CN205602128U - Multiaxis unmanned aerial vehicle - Google Patents
Multiaxis unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205602128U CN205602128U CN201620388767.0U CN201620388767U CN205602128U CN 205602128 U CN205602128 U CN 205602128U CN 201620388767 U CN201620388767 U CN 201620388767U CN 205602128 U CN205602128 U CN 205602128U
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- CN
- China
- Prior art keywords
- undercarriage
- unmanned plane
- multiaxis unmanned
- added
- side frame
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Abstract
The utility model discloses a multiaxis unmanned aerial vehicle, include: the organism, be provided with a plurality of rotor subassemblies on the organism, the bilateral symmetry is provided with the undercarriage subassembly that automatic control goes up and down on the organism, the undercarriage subassembly including put on the shelf, undercarriage and side bearer, the one end of side bearer is connected with putting on the shelf, and the other end is connected with the undercarriage, put on the shelf with the one end swing joint of undercarriage on the organism, still be connected with the support frame between undercarriage and the side bearer, still be connected with the secondary rotor wing subassembly on the undercarriage subassembly. In this way, the utility model discloses multiaxis unmanned aerial vehicle can save the unmanned aerial vehicle space, reduces manufacturing cost, simplifies the structure, safe and reliable, convenient to use.
Description
Technical field
This utility model relates to unmanned plane field, particularly relates to a kind of multiaxis unmanned plane.
Background technology
The use of unmanned plane is more and more extensive in daily life.The collapsible undercarriage majority of many rotor wing unmanned aerial vehicles is to use double steering engine multi-grade lever principle design, in general rotor and the undercarriage of unmanned plane is all provided separately, independent operating, but add weight and the size of unmanned plane in this case, and manufacturing cost also increases.
Summary of the invention
This utility model is mainly solving the technical problems that provide a kind of multiaxis unmanned plane, it is possible to saves unmanned plane space, reduces manufacturing cost, simplifies structure, safe and reliable, easy to use.
For solving above-mentioned technical problem, the technical scheme that this utility model uses is: provide a kind of multiaxis unmanned plane, including: body, multiple rotor assemblies it is provided with on described body, on described body, lateral symmetry is provided with the landing gear assembly automatically controlling lifting, described landing gear assembly includes added, undercarriage and side frame, one end of described side frame is connected with added, the other end is connected with undercarriage, described added and undercarriage one end is movably connected on body, it is also associated with bracing frame between described undercarriage and side frame, secondary rotor assemblies it is also associated with on described landing gear assembly.
In one preferred embodiment of this utility model, described secondary rotor assemblies includes rotor arm and is connected to the rotor on rotor arm, and one end of described rotor arm is connected with added and side frame.
In one preferred embodiment of this utility model, described added, undercarriage, vehicle frame and body connect formation parallelogram sturcutre.
In one preferred embodiment of this utility model, support frame as described above is connected with undercarriage and side frame respectively, and support frame as described above is vertical setting with undercarriage and support.
In one preferred embodiment of this utility model, being provided with controller and control portion in described body, described controller controls control portion and drives landing gear assembly automatically rise or decline.
The beneficial effects of the utility model are: this utility model multiaxis unmanned plane, it is possible to save unmanned plane space, reduce manufacturing cost, simplify structure, safe and reliable, easy to use.
Accompanying drawing explanation
In order to be illustrated more clearly that the technical scheme in this utility model embodiment, in describing embodiment below, the required accompanying drawing used is briefly described, apparently, accompanying drawing in describing below is only embodiments more of the present utility model, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings, wherein:
Fig. 1 is the perspective view of this utility model multiaxis unmanned plane landing state；
Fig. 2 is the front view of multiaxis unmanned plane shown in Fig. 1；
Fig. 3 is the perspective view of this utility model multiaxis unmanned plane takeoff condition；
In accompanying drawing, the labelling of each parts is as follows: 1, body, and 2, rotor assemblies, 3, landing gear assembly, 4, added, 5, undercarriage, 6, side frame, 7, bracing frame, 8, secondary rotor assemblies, 9, rotor arm, 10, rotor.
Detailed description of the invention
Technical scheme in this utility model embodiment will be clearly and completely described below, it is clear that described embodiment is only a part of embodiment of the present utility model rather than whole embodiments.Based on the embodiment in this utility model, all other embodiments that those of ordinary skill in the art are obtained under not making creative work premise, broadly fall into the scope of this utility model protection.
Refer to Fig. 1 to Fig. 3, a kind of multiaxis unmanned plane, including: body 1, body 1 is provided with multiple rotor assemblies 2, on body 1, lateral symmetry is provided with the landing gear assembly 3 automatically controlling lifting, landing gear assembly 3 includes added 4, undercarriage 5 and side frame 6, one end of side frame 6 is connected with added 4, and the other end is connected with undercarriage 5, added 4 and one end of undercarriage 5 be movably connected on body 1, it is also associated with bracing frame 7 between undercarriage 5 and side frame 6, landing gear assembly 3 is also associated with secondary rotor assemblies 8.
It addition, secondary rotor assemblies 8 includes rotor arm 9 and the rotor 10 being connected on rotor arm 9, one end of rotor arm 9 is connected with added 4 and side frame 6.
It addition, added 4, undercarriage 5, vehicle frame 6 and body 1 connect forms parallelogram sturcutre.
It addition, bracing frame 7 is connected with undercarriage 5 and side frame 6 respectively, bracing frame 7 is vertical setting with undercarriage 5 and support 6.
It addition, be provided with controller and control portion in body 1, controller controls control portion and drives landing gear assembly 3 automatically rise or decline.
This utility model multiaxis unmanned plane specific works principle is as follows: when unmanned plane takes off, controller controls control portion makes landing gear assembly 3 lifting, the secondary rotor assemblies 8 being arranged on landing gear assembly is raised to and rotor assemblies 2 same level, unmanned plane normal flight.When needing landing, control portion automatically controls 3 fall under landing gear assembly, makes bracing frame 7 contact ground, and unmanned plane declines and stops flight.
It is different from prior art, this utility model multiaxis unmanned plane, it is possible to save unmanned plane space, reduces manufacturing cost, simplify structure, safe and reliable, easy to use.
The foregoing is only embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every equivalent structure utilizing this utility model description to be made or equivalence flow process conversion; or directly or indirectly it is used in other relevant technical field, the most in like manner it is included in scope of patent protection of the present utility model.
Claims (5)
1. a multiaxis unmanned plane, it is characterized in that, including: body, described body is provided with multiple rotor assemblies, on described body, lateral symmetry is provided with the landing gear assembly automatically controlling lifting, described landing gear assembly includes added, undercarriage and side frame, one end of described side frame is connected with added, and the other end is connected with undercarriage, and described added and undercarriage one end is movably connected on body, it is also associated with bracing frame between described undercarriage and side frame, described landing gear assembly is also associated with secondary rotor assemblies.
Multiaxis unmanned plane the most according to claim 1, it is characterised in that described secondary rotor assemblies includes rotor arm and is connected to the rotor on rotor arm, and one end of described rotor arm is connected with added and side frame.
Multiaxis unmanned plane the most according to claim 1, it is characterised in that described added, undercarriage, vehicle frame and body connect formation parallelogram sturcutre.
Multiaxis unmanned plane the most according to claim 1, it is characterised in that support frame as described above is connected with undercarriage and side frame respectively, support frame as described above is vertical setting with undercarriage and support.
Multiaxis unmanned plane the most according to claim 1, it is characterised in that be provided with controller and control portion in described body, described controller controls control portion and drives landing gear assembly automatically rise or decline.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620388767.0U CN205602128U (en) | 2016-05-04 | 2016-05-04 | Multiaxis unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620388767.0U CN205602128U (en) | 2016-05-04 | 2016-05-04 | Multiaxis unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205602128U true CN205602128U (en) | 2016-09-28 |
Family
ID=56968663
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620388767.0U Expired - Fee Related CN205602128U (en) | 2016-05-04 | 2016-05-04 | Multiaxis unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205602128U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105947208A (en) * | 2016-05-04 | 2016-09-21 | 无锡觅睿恪科技有限公司 | Multi-axis unmanned aerial vehicle |
-
2016
- 2016-05-04 CN CN201620388767.0U patent/CN205602128U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105947208A (en) * | 2016-05-04 | 2016-09-21 | 无锡觅睿恪科技有限公司 | Multi-axis unmanned aerial vehicle |
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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 |
Granted publication date: 20160928 Termination date: 20190504 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |