CN206552254U - Portable unmanned machine - Google Patents
Portable unmanned machine Download PDFInfo
- Publication number
- CN206552254U CN206552254U CN201720234113.7U CN201720234113U CN206552254U CN 206552254 U CN206552254 U CN 206552254U CN 201720234113 U CN201720234113 U CN 201720234113U CN 206552254 U CN206552254 U CN 206552254U
- Authority
- CN
- China
- Prior art keywords
- fixed
- telescopic bar
- motor
- undercarriage
- auxiliary telescopic
- 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
Landscapes
- Toys (AREA)
Abstract
The utility model is related to a kind of Portable unmanned machine, belong to unmanned air vehicle technique field, it is simple in construction there is provided one kind, it is reasonable in design, it is easy to use, it disclosure satisfy that the Portable unmanned machine of various landform, the technical scheme used is provided with transmission horn for the both sides of body, rotor is provided with the transmission horn, the organism bottom is fixed with undercarriage, auxiliary telescopic bar is fixed with the inside of the undercarriage, motor is connected with the auxiliary telescopic bar, the auxiliary telescopic bar is separately fixed on four supporting legs of undercarriage, the control button for connecting each motor is provided with the unmanned aerial vehicle (UAV) control device;The utility model is widely used in unmanned plane.
Description
Technical field
The utility model is related to a kind of Portable unmanned machine, belongs to unmanned air vehicle technique field.
Background technology
With the development of the social economy, unmanned plane(For example:Multi-axis aircraft)With its dexterity, convenience and easily manipulation
Property, gradually it is widely used in all trades and professions.By taking Multi-axis aircraft as an example, the usual aircraft includes body, horn, spiral
The devices such as oar, motor and flight control.
At present, the undercarriage of existing unmanned plane is mainly using fixed structure, so in the wild in use, due to ground
Injustice, unmanned plane can not stable landing, cause unmanned plane to topple over, cause rotor to damage.
Utility model content
To solve the technical problem that prior art is present, the utility model is reasonable in design there is provided a kind of simple in construction, makes
With convenient, the Portable unmanned machine of various landform disclosure satisfy that.
To achieve the above object, the technical scheme that the utility model is used for Portable unmanned machine, including:Body and nothing
Human-machine Control device, the both sides of the body, which are provided with transmission horn, the transmission horn, is provided with rotor, the organism bottom
It is fixed with the inside of undercarriage, the undercarriage and is fixed with auxiliary telescopic bar, motor is connected with the auxiliary telescopic bar,
The auxiliary telescopic bar is separately fixed on four supporting legs of undercarriage, is provided with the unmanned aerial vehicle (UAV) control device every for connecting
The control button of individual motor.
It is preferred that, the auxiliary telescopic bar is mainly made up of fixed sleeving, moving casing and drive lead screw, the fixed cover
Flange is provided with the top of pipe, the motor is fixed on flange, the output shaft phase of the drive lead screw and motor
Connection, the moving casing is slidably mounted in fixed sleeving, is provided with the fixed sleeving for supporting drive lead screw
Hold-down support, described moving casing one end is internally provided with screw, and the other end is internally provided with guide sleeve, the moving casing
End is fixed with baffle plate.
It is preferred that, hemispherical support rubber bodies are fixed with the baffle plate.
Compared with prior art, the utility model has following technique effect:The utility model is simple in construction, user
Just, auxiliary telescopic bar is installed using in the inner side of undercarriage, when running into the landform of injustice, by adjusting the length of expansion link,
Unmanned plane is supported, it is ensured that unmanned plane landing is more steady.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the structural representation of auxiliary telescopic bar in the utility model.
Embodiment
In order that technical problem to be solved in the utility model, technical scheme and beneficial effect are more clearly understood, with
Lower combination drawings and Examples, the utility model is further elaborated.It should be appreciated that specific reality described herein
Example is applied only to explain the utility model, is not used to limit the utility model.
As shown in Figure 1 and Figure 2, Portable unmanned machine, including:Body 1 and unmanned aerial vehicle (UAV) control device, the both sides of body 1 are provided with
It is driven on horn 2, transmission horn 2 and is provided with rotor 3, the bottom of body 1 is fixed with undercarriage 4, the inner side of undercarriage 4 is fixed with auxiliary
Help and motor 6 is connected with expansion link 5, auxiliary telescopic bar 5, auxiliary telescopic bar 5 is separately fixed at four supporting legs of undercarriage 4
On, the control button for connecting each motor is provided with unmanned aerial vehicle (UAV) control device.
Wherein, auxiliary telescopic bar 5 is mainly made up of fixed sleeving 7, moving casing 8 and drive lead screw 9, fixed sleeving 7
Top is provided with flange 10, and motor 6 is fixed on flange 10, and drive lead screw 9 is connected with the output shaft of motor 6,
Moving casing 8 is slidably mounted in fixed sleeving 7, and the hold-down support 12 for supporting drive lead screw is provided with fixed sleeving 7,
The one end of moving casing 8 is internally provided with screw 13, and the other end is internally provided with guide sleeve 14, and the end of moving casing 8 is fixed with
Hemispherical support rubber bodies 11 are fixed with baffle plate 15, baffle plate 15.
