CN204297114U - A kind of can high-altitude location four-axle aircraft - Google Patents
A kind of can high-altitude location four-axle aircraft Download PDFInfo
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- CN204297114U CN204297114U CN201420755175.9U CN201420755175U CN204297114U CN 204297114 U CN204297114 U CN 204297114U CN 201420755175 U CN201420755175 U CN 201420755175U CN 204297114 U CN204297114 U CN 204297114U
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Abstract
The utility model disclose a kind of can high-altitude location four-axle aircraft, mainly comprise: form the body with four horns by upper machine body shell and lower body shell two parts, six axle gyroscope equipments, filming apparatus and treater, treater is connected to six axle gyroscope equipments, filming apparatus, engine installation, battery and voice activated control, voice activated control for controlling flare maneuver is set at body top, the The Cloud Terrace installed for filming apparatus is provided with at organism bottom, four horn inside of body install the brushless motor plate of engine installation respectively, brushless motor and screw propeller is provided with at four horn ends, body is connected to filming apparatus by The Cloud Terrace, The Cloud Terrace is primarily of standing finish, two-layer adapter plate and buffering ball three part composition, protective case is provided with below screw propeller, protective case is fixed on four horn end top of body, meet the operation requirements of user, can allow the flight of aircraft held stationary, not only simply easy to operate, and shooting effect is strengthened very well.
Description
Technical field
The utility model relates to one and to take photo by plane field, particularly relate to a kind of can the four-axle aircraft of location, high-altitude.
Background technology
Now along with the fast development of science and technology, people are increasingly deep for the research of aircraft, and all kinds of aircraft is applied in increasing occasion.Four rotor unmanned aircrafts are compared with other aircraft, and its physical construction is simply compact, and take action more flexible, landing environmental requirement is lower, has good operating characteristic, can realize among a small circle taking off, hover, landing.Due to these features, the numerous areas such as quadrotor has been widely used in taking photo by plane, monitor, investigate, search and rescue, control of agricultural pest.
Four-axle aircraft is a kind of common pattern of Multi-axis aircraft in small aircraft, because of the feature that it is dexterous, motor-driven, is widely used in low latitude and takes photo by plane, the aerial mission activity under the MODEL OVER COMPLEX TOPOGRAPHY such as disaster area exploration.And four-axle aircraft performs the ability of aerial mission under MODEL OVER COMPLEX TOPOGRAPHY, demarcated by flare maneuver executable in its flight course, the airflight attitude of conventional four-axle aircraft needs to keep fuselage overall close to level mostly, and degree of freedom is low, and operability is little.
Summary of the invention
The purpose of this utility model be to provide a kind of can the four-axle aircraft of location, high-altitude.
For achieving the above object, the utility model adopts following technical scheme: a kind of can high-altitude location four-axle aircraft, mainly comprise: form the body with four horns by upper machine body shell and lower body shell two parts, six axle gyroscope equipments, filming apparatus and treater, described treater is connected to six axle gyroscope equipments, filming apparatus, engine installation, battery and voice activated control, voice activated control for controlling flare maneuver is set at body top, the The Cloud Terrace installed for filming apparatus is provided with at organism bottom, four horn inside of body install the brushless motor plate of engine installation respectively, brushless motor and screw propeller is provided with at four horn ends.
Further, six described axle gyroscope equipments form primarily of six axle sensor sum counter two parts, and six axle sensors are connected to treater by counting machine.
Further, it is 0 degree to 45 degree that described body controls flight angle of inclination by engine installation.
Further, described body is connected to filming apparatus by The Cloud Terrace, and filming apparatus is fixed on bottom The Cloud Terrace by standing finish.
Further, described The Cloud Terrace is primarily of standing finish, two-layer adapter plate and buffering ball three part composition, and at least one buffering ball is arranged between two-layer adapter plate.
Further, described filming apparatus is primarily of camera, camera connecting element and can launch wireless camera control desk.
In such scheme, be provided with the protective case for the protection of screw propeller below described screw propeller, protective case is fixed on four horn end top of body.
In such scheme, described body adopts ABS plastic raw material to make.
As the further preferred version of the utility model, it is characterized in that:
1, four-axle aircraft controls the flare maneuver of four-axle aircraft by voice activated control, more intelligent, and save complicated control step, compare the four-axle aircraft only using remote controller operation with tradition, operating mode is more various, and playability is higher;
2, four-axle aircraft installs six axle gyroscope equipments, six axle gyroscope equipments are by the moving calculation of six axle sensor sum counters, meet the operation requirements of user, can allow the flight of aircraft held stationary, compare and conventional aircraft, not only simply easy to operate, be applicable to various age level, and shooting effect is strengthened very well;
3, the protective case of four-axle aircraft four horn ends can not only protect screw propeller and body by actv., and avoids the screw propeller of aircraft in flight course rotates to collide other objects, causes air crash out of control; Brushless motor makes the flying power of four-axle aircraft and flight life-span increase substantially.
accompanying drawing illustrates:
Accompanying drawing 1 is constructional delails figure of the present utility model;
Accompanying drawing 2 is block diagram of the present utility model;
Accompanying drawing 3 is front view of the present utility model;
Accompanying drawing 4 is circuit connection diagram of the present utility model.
detailed description of the invention:
Below in conjunction with accompanying drawing 1-4, the utility model is further illustrated.
A kind of can high-altitude location four-axle aircraft, mainly comprise: form the body 1 with four horns 13 by upper machine body shell 11 and lower body shell 12 two parts, six axle gyroscope equipments 2, filming apparatus 3 and treater 4, described treater 4 is connected to six axle gyroscope equipments 2, filming apparatus 3, engine installation 6, battery 7 and voice activated control 8, voice activated control 8 for controlling flare maneuver is set at body 1 top, its voice activated control 8 is made up of voice command recognizer and data memory two parts, voice command recognizer is for performing voice command identification to export voice command recognition, data memory is for recording voice command, user is by simple Voice command four-axle aircraft, six axle gyroscope equipments 2 form primarily of six axle sensor 21 sum counter 22 two parts, six axle sensors 21 are made up of the three-axis gyroscope two parts detecting three axle accelerators and the detection angles spin balancing laterally accelerated, six axle sensors 21 are by the computing of counting machine 22 and service contamination is sent to treater 4, the The Cloud Terrace 5 installed for filming apparatus 3 is provided with bottom body 1, four horn 13 inside of body 1 install the brushless motor plate 61 of engine installation 6 respectively, brushless motor 62 and screw propeller 63 is provided with at four horn 13 ends, the brushless motor plate 61 of engine installation 6 manipulates heading and the speed of four-axle aircraft by controlling brushless motor 62 rotating speed, the flying power of four-axle aircraft and flight life-span are increased substantially, body 1 regulates the power of brushless brushless motor 62 by engine installation 6, controlling flight angle of inclination is 0 degree to 45 degree, the very big flexibility ratio that must improve four-axle aircraft, can in the landform flight of complexity and shooting.
Described body 1 is connected to filming apparatus 3 by The Cloud Terrace 5, filming apparatus 3 is fixed on bottom The Cloud Terrace 5 by standing finish 51, The Cloud Terrace 5 is primarily of standing finish 51, two-layer adapter plate 52 and buffering ball 53 3 part composition, at least one buffering ball 53 is arranged between two-layer adapter plate 52, filming apparatus 3 and body 1 is avoided mutually to collide, play good buffer action, buffering ball 53 can protect filming apparatus 3 by actv., filming apparatus 3 is primarily of camera 31, camera connecting element 32 and wireless camera control desk 33 can be launched, its camera control desk 33 propagates the picture of shooting by launching wifi and 2.4GHz, realize remote control shooting, the protective case 631 for the protection of screw propeller 63 is provided with below screw propeller 63, protective case 631 is fixed on four horn 13 end top of body 1, screw propeller 63 and body 1 can not only be protected by actv., and avoid aircraft to collide other objects at flight course screw propeller 63, cause air crash out of control, body 1 adopts ABS plastic raw material to make, the crash resistance of product is strengthened.
During use, start four-axle aircraft to switch on power, and realize the Long-distance Control of user to aircraft, aircraft utilizes voice activated control 8 to identify the voice that user sends, and send instruction to six axle gyroscope equipments 2, filming apparatus 3 and engine installation 6 by treater 4, start the brushless motor 62 of engine installation 6 and screw propeller 63, four-axle aircraft produces downward wind-force by twirl screw propeller 63, so that four-axle aircraft can free flight; Four-axle aircraft utilizes six axle gyroscope equipments 2 to locate for a long time aloft, six axle sensors 21 detect and laterally accelerate and angle spin balancing, and send instruction to treater 4 by counting machine 22 computing, engine installation 6 is finely tuned, thus reaches the function of location, high-altitude.
Certainly, above diagram is only the utility model better embodiment, not limits range of use of the present utility model with this, therefore, every make in the utility model principle equivalence change all should be included in protection domain of the present utility model.
Claims (8)
1. one kind can high-altitude location four-axle aircraft, mainly comprise: be made up of the body (1) with four horns (13) upper machine body shell (11) and lower body shell (12) two parts, six axle gyroscope equipments (2), filming apparatus (3) and treater (4), it is characterized in that: described treater (4) is connected to six axle gyroscope equipments (2), filming apparatus (3), engine installation (6), battery (7) and voice activated control (8), voice activated control (8) for controlling flare maneuver is set at body (1) top, the The Cloud Terrace (5) installed for filming apparatus (3) is provided with in body (1) bottom, four horn (13) inside of body (1) install the brushless motor plate (61) of engine installation (6) respectively, brushless motor (62) and screw propeller (63) is provided with at four horn (13) ends.
2. according to claim 1 a kind of can high-altitude location four-axle aircraft, it is characterized in that: six described axle gyroscope equipments (2) are primarily of six axle sensors (21) sum counter (22) two parts composition, and six axle sensors (21) are connected to treater (4) by counting machine (22).
3. according to claim 2 a kind of can high-altitude location four-axle aircraft, it is characterized in that: described body (1) by engine installation (6) control flight angle of inclination be 0 degree to 45 degree.
4. according to claim 2 a kind of can high-altitude location four-axle aircraft, it is characterized in that: described body (1) is connected to filming apparatus (3) by The Cloud Terrace (5), filming apparatus (3) is fixed on The Cloud Terrace (5) bottom by standing finish (51).
5. according to claim 4 a kind of can high-altitude location four-axle aircraft, it is characterized in that: described The Cloud Terrace (5) is primarily of standing finish (51), two-layer adapter plate (52) and buffering ball (53) three part composition, and at least one buffering ball (53) is arranged between two-layer adapter plate (52).
6. according to claim 4 a kind of can high-altitude location four-axle aircraft, it is characterized in that: described filming apparatus (3) is primarily of camera (31), camera connecting element (32) and can launch wireless camera control desk (33).
7. according to claim 1-6 any one a kind of can high-altitude location four-axle aircraft; it is characterized in that: described screw propeller (63) below is provided with the protective case (631) for the protection of screw propeller (63), and protective case (631) is fixed on four horn (13) end top of body (1).
8. a kind of according to claim 1-6 any one can the four-axle aircraft of location, high-altitude, it is characterized in that: described body (1) adopts ABS plastic raw material to make.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420755175.9U CN204297114U (en) | 2014-12-05 | 2014-12-05 | A kind of can high-altitude location four-axle aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420755175.9U CN204297114U (en) | 2014-12-05 | 2014-12-05 | A kind of can high-altitude location four-axle aircraft |
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| Publication Number | Publication Date |
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| CN204297114U true CN204297114U (en) | 2015-04-29 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201420755175.9U Expired - Fee Related CN204297114U (en) | 2014-12-05 | 2014-12-05 | A kind of can high-altitude location four-axle aircraft |
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| CN (1) | CN204297114U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104986331A (en) * | 2015-07-27 | 2015-10-21 | 致导科技（北京）有限公司 | Unmanned aerial vehicle rotor wing protection frame and unmanned aerial vehicle |
| CN106184794A (en) * | 2016-08-30 | 2016-12-07 | 成都汇丁科技有限公司 | A kind of unmanned plane for taking photo by plane |
| CN106314771A (en) * | 2015-06-27 | 2017-01-11 | 深圳市大疆创新科技有限公司 | Aircraft and power device |
| CN107000840A (en) * | 2016-01-26 | 2017-08-01 | 深圳市大疆创新科技有限公司 | Unmanned vehicle and many mesh imaging systems |
| WO2017128313A1 (en) * | 2016-01-29 | 2017-08-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and arm mechanism thereof |
| CN107776867A (en) * | 2016-08-31 | 2018-03-09 | 北京臻迪科技股份有限公司 | A kind of unmanned plane horn device |
| CN108528716A (en) * | 2018-03-07 | 2018-09-14 | 芜湖翼讯飞行智能装备有限公司 | A kind of rotor protective cover installation quick-disassembly structure |
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2014
- 2014-12-05 CN CN201420755175.9U patent/CN204297114U/en not_active Expired - Fee Related
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106314771A (en) * | 2015-06-27 | 2017-01-11 | 深圳市大疆创新科技有限公司 | Aircraft and power device |
| CN106314771B (en) * | 2015-06-27 | 2019-10-29 | 深圳市大疆创新科技有限公司 | Aircraft and its power device |
| CN104986331A (en) * | 2015-07-27 | 2015-10-21 | 致导科技（北京）有限公司 | Unmanned aerial vehicle rotor wing protection frame and unmanned aerial vehicle |
| CN107000840A (en) * | 2016-01-26 | 2017-08-01 | 深圳市大疆创新科技有限公司 | Unmanned vehicle and many mesh imaging systems |
| US10681285B2 (en) | 2016-01-26 | 2020-06-09 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and multi-ocular imaging system |
| US11343443B2 (en) | 2016-01-26 | 2022-05-24 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and multi-ocular imaging system |
| WO2017128313A1 (en) * | 2016-01-29 | 2017-08-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and arm mechanism thereof |
| CN107108011A (en) * | 2016-01-29 | 2017-08-29 | 深圳市大疆创新科技有限公司 | Unmanned plane and its horn mechanism |
| CN109747807A (en) * | 2016-01-29 | 2019-05-14 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| CN106184794A (en) * | 2016-08-30 | 2016-12-07 | 成都汇丁科技有限公司 | A kind of unmanned plane for taking photo by plane |
| CN107776867A (en) * | 2016-08-31 | 2018-03-09 | 北京臻迪科技股份有限公司 | A kind of unmanned plane horn device |
| CN108528716A (en) * | 2018-03-07 | 2018-09-14 | 芜湖翼讯飞行智能装备有限公司 | A kind of rotor protective cover installation quick-disassembly structure |
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Legal Events
| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 515000 Shantou new industrial zone, Chenghai, Guangdong Patentee after: GUANGDONG CHENGXING UNMANNED AERIAL VEHICLE COMPANY LIMITED Address before: 515000 Shantou new industrial zone, Chenghai, Guangdong Patentee before: Guangdong Chengxing Modelairplane Science Company Limted |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150429 Termination date: 20181205 |
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| CF01 | Termination of patent right due to non-payment of annual fee |