CN205293096U - Take unmanned aerial vehicle of structure of acting as go -between - Google Patents
Take unmanned aerial vehicle of structure of acting as go -between Download PDFInfo
- Publication number
- CN205293096U CN205293096U CN201520852738.0U CN201520852738U CN205293096U CN 205293096 U CN205293096 U CN 205293096U CN 201520852738 U CN201520852738 U CN 201520852738U CN 205293096 U CN205293096 U CN 205293096U
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- assembly
- unmanned plane
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Abstract
The utility model discloses a take unmanned aerial vehicle of structure of acting as go -between, including four group's screw arm of force subassemblies, cubic bracket component, wire -rewinding machine subassembly, battery case and support plate component, four tip at cubic bracket component are fixed respectively to four group's screw arm of force subassemblies, the battery case is fixed on cubic bracket component, the one side at support plate component is fixed to the four directions bracket component, the another side at support plate component is fixed to the wire -rewinding machine subassembly, the battery is connected with wire -rewinding machine subassembly electricity in the battery case, control terminal provides ascending power through wireless connection mode control screw arm of force subassembly, and drive cubic bracket component, the wire -rewinding machine subassembly, battery case and support plate component break away from ground, conductor rope on the wire -rewinding machine subassembly is according to the continuous unwrapping wire of track that rises at this moment. Through independently coming out battery case and wire -rewinding machine subassembly, directly use cubic bracket component and support plate component to support, reduced unmanned aerial vehicle's quality and area greatly, also made things convenient for individual installation and dismantlement simultaneously.
Description
Technical field
This utility model relates to the technical field of unmanned plane, particularly relates to a kind of unmanned plane with guy structure.
Background technology
Unmanned plane, i.e. UAV, its english abbreviation is " UAV ", is the not manned aircraft of the presetting apparatus manipulation utilizing radio robot with providing for oneself. Can be divided into from technical standpoint definition: these several big classes of depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol. Military unmanned air vehicle and civilian unmanned plane can be divided into from the classification of purposes aspect. Military aspect, can be used for battle reconnaissance and supervision, school, location are penetrated, injured assessment, electronic warfare, and civilian aspect, can be used for border patrol, nuclear radiation detection, aeroplane photography, mineral exploration aviation, the condition of a disaster monitor, traffic patrolling and security monitoring.
Unmanned aerial vehicle onboard pay off rack refers in unmanned plane transmission line of electricity just conductor rope unfolding construction field, is loaded on unmanned plane for the pay off rack of carry just conductor rope; At present in transmission line of electricity line laying work, typically require employing unmanned plane (such as many rotor wing unmanned aerial vehicles, depopulated helicopter) unfolding just conductor rope (preliminary leading rope), namely on unmanned plane, load special pay off rack carry just conductor rope, thus aloft first conductor rope being loaded tension force, lay mode is adopted to carry out soaring unwrapping wire; Wherein special pay off rack and unmanned plane can take separable connected mode.
Utility model content
For the weak point existed in above-mentioned technology, this utility model provide a kind of shrink freely, the easily controllable unmanned plane with guy structure.
In order to achieve the above object, a kind of unmanned plane with guy structure of this utility model, control assembly, take-up electric machine assembly, battery case and blade assemblies including four groups of propeller force arm components, square support assembly, take-up, described four groups of propeller force arm components are separately fixed at four ends of square support assembly, described battery case is fixed on square support assembly, described square support assembly is fixed on the one side of blade assemblies, described take-up electric machine assembly is fixed on the another side of blade assemblies, in described battery case, battery electrically connects with take-up electric machine assembly, described take-up electric machine assembly controls assembly with take-up and electrically connects, control terminal and control propeller force arm component offer lifting power by wireless telecommunications connected mode, and drive square support assembly, take-up electric machine assembly, battery case and blade assemblies depart from ground, now the conductor rope on take-up electric machine assembly is according to the continuous unwrapping wire of ascending track.
Wherein, described take-up electric machine assembly includes supporting frame, the unwrapping wire bearing of folding and unfolding conductor rope after being supported by supporting frame, and controls the self-locking structure of unwrapping wire bearing stopping folding and unfolding conductor rope, and support frame as described above body includes girder plate and two pieces of side shields; Described two pieces of side shields be arranged in parallel, and the top of each side shield is connected by tie-beam is vertical with the end of described girder plate, and described unwrapping wire bearing two ends are separately fixed on two side shields, and described self-locking structure is fixed on a side shield.
Wherein, described take-up electric machine assembly also includes electromotor, and described electromotor is fixing with unwrapping wire bearing to be connected, described electromotor electrically connects with battery in battery case, and in unwrapping wire process, paying out reel is forwarded and moved as after electromotor offer kinetic energy, electromotor produces electric energy, and delivers the power in battery case.