When in use, when unmanned plane lands, according to the situation on ground, by the control button on unmanned aerial vehicle (UAV) control device,
The motor on each supporting leg is controlled to be acted, motor driving drive lead screw is rotated, and makes the screw in moving casing
Moving casing is driven along fixed cover in-pipe, so as to be supported to nobody, it is ensured that unmanned plane landing is more steady.
Preferred embodiment of the present utility model is the foregoing is only, it is all at this not to limit the utility model
Any modifications, equivalent substitutions and improvements made within the spirit and principle of utility model etc., all should be wrapped in the utility model model
In enclosing.
Claims (3)
1. Portable unmanned machine, including:Body and unmanned aerial vehicle (UAV) control device, the both sides of the body are provided with transmission horn, described
Rotor is provided with transmission horn, the organism bottom is fixed with undercarriage, it is characterised in that:The inner side of the undercarriage is fixed
Have and motor is connected with auxiliary telescopic bar, the auxiliary telescopic bar, the auxiliary telescopic bar is separately fixed at undercarriage
On four supporting legs, the control button for connecting each motor is provided with the unmanned aerial vehicle (UAV) control device.
2. Portable unmanned machine according to claim 1, it is characterised in that:The auxiliary telescopic bar is main by fixed cover
Pipe, moving casing and drive lead screw are constituted, and are provided with flange at the top of the fixed sleeving, the motor is fixed on flange
On, the drive lead screw is connected with the output shaft of motor, and the moving casing is slidably mounted in fixed sleeving, described
The hold-down support for supporting drive lead screw is provided with fixed sleeving, described moving casing one end is internally provided with screw, separately
One end is internally provided with guide sleeve, and the end of the moving casing is fixed with baffle plate.
3. Portable unmanned machine according to claim 2, it is characterised in that:Hemispherical support rubber is fixed with the baffle plate
Colloid.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720234113.7U CN206552254U (en) | 2017-03-12 | 2017-03-12 | Portable unmanned machine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720234113.7U CN206552254U (en) | 2017-03-12 | 2017-03-12 | Portable unmanned machine |
Publications (1)
Publication Number | Publication Date |
---|---|
CN206552254U true CN206552254U (en) | 2017-10-13 |
Family
ID=60363096
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201720234113.7U Expired - Fee Related CN206552254U (en) | 2017-03-12 | 2017-03-12 | Portable unmanned machine |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN206552254U (en) |
-
2017
- 2017-03-12 CN CN201720234113.7U patent/CN206552254U/en not_active Expired - Fee Related
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN206125436U (en) | Many rotors of abnormal shape plant protection unmanned aerial vehicle | |
CN202717030U (en) | Eight-axis rotor craft | |
CN206243457U (en) | A kind of automatic deploying and retracting landing gear structure for multi-rotor unmanned aerial vehicle | |
CN104908936A (en) | Unmanned helicopter | |
CN107554783A (en) | A kind of amphibious unmanned plane of VTOL | |
CN104986328A (en) | Variable-propeller-pitch multi-rotor aircraft driven by multiple oil engines | |
CN201376667Y (en) | Mid-air air pollution measurement sampling patrol robot | |
CN206552254U (en) | Portable unmanned machine | |
CN202666408U (en) | Six-arm model aerial propeller | |
CN206031802U (en) | Unmanned plane megaphone | |
CN206374990U (en) | A kind of new unmanned plane motor cabinet | |
CN206336422U (en) | Vertical fin duct steering driving mechanism under power-line patrolling unmanned airship | |
CN205087140U (en) | Oil moves six coaxial rotor unmanned aerial vehicle frame systems of displacement | |
CN205345319U (en) | Tailplane can vert with power unit | |
CN207417138U (en) | Multi-rotor unmanned aerial vehicle | |
CN203332262U (en) | Extensible robot chassis | |
CN202499276U (en) | Electric flying platform | |
CN106606871A (en) | Aircraft having flight protection system | |
CN207346095U (en) | A kind of fixed-wing system of verting that can efficiently take off and fly before efficient | |
CN201597754U (en) | Helicopter with elevation assisting device | |
CN205730359U (en) | A kind of aeromodelling airplane of band multifunctional detecting device | |
CN207875993U (en) | A kind of unmanned helicopter dynamical system | |
CN206107561U (en) | Long flight time aircraft | |
CN107097945A (en) | multi-rotor unmanned aerial vehicle | |
CN108033022A (en) | Spray aircraft in a kind of whirlpool |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171013 Termination date: 20180312 |
|
CF01 | Termination of patent right due to non-payment of annual fee |