17 2020-08-17 伸缩装置以及应用该伸缩装置的无人机

Country Status (2)

Country Link
CN (1) CN111874207A (fr)
WO (1) WO2022036732A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022036731A1 (fr) * 2020-08-17 2022-02-24 哈尔滨工业大学(深圳) Dispositif extensible de type ciseaux et véhicule aérien sans pilote utilisant celui-ci

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114408173B (zh) * 2022-03-02 2023-11-17 吉林大学 一种x型四旋翼可变结构无人机

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN205131639U (zh) * 2015-09-01 2016-04-06 湖南云顶智能科技有限公司 一种多旋翼无人机
JP2017109626A (ja) * 2015-12-17 2017-06-22 株式会社ザクティ 飛行体
CN105460211B (zh) * 2015-12-30 2018-10-12 联想(北京)有限公司 一种飞行装置
CN207791152U (zh) * 2017-12-15 2018-08-31 汕头市欧兰斯模型科技有限公司 一种飞行器驱动机构及飞行器
CN208036470U (zh) * 2018-04-09 2018-11-02 洛阳理工学院 一种兼具飞行与爬行功能的仿生机器人
CN111301663A (zh) * 2020-03-16 2020-06-19 王会涛 一种用于多旋翼机的机臂折叠和转动的装置
CN212890891U (zh) * 2020-08-17 2021-04-06 哈尔滨工业大学(深圳) 伸缩装置以及应用该伸缩装置的无人机

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022036731A1 (fr) * 2020-08-17 2022-02-24 哈尔滨工业大学(深圳) Dispositif extensible de type ciseaux et véhicule aérien sans pilote utilisant celui-ci

Also Published As

Publication number Publication date
WO2022036732A1 (fr) 2022-02-24

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Inventor after: Li Peng

Inventor after: Yang Tao

Inventor after: Liu Yunhui

Inventor before: Yang Tao

Inventor before: Li Peng

Inventor before: Liu Yunhui