AU2013403751B2 - Rotor driving system - Google Patents

Rotor driving system Download PDF

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Publication number
AU2013403751B2
AU2013403751B2 AU2013403751A AU2013403751A AU2013403751B2 AU 2013403751 B2 AU2013403751 B2 AU 2013403751B2 AU 2013403751 A AU2013403751 A AU 2013403751A AU 2013403751 A AU2013403751 A AU 2013403751A AU 2013403751 B2 AU2013403751 B2 AU 2013403751B2
Authority
AU
Australia
Prior art keywords
rotor
rod
swashplate
blade
clamp
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.)
Active
Application number
AU2013403751A
Other languages
English (en)
Other versions
AU2013403751A1 (en
Inventor
Gangyin TIAN
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 United Aircraft Technology Co Ltd
Original Assignee
Shenzhen United Aircraft Technology Co Ltd
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 United Aircraft Technology Co Ltd filed Critical Shenzhen United Aircraft Technology Co Ltd
Priority to AU2016100487A priority Critical patent/AU2016100487A4/en
Publication of AU2013403751A1 publication Critical patent/AU2013403751A1/en
Application granted granted Critical
Publication of AU2013403751B2 publication Critical patent/AU2013403751B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/59—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical
    • B64C27/605—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including swash plate, spider or cam mechanisms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/17—Helicopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B64U30/24—Coaxial rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U40/00—On-board mechanical arrangements for adjusting control surfaces or rotors; On-board mechanical arrangements for in-flight adjustment of the base configuration
    • B64U40/10—On-board mechanical arrangements for adjusting control surfaces or rotors; On-board mechanical arrangements for in-flight adjustment of the base configuration for adjusting control surfaces or rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/20—Transmission of mechanical power to rotors or propellers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Transmission Devices (AREA)
  • Catching Or Destruction (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
AU2013403751A 2013-10-23 2013-10-23 Rotor driving system Active AU2013403751B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU2016100487A AU2016100487A4 (en) 2013-10-23 2016-04-29 Rotor driving system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CN2013/085745 WO2015058364A1 (zh) 2013-10-23 2013-10-23 旋翼驱动系统

Related Child Applications (1)

Application Number Title Priority Date Filing Date
AU2016100487A Division AU2016100487A4 (en) 2013-10-23 2016-04-29 Rotor driving system

Publications (2)

Publication Number Publication Date
AU2013403751A1 AU2013403751A1 (en) 2016-05-19
AU2013403751B2 true AU2013403751B2 (en) 2016-12-01

Family

ID=52992130

Family Applications (2)

Application Number Title Priority Date Filing Date
AU2013403751A Active AU2013403751B2 (en) 2013-10-23 2013-10-23 Rotor driving system
AU2016100487A Expired AU2016100487A4 (en) 2013-10-23 2016-04-29 Rotor driving system

Family Applications After (1)

Application Number Title Priority Date Filing Date
AU2016100487A Expired AU2016100487A4 (en) 2013-10-23 2016-04-29 Rotor driving system

Country Status (7)

Country Link
US (1) US10081423B2 (https=)
EP (1) EP3061688B1 (https=)
JP (1) JP6099836B2 (https=)
AU (2) AU2013403751B2 (https=)
BR (1) BR112016008922B1 (https=)
RU (1) RU2641396C2 (https=)
WO (1) WO2015058364A1 (https=)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106915457B (zh) * 2017-02-22 2019-05-17 北京航空航天大学 一种上下旋翼倾斜器平行度可变的共轴式直升机操纵系统
CN109533322B (zh) * 2018-11-15 2020-09-25 中国直升机设计研究所 一种自动倾斜器
CN112173099A (zh) * 2020-11-26 2021-01-05 尚良仲毅(沈阳)高新科技有限公司 一种用于无人机的变距装置、变距控制方法及无人机

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2155702C1 (ru) * 1999-04-15 2000-09-10 Кумертауское авиационное производственное предприятие Система двух соосных несущих винтов летательного аппарата
EP1944234A1 (de) * 2007-01-12 2008-07-16 Rotorfly Ltd. Rotorsystem
CN102658865A (zh) * 2012-05-17 2012-09-12 李游 共轴反转旋翼直升机的共轴传动和控制结构
CN103318407A (zh) * 2013-06-05 2013-09-25 王开林 一种共轴式双旋翼无人直升机操纵系统的分立控制系统

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES8102955A1 (es) * 1980-04-18 1981-02-16 Campos Herruzo Juan Sistema control de direccion de helicoptero coaxial, paso colectivo a la vez que tambien variable simultaneamente con signo contrario
RU2485017C2 (ru) * 2011-08-24 2013-06-20 Сергей Александрович Задорожный Механизм автомата перекоса вертолета

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2155702C1 (ru) * 1999-04-15 2000-09-10 Кумертауское авиационное производственное предприятие Система двух соосных несущих винтов летательного аппарата
EP1944234A1 (de) * 2007-01-12 2008-07-16 Rotorfly Ltd. Rotorsystem
CN102658865A (zh) * 2012-05-17 2012-09-12 李游 共轴反转旋翼直升机的共轴传动和控制结构
CN103318407A (zh) * 2013-06-05 2013-09-25 王开林 一种共轴式双旋翼无人直升机操纵系统的分立控制系统

Also Published As

Publication number Publication date
BR112016008922A2 (https=) 2017-08-01
BR112016008922B1 (pt) 2021-09-14
JP6099836B2 (ja) 2017-03-22
US10081423B2 (en) 2018-09-25
EP3061688A1 (en) 2016-08-31
US20160264238A1 (en) 2016-09-15
WO2015058364A1 (zh) 2015-04-30
AU2016100487A4 (en) 2016-06-09
RU2641396C2 (ru) 2018-01-17
AU2013403751A1 (en) 2016-05-19
EP3061688B1 (en) 2018-09-05
EP3061688A4 (en) 2017-07-19
RU2016117177A (ru) 2017-11-28
JP2016538196A (ja) 2016-12-08

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FGA Letters patent sealed or granted (standard patent)