CN204937508U - A kind of unmanned plane - Google Patents
A kind of unmanned plane Download PDFInfo
- Publication number
- CN204937508U CN204937508U CN201520701054.0U CN201520701054U CN204937508U CN 204937508 U CN204937508 U CN 204937508U CN 201520701054 U CN201520701054 U CN 201520701054U CN 204937508 U CN204937508 U CN 204937508U
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- China
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- upper plate
- frame
- lower plate
- main body
- unmanned plane
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Abstract
The utility model provides a kind of unmanned plane, comprises a support, and one is arranged at the main body on support and is arranged at the some rotors in main body, and the housing parts of described main body comprises: a lower plate; One upper plate, described upper plate is connected to described lower plate; Frame, described frame is longitudinally arranged at the surrounding that described upper plate and lower plate connect, in the top of the corresponding described frame of surrounding of described upper plate and lower plate and be provided with frame mounting groove below; The middle part of described upper plate arranges a battery cover board; Described lower plate, upper plate and described frame are connected to form a main body cover closed.Have base portion sealing effect good, effectively can alleviate fuselage weight, can effectively avoid in-flight because vibrations occur that snap close is thrown off and the advantage of the aspect such as to meet accident simultaneously.
Description
Technical field
The utility model relates to a kind of unmanned plane, particularly relates to a kind of structure of unmanned plane.
Background technology
China is as large agricultural country, and 1,800,000,000 mu of basic farmlands, the agricultural plant protection operation that annual needs are a large amount of, the annual pesticide poisoning number of China has the crowd of 100,000, fatal rate about 20%.Residues of pesticides and pollute the number of dying of illness that causes and there is no official statistics so far, probably a surprising numeral especially.
Unmanned plane serving agriculture is developed rapidly in developed countries such as Japan, the U.S..Nineteen ninety, Japanese Shan Ye company takes the lead in releasing first unmanned plane in the world, is mainly used in spraying insecticide.First south China is applied to the pesticide spraying of paddy fields.
Unmanned plane; it is the robot airplane for comprising agriculture and forestry plant protection operation; this type unmanned aerial vehicle has flying platform (fixed-wing, single rotor, many rotors), GPS flies the part compositions such as control; control is flown by ground remote control or GPS; realize application target; as spraying operation, can spraying agent, seed, pulvis etc.
It is non-enclosed that the unmanned plane of prior art exists main control part, and corrosive property agricultural chemicals water smoke etc. easily enters main control part, can damage flight control system; Aloft vibrations can cause the folding snap close of unmanned plane to loosen, and occur the deficiency of the aspect such as folding problem under horn.
Summary of the invention
The main control part existed in view of unmanned plane in prior art is non-enclosed, and corrosive property agricultural chemicals water smoke easily enters main control part, can damage flight control system; Aloft vibrations can cause the folding snap close of unmanned plane to loosen, and occur the deficiency of the aspect such as folding problem under horn.The purpose of this utility model be to provide one have main control part sealing effect good, effectively can alleviate fuselage weight, can effectively avoid in-flight because vibrations occur that snap close is thrown off and the unmanned plane of the aspect advantage such as to meet accident simultaneously.
For realizing above-mentioned purpose of the present utility model, the utility model provides a kind of unmanned plane, comprises a support, and one is arranged at the main body on support and is arranged at the some rotors in main body, and the housing parts of described main body comprises: a lower plate; One upper plate, described upper plate is connected to described lower plate; Frame, described frame is longitudinally arranged at the surrounding that described upper plate and lower plate connect, in the top of the corresponding described frame of surrounding of described upper plate and lower plate and be provided with frame mounting groove below; The middle part of described upper plate arranges a battery cover board; Described lower plate, upper plate and described frame are connected to form a main body cover closed.
According to above-mentioned design of the present utility model, the top of described frame and below on be provided with and protrude from described top and following jut, the frame mounting groove in described upper plate and lower plate is the through hole of corresponding described top and following jut.
According to above-mentioned design of the present utility model, the top of described frame and below on the equidistant or Unequal distance of jut arrange.
According to above-mentioned design of the present utility model, described rotor is fixed in main body respectively by a folding snap close and elasticity bead.
According to above-mentioned design of the present utility model, described frame is stack pile carbon fiber board frame.
According to above-mentioned design of the present utility model, described rotor is four.
Advantage of the present utility model and beneficial effect are: have base portion sealing effect good, effectively can alleviate fuselage weight, can effectively avoid in-flight because vibrations occur that snap close is thrown off and the advantage of the aspect such as to meet accident simultaneously.
Accompanying drawing explanation
The perspective view of Fig. 1 a kind of unmanned plane of the present utility model.
The decomposition texture schematic diagram of Fig. 2 a kind of unmanned plane of the present utility model.
Detailed description of the invention
In order to further illustrate principle of the present utility model and structure, now by reference to the accompanying drawings preferred embodiment of the present utility model is described in detail, but described embodiment is only the use providing and illustrate with explanation, can not be used for limiting scope of patent protection of the present utility model.
As shown in Figures 1 and 2 be a kind of unmanned plane of the present utility model, comprise some rotors 3 that a support 1, is arranged at the main body 2 on support 1 and is arranged in main body 2, the housing parts of described main body 2 comprises: a lower plate 21; One upper plate 22, described upper plate 22 is connected to described lower plate 21; Frame 23, described frame 23 is longitudinally arranged at the surrounding that described upper plate 22 and lower plate 21 connect, in the top of the corresponding described frame 23 of surrounding of described upper plate 22 and lower plate 21 and be provided with frame mounting groove 4 below; The middle part of described upper plate 22 arranges a battery cover board 221; Described lower plate 21, upper plate 22 and described frame 23 are connected to form main body 2 shell closed.
According to above-mentioned design of the present utility model, the top of described frame 23 and below on be provided with and protrude from described top and following jut 231, the frame mounting groove 4 in described upper plate and lower plate is the through hole of corresponding described top and following jut.
According to above-mentioned design of the present utility model, the top of described frame 23 and below on the equidistant or Unequal distance of jut 231 arrange.
According to above-mentioned design of the present utility model, described rotor 3 is fixed in main body 2 respectively by a folding snap close 5 and elasticity bead 6.
According to above-mentioned design of the present utility model, described frame 23 is stack pile carbon fiber board frame.
According to above-mentioned design of the present utility model, described rotor 3 is four.
Advantage of the present utility model and beneficial effect are: have base portion sealing effect good, effectively can alleviate fuselage weight, can effectively avoid in-flight because vibrations occur that snap close is thrown off and the advantage of the aspect such as to meet accident simultaneously.
The variant that foregoing is only preferred embodiment of the present utility model and exemplifies; be not used for limiting the utility model; every within spirit of the present utility model and principle; done any need not the amendment of creative thinking and improvement, all should be included within protection domain of the present utility model.
Claims (6)
1. a unmanned plane, comprises a support, and one is arranged at the main body on support and is arranged at the some rotors in main body, it is characterized in that:
The housing parts of described main body comprises:
One lower plate;
One upper plate, described upper plate is connected to described lower plate;
Frame, described frame is longitudinally arranged at the surrounding that described upper plate and lower plate connect, in the top of the corresponding described frame of surrounding of described upper plate and lower plate and be provided with frame mounting groove below;
The middle part of described upper plate arranges a battery cover board;
Described lower plate, upper plate and described frame are connected to form a main body cover closed.
2. a kind of unmanned plane according to claim 1, is characterized in that:
The top of described frame and below on be provided with and protrude from described top and following jut, the frame mounting groove in described upper plate and lower plate is the through hole of corresponding described top and following jut.
3. a kind of unmanned plane according to claim 2, is characterized in that:
The top of described frame and below on the equidistant or Unequal distance of jut arrange.
4. a kind of unmanned plane according to claim 1, is characterized in that:
Described rotor is fixed in main body respectively by a folding snap close and elasticity bead.
5. a kind of unmanned plane according to claim 1, is characterized in that:
Described frame is stack pile carbon fiber board frame.
6. a kind of unmanned plane according to claim 1, is characterized in that:
Described rotor is four.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520701054.0U CN204937508U (en) | 2015-09-11 | 2015-09-11 | A kind of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520701054.0U CN204937508U (en) | 2015-09-11 | 2015-09-11 | A kind of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204937508U true CN204937508U (en) | 2016-01-06 |
Family
ID=55004953
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520701054.0U Expired - Fee Related CN204937508U (en) | 2015-09-11 | 2015-09-11 | A kind of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204937508U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106428622A (en) * | 2016-11-08 | 2017-02-22 | 芜湖万户航空航天科技有限公司 | Method for fixing body upper plate of helicopter |
| CN106741825A (en) * | 2016-11-21 | 2017-05-31 | 西安三翼航空科技有限公司 | A kind of six rotor unmanned aircrafts |
| WO2017185487A1 (en) * | 2016-04-28 | 2017-11-02 | 深圳市龙云创新航空科技有限公司 | Battery fixing and mounting structure for battery self-dismounting unmanned aerial vehicle |
| CN108177780A (en) * | 2018-02-09 | 2018-06-19 | 广东莱盛隆电子股份有限公司 | A kind of strong plant protection unmanned plane of stability |
| CN109927875A (en) * | 2019-04-08 | 2019-06-25 | 武夷学院 | A kind of aircraft frame |
-
2015
- 2015-09-11 CN CN201520701054.0U patent/CN204937508U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017185487A1 (en) * | 2016-04-28 | 2017-11-02 | 深圳市龙云创新航空科技有限公司 | Battery fixing and mounting structure for battery self-dismounting unmanned aerial vehicle |
| CN106428622A (en) * | 2016-11-08 | 2017-02-22 | 芜湖万户航空航天科技有限公司 | Method for fixing body upper plate of helicopter |
| CN106741825A (en) * | 2016-11-21 | 2017-05-31 | 西安三翼航空科技有限公司 | A kind of six rotor unmanned aircrafts |
| CN108177780A (en) * | 2018-02-09 | 2018-06-19 | 广东莱盛隆电子股份有限公司 | A kind of strong plant protection unmanned plane of stability |
| CN109927875A (en) * | 2019-04-08 | 2019-06-25 | 武夷学院 | A kind of aircraft frame |
| CN109927875B (en) * | 2019-04-08 | 2023-12-15 | 武夷学院 | Aircraft frame |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 523932 Guangdong province Dongguan city Humen town gate five MINCHANG road two Lane 5 Patentee after: Guangdong Li Ding long Power Technology Co Ltd Address before: 523932 Guangdong province Dongguan city Humen town gate five MINCHANG road two Lane 5 Patentee before: Five metals plasthetics Co., Ltd of Dongguan City auspicious section |
|
| CP01 | Change in the name or title of a patent holder | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160106 Termination date: 20190911 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |