CN207045736U - A kind of unmanned plane of the suitable emergent topographic support in city high rise building area - Google Patents
A kind of unmanned plane of the suitable emergent topographic support in city high rise building area Download PDFInfo
- Publication number
- CN207045736U CN207045736U CN201720949315.XU CN201720949315U CN207045736U CN 207045736 U CN207045736 U CN 207045736U CN 201720949315 U CN201720949315 U CN 201720949315U CN 207045736 U CN207045736 U CN 207045736U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- water conservancy
- conservancy diversion
- diversion axle
- rise building
- 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
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The utility model discloses a kind of unmanned plane of the suitable emergent topographic support in city high rise building area, deflector is set between existing Double layer rotating wing, including the vertical water conservancy diversion axle being located between Double layer rotating wing, the support member of guide vane and connection water conservancy diversion axle on water conservancy diversion axle, the rotating shaft of upper strata rotor blade and the rotating shaft of lower floor's rotor blade are by main shaft, countershaft and the shaft coupling of connection main shaft and countershaft form, support member is fixed on shaft coupling, the axis hole of water conservancy diversion axle insertion is provided with support member, the limit assembly for setting restricted water conservancy diversion axle to rotate in support member.Operator can control the rotation of water conservancy diversion axle by limit assembly, and then adjust the direction of deflector, on the one hand, the rapid increase of emergency condition can be ensured when deflector can increase the stability of unmanned plane, particularly wind direction disorder and is stably used；On the other hand, deflector can realize the fast steering of unmanned plane, improve sensitivity and controllability of the unmanned plane in the emergent mapping in city high rise building area.
Description
Technical field
The utility model belongs to unmanned plane construction applications, is a kind of suitable emergent mapping in city high rise building area specifically
The unmanned plane of guarantee.
Background technology
Unmanned plane has very important effect in mapping, can be with airborne sensory equipment, such as high resolution CCD number phase
Machine, light optical camera, infrared scanner, laser scanner, magnetic determining device etc. obtain information.For existing city high rise building area
, it is necessary to which surveying and drawing unmanned plane meets following characteristics during emergent mapping operation：（1）Can quickly it be taken off under emergency rating, the rate of climb is fast,
And flying speed is high；（2）Flight stability performance is good, meanwhile, there is good regulation performance, multi-obstacle avoidance can be realized by control
Flight.Existing patent document CN204368426U（A kind of double-deck rotor wing unmanned aerial vehicle, 2015.06.03）The double-deck rotation disclosed
Wing unmanned plane, including fuselage and three rotors on fuselage, each rotor are Dual-layer structure, Dual-layer knot
The rotor of structure drives rotation using coaxial rotor bar, and double-deck rotor structure may be such that unmanned plane during flying speed greatly improves, on
Lifting speed is accelerated.Although the double-deck rotor wing unmanned aerial vehicle improves the rate of climb and flying speed of unmanned machine equipment, but unmanned plane
Controllability need to be improved.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane of the suitable emergent topographic support in city high rise building area, existing
Having increases deflector between Double layer rotating wing, and operator can control the rotation of water conservancy diversion axle by limit assembly, and then adjust
The direction of deflector, on the one hand, emergency condition can be ensured when deflector can increase the stability of unmanned plane, particularly wind direction disorder
Rapid increase and stably use；On the other hand, deflector can realize the fast steering of unmanned plane, improve unmanned plane in city height
The sensitivity of the emergent mapping in building area and controllability.
The utility model is achieved through the following technical solutions：A kind of emergent topographic support in suitable city high rise building area nobody
Machine, including Double layer rotating wing setting up and down, the rotating shaft of upper strata rotor blade is coaxial with the rotating shaft of lower floor's rotor blade, Yu Shuan
Deflector is set between layer rotor blade, the deflector include the vertical water conservancy diversion axle being located between Double layer rotating wing,
The support member of guide vane and connection water conservancy diversion axle on water conservancy diversion axle, the rotating shaft of the upper strata rotor blade and lower floor's rotation
The rotating shaft of wing is formed by main shaft, countershaft and the shaft coupling of connection main shaft and countershaft, and support member is fixed on shaft coupling, is propped up
The axis hole of water conservancy diversion axle insertion, the limit assembly for setting restricted water conservancy diversion axle to rotate in support member are provided with support member.
The limit assembly is located at axis hole outside and acts on the relay controller of water conservancy diversion axle.
Accommodating chamber is set in the fuselage bottom of the unmanned plane, the bottom of accommodating chamber sets opening, telescopic cylinder is set in accommodating chamber,
The cylinder barrel of telescopic cylinder is fixed at the top of accommodating chamber, the piston rod connection mounting bracket of telescopic cylinder.
The opening sets cover plate and back-moving spring, back-moving spring one end connecting cover plate, back-moving spring other end connection cover
Plate, the mounting bracket are the installing mechanism of fixed instrument of surveying and mapping, and the pole for cover plate is provided as on mounting bracket.
The opening uses the split setting of two cover plates, and the pole is acted on two cover plates.
The utility model compared with prior art, has advantages below and beneficial effect：
（1）The utility model sets up deflector between existing Double layer rotating wing, deflector using water conservancy diversion axle and
Deflector is formed, and water conservancy diversion axle is worked by limit assembly to stop operating, and then controls the angle of deflector, when wind direction is disorderly
When, control the direction of deflector to increase the stability of unmanned plane, can particularly ensure the rapid increase and stably of emergency condition
Use, in addition, the turning velocity of unmanned plane can also be improved rapidly by changing the direction of deflector, especially suitable for city high rise building
The emergent mapping in area.
（2）The limit assembly that the utility model is related to can use relay controller, and unmanned aerial vehicle (UAV) control device is connected by circuit,
Operator can use the power on/off of remote control equipment control relay controller, and then realize the control in deflector direction, simple to operate
It is and easy to control.
（3）The utility model is provided with accommodating chamber in unmanned aerial vehicle body bottom, and instrument of surveying and mapping can be accommodated in by installed part
In accommodating chamber, in the emergent mapping of city high rise building, instrument of surveying and mapping can be avoided, which to receive collision, influences measurement effect, when needing to take pictures or
During measurement, operator controls cylinder piston to stretch out and shot by remote control equipment, simple in construction, and practicality is high.
Brief description of the drawings
Fig. 1 is the structural representation of the utility model deflector（One）.
Fig. 2 is the structural representation of the utility model deflector（Two）.
Fig. 3 is the structural representation of A shown in Fig. 1.
Fig. 4 is the structural representation of the utility model mounting bracket（One）.
Fig. 5 is the structural representation of the utility model mounting bracket（Two）.
Fig. 6 is the structural representation of the utility model cover plate.
Wherein, 1-upper strata rotor blade, 2-lower floor rotor blade, 3-water conservancy diversion axle, 4-guide vane, 5-support member,
6-main shaft, 7-countershaft, 8-shaft coupling, 9-axis hole, 10-limit assembly, 11-accommodating chamber, 12-opening, 13-stretch gas
Cylinder, 14-mounting bracket, 15-cover plate, 16-back-moving spring, 17-pole, 18-guiding gutter, 19-instrument of surveying and mapping.
Embodiment
The utility model is described in further detail with reference to embodiment, but embodiment of the present utility model is not
It is limited to this.
Embodiment 1：
The present embodiment proposes a kind of unmanned plane of the suitable emergent topographic support in city high rise building area.As shown in Fig. 1 structures,
The unmanned plane includes Double layer rotating wing setting up and down, and the rotating shaft of upper strata rotor blade 1 and the rotating shaft of lower floor rotor blade 2 are total to
Axle.To improve the performance of existing unmanned plane, deflector is provided between Double layer rotating wing, as shown in Figure 1 and Figure 2,
Deflector is using the vertically water conservancy diversion axle 3 between Double layer rotating wing, the guide vane 4 on water conservancy diversion axle 3 and connects
The support member 5 for connecing water conservancy diversion axle 3 forms, and the rotating shaft of upper strata rotor blade 1 and the rotating shaft of lower floor's rotor blade 2 are by main shaft 6, countershaft
7 and connect main shaft 6 and countershaft 7 shaft coupling 8 form, support member 5 is fixed on shaft coupling 8, and water conservancy diversion is provided with support member 5
The axis hole 9 that axle 3 inserts, the interior limit assembly 10 for setting restricted water conservancy diversion axle 3 to rotate of support member 5, as shown in figure 3, limit assembly
10, using being located at the outside of axis hole 9 and acting on the relay controller of water conservancy diversion axle 3, can connect the controller of unmanned plane by circuit,
Use the power on/off of remote control equipment control relay controller, you can realize the control in deflector direction.