Wherein, described square support assembly includes pressing from both sides under folder and pipe fitting on carbon fiber pipe, pipe fitting, on described pipe fitting, folder encloses with folder under pipe fitting and forms the accommodating cast cavity being mutually perpendicular to carbon fiber pipe, four groups of carbon fiber pipes are end to end, sequentially access after in four groups of tubular cavity, form the square rack structure of corner balance.
Wherein, described propeller force arm component includes the first rotational structure, and described square support assembly is provided with second rotational structure suitable with the first rotational structure, and described first rotational structure is rotatably connected by bearing after aliging with the second rotational structure.
Wherein, described propeller force arm component also includes extension rod and spiral fan, described extension rod one end is connected with the first rotational structure, the extension rod other end is connected with spiral fan, when described extension rod rotates to parallel with the carbon fiber pipe on square support assembly, propeller force arm component is in folded state, and when described extension rod rotates to the diagonal being in square support assembly, propeller force arm component is in deployed condition.
Wherein, this unmanned plane also includes U-shaped fixed support, described square support assembly is provided with the fixing hole suitable with U-shaped fixed support exit, described blade assemblies is provided with the cell body trepanning suitable with U-shaped fixed support cell body, is connected by two symmetrically arranged described U-shaped fixed supports are fixing between described square support assembly and blade assemblies.
Wherein, this unmanned plane also includes bipod assembly, and described foot rest assembly is inverted T-shaped foot rest shape, and in described blade assemblies, symmetry stretches out two chucking lugs, described foot rest assembly is fixed on two chucking lugs by screw structural symmetry, and foot rest assembly tilts to be fixed in blade assemblies.
The beneficial effects of the utility model are:
Compared with prior art, unmanned plane with guy structure of the present utility model, by by independent to battery case and take-up electric machine assembly, directly use square support assembly and blade assemblies to be supported, substantially reduce quality and the floor space of unmanned plane, be also convenient for individual installation and dismounting simultaneously, four groups of propeller force arm components are set in the end of square support assembly simultaneously, increase horsepower per liter so that unmanned plane during flying speed faster, also makes the balance flight of unmanned plane be more easy to adjustment. Setting by take-up electric machine assembly so that unmanned plane can without departing from the control of manipulator, motor or fly control go wrong time, still can control the flight of unmanned plane to a certain extent.
Accompanying drawing explanation
Fig. 1 is the explosive view of this utility model unmanned plane with guy structure;
Fig. 2 is the structure chart of this utility model unmanned plane with guy structure;
Fig. 3 is the local structural graph of this utility model take-up electric machine assembly;
Fig. 4 is the explosive view of this utility model square support assembly.
Main element symbol description is as follows:
10, battery case 11, square support assembly
12, propeller force arm component 13, take-up electric machine assembly
14, blade assemblies 15, U-shaped fixed support
16, foot rest assembly 17, take-up control assembly
111, carbon fiber pipe 112, folder on pipe fitting
113, press from both sides under pipe fitting
121, the first rotational structure 122, spiral fan
123, extension rod
131, supporting frame 132, unwrapping wire bearing
133, self-locking structure.
Detailed description of the invention
In order to more clearly state this utility model, below in conjunction with accompanying drawing, this utility model is further described.
Consult Fig. 1-2, a kind of unmanned plane with guy structure of this utility model, control assembly 17, take-up electric machine assembly 13, battery case 10 and blade assemblies 14 including four groups of propeller force arm components 12, square support assembly 11, take-up, four groups of propeller force arm components 12 are separately fixed at four ends of square support assembly 11, battery case 10 is fixed on square support assembly 11, square support assembly 11 is fixed on the one side of blade assemblies 14, take-up electric machine assembly 13 is fixed on the another side of blade assemblies 14, in battery case 10, battery electrically connects with take-up electric machine assembly 13, take-up electronic building brick controls assembly 17 with take-up and electrically connects, control terminal and provide lifting power by wireless telecommunications connected mode control propeller force arm component 12, and drive square support assembly 11, take-up electric machine assembly 13, battery case 10 and blade assemblies 14 depart from ground, now the conductor rope on take-up electric machine assembly 13 is according to the continuous unwrapping wire of ascending track.
Compared to prior art, unmanned plane with guy structure of the present utility model, by by independent to battery case 10 and take-up electric machine assembly 13, square support assembly 11 and blade assemblies 14 is directly used to be supported, substantially reduce quality and the floor space of unmanned plane, individual installation and dismounting it have been also convenient for simultaneously, four groups of propeller force arm components 12 are set in the end of square support assembly 11 simultaneously, increase horsepower per liter, make unmanned plane during flying speed faster, also make the balance flight of unmanned plane be more easy to adjustment. Setting by take-up electric machine assembly 13 so that unmanned plane can without departing from the control of manipulator, motor or fly control go wrong time, still can control the flight of unmanned plane to a certain extent.
