CN2882744Y - Fant assembling and disassembling gear for flat vertical tails of model airplane and mini pilotless plane - Google Patents
Fant assembling and disassembling gear for flat vertical tails of model airplane and mini pilotless plane Download PDFInfo
- Publication number
- CN2882744Y CN2882744Y CN 200620018999 CN200620018999U CN2882744Y CN 2882744 Y CN2882744 Y CN 2882744Y CN 200620018999 CN200620018999 CN 200620018999 CN 200620018999 U CN200620018999 U CN 200620018999U CN 2882744 Y CN2882744 Y CN 2882744Y
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- model
- horizontal tail
- vertical fin
- screw pin
- link
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Abstract
A fast assembling and disassembling structure for areomodel and horizontal tail rotor of minisize unmanned aircraft is provided, which can be applied to areomodel and minisize unmanned aircraft. The utility model is characterized in that: a front connecting support and a rear connecting support are positioned in a pin hole at a tail rod of the model body via a set screw of connecting support; a horizontal tail is positioned on the plane at the bottom of the front and rear connecting supports via the set screw of horizontal tail; a longitudinal tail is positioned in the vertical clamping groove of the front and rear connecting supports via the set screw of longitudinal tail. The utility model ensures express and convenient assembly and disassembly of aeromodel or minisize unmanned aircraft, thus bringing much facility for carrying and transportation. Besides, the utility model, with excellent stability and reliability, has the advantages of being able to be carried by single person, simple structure, excellent economy and practicality and no need for maintenance.
Description
Technical field: the utility model relates to a kind of model plane and the quick mounting mechanism of the flat vertical fin wing of micro-unmanned aircraft, and it is applicable on model airplane and the micro-unmanned aircraft.
Background technology: in background technology, the wing of model plane and micro-unmanned aircraft can be taken apart mostly, but flat, vertical fin directly consolidates extremely usually on fuselage, is not easy to carry and transport.For addressing this problem, model plane and the quick mounting mechanism of the flat vertical fin wing of micro-unmanned aircraft are developed.
Summary of the invention: technical problem to be solved in the utility model is that a kind of model plane and the quick mounting mechanism of the flat vertical fin wing of micro-unmanned aircraft will be provided, and it is faster, easy that it can make model plane or MAV dismantle, and is convenient for carrying and transports, simultaneously firmly and reliably.
The technical scheme that its technical problem that solves the utility model adopts is that it comprises fuselage foot piece, horizontal tail vertical fin, preceding link, rear connecting frame, horizontal tail attachment screw pin, link hold-down screw pin and vertical fin attachment screw pin, preceding link and rear connecting frame are installed on the afterbody pin-and-hole of fuselage foot piece by link hold-down screw pin, horizontal tail is installed on the base plane of forward and backward link by horizontal tail attachment screw pin, and vertical fin is installed in the vertical clamping slot of forward and backward link by vertical fin attachment screw pin.
The utility model is compared the beneficial effect that is produced with background technology:
1, because the utility model adopts forward and backward link plane to locate, guarantee relative position flat, vertical fin like this, thereby guaranteed model plane or the original aerodynamic arrangement of MAV, solved the quick distachable problem simultaneously.
2, because the utility model adopts screw pin to connect, reach and be convenient for carrying and transport, and only need carry simple tools and just can finish connection, reach easy, also need not keep in repair, guaranteed the economy and the versatility of mechanism, reliable firm.
Description of drawings: Fig. 1 is a structure chart of the present utility model.
Fig. 2 is the left view of Fig. 1.
The specific embodiment: referring to accompanying drawing 1, accompanying drawing 2, preceding link 2 and rear connecting frame 3 are installed on the afterbody pin-and-hole of fuselage foot piece 1 by link hold-down screw pin 7, horizontal tail 4 is installed in by horizontal tail attachment screw pin 6 on the base plane of forward and backward link 2,3, and vertical fin 5 is installed in the vertical clamping slot of forward and backward link 2,3 by vertical fin attachment screw pin 8.The utility model is installed in model plane and micro-unmanned airplane tail group.
