CN208602705U - A kind of mapping unmanned plane for capableing of VTOL - Google Patents
A kind of mapping unmanned plane for capableing of VTOL Download PDFInfo
- Publication number
- CN208602705U CN208602705U CN201821255849.3U CN201821255849U CN208602705U CN 208602705 U CN208602705 U CN 208602705U CN 201821255849 U CN201821255849 U CN 201821255849U CN 208602705 U CN208602705 U CN 208602705U
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- China
- Prior art keywords
- mapping
- unmanned plane
- driving
- protective shell
- vtol
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Abstract
The utility model discloses the mapping unmanned planes that one kind is capable of VTOL; including four axis unmanned planes and mapping radar; there are four propellers for the corresponding installation in the drive shaft top on four axis unmanned plane tops two sides; it is bolted to connection in the middle part of four axis uav bottoms in the top of protective shell; the utility model; it is rotated using traveling motor driven screw rod; it is mobile by the rotate driving feed screw nut of screw rod; feed screw nut is mobile to drive the mobile control mapping radar lifting of straight-bar, protects mapping radar convenient for protective case；Become driving driving gear after turning round using driving motor output power and by retarder to rotate; shaft rotation is driven by driving gear driving driven gear; shaft drives the U-shaped leg rotation of supporting leg; adjust leg location; influence of the supporting leg to four axis unmanned plane during flying postures is reduced, the supporting leg of horizontality is conducive to four axis unmanned planes of protection and propeller.
Description
Technical field
The utility model relates to unmanned plane correlative technology field, specially a kind of mapping unmanned plane for capableing of VTOL.
Background technique
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, are carried out with computer to image information
Processing, and image is fabricated to according to certain required precision.For the total demand for adapting to town development, comprehensive geographic, resource are provided
Information.Correctly, completely information material be science decision basis.Mapping radar is a kind of very widely used application mapping
Mapping radar is applied in unmanned plane and is conducive to mapping radar and surveys and draws by device, the four axis unmanned plane supporting legs to take off vertically
Its flight attitude is influenced, the blade of four axis unmanned planes, which is exposed to outside, is exposed to outer plotting board vulnerable to destruction in unmanned plane
Plotting board is hit vulnerable to destruction in the case of the vibration or unmanned plane aircraft bombing that generate in flight course, influences to survey and draw work
That makees is normally carried out.It is capable of the mapping unmanned plane of VTOL the utility model proposes one kind thus for solving the above problems.
Utility model content
The purpose of this utility model is to provide the mapping unmanned planes that one kind is capable of VTOL, to solve above-mentioned background skill
The problem of being proposed in art.
To achieve the above object, the utility model provides the following technical solutions: one kind be capable of VTOL mapping nobody
Machine, including four axis unmanned planes and mapping radar, there are four the corresponding installations in the drive shaft top of the four axis unmanned plane top two sides
Propeller is bolted to connection in the middle part of the four axis uav bottom at the top of the top of protective shell, the protective shell
Seal chamber inner vertical traveling motor is installed, the top of the output shaft end connection wire rod of the traveling motor, the silk
Bar is threadedly coupled feed screw nut, and the feed screw nut side is welded with straight-bar vertically, and the bottom end of the straight-bar is fixedly connected with mapping
The center of radar top surface, the lower part of the protective shell two sides, which corresponds to, is horizontally installed with two groups of driving box, in the driving box
The lower part of side is horizontally installed with shaft along its length, and the middle position of the shaft is vertically-mounted driven gear, described
The top of driven gear is engaged with driving gear, and the driving gear is vertically installed at the output shaft end of retarder, described to subtract
The output shaft end of the input axis connection driving motor of fast device, the driving motor are horizontally arranged at the upside inside driving box,
The both ends of the shaft is correspondingly connected with the both ends of supporting leg, and the supporting leg includes U-shaped leg and connector sleeve, and the both ends of the U-shaped leg are corresponding
Two groups of connector sleeves are welded with vertically, connector sleeve described in two groups is correspondingly sleeved on the outside of both ends of the shaft.
Preferably, the supporting leg further includes limit hole, and the corresponding supporting leg two sides that are provided with of two limit holes are close to driving
The position of case.
Preferably, it states the two sides correspondence inside driving box and is horizontally installed with two groups of cylinders, the piston rod of cylinder described in two groups
End is corresponding to be equipped with two pieces of rubber blocks, the limit hole when piston-rod end position of cylinder described in two groups and supporting leg tilt upwards
Position matches.