It is smaller in calm or air quantity when the unmanned plane that the present embodiment is related to carries out emergent mapping operations in city high rise building area
When being not enough to influence flight, remote control equipment control unmanned aerial vehicle (UAV) control device powers off relay controller, and water conservancy diversion axle 3 can be in support member 5
Axis hole 9 in arbitrarily rotate, have no effect on flying speed；When air quantity increase or wind direction disorder influence flight, remote control equipment control
Unmanned aerial vehicle (UAV) control device processed makes relay controller be powered, and water conservancy diversion axle 3 is limited by relay controller and rotated, and deflector is fixed such as Fig. 1
Or 2 shown in structure, guiding gutter 18 is set on deflector, passes through the distinguished and admirable guiding gutter 18 by deflector between Double layer rotating wing
Export, avoids impacting ascending air caused by Double layer rotating wing, improves the stability of unmanned plane.Except this it
Outside, it is distinguished and admirable to pass through from guiding gutter 18 after deflector is fixed, moreover it is possible to the turning velocity of unmanned plane is improved, therefore, especially suitable for
The emergent mapping in city high rise building area.
Embodiment 2：
The present embodiment proposes the design of accommodating chamber 11 on the basis of embodiment 1, as shown in figure 4, in the fuselage of unmanned plane
Bottom sets accommodating chamber 11, and the bottom of accommodating chamber 11 sets opening 12, telescopic cylinder 13, the cylinder of telescopic cylinder 13 are set in accommodating chamber 11
Cylinder is fixed on the top of accommodating chamber 11 and connects unmanned aerial vehicle (UAV) control device, the piston rod connection mounting bracket 14 of telescopic cylinder 13, mounting bracket
14 are used to fix instrument of surveying and mapping 19.As shown in Figure 5, Figure 6, the present embodiment is provided with cover plate 15 and back-moving spring at opening 12
16, one end connecting cover plate 15 of back-moving spring 16, the other end connecting cover plate 15 of back-moving spring 16, it is provided as being used for cover plate on mounting bracket 14
15 pole 17.
In use, operator takes off unmanned plane to specified altitude assignment, unmanned aerial vehicle (UAV) control device is controlled to open by remote control equipment
Dynamic telescopic cylinder 13, the piston action of telescopic cylinder 13 drive the instrument of surveying and mapping 19 on mounting bracket 14 to move downward, mounting bracket 14 to
In lower motion process, pole 17 acts on cover plate 15 therewith, as shown in fig. 6, the cover plate 15 at opening 12 uses two cover plates 15
The mode of split setting, when pole 17 is acted on cover plate 15, cover plate 15 is opened therewith, and instrument of surveying and mapping 19 extends downwardly from accommodating
Chamber 11.After the completion of mapping, telescopic cylinder 13 is controlled by unmanned aerial vehicle (UAV) control device to be resetted, and cover plate 15 is in the presence of back-moving spring 16
It is closed at the opening 12 of accommodating chamber 11.
It is described above, only it is preferred embodiment of the present utility model, any formal limit is not done to the utility model
System, every any simple modification made according to the technical essence of the utility model to above example, equivalent variations, each falls within
Within the scope of protection of the utility model.
Claims (5)
1. a kind of unmanned plane of the suitable emergent topographic support in city high rise building area, including Double layer rotating wing setting up and down, on
Layer rotor blade（1）Rotating shaft and lower floor's rotor blade（2）Rotating shaft it is coaxial, it is characterised in that：Between Double layer rotating wing
Deflector is set, and the deflector includes the vertical water conservancy diversion axle being located between Double layer rotating wing（3）, located at water conservancy diversion axle
（3）On guide vane（4）And connection water conservancy diversion axle（3）Support member（5）, the upper strata rotor blade（1）Rotating shaft and under
Layer rotor blade（2）Rotating shaft by main shaft（6）, countershaft（7）And connection main shaft（6）With countershaft（7）Shaft coupling（8）Group
Into support member（5）It is fixed on shaft coupling（8）On, support member（5）On be provided with water conservancy diversion axle（3）The axis hole of insertion（9）, support member
（5）It is interior that restricted water conservancy diversion axle is set（3）The limit assembly of rotation（10）.
A kind of 2. unmanned plane of suitable emergent topographic support in city high rise building area according to claim 1, it is characterised in that：
The limit assembly（10）For located at axis hole（9）Outside simultaneously acts on water conservancy diversion axle（3）Relay controller.
