CN104554717A - 旋翼驱动系统 - Google Patents
旋翼驱动系统 Download PDFInfo
- Publication number
- CN104554717A CN104554717A CN201310502865.3A CN201310502865A CN104554717A CN 104554717 A CN104554717 A CN 104554717A CN 201310502865 A CN201310502865 A CN 201310502865A CN 104554717 A CN104554717 A CN 104554717A
- Authority
- CN
- China
- Prior art keywords
- rotor
- bar
- swash plate
- lower rotor
- rotary wing
- 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
Links
- 230000000694 effects Effects 0.000 claims description 9
- 230000001360 synchronised effect Effects 0.000 claims description 9
- 230000005540 biological transmission Effects 0.000 claims description 6
- 230000000712 assembly Effects 0.000 claims description 4
- 238000000429 assembly Methods 0.000 claims description 4
- 238000000034 method Methods 0.000 abstract description 16
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 238000012423 maintenance Methods 0.000 abstract description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 19
- FGUUSXIOTUKUDN-IBGZPJMESA-N C1(=CC=CC=C1)N1C2=C(NC([C@H](C1)NC=1OC(=NN=1)C1=CC=CC=C1)=O)C=CC=C2 Chemical compound C1(=CC=CC=C1)N1C2=C(NC([C@H](C1)NC=1OC(=NN=1)C1=CC=CC=C1)=O)C=CC=C2 FGUUSXIOTUKUDN-IBGZPJMESA-N 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
Landscapes
- Toys (AREA)
Abstract
Description
Claims (8)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310502865.3A CN104554717B (zh) | 2013-10-23 | 2013-10-23 | 旋翼驱动系统 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310502865.3A CN104554717B (zh) | 2013-10-23 | 2013-10-23 | 旋翼驱动系统 |
Publications (2)
Publication Number | Publication Date |
---|---|
CN104554717A true CN104554717A (zh) | 2015-04-29 |
CN104554717B CN104554717B (zh) | 2016-09-28 |
Family
ID=53071995
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201310502865.3A Active CN104554717B (zh) | 2013-10-23 | 2013-10-23 | 旋翼驱动系统 |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN104554717B (zh) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104913912A (zh) * | 2015-05-19 | 2015-09-16 | 北京航空航天大学 | 吊挂式共轴反转旋翼试验装置 |
CN105799925A (zh) * | 2016-03-14 | 2016-07-27 | 石玉玉 | 一种无人机 |
CN106438663A (zh) * | 2016-11-08 | 2017-02-22 | 芜湖万户航空航天科技有限公司 | 无人机桨夹轴组件 |
CN107200126A (zh) * | 2017-05-06 | 2017-09-26 | 西安多杰机器人有限公司 | 一种大荷载长航时无人直升机 |
CN108116673A (zh) * | 2017-12-22 | 2018-06-05 | 中国兵器工业计算机应用技术研究所 | 一种共轴双桨直升机桨距操纵系统 |
CN108216631A (zh) * | 2018-03-07 | 2018-06-29 | 天津曙光天成科技有限公司 | 一种变矩系统及无人多旋翼飞行器 |
CN108791859A (zh) * | 2018-07-12 | 2018-11-13 | 西安君晖航空科技有限公司 | 一种快速抵近的旋翼无人机 |
CN111392031A (zh) * | 2020-02-24 | 2020-07-10 | 深圳联合飞机科技有限公司 | 一种旋翼变距装置 |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111377050B (zh) * | 2020-02-24 | 2022-02-25 | 深圳联合飞机科技有限公司 | 一种共轴旋翼操纵装置 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1876494A (zh) * | 2006-06-28 | 2006-12-13 | 孙为红 | 共轴双桨自旋翼飞行器的同步换向调节装置 |
WO2009088491A2 (en) * | 2008-01-02 | 2009-07-16 | Sikorsky Aircraft Corporation | Planetary de-rotation system for a shaft fairing system |
US20110158809A1 (en) * | 2009-12-31 | 2011-06-30 | Zhihong Luo | Dual-rotor model helicopter control system |
US20120156033A1 (en) * | 2009-12-18 | 2012-06-21 | Sikorsky Aircraft Corporation | Helicopter rotor control system |
CN202624632U (zh) * | 2012-05-24 | 2012-12-26 | 孙朝辉 | 直升机的共轴双旋翼结构 |
-
2013
- 2013-10-23 CN CN201310502865.3A patent/CN104554717B/zh active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1876494A (zh) * | 2006-06-28 | 2006-12-13 | 孙为红 | 共轴双桨自旋翼飞行器的同步换向调节装置 |
WO2009088491A2 (en) * | 2008-01-02 | 2009-07-16 | Sikorsky Aircraft Corporation | Planetary de-rotation system for a shaft fairing system |
US20120156033A1 (en) * | 2009-12-18 | 2012-06-21 | Sikorsky Aircraft Corporation | Helicopter rotor control system |
US20110158809A1 (en) * | 2009-12-31 | 2011-06-30 | Zhihong Luo | Dual-rotor model helicopter control system |
CN202624632U (zh) * | 2012-05-24 | 2012-12-26 | 孙朝辉 | 直升机的共轴双旋翼结构 |
Non-Patent Citations (1)
Title |
---|
袁夏明 等: "一种共轴式直升机操纵机构的运动学建模与分析", 《航空学报》 * |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104913912A (zh) * | 2015-05-19 | 2015-09-16 | 北京航空航天大学 | 吊挂式共轴反转旋翼试验装置 |
CN105799925A (zh) * | 2016-03-14 | 2016-07-27 | 石玉玉 | 一种无人机 |
CN105799925B (zh) * | 2016-03-14 | 2018-01-16 | 石玉玉 | 一种无人机 |
CN106438663A (zh) * | 2016-11-08 | 2017-02-22 | 芜湖万户航空航天科技有限公司 | 无人机桨夹轴组件 |
CN107200126A (zh) * | 2017-05-06 | 2017-09-26 | 西安多杰机器人有限公司 | 一种大荷载长航时无人直升机 |
CN108116673A (zh) * | 2017-12-22 | 2018-06-05 | 中国兵器工业计算机应用技术研究所 | 一种共轴双桨直升机桨距操纵系统 |
CN108116673B (zh) * | 2017-12-22 | 2020-06-02 | 中国兵器工业计算机应用技术研究所 | 一种共轴双桨直升机桨距操纵系统 |
CN108216631A (zh) * | 2018-03-07 | 2018-06-29 | 天津曙光天成科技有限公司 | 一种变矩系统及无人多旋翼飞行器 |
CN108791859A (zh) * | 2018-07-12 | 2018-11-13 | 西安君晖航空科技有限公司 | 一种快速抵近的旋翼无人机 |
CN108791859B (zh) * | 2018-07-12 | 2024-02-06 | 西安君晖航空科技有限公司 | 一种快速抵近的旋翼无人机 |
CN111392031A (zh) * | 2020-02-24 | 2020-07-10 | 深圳联合飞机科技有限公司 | 一种旋翼变距装置 |
CN111392031B (zh) * | 2020-02-24 | 2022-05-06 | 深圳联合飞机科技有限公司 | 一种旋翼变距装置 |
Also Published As
Publication number | Publication date |
---|---|
CN104554717B (zh) | 2016-09-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN104554717A (zh) | 旋翼驱动系统 | |
CN201376668Y (zh) | 双层旋翼直升飞机倾斜控制器 | |
CN104139855B (zh) | 一种用于共轴式直升机的航向操纵系统 | |
CN104458197A (zh) | 一种基于平行四边形机构的风洞试验模型支撑机构 | |
CN104552278B (zh) | 一种机器人化螺旋制孔系统 | |
AU2016100487A4 (en) | Rotor driving system | |
CN107161330A (zh) | 一种可变异型结构的变距多旋翼无人机 | |
CN104554719A (zh) | 旋翼驱动方法及装置 | |
AU2016100485A4 (en) | Method and device for driving rotor | |
CN206050067U (zh) | 一种共轴直升机 | |
CN209112440U (zh) | 一种倾转旋翼直升机及其传动装置 | |
CN104802989B (zh) | 一种导轮式滚筒翼推力生成装置 | |
CN106081094A (zh) | 一种共轴直升机 | |
CN206265299U (zh) | 一种共轴直升机操纵机构 | |
CN108706096A (zh) | 一种通过调整旋翼距离控制四旋翼无人机运动的支架 | |
CN204487550U (zh) | 一种机器人化螺旋制孔系统 | |
CN206984336U (zh) | 一种可变翼型结构的变距多旋翼无人机 | |
CN110979656A (zh) | 一种飞行无人机可变旋翼结构 | |
CN104773286A (zh) | 一种机械传动滚筒翼升力生成装置 | |
CN204606202U (zh) | 一种翼尖风球式滚筒翼升力生成装置 | |
CN204979232U (zh) | 电动变桨距多旋翼飞行器 | |
CN109018334A (zh) | 一种倾转旋翼直升机的传动装置 | |
CN216916275U (zh) | 顶部直驱的旋翼装置 | |
CN204642156U (zh) | 一种电动滚筒翼推力生成装置 | |
RU147490U1 (ru) | Соосная несущая система |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C41 | Transfer of patent application or patent right or utility model | ||
TR01 | Transfer of patent right |
Effective date of registration: 20170111 Address after: Futian District Shenzhen City, Guangdong province 518026 Shennan Road No. 1006 Shenzhen International Innovation Center C block 17 layer Patentee after: Shenzhen United Aircraft Technology Co., Ltd. Address before: 100176 Daxing District economic and Technological Development Zone, Yizhuang, East Road, sea road, No. 58, building No. five, building 6, floor 5 Patentee before: Tian Gangyin |
|
PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of invention: Rotor wing driving system Effective date of registration: 20191030 Granted publication date: 20160928 Pledgee: Zhongguancun Beijing technology financing Company limited by guarantee Pledgor: Shenzhen United Aircraft Technology Co., Ltd. Registration number: Y2019990000426 |
|
PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
TR01 | Transfer of patent right |
Effective date of registration: 20200610 Address after: 100176 Beijing Daxing District Beijing Economic and Technological Development Zone, No. 20 Tongjin Road, 1 Building and 1 Floor Patentee after: BEIJING ZHONGHANGZHI TECHNOLOGY Co.,Ltd. Address before: Futian District Shenzhen City, Guangdong province 518026 Shennan Road No. 1006 Shenzhen International Innovation Center C block 17 layer Patentee before: SHENZHEN LIANHE AIRPLANE TECHNOLOGY Co.,Ltd. |
|
TR01 | Transfer of patent right | ||
PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20201019 Granted publication date: 20160928 Pledgee: Zhongguancun Beijing technology financing Company limited by guarantee Pledgor: SHENZHEN LIANHE AIRPLANE TECHNOLOGY Co.,Ltd. Registration number: Y2019990000426 |
|
PC01 | Cancellation of the registration of the contract for pledge of patent right |