CN106458313A - 航模机及其舵机组装结构 - Google Patents
航模机及其舵机组装结构 Download PDFInfo
- Publication number
- CN106458313A CN106458313A CN201480001179.0A CN201480001179A CN106458313A CN 106458313 A CN106458313 A CN 106458313A CN 201480001179 A CN201480001179 A CN 201480001179A CN 106458313 A CN106458313 A CN 106458313A
- Authority
- CN
- China
- Prior art keywords
- steering engine
- bracket
- screw holes
- fixedly connected
- assembly structure
- 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
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Classifications
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
Abstract
一种舵机组装结构,设置在碳管(10)与电机系统(30)之间,包括第一支架(41)、金属轴(43)、管夹(45)、第二支架(47)以及舵机(49);所述第一支架(41)与电机系统(30)固定连接,并用于固定所述金属轴(43),所述管夹(45)套设在所述金属轴(43)外,所述第二支架(47)同时与所述管夹(45)、所述舵机(49)以及所述第一支架(41)固定连接,用于收容且固定所述舵机(49),所述舵机(49)同时与所述第一支架(41)固定连接。通过在航模上采用上述舵机组装结构,使舵机系统无需占用额外的体积,并且,当航模机快速降落时,第二支架受到的冲击力直接传导到碳管上,而不会传导到金属轴上,降低了舵机主体受到外力损坏的可能性。
Description
PCT国内申请,说明书已公开。
Claims (10)
- PCT国内申请,权利要求书已公开。
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/CN2014/089572 WO2016065509A1 (zh) | 2014-10-27 | 2014-10-27 | 航模机及其舵机组装结构 |
Publications (1)
Publication Number | Publication Date |
---|---|
CN106458313A true CN106458313A (zh) | 2017-02-22 |
Family
ID=55856334
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201480001179.0A Pending CN106458313A (zh) | 2014-10-27 | 2014-10-27 | 航模机及其舵机组装结构 |
Country Status (2)
Country | Link |
---|---|
CN (1) | CN106458313A (zh) |
WO (1) | WO2016065509A1 (zh) |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2208962Y (zh) * | 1994-07-04 | 1995-10-04 | 邹声通 | 航模直升飞机 |
DE29906737U1 (de) * | 1999-04-15 | 1999-08-12 | Streich Uli | Modellhubschrauber |
CN1631733A (zh) * | 2003-12-22 | 2005-06-29 | 上海雏鹰科技有限公司 | 超视距自主飞行无人驾驶直升机系统 |
TWM278461U (en) * | 2005-05-26 | 2005-10-21 | Jian-Jau Chen | Improved server fixing base structure of remote control helicopter |
CN2759542Y (zh) * | 2005-01-24 | 2006-02-22 | 罗之洪 | 电动玩具直升机 |
CN2790551Y (zh) * | 2005-04-15 | 2006-06-28 | 罗之洪 | 电动玩具直升机 |
CN2882743Y (zh) * | 2006-01-23 | 2007-03-28 | 罗之洪 | 航模 |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3008347B1 (ja) * | 1998-08-18 | 2000-02-14 | 京商株式会社 | ヘリコプター玩具のエルロン用サーボ取付構造 |
CN2889424Y (zh) * | 2006-04-10 | 2007-04-18 | 罗之洪 | 航模的主体架组件 |
CN200957295Y (zh) * | 2006-06-28 | 2007-10-10 | 罗之洪 | 航模的转向机构组件 |
CN201253490Y (zh) * | 2008-09-16 | 2009-06-10 | 四川中邦模具有限公司 | 无线电遥控模型飞机的伺服系统多配件综合支架 |
CN203666975U (zh) * | 2013-11-30 | 2014-06-25 | 淮北市天路航空科技股份有限公司 | 一种无人机舵机安装固定装置 |
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2014
- 2014-10-27 WO PCT/CN2014/089572 patent/WO2016065509A1/zh active Application Filing
- 2014-10-27 CN CN201480001179.0A patent/CN106458313A/zh active Pending
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2208962Y (zh) * | 1994-07-04 | 1995-10-04 | 邹声通 | 航模直升飞机 |
DE29906737U1 (de) * | 1999-04-15 | 1999-08-12 | Streich Uli | Modellhubschrauber |
CN1631733A (zh) * | 2003-12-22 | 2005-06-29 | 上海雏鹰科技有限公司 | 超视距自主飞行无人驾驶直升机系统 |
CN2759542Y (zh) * | 2005-01-24 | 2006-02-22 | 罗之洪 | 电动玩具直升机 |
CN2790551Y (zh) * | 2005-04-15 | 2006-06-28 | 罗之洪 | 电动玩具直升机 |
TWM278461U (en) * | 2005-05-26 | 2005-10-21 | Jian-Jau Chen | Improved server fixing base structure of remote control helicopter |
CN2882743Y (zh) * | 2006-01-23 | 2007-03-28 | 罗之洪 | 航模 |
Also Published As
Publication number | Publication date |
---|---|
WO2016065509A1 (zh) | 2016-05-06 |
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WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170222 |
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WD01 | Invention patent application deemed withdrawn after publication |