CN205418107U - Single portable scounting aeroplane - Google Patents
Single portable scounting aeroplane Download PDFInfo
- Publication number
- CN205418107U CN205418107U CN201521115099.6U CN201521115099U CN205418107U CN 205418107 U CN205418107 U CN 205418107U CN 201521115099 U CN201521115099 U CN 201521115099U CN 205418107 U CN205418107 U CN 205418107U
- Authority
- CN
- China
- Prior art keywords
- controller
- wing
- undercarriage
- motor
- mounting panel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Abstract
The utility model discloses a single portable scounting aeroplane, including controller, mounting panel, wing, fin, undercarriage and shooting device, the controller is installed on the undercarriage, shoots the device and installs in the undercarriage, and the gyro wheel is installed to the bottom of undercarriage, the mounting panel is installed to the both sides of controller, and the motor is installed to the rotatable wing of installing on the every mounting panel on the mounting panel, the screw is installed to the motor front end, installs the air brake on the controller, and the fin is installed in the rear side of controller, and the fin is connected with the controller through the connecting rod, and the controller is connected with the shooting device with the motor. The utility model discloses can the wing is collapsible install on the mounting panel, can fold the too big problem of lateral length that solves with the wing when not using, the simultaneous design ingenious air brake, the wing has also been guaranteed to the air brake when bearing the speed reduction function expansion is with folding to the needs of mechanical structure with pneumatic appearance.
Description
[technical field]
This utility model relates to the technical field of unmanned plane, the technical field of the scounting aeroplane of a kind of single-person portable.
[background technology]
Along with the development of General Aviation, aircraft enters the life of general public gradually.The unmanned plane wherein grown up along with electronic information technology has given play to irreplaceable effect in civil and military field especially.Aeroplane photography at civil area, earthquake relief work, aerial inspection, meteorological detection and scientific experiments, the scouting of military domain, strike mission execution aspect, unmanned plane all has advantageous advantage, but for comparing more most ground equipment, unmanned plane still has transport difficult, how the shortcomings such as time length, overcome these shortcomings to become a key point of Development of UAV.
[utility model content]
The purpose of this utility model solves the problems of the prior art exactly, proposes the scounting aeroplane of a kind of single-person portable, it is possible to wing is collapsible to be installed on installing plate, can carry out folding by wing solve the problem that lateral length is excessive when not using.Make aircraft can be conveniently located into rectangular box, it is easy to vehicle transport carry with single, have employed double motive design, propeller is allowed to avoid camera fields of view, make whole aircraft monitors that visual angle has reached at a relatively high degree, devising flap cleverly, flap also ensure that the expansion of wing while bearing deceleration and folds the needs to frame for movement Yu pneumatic external form simultaneously.
For achieving the above object, the utility model proposes the scounting aeroplane of a kind of single-person portable, including controller, installing plate, wing, empennage, undercarriage and filming apparatus, described controller is installed on undercarriage, filming apparatus is installed in undercarriage, the bottom of undercarriage is provided with roller, the both sides of described controller are provided with installing plate, rotatably mounted on every piece of installing plate have wing, motor is installed on installing plate, described motor front end is provided with propeller, flap is installed on controller, empennage is installed on the rear side of controller, empennage is connected with controller by connecting rod, controller is connected with motor and filming apparatus.
As preferably, the front end of described controller is pyramidal structure, and flap tilts to be installed on controller.
As preferably, described wing is installed on the bottom of installing plate by rotating mechanism, and controller is connected with rotating mechanism.
As preferably, the both sides of described filming apparatus are separately installed with a motor, and motor is connected with propeller by rotating shaft.
As preferably, described empennage is vertically installed with balance riser.
The beneficial effects of the utility model: this utility model can wing be collapsible is installed on installing plate, can carry out folding by wing when not using and solve the problem that lateral length is excessive.Make aircraft can be conveniently located into rectangular box, it is easy to vehicle transport carry with single, have employed double motive design, propeller is allowed to avoid camera fields of view, make whole aircraft monitors that visual angle has reached at a relatively high degree, devising flap cleverly, flap also ensure that the expansion of wing while bearing deceleration and folds the needs to frame for movement Yu pneumatic external form simultaneously.
Feature of the present utility model and advantage will combine accompanying drawing by embodiment and be described in detail.
[accompanying drawing explanation]
Fig. 1 is the front view of the scounting aeroplane of a kind of single-person portable of this utility model；
Fig. 2 is the top view of the scounting aeroplane of a kind of single-person portable of this utility model.
