CN202499276U - Electric flying platform - Google Patents
Electric flying platform Download PDFInfo
- Publication number
- CN202499276U CN202499276U CN2012200618335U CN201220061833U CN202499276U CN 202499276 U CN202499276 U CN 202499276U CN 2012200618335 U CN2012200618335 U CN 2012200618335U CN 201220061833 U CN201220061833 U CN 201220061833U CN 202499276 U CN202499276 U CN 202499276U
- Authority
- CN
- China
- Prior art keywords
- flying platform
- contained
- rotor
- fuselage
- empennage
- 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.)
- Expired - Fee Related
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- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
The utility model provides an electric flying platform which mainly comprises a body, a rotor, an undercarriage, a tail gear and a tail assembly. The rotor is mounted on a rotating shaft extending out of the upper portion of the body. The undercarriage is disposed below the body. The tail gear is mounted at the rear of the body through a tail pipe. The tail assembly is mounted on a rotating shaft of the tail gear. The electric flying platform is characterized in that the rotating shaft for mounting the rotor is driven by a motor mounted inside the body through a gearbox. The electric flying platform has the advantages that photography is effective because of low overall vibration, mechanical fatigue of parts of the electric flying platform is reduced, and the electric flying platform without ailerons is simple in structure and convenient to maintain.
Description
Technical field
The utility model relates to RC Goblin.
Background technology
It is power that existing flying platform---RC Goblin adopts oil-burning machine as transport plane, and its shortcoming is that vibrations are big, is not suitable for take photo by plane one type the task of picture of carrying out.
Summary of the invention
The purpose of the utility model is to provide a kind of RC Goblin---flying platform of extremely slight vibrations.
The utility model provides a kind of electronic flying platform; Mainly comprise fuselage, rotor, alighting gear, coda wave case and empennage; Rotor is contained on the S. A. that stretches out back, and alighting gear places the fuselage below, and the coda wave case is contained in the rear of fuselage through tail pipe; Empennage is contained on the S. A. of coda wave case, it is characterized in that: the S. A. that rotor is adorned is to be driven through change speed gear box by the electrical motor that is contained in the fuselage.The employing electrical motor is a power, reduces the integral body vibrations of flying platform, strengthens photographic effects, reduces the mechanical fatigue of parts simultaneously.
The electronic flying platform that the utility model provides, its electrical motor can drive change speed gear box through synchronous band, adopts synchronous band can filter out the vibrations that motor causes.
The electronic flying platform that the utility model provides, the S. A. that its empennage is adorned can be by being contained in electric motor driven in the coda wave case, to reduce the kinetic equation loss in the mechanical transfer process.
The electronic flying platform that the utility model provides, its advantage is: whole vibrations are little, and photographic effects is good; Reduce the mechanical fatigue of parts; No aileron, simple in structure, be convenient to safeguard.
Description of drawings
Fig. 1 is the structural representation of electronic flying platform.
The specific embodiment
Embodiment 1
A kind of electronic flying platform, its structure is as shown in Figure 1, comprises fuselage 4, rotor (not shown), alighting gear 3, coda wave case 8 and empennage (not shown); Rotor is contained on the S. A. 1 that stretches out fuselage 4 tops, and alighting gear 3 places fuselage 4 belows, and coda wave case 8 is contained in the rear of fuselage 4 through tail pipe 7 and shoe bar 6; Empennage is contained on the S. A. of coda wave case 8; The S. A. 1 that rotor is adorned is to be driven through oil immersed type change speed gear box 5 by the high-power brushless electrical motor that is contained in 4 li on fuselage 2, and high-power brushless electrical motor 2 drives oil immersed type change speed gear box 5 through being with synchronously, and ring gear adopts the POM self-lubricating material in the oil immersed type change speed gear box 5; The S. A. that empennage is adorned is by the direct motor drive that is contained in 8 li in coda wave case; Fuselage 4 is connected the two push-and-pull tail displacement assemblies of employing with coda wave case 8, to reduce structure interval, improve tail displacement precision.
Claims (4)
1. electronic flying platform; Mainly comprise fuselage, rotor, alighting gear, coda wave case and empennage; Rotor is contained on the S. A. that stretches out back, and alighting gear places the fuselage below, and the coda wave case is contained in the rear of fuselage through tail pipe; Empennage is contained on the S. A. of coda wave case, it is characterized in that: the S. A. that rotor is adorned is to be driven through change speed gear box by the electrical motor that is contained in the fuselage.
2. according to the described electronic flying platform of claim 1, it is characterized in that: said electrical motor drives change speed gear box through synchronous band.
3. according to the described electronic flying platform of claim 1, it is characterized in that: the S. A. that said empennage is adorned is by being contained in electric motor driven in the coda wave case.
4. according to the described electronic flying platform of claim 2, it is characterized in that: the S. A. that said empennage is adorned is by being contained in electric motor driven in the coda wave case.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012200618335U CN202499276U (en) | 2012-02-24 | 2012-02-24 | Electric flying platform |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012200618335U CN202499276U (en) | 2012-02-24 | 2012-02-24 | Electric flying platform |
Publications (1)
Publication Number | Publication Date |
---|---|
CN202499276U true CN202499276U (en) | 2012-10-24 |
Family
ID=47035899
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2012200618335U Expired - Fee Related CN202499276U (en) | 2012-02-24 | 2012-02-24 | Electric flying platform |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN202499276U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103192992A (en) * | 2013-04-03 | 2013-07-10 | 无锡汉和航空技术有限公司 | Dynamic structure and application method of electric mini unmanned helicopter |
CN103523199A (en) * | 2013-09-29 | 2014-01-22 | 郭献民 | Novel tubular-structure electric unmanned helicopter |
-
2012
- 2012-02-24 CN CN2012200618335U patent/CN202499276U/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103192992A (en) * | 2013-04-03 | 2013-07-10 | 无锡汉和航空技术有限公司 | Dynamic structure and application method of electric mini unmanned helicopter |
CN103523199A (en) * | 2013-09-29 | 2014-01-22 | 郭献民 | Novel tubular-structure electric unmanned helicopter |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20121024 Termination date: 20190224 |
|
CF01 | Termination of patent right due to non-payment of annual fee |