Further regard to Fig. 3, take-up electric machine assembly 13 includes supporting frame 131, by the unwrapping wire bearing 132 of folding and unfolding conductor rope after supporting frame 131 support, and control unwrapping wire bearing 132 stops the self-locking structure 133 of folding and unfolding conductor rope, and supporting frame 131 includes girder plate and two pieces of side shields; Two pieces of side shields be arranged in parallel, and the top of each side shield is connected by tie-beam is vertical with the end of girder plate, and unwrapping wire bearing 132 two ends are separately fixed on two side shields, and self-locking structure 133 is fixed on a side shield. Unmanned plane is in static in the air or when being in hovering state, starting self-locking structure 133 makes bobbin not be rotated further by, stop unwrapping wire, to prevent because continuing outlet interference unmanned plane during flying, prevent unnecessary conductor rope internal at actinobacillus device simultaneously or exit is wound around.
In the present embodiment, take-up electric machine assembly 13 also includes electromotor, electromotor is fixing with unwrapping wire bearing 132 to be connected, electromotor electrically connects with battery in battery case 10, in unwrapping wire process, unwrapping wire bearing 132 rotates after providing kinetic energy into electromotor, and electromotor produces electric energy, and delivers the power in battery case 10.Unwrapping wire process middle (center) bearing is rotated the kinetic energy Appropriate application produced by arranging of electromotor, thus both having saved the energy, what also make that the battery of this unmanned plane can support is more of a specified duration simultaneously.
Further regard to Fig. 4, square support assembly 11 includes pressing from both sides folder 113 under 112 and pipe fitting on carbon fiber pipe 111, pipe fitting, pipe fitting presss from both sides folder 113 under 112 and pipe fitting and encloses the accommodating cast cavity being mutually perpendicular to carbon fiber pipe 111 of formation, four groups of carbon fiber pipes 111 are end to end, sequentially access after in four groups of tubular cavity, form the square rack structure of corner balance. By folder 113 under folder 112, pipe fitting on dismountable pipe fitting and carbon fiber pipe 111 mounting means, be conducive to the making of standard component on the one hand, to improve work efficiency, on the other hand, can install according to the carbon fiber pipe 111 of the selected different length of different situations, to adapt to the collocation of different propeller force arm components 12 and battery case 10.
In the present embodiment, propeller force arm component 12 includes the first rotational structure 121, being provided with second rotational structure suitable with the first rotational structure 121 on square support assembly 11, the first rotational structure 121 is rotatably connected by bearing after aliging with the second rotational structure. Propeller force arm component 12 also includes extension rod 123 and spiral fan 122, extension rod 123 one end is connected with the first rotational structure 121, extension rod 123 other end is connected with spiral fan 122, when extension rod 123 rotates to parallel with the carbon fiber pipe 111 on square support assembly 11, propeller force arm component 12 is in folded state, when extension rod 123 rotates to the diagonal being in square support assembly 11, propeller force arm component 12 is in deployed condition. The setting of the first rotational structure 121 and the second rotational structure so that propeller force arm component 12 is collapsible, deployable, and the transport facilitating this unmanned plane picks and places.
In the present embodiment, this unmanned plane also includes U-shaped fixed support, square support assembly 11 is provided with the fixing hole suitable with U-shaped fixed support exit, blade assemblies 14 is provided with the cell body trepanning suitable with U-shaped fixed support cell body, is connected by two symmetrically arranged U-shaped fixed supports are fixing between square support assembly 11 with blade assemblies 14. This unmanned plane also includes bipod assembly 16, foot rest assembly 16 is in inverted T-shaped foot rest shape, in blade assemblies 14, symmetry stretches out two chucking lugs, and foot rest assembly 16 is fixed on two chucking lugs by screw structural symmetry, and foot rest assembly 16 tilts to be fixed in blade assemblies 14. U-shaped fixed support 15 and foot rest assembly 16 all serve supporting role, and the two, while ensureing stable support, decreasing consumptive material as far as possible, so both having saved material, alleviating again the weight of unmanned plane.
Disclosed above being only several specific embodiment of the present utility model, but this utility model is not limited to this, the changes that any person skilled in the art can think of all should fall into protection domain of the present utility model.
Claims (8)
1. the unmanned plane with guy structure, it is characterised in that include four groups of propeller force arm components, square support assembly, take-up control assembly, take-up electric machine assembly, battery case and blade assemblies, described four groups of propeller force arm components are separately fixed at four ends of square support assembly, described battery case is fixed on square support assembly, described square support assembly is fixed on the one side of blade assemblies, described take-up electric machine assembly is fixed on the another side of blade assemblies, in described battery case, battery electrically connects with take-up electric machine assembly, described take-up electric machine assembly controls assembly with take-up and electrically connects, control terminal and control propeller force arm component offer lifting power by wireless telecommunications connected mode, and drive square support assembly, take-up electric machine assembly, battery case and blade assemblies depart from ground, now the conductor rope on take-up electric machine assembly is according to the continuous unwrapping wire of ascending track.
2. the unmanned plane with guy structure according to claim 1, it is characterized in that, described take-up electric machine assembly includes supporting frame, supported by supporting frame after the unwrapping wire bearing of folding and unfolding conductor rope and control unwrapping wire bearing and stop the self-locking structure of folding and unfolding conductor rope, support frame as described above body includes girder plate and two pieces of side shields; Described two pieces of side shields be arranged in parallel, and the top of each side shield is connected by tie-beam is vertical with the end of described girder plate, and described unwrapping wire bearing two ends are separately fixed on two side shields, and described self-locking structure is fixed on a side shield.
3. the unmanned plane with guy structure according to claim 2, it is characterized in that, described take-up electric machine assembly also includes electromotor, described electromotor is fixing with unwrapping wire bearing to be connected, described electromotor electrically connects with battery in battery case, and in unwrapping wire process, paying out reel is forwarded and moved as after electromotor offer kinetic energy, electromotor produces electric energy, and delivers the power in battery case.
4. the unmanned plane with guy structure according to claim 1, it is characterized in that, described square support assembly includes pressing from both sides under folder and pipe fitting on carbon fiber pipe, pipe fitting, on described pipe fitting, folder encloses with folder under pipe fitting and forms the accommodating cast cavity being mutually perpendicular to carbon fiber pipe, four groups of carbon fiber pipes are end to end, sequentially access after in four groups of tubular cavity, form the square rack structure of corner balance.
5. the unmanned plane with guy structure according to claim 4, it is characterized in that, described propeller force arm component includes the first rotational structure, being provided with second rotational structure suitable with the first rotational structure on described square support assembly, described first rotational structure is rotatably connected by bearing after aliging with the second rotational structure.
6. the unmanned plane with guy structure according to claim 5, it is characterized in that, described propeller force arm component also includes extension rod and spiral fan, described extension rod one end is connected with the first rotational structure, the extension rod other end is connected with spiral fan, when described extension rod rotates to parallel with the carbon fiber pipe on square support assembly, propeller force arm component is in folded state, when described extension rod rotates to the diagonal being in square support assembly, propeller force arm component is in deployed condition.
7. the unmanned plane with guy structure according to claim 6, it is characterized in that, this unmanned plane also includes U-shaped fixed support, described square support assembly is provided with the fixing hole suitable with U-shaped fixed support exit, described blade assemblies is provided with the cell body trepanning suitable with U-shaped fixed support cell body, is connected by two symmetrically arranged described U-shaped fixed supports are fixing between described square support assembly and blade assemblies.
8. the unmanned plane with guy structure according to claim 7, it is characterized in that, this unmanned plane also includes bipod assembly, described foot rest assembly is inverted T-shaped foot rest shape, in described blade assemblies, symmetry stretches out two chucking lugs, described foot rest assembly is fixed on two chucking lugs by screw structural symmetry, and foot rest assembly tilts to be fixed in blade assemblies.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520852738.0U CN205293096U (en) | 2015-10-30 | 2015-10-30 | Take unmanned aerial vehicle of structure of acting as go -between |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520852738.0U CN205293096U (en) | 2015-10-30 | 2015-10-30 | Take unmanned aerial vehicle of structure of acting as go -between |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205293096U true CN205293096U (en) | 2016-06-08 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520852738.0U Expired - Fee Related CN205293096U (en) | 2015-10-30 | 2015-10-30 | Take unmanned aerial vehicle of structure of acting as go -between |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205293096U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105235906A (en) * | 2015-10-30 | 2016-01-13 | 深圳高启科技有限公司 | Unmanned aerial vehicle with stay wire structure and application method thereof |
| WO2020166054A1 (en) * | 2019-02-15 | 2020-08-20 | 株式会社テクノスヤシマ | Flying body |
-
2015
- 2015-10-30 CN CN201520852738.0U patent/CN205293096U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105235906A (en) * | 2015-10-30 | 2016-01-13 | 深圳高启科技有限公司 | Unmanned aerial vehicle with stay wire structure and application method thereof |
| CN105235906B (en) * | 2015-10-30 | 2018-04-24 | 深圳高启科技有限公司 | Unmanned plane and its application method with guy structure |
| WO2020166054A1 (en) * | 2019-02-15 | 2020-08-20 | 株式会社テクノスヤシマ | Flying body |
| JP6754515B1 (en) * | 2019-02-15 | 2020-09-16 | 株式会社テクノスヤシマ | Aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160608 Termination date: 20191030 |