CN205098461U - Novel unmanned aerial vehicle fin folding mechanism - Google Patents
Novel unmanned aerial vehicle fin folding mechanism Download PDFInfo
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- CN205098461U CN205098461U CN201520921263.6U CN201520921263U CN205098461U CN 205098461 U CN205098461 U CN 205098461U CN 201520921263 U CN201520921263 U CN 201520921263U CN 205098461 U CN205098461 U CN 205098461U
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- fuselage
- aerial vehicle
- unmanned aerial
- elastic component
- empennage
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- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims description 3
- 238000000034 method Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
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Abstract
The utility model discloses a novel unmanned aerial vehicle fin folding mechanism, including the connecting piece, the connecting piece passes through the screw thread and links to each other with the fuselage, the fin is installed to the left end of fuselage, and the fin passes through elastic component and fuselage and link to each other, the elastic component links to each other with the shop bolt. This novel unmanned aerial vehicle fin folding mechanism through set up elastic component, connecting piece and shop bolt on the fuselage, can make unmanned aerial vehicle under fold condition, and convenient to carry saves space, reaches through rapid expansion of wing during the use and satisfies unmanned aerial vehicle running state.
Description
Technical field
The utility model relates to unmanned air vehicle technique field, is specially a kind of novel unmanned airplane empennage fold mechanism.
Background technology
Robot airplane is called for short " unmanned plane ", is the not manned aircraft utilizing radio robot to handle with the process controller provided for oneself.Without driving compartment on machine, but the equipment such as autopilot, process controller is installed.On ground, naval vessels or machine tool command and control station personnel by equipment such as radars, it is followed the tracks of, locates, remote control, remote measurement and digital communication.Can take off as conventional airplane under radio telecommand or launch with booster rocket, also can be taken to by machine tool and throw in flight in the air.During recovery, the available mode automatic Landing the same with conventional airplane landing mission, also reclaims by remote control parachute or block.
But existing unmanned plane carries not to be put just, wasting space, we need a kind of novel unmanned plane for this reason cannot to launch rapidly to reach the state of operation time practical.
Utility model content
The purpose of this utility model is to provide a kind of novel unmanned airplane empennage fold mechanism, to solve the problem proposed in above-mentioned background technology.
For achieving the above object, the utility model provides following technical scheme: a kind of novel unmanned airplane empennage fold mechanism, comprise attaching parts, described attaching parts is connected with fuselage by screw thread, the rear end of described fuselage is provided with empennage, and empennage is connected with fuselage by elastic component, described elastic component is connected with tommy.
Preferably, described elastic component is spring structure.
Preferably, described attaching parts is aluminum alloy material.
Preferably, described empennage has two at least.
Compared with prior art, the beneficial effects of the utility model are: this novel unmanned airplane empennage fold mechanism, by arranging elastic component, attaching parts and tommy on fuselage, unmanned plane can be made in a folded configuration, easy to carry, save space, launched rapidly by wing during use and reach and meet unmanned plane running state.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation;
Fig. 2 is part structure for amplifying schematic diagram of the present utility model.
In figure: 1, elastic component, 2, attaching parts, 3, tommy, 4, fuselage, 5, empennage.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
Refer to Fig. 1-2, the utility model provides a kind of technical scheme: a kind of novel unmanned airplane empennage fold mechanism, comprise attaching parts 2, described attaching parts 2 is connected with fuselage 4 by screw thread, and described attaching parts 2 is aluminum alloy material, and the right side of described fuselage 4 is provided with empennage 5, described empennage 5 has two, and empennage 5 is connected with fuselage 5 by elastic component 1, described elastic component 1 is spring structure, and described elastic component 1 is connected with fuselage 4.
Working process: first attaching parts 2 is connected with fuselage 4 by screw thread, under the effect of elastic component 1, empennage 5 is in and fuselage 4 parastate, now tommy 3 is compressed to fuselage interior due to the effect of its contained spring, when fuselage 4 due to the spring return of spring to shown position time, tommy 3 ejects by tommy 3 inner spring, and empennage 5 is positioned at this position, ensure at unmanned plane in flight course, empennage is fixed on this position.
Although illustrate and described embodiment of the present utility model, for the ordinary skill in the art, be appreciated that and can carry out multiple change, amendment, replacement and modification to these embodiments when not departing from principle of the present utility model and spirit, scope of the present utility model is by claims and equivalents thereof.
Claims (4)
1. a novel unmanned airplane empennage fold mechanism, is characterized in that: comprise attaching parts, and described attaching parts is connected with fuselage by screw thread, and the rear end of described fuselage is provided with empennage, and empennage is connected with fuselage by elastic component, and described elastic component is connected with tommy.
2. the novel unmanned airplane empennage fold mechanism of one according to claim 1, is characterized in that: described elastic component is spring structure.
3. the novel unmanned airplane empennage fold mechanism of one according to claim 1, is characterized in that: described attaching parts is aluminum alloy material.
4. the novel unmanned airplane empennage fold mechanism of one according to claim 1, is characterized in that: described empennage has two at least.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520921263.6U CN205098461U (en) | 2015-11-18 | 2015-11-18 | Novel unmanned aerial vehicle fin folding mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520921263.6U CN205098461U (en) | 2015-11-18 | 2015-11-18 | Novel unmanned aerial vehicle fin folding mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205098461U true CN205098461U (en) | 2016-03-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520921263.6U Active CN205098461U (en) | 2015-11-18 | 2015-11-18 | Novel unmanned aerial vehicle fin folding mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205098461U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111942572A (en) * | 2020-09-21 | 2020-11-17 | 中国工程物理研究院总体工程研究所 | Side single vertical tail flying patrol device with vertical tail unfolding device |
-
2015
- 2015-11-18 CN CN201520921263.6U patent/CN205098461U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111942572A (en) * | 2020-09-21 | 2020-11-17 | 中国工程物理研究院总体工程研究所 | Side single vertical tail flying patrol device with vertical tail unfolding device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Novel unmanned aerial vehicle fin folding mechanism Effective date of registration: 20190117 Granted publication date: 20160323 Pledgee: Shaanxi Changan financing guarantee Limited by Share Ltd. Pledgor: SHAANXI ZHONGKE BOYI ELECTRONIC TECHNOLOGY Co.,Ltd. Registration number: 2019610000013 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Granted publication date: 20160323 Pledgee: Shaanxi Changan financing guarantee Limited by Share Ltd. Pledgor: SHAANXI ZHONGKE BOYI ELECTRONIC TECHNOLOGY Co.,Ltd. Registration number: 2019610000013 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right |