A kind of 3. unmanned plane of suitable emergent topographic support in city high rise building area according to claim 1, it is characterised in that：
Accommodating chamber is set in the fuselage bottom of the unmanned plane（11）, accommodating chamber（11）Bottom set opening（12）, accommodating chamber（11）Inside set
Telescopic cylinder（13）, telescopic cylinder（13）Cylinder barrel be fixed on accommodating chamber（11）Top, telescopic cylinder（13）Piston rod connection
Mounting bracket（14）.
A kind of 4. unmanned plane of suitable emergent topographic support in city high rise building area according to claim 3, it is characterised in that：
The opening（12）Place sets cover plate（15）And back-moving spring（16）, back-moving spring（16）One end connecting cover plate（15）, back-moving spring
（16）Other end connecting cover plate（15）, the mounting bracket（14）For fixed instrument of surveying and mapping（19）Installing mechanism, mounting bracket（14）
On be provided as being used for cover plate（15）Pole（17）.
A kind of 5. unmanned plane of suitable emergent topographic support in city high rise building area according to claim 4, it is characterised in that：
The opening（12）Using two cover plates（15）Split setting, the pole（17）Act on two cover plates（15）On.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720949315.XU CN207045736U (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane of the suitable emergent topographic support in city high rise building area |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720949315.XU CN207045736U (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane of the suitable emergent topographic support in city high rise building area |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207045736U true CN207045736U (en) | 2018-02-27 |
Family
ID=61498849
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720949315.XU Expired - Fee Related CN207045736U (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane of the suitable emergent topographic support in city high rise building area |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207045736U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114571931A (en) * | 2022-04-24 | 2022-06-03 | 浙江大学 | Amphibious unmanned aerial vehicle |
-
2017
- 2017-08-01 CN CN201720949315.XU patent/CN207045736U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114571931A (en) * | 2022-04-24 | 2022-06-03 | 浙江大学 | Amphibious unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106347675A (en) | Remote control parachute | |
| CN105691606B (en) | A kind of the unmanned plane device and control method in high cruise duration | |
| CN205916329U (en) | Coaxial double -oar unmanned vehicles | |
| CN104828245A (en) | Aircraft | |
| CN107963209A (en) | Tandem wing tilting rotor wing unmanned aerial vehicle | |
| CN106240809A (en) | Novel guide based on fanjet controls multi-rotor aerocraft and control method | |
| CN107985589A (en) | Vertical take-off and landing drone with vectored thrust duct engine | |
| CN105468029A (en) | Unmanned aerial vehicle aerial shooting device and unmanned aerial vehicle aerial shooting method | |
| CN116639273A (en) | Unmanned aerial vehicle mapping data acquisition device and acquisition method thereof | |
| CN207045736U (en) | A kind of unmanned plane of the suitable emergent topographic support in city high rise building area | |
| CN105129088B (en) | Spherical uniaxial rudder oriented intelligent aircraft | |
| WO2020238137A1 (en) | Unmanned aerial vehicle parking device and unmanned aerial vehicle shutdown system | |
| CN106406341A (en) | Flight control method for quadrotor unmanned aerial vehicle | |
| Li et al. | The design and testing of a LiDAR Platform for a UAV for heritage mapping | |
| CN110143274B (en) | Wing assembly, unmanned aerial vehicle and control method of wing assembly | |
| CN106314789A (en) | Wing, fixed-wing aircraft and fixed-wing aircraft lifting method | |
| CN113799969A (en) | Side window slipstream formula duct unmanned aerial vehicle | |
| CN106428524A (en) | Multi-rotor wing aircraft with free wing | |
| CN109592007A (en) | Double mode unmanned plane working method and double mode unmanned plane | |
| WO2022130542A1 (en) | Landing facility, landing method | |
| CN212709964U (en) | But VTOL aircraft based on rotor and fan wing | |
| CN104843191A (en) | Non-contact type intelligent rainproof device for unmanned aerial vehicle | |
| CN206096947U (en) | Four rotor crafts suitable for indoor autonomous flight | |
| CN202219839U (en) | Omnidirectional flight wing structure of vertically taking-off and landing aircraft | |
| CN205440866U (en) | Rotorcraft aircraft verts |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20180227 Termination date: 20190801 |