CN201163658Y - Antenna apparatus of simulated aeromodelling airplane - Google Patents
Antenna apparatus of simulated aeromodelling airplane Download PDFInfo
- Publication number
- CN201163658Y CN201163658Y CNU2008200893463U CN200820089346U CN201163658Y CN 201163658 Y CN201163658 Y CN 201163658Y CN U2008200893463 U CNU2008200893463 U CN U2008200893463U CN 200820089346 U CN200820089346 U CN 200820089346U CN 201163658 Y CN201163658 Y CN 201163658Y
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- Prior art keywords
- built
- socket
- antenna
- aerial
- airplane
- Prior art date
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- Expired - Fee Related
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Abstract
The utility model provides an emulational aeromodelling airplane antenna device, belonging to an aeromodelling aerocraft for sports and recreation. The emulational aeromodelling airplane antenna device has a structure as follows: a built-in antenna is arranged inside an airplane body, a socket is fixedly arranged on the tarl end of the airplane body or the upper part on the tail end of an airvane, the rear end of the built-in antenna is fixed with the socket, a plug is arranged on one terminal of an external antenna, the plug is inserted on the socket, and the built-in antenna is connected with the external antenna. The device has the advantages of reasonable configuration, simple structure, long service life and convenient transportation and storage, and favarability for the protection and the beautiful appearance of the aeromodelling airplane antenna.
Description
Technical field
The utility model belongs to sports and amusement model plane aircraft, relates generally to the receiving antenna device of simulated model airplane.
Background technology
Its flight control reception antenna of present aeromodelling airplane all is to be made of an antenna integral type, the reception antenna of aeromodelling airplane afterbody all exposes at fuselage outer side, lower for general performance, cheap this structure of plain edition aeromodelling airplane is still applicable, but it is higher for performance, the simulated model airplane that price is more expensive, such configuration structure is not only not attractive in appearance, and use and take care of the damage that very easily causes model plane and reception antenna when depositing in flight, reduced aeromodelling airplane useful life, I am at the utility model patent of application in 2007, see that application number is that " No. 200720115677.5 simulated model airplane antenna assemblies " weak point is only suitable and is useful for direction wing tail end, define the scope of application.
Summary of the invention
The purpose of this utility model is exactly the problem that exists at above-mentioned prior art, design provides a kind of simulated model airplane antenna assembly of separate assembling reception antenna, reaches raising simulated model airplane sight and reserve value, has avoided causing the aeromodelling airplane damage, reached safe handling and taking care of purpose easily because of the damage of reception antenna.
Basic design of the present utility model is, disposes the installation built-in aerial from front to back in fuselage interior, and two sockets are fitted over back body and direction wing top tail end admittedly, selective use, and built-in aerial rear end and two sockets are affixed; Equipped plug on a termination of external antenna, on the plug inserting socket therein, built-in aerial and external antenna are connected, and so far constitute the simulated model airplane antenna assembly.The utility model is simple in structure, and is easy to use, and increased substantially the overall aesthetics and the reserve value of simulated model airplane, reduces and avoided the damage of model plane and reception antenna, prolonged the useful life of aeromodelling airplane.
Description of drawings
Accompanying drawing is a simulated model airplane antenna device arrangement schematic diagram.
Piece number explanation among the figure:
1, external antenna, 2, plug, 3, socket
1, 4, break, 6, built-in aerial, 7, fuselage, 8, the direction wing, 9, socket on break, 5, the built-in aerial behind the built-in aerial
2
Embodiment
Below in conjunction with accompanying drawing the utility model optimum implementation is described in detail.The simulated model airplane antenna assembly comprises fuselage 7, the direction wing 8, disposes from front to back in fuselage 7 inside built-in aerial 6, socket are installed
13 fit on the direction wing 8 afterbody upper ends socket admittedly
29 fit on fuselage 7 tail ends admittedly, built-in aerial 6 rear ends respectively with socket
13 affixed and sockets
29 is affixed; Equipped plug 2 on a termination of external antenna 1, plug 2 insertings are at socket
1On 3 or inserting at socket
2On 9, built-in aerial 6 is connected with external antenna 1.At built-in aerial 6 and socket
13 rear lateral portion when affixed are provided with on the built-in aerial break 4 behind the break 5 and built-in aerial.Built-in aerial 6 front ends are connected with receiver.
During flight, radio remote-controlled signal is received by external antenna 1 and built-in aerial 6 after plug 2, socket
13 or socket
29, built-in aerial 6 enters in the receiver, receiver control aeromodelling airplane flight attitude.Transportation and when preserving, with plug 2 from socket
1On 3 or socket
2Pull up on 9, external antenna 1 is separated with aeromodelling airplane, reduce the complete machine scope that takes up space, help depositing, and avoid the damage of model plane and reception antenna.
Claims (2)
1, a kind of simulated model airplane antenna assembly comprises fuselage (7), the direction wing (8), it is characterized in that disposing from front to back in fuselage (7) inside built-in aerial (6), socket be installed
1(3) fit on the direction wing (8) the afterbody upper end socket admittedly
2(9) fit over the tail end of fuselage (7) admittedly, built-in aerial (6) rear end and socket
1(3) and socket
2(9) affixed; Equipped plug (2) on a termination of external antenna (1), plug (2) inserting is at socket
1(3) go up or inserting at socket
2(9) on, built-in aerial (6) is connected with external antenna (1).
2, simulated model airplane antenna assembly according to claim 1, built-in aerial (6) rear end and socket
1(3) affixed, it is characterized in that break (4) after being provided with break on the built-in aerial (5) and built-in aerial on the rear lateral portion of built-in aerial (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008200893463U CN201163658Y (en) | 2008-03-03 | 2008-03-03 | Antenna apparatus of simulated aeromodelling airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008200893463U CN201163658Y (en) | 2008-03-03 | 2008-03-03 | Antenna apparatus of simulated aeromodelling airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201163658Y true CN201163658Y (en) | 2008-12-10 |
Family
ID=40184586
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008200893463U Expired - Fee Related CN201163658Y (en) | 2008-03-03 | 2008-03-03 | Antenna apparatus of simulated aeromodelling airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201163658Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106797070A (en) * | 2016-09-27 | 2017-05-31 | 深圳市大疆创新科技有限公司 | Movable fixture |
| RU2810828C1 (en) * | 2023-05-05 | 2023-12-28 | Публичное акционерное общество "Объединенная авиастроительная корпорация" (ПАО "ОАК") | Method for reducing radar signature of aircraft antennas |
-
2008
- 2008-03-03 CN CNU2008200893463U patent/CN201163658Y/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106797070A (en) * | 2016-09-27 | 2017-05-31 | 深圳市大疆创新科技有限公司 | Movable fixture |
| WO2018058329A1 (en) * | 2016-09-27 | 2018-04-05 | 深圳市大疆创新科技有限公司 | Mobile device |
| CN106797070B (en) * | 2016-09-27 | 2020-03-27 | 深圳市大疆创新科技有限公司 | Movable device |
| US11171413B2 (en) | 2016-09-27 | 2021-11-09 | SZ DJI Technology Co., Ltd. | Movable device |
| RU2810828C1 (en) * | 2023-05-05 | 2023-12-28 | Публичное акционерное общество "Объединенная авиастроительная корпорация" (ПАО "ОАК") | Method for reducing radar signature of aircraft antennas |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20081210 Termination date: 20110303 |