This mechanism can make flat vertical fin separate with body before installing, and back mechanism is installed is fixed on model plane and the micro-unmanned aircraft, guarantees its original aerodynamic arrangement and normal flight.
Claims (1)
1, the quick mounting mechanism of the flat vertical fin wing of a kind of model plane and micro-unmanned aircraft, it comprises fuselage foot piece (1), horizontal tail (4) and vertical fin (5), it is characterized in that also comprising preceding link (2), rear connecting frame (3), horizontal tail attachment screw pin (6), link hold-down screw pin (7) and vertical fin attachment screw pin (8)
Preceding link (2) and rear connecting frame (3) are installed on the afterbody pin-and-hole of fuselage foot piece (1) by link hold-down screw pin (7), horizontal tail (4) is installed in by horizontal tail attachment screw pin (6) on the base plane of forward and backward link (2,3), and vertical fin (5) is installed in the vertical clamping slot of forward and backward link (2,3) by vertical fin attachment screw pin (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620018999 CN2882744Y (en) | 2006-04-05 | 2006-04-05 | Fant assembling and disassembling gear for flat vertical tails of model airplane and mini pilotless plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620018999 CN2882744Y (en) | 2006-04-05 | 2006-04-05 | Fant assembling and disassembling gear for flat vertical tails of model airplane and mini pilotless plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2882744Y true CN2882744Y (en) | 2007-03-28 |
Family
ID=37955805
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200620018999 Expired - Fee Related CN2882744Y (en) | 2006-04-05 | 2006-04-05 | Fant assembling and disassembling gear for flat vertical tails of model airplane and mini pilotless plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2882744Y (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101462596B (en) * | 2009-01-12 | 2011-05-04 | 北京航空航天大学 | Tail wing connection structure suitable for small-sized unmanned plane with tailboom |
| CN104771913A (en) * | 2015-04-22 | 2015-07-15 | 鹿寨县初级实验中学 | Remote control model airplane |
| CN105882941A (en) * | 2014-12-31 | 2016-08-24 | 航天神舟飞行器有限公司 | Rapid connector for vertical tail and horizontal tail of small portable unmanned aerial vehicle |
| CN109808870A (en) * | 2019-04-01 | 2019-05-28 | 西北工业大学 | A kind of fast assembling disassembling structure of the vertical horizontal tail connection of unmanned plane |
-
2006
- 2006-04-05 CN CN 200620018999 patent/CN2882744Y/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101462596B (en) * | 2009-01-12 | 2011-05-04 | 北京航空航天大学 | Tail wing connection structure suitable for small-sized unmanned plane with tailboom |
| CN105882941A (en) * | 2014-12-31 | 2016-08-24 | 航天神舟飞行器有限公司 | Rapid connector for vertical tail and horizontal tail of small portable unmanned aerial vehicle |
| CN104771913A (en) * | 2015-04-22 | 2015-07-15 | 鹿寨县初级实验中学 | Remote control model airplane |
| CN109808870A (en) * | 2019-04-01 | 2019-05-28 | 西北工业大学 | A kind of fast assembling disassembling structure of the vertical horizontal tail connection of unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee |
Owner name: JIANGNAN INDUSTRIES GROUP CO., LTD. Free format text: FORMER NAME: JIANGNAN MACHINERY (GROUP) CO., LTD. |
|
| CP03 | Change of name, title or address |
Address after: Bamboo town Yuhu District 411207 Hunan city of Xiangtan Province Patentee after: Jiangnan Industries Group Co., Ltd. Address before: 411207 Hunan city of Xiangtan Province bamboo Patentee before: Jiangnan Machinery (Group) Co., Ltd. |
|
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20070328 Termination date: 20140405 |