Preferably, corresponding be fitted into is equipped with two groups of bearings, the shaft in the through-hole that the driving lower box part two sides open up
Both ends it is corresponding across two groups of bearings.
Preferably, the two sides inside the protective shell are corresponding is welded with two guide rails, the side of two guide rails vertically
It is corresponding to be slidably fitted with two pieces of slides, the corresponding two sides connected at the top of mapping radar by two connecting rods of two pieces of slides, institute
The middle position for stating protective shell bottom offers the through-hole passed through for straight-bar.
Preferably, the bottom of the protective shell is welded with protective case, and the mapping radar is mounted on the inside of protective case, institute
The top vertical for stating protective shell is welded with connecting plate.
Preferably, it is socketed with rubber sleeve outside the bolt of the four axis unmanned plane connection protective shell, the propeller is four
Leaf.
Compared with prior art, the utility model has the beneficial effects that
1. being rotated using traveling motor driven screw rod, mobile by the rotate driving feed screw nut of screw rod, feed screw nut is mobile
The mobile control mapping radar lifting of straight-bar is driven, protects mapping radar convenient for protective case；
2. becoming driving driving gear after turning round using driving motor output power and by retarder to rotate, driven by driving gear
Dynamic driven gear drives shaft rotation, and shaft drives the U-shaped leg rotation of supporting leg, adjusts leg location, reduce supporting leg to four axis without
The supporting leg of the influence of man-machine flight attitude, horizontality is conducive to four axis unmanned planes of protection and propeller；
3, it is mounted between four axis unmanned planes and protective shell using rubber sleeve, is conducive to buffering vibration, protects mapping radar
Safety.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the protective shell the schematic diagram of the section structure of the utility model；
Fig. 3 is the driving box the schematic diagram of the section structure of the utility model.
In figure: four axis unmanned planes 1, propeller 2, protective shell 3, supporting leg 4, U-shaped leg 41, connector sleeve 42, limit hole 43, driving
Case 5, rubber sleeve 6, traveling motor 7, screw rod 8, straight-bar 9, mapping radar 10, guide rail 11, slide 12, protective case 13, connecting plate 14,
Shaft 15, driven gear 16, driving gear 17, retarder 18, driving motor 19, cylinder 20, feed screw nut 21, bearing 22.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3 is please referred to, the utility model provides a kind of technical solution: one kind capableing of the mapping unmanned plane of VTOL,
Including four axis unmanned planes 1 and mapping radar 10, there are four spirals for the corresponding installation in the drive shaft top of four axis unmanned planes, 1 top two sides
Paddle 2 is bolted to connection in the middle part of four axis unmanned planes, 1 bottom in the top of protective shell 3, the seal chamber at 3 top of protective shell
Inner vertical is equipped with traveling motor 7, the top of the output shaft end connection wire rod 8 of traveling motor 7, and screw rod 8 is threadedly coupled silk
Stem nut 21,21 side of feed screw nut are welded with straight-bar 9 vertically, and the bottom end of straight-bar 9 is fixedly connected in 10 top surface of mapping radar
Heart position, traveling motor 7 drive screw rod 8 to rotate, and mobile by the rotate driving feed screw nut 21 of screw rod 8, feed screw nut 21 is mobile
It drives the mobile control mapping radar 10 of straight-bar 9 to go up and down, protects mapping radar 10, the lower part of 3 two sides of protective shell convenient for protective case 13
Corresponding to be horizontally installed with two groups of driving box 5, the lower part of 5 inside of driving box is horizontally installed with shaft 15, shaft along its length
15 middle position is vertically-mounted driven gear 16, and the top of driven gear 16 is engaged with driving gear 17, driving gear 17
It is vertically installed at the output shaft end of retarder 18, the output shaft end of the input axis connection driving motor 19 of retarder 18 drives
Dynamic motor 19 is horizontally arranged at the upside inside driving box 5, and 15 both ends of shaft are correspondingly connected with the both ends of supporting leg 4, and supporting leg 4 includes U
Type leg 41 and connector sleeve 42, the both ends of U-shaped leg 41 are corresponding to be welded with two groups of connector sleeves 42, the corresponding socket of two groups of connector sleeves 42 vertically
In the outside at 15 both ends of shaft, 19 output power of driving motor is simultaneously rotated by driving driving gear 17 after the change torsion of retarder 18,
Drive driven gear 16 that shaft 15 is driven to rotate by driving gear 17, shaft 15 drives the U-shaped leg 41 of supporting leg 4 to rotate, adjustment branch
4 position of leg, reduces influence of the supporting leg 4 to four axis unmanned planes, 1 flight attitude, the supporting leg 4 of horizontality be conducive to four axis of protection nobody
Machine 1 and propeller 2.