[detailed description of the invention]
Refering to Fig. 1, Fig. 2, the scounting aeroplane of a kind of single-person portable of this utility model, including controller 1, installing plate 2, wing 3, empennage 4, undercarriage 5 and filming apparatus 6, described controller 1 is installed on undercarriage 5, filming apparatus 6 is installed in undercarriage 5, the bottom of undercarriage 5 is provided with roller 51, the both sides of described controller 1 are provided with installing plate 2, rotatably mounted on every piece of installing plate 2 have wing 3, motor 21 is installed on installing plate 2, described motor 21 front end is provided with propeller 22, flap 11 is installed on controller 1, empennage 4 is installed on the rear side of controller 1, empennage 4 is connected with controller 1 by connecting rod 41, controller 1 is connected with motor 21 and filming apparatus 6.
The front end of described controller 1 is pyramidal structure, flap 11 tilts to be installed on controller 1, described wing 3 is installed on the bottom of installing plate 2 by rotating mechanism 31, controller 1 is connected with rotating mechanism 31, the both sides of described filming apparatus 6 are separately installed with a motor 21, motor 21 is connected with propeller 22 by rotating shaft 23, and described empennage 4 is vertically installed with balance riser 42.
Utility model works process:
The scounting aeroplane of a kind of single-person portable of this utility model is in the course of the work, it is possible to wing 3 is collapsible to be installed on installing plate 2, can carry out folding by wing 3 solve the problem that lateral length is excessive when not using.Make aircraft can be conveniently located into rectangular box, it is easy to vehicle transport carry with single, the both sides of filming apparatus 6 are separately installed with a motor 21, motor 21 is connected with propeller 22 by rotating shaft 23, have employed double motive design, propeller 22 is allowed to avoid camera fields of view, make whole aircraft monitors that visual angle has reached at a relatively high degree, devise flap 11 cleverly simultaneously, flap 11 also ensure that the expansion of wing 3 while bearing deceleration and folds the needs to frame for movement Yu pneumatic external form, this utility model has used folded wing 3 structure of autonomous Design, simple efficient, undercarriage 5 is coordinated can effectively to adapt to complicated landing environment, ingenious utilization is double sends out advantage, create the excellent visual field, the advantage simply taken off.Overall carrying capacity is promoted, it is possible to apply to mapping of taking photo by plane, information search on the basis of carrying convenience.Respond is rapid, adapts to wild environment, is suitable for natural disaster and searches and rescues, military tactical investigation etc..
Above-described embodiment is to explanation of the present utility model, is not to restriction of the present utility model, any scheme after this utility model simple transformation is belonged to protection domain of the present utility model.
Claims (5)
- null1. the scounting aeroplane of a single-person portable，It is characterized in that: include controller (1)、Installing plate (2)、Wing (3)、Empennage (4)、Undercarriage (5) and filming apparatus (6)，Described controller (1) is installed on undercarriage (5)，Filming apparatus (6) is installed in undercarriage (5)，The bottom of undercarriage (5) is provided with roller (51)，The both sides of described controller (1) are provided with installing plate (2)，The most rotatably mounted on every piece of installing plate (2) have wing (3)，Motor (21) is installed on installing plate (2)，Described motor (21) front end is provided with propeller (22)，Flap (11) is installed on controller (1)，Empennage (4) is installed on the rear side of controller (1)，Empennage (4) is connected with controller (1) by connecting rod (41)，Controller (1) is connected with motor (21) and filming apparatus (6).
- The scounting aeroplane of a kind of single-person portable the most as claimed in claim 1, it is characterised in that: the front end of described controller (1) is pyramidal structure, and flap (11) tilts to be installed on controller (1).
- The scounting aeroplane of a kind of single-person portable the most as claimed in claim 1, it is characterized in that: described wing (3) is installed on the bottom of installing plate (2) by rotating mechanism (31), and controller (1) is connected with rotating mechanism (31).
- The scounting aeroplane of a kind of single-person portable the most as claimed in claim 1, it is characterized in that: the both sides of described filming apparatus (6) are separately installed with a motor (21), motor (21) is connected with propeller (22) by rotating shaft (23).
- The scounting aeroplane of a kind of single-person portable the most as claimed in claim 1, it is characterised in that: it is vertically installed with balance riser (42) on described empennage (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521115099.6U CN205418107U (en) | 2015-12-28 | 2015-12-28 | Single portable scounting aeroplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521115099.6U CN205418107U (en) | 2015-12-28 | 2015-12-28 | Single portable scounting aeroplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205418107U true CN205418107U (en) | 2016-08-03 |
Family
ID=56539017
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521115099.6U Expired - Fee Related CN205418107U (en) | 2015-12-28 | 2015-12-28 | Single portable scounting aeroplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205418107U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109866915A (en) * | 2019-02-02 | 2019-06-11 | 东北农业大学 | Unmanned autogyro brake gear |
-
2015
- 2015-12-28 CN CN201521115099.6U patent/CN205418107U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109866915A (en) * | 2019-02-02 | 2019-06-11 | 东北农业大学 | Unmanned autogyro brake gear |
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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: 20160803 Termination date: 20161228 |