Further, supporting leg 4 further includes limit hole 43, and corresponding 4 two sides of supporting leg that are provided with of two limit holes 43 are close to driving
The position of case 5.
Further, the two sides correspondence inside driving box 5 is horizontally installed with two groups of cylinders 20, the piston rod of two groups of cylinders 20
End is corresponding to be equipped with two pieces of rubber blocks, the limit hole when piston-rod end position of two groups of cylinders 20 and supporting leg 4 tilt upwards
43 positions match.
Further, corresponding be fitted into is equipped with two groups of bearings 22 in the through-hole that 5 lower part two sides of driving box open up, shaft 15
Both ends are corresponding across two groups of bearings 22.
Further, the two sides inside protective shell 3 are corresponding is welded with two guide rails 11, the side pair of two guide rails 11 vertically
Two pieces of slides 12 should be slidably fitted with, the corresponding two sides that 10 top of mapping radar is connected by two connecting rods of two pieces of slides 12 are protected
The middle position of 3 bottom of protective case offers the through-hole passed through for straight-bar 9.
Further, the bottom of protective shell 3 is welded with protective case 13, and mapping radar 10 is mounted on the inside of protective case 13,
The top vertical of protective shell 3 is welded with connecting plate 14.
Further, it is socketed with rubber sleeve 6 outside the bolt of four axis unmanned planes 1 connection protective shell 3, rubber sleeve 6 is mounted on
Between the 3 of four axis unmanned planes 1 and protective shell, it is conducive to buffering vibration, protects the safety of mapping radar 10, propeller 2 is four leaves.
Working principle: in actual work, operator control four axis unmanned planes 1 take off vertically after control mapping radar 10 into
Row mapping operations, driving box 5 works when four axis unmanned planes 1 take off, and the driving motor 19 inside driving box 5 works output power simultaneously
Output driving driving gear 17 rotates after retarder 18 becomes and turns round, the rotation of 17 rotate driving driven gear 16 of driving gear, by
The rotation of driven gear 16 drives shaft 15 to rotate, and shaft 15 smoothly rotates under the action of two groups of bearing 22, shaft 22
Rotation drives the U-shaped leg 41 connected by connector sleeve 42 to rotate and U-shaped 41 vertical state of leg is adjusted to acclivitous state, reduces
Influence of the supporting leg 4 when four axis unmanned planes 1 are mobile to flight attitude, while the branch at 2 edge of propeller of prominent four axis unmanned planes 1
It protects four axis unmanned planes 1 and propeller 2 on the outside of the U-shaped leg 41 of leg 4, reduces in four axis unmanned planes, 1 flight course and touched with object
It hits, protects the safety of body, the adjustment of 4 position of supporting leg completes exhaust hood 20 and works, and the piston rod stretching of cylinder 20 makes its end
U-shaped leg 41 is positioned in rubber block insertion limit hole 43, whole process is reversed when four axis unmanned planes 1 land；Unmanned plane into
Operator controls the rotation of 7 task driven screw rod 8 of traveling motor when row mapping, is moved by the rotate driving feed screw nut 21 of screw rod 8
Dynamic, the movement of feed screw nut 21 drives the mobile control mapping radar 10 of straight-bar 9 mobile, to control the stretching of mapping radar 10 or retraction
Inside protective case 13, mapping radar 10 is avoided to come to harm.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (7)
1. one kind is capable of the mapping unmanned plane of VTOL, including four axis unmanned planes (1) and mapping radar (10), feature exists
In: four axis unmanned plane (1) top two sides the corresponding installation in drive shaft top there are four propeller (2), four axis nobody
It is bolted to connection in the middle part of machine (1) bottom in the seal chamber at the top of the top of protective shell (3), the protective shell (3)
Portion is vertically-mounted to be had traveling motor (7), the top of the output shaft end connection wire rod (8) of the traveling motor (7), the screw rod
(8) feed screw nut (21) are threadedly coupled, feed screw nut (21) side is welded with straight-bar (9) vertically, the bottom of the straight-bar (9)
End is fixedly connected with the center of mapping radar (10) top surface, and the lower part correspondence of protective shell (3) two sides is horizontally installed with two
It organizes driving box (5), the lower part on the inside of the driving box (5) is horizontally installed with shaft (15), the shaft along its length
(15) middle position is vertically-mounted to be had driven gear (16), and top and the driving gear (17) of the driven gear (16) are nibbled
It closes, the driving gear (17) is vertically installed at the output shaft end of retarder (18), and the input shaft of the retarder (18) connects
The output shaft end of driving motor (19) is connect, the driving motor (19) is horizontally arranged at the internal upside of driving box (5), described
Shaft (15) both ends are correspondingly connected with the both ends of supporting leg (4), and the supporting leg (4) includes U-shaped leg (41) and connector sleeve (42), the U
The both ends correspondence of type leg (41) is welded with two groups of connector sleeves (42) vertically, and connector sleeve described in two groups (42) is correspondingly sleeved on shaft
(15) outside at both ends.
2. the mapping unmanned plane that one kind according to claim 1 is capable of VTOL, it is characterised in that: the supporting leg (4)
It further include limit hole (43), two limit hole (43) correspondences are provided with supporting leg (4) two sides close to the position of driving box (5).
3. the mapping unmanned plane that one kind according to claim 1 is capable of VTOL, it is characterised in that: the driving box
(5) internal two sides are corresponding is horizontally installed with two groups of cylinders (20), the corresponding installation of the piston-rod end of cylinder described in two groups (20)
There are two pieces of rubber blocks, the limit hole (43) when the piston-rod end position and supporting leg (4) of cylinder described in two groups (20) tilt upwards
Position matches.
4. the mapping unmanned plane that one kind according to claim 1 is capable of VTOL, it is characterised in that: the driving box
(5) corresponding chimeric in the through-hole that lower part two sides open up that two groups of bearings (22) are installed, the both ends of the shaft (15) it is corresponding across
Two groups of bearings (22).
5. the mapping unmanned plane that one kind according to claim 1 is capable of VTOL, it is characterised in that: the protective shell
(3) internal two sides are corresponding is welded with two guide rails (11) vertically, and the side correspondence of two guide rails (11) is slidably fitted with
Two pieces of slides (12), the corresponding two sides by the top of two connecting rod connections mapping radar (10) of two pieces of slides (12) are described
The middle position of protective shell (3) bottom offers the through-hole passed through for straight-bar (9).
6. the mapping unmanned plane that one kind according to claim 1 is capable of VTOL, it is characterised in that: the protective shell
(3) bottom is welded with protective case (13), and the mapping radar (10) is mounted on the inside of protective case (13), the protective shell
(3) top vertical is welded with connecting plate (14).
7. the mapping unmanned plane that one kind according to claim 1 is capable of VTOL, it is characterised in that: four axis nobody
It is socketed with rubber sleeve (6) outside the bolt of machine (1) connection protective shell (3), the propeller (2) is four leaves.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821255849.3U CN208602705U (en) | 2018-08-05 | 2018-08-05 | A kind of mapping unmanned plane for capableing of VTOL |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821255849.3U CN208602705U (en) | 2018-08-05 | 2018-08-05 | A kind of mapping unmanned plane for capableing of VTOL |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208602705U true CN208602705U (en) | 2019-03-15 |
Family
ID=65671531
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821255849.3U Active CN208602705U (en) | 2018-08-05 | 2018-08-05 | A kind of mapping unmanned plane for capableing of VTOL |
Country Status (1)
| Country | Link |
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| CN (1) | CN208602705U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110203393A (en) * | 2019-06-19 | 2019-09-06 | 山西大学 | A kind of quickly mapping multi-rotor unmanned aerial vehicle and its mapping method |
| CN114735218A (en) * | 2022-04-12 | 2022-07-12 | 江苏信博建设项目管理有限公司 | Three-dimensional topography mapping device based on unmanned aerial vehicle |
| CN117054973A (en) * | 2023-10-11 | 2023-11-14 | 深圳市金众工程检验检测有限公司 | Wireless directional radar equipment for surveying and mapping engineering |
-
2018
- 2018-08-05 CN CN201821255849.3U patent/CN208602705U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110203393A (en) * | 2019-06-19 | 2019-09-06 | 山西大学 | A kind of quickly mapping multi-rotor unmanned aerial vehicle and its mapping method |
| CN114735218A (en) * | 2022-04-12 | 2022-07-12 | 江苏信博建设项目管理有限公司 | Three-dimensional topography mapping device based on unmanned aerial vehicle |
| CN117054973A (en) * | 2023-10-11 | 2023-11-14 | 深圳市金众工程检验检测有限公司 | Wireless directional radar equipment for surveying and mapping engineering |
| CN117054973B (en) * | 2023-10-11 | 2023-12-12 | 深圳市金众工程检验检测有限公司 | Wireless directional radar equipment for surveying and mapping engineering |
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