CN207015575U - Take photo by plane unmanned plane - Google Patents
Take photo by plane unmanned plane Download PDFInfo
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- CN207015575U CN207015575U CN201720645054.2U CN201720645054U CN207015575U CN 207015575 U CN207015575 U CN 207015575U CN 201720645054 U CN201720645054 U CN 201720645054U CN 207015575 U CN207015575 U CN 207015575U
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Abstract
Taken photo by plane unmanned plane the utility model discloses one kind, including head, two wings, fuselage, tail, two empennages, two groups of advancing slip wheel carriers, two groups of rear wheel framves and four wheels, head is arranged on the head of fuselage, wing is located at the both sides of fuselage, empennage is arranged on the both sides of tail, and fuselage has the first chamber of upper lid, placing battery and flight controller, places the second chamber of camera and places the 3rd chamber of data radio station；The empennage of tail both sides is in splayed downwards, the side of tail is provided with outwardly erecting bed, two sides of erecting bed are provided with inside cone groove, the top of empennage is provided with two hook plates, the madial wall for hooking the top of plate is provided with the hook being used cooperatively with cone groove, hooking in cone groove makes tail be fixedly connected with empennage, and the top of empennage, which is provided with, covers on erecting bed with hooking the connection shell on the outside of plate.Empennage of the present utility model is downward, avoid unmanned plane drop to ground after empennage collided.
Description
Technical field
The technical field of unmanned plane is the utility model is related to, it is especially a kind of simple in construction, easy disassembly to take photo by plane nobody
Machine.
Background technology
Unmanned plane because have the advantages that mobility strong, the visual field extensively, flight path do not limited by landform, and be widely used
In survey and draw, take photo by plane, traffic monitoring, security protection agricultural and express delivery dispatching etc. multiple fields.
With the continuous development of modern unmanned air vehicle technique, unmanned plane also gradually from the change that becomes popular of specialization,
The continuous popularization of unmanned air vehicle technique, the unmanned plane species for taking photo by plane is also more and more, but it is work high above the ground to have unmanned plane,
Stability Analysis of Structures is extremely important, but the assembling of unmanned plane is all more complicated now, and accuracy is higher, it is not easy to operates, damages
Afterwards, it is more to repair or change the expense of parts, user is caused to perplex, simultaneously because empennage is upward, unmanned plane drop
It can be released a parachute when falling, unmanned plane is overturn 180 °, upward empennage, when unmanned plane drops to ground, empennage can be damaged.
The content of the invention
The technical problems to be solved in the utility model is：In order to solve to be asked existing for the prior art in above-mentioned background technology
A kind of topic, there is provided improved unmanned plane of taking photo by plane.
Technical scheme is used by the utility model solves its technical problem：One kind is taken photo by plane unmanned plane, including head, two
Individual wing, fuselage, tail, two empennages, two groups of advancing slip wheel carriers, two groups of rear wheel framves and four wheels, head are arranged on fuselage
Head, wing is located at the both sides of fuselage, and empennage is arranged on the both sides of tail, described fuselage have upper lid, placing battery and
The first chamber (32) of flight controller, the second chamber for placing camera and the 3rd chamber for placing data radio station；
The empennage of described tail both sides is in splayed downwards, and the side of described tail is provided with outwardly installation
Platform, two sides of erecting bed are provided with inside cone groove, and the top of described empennage is provided with two hook plates, hooks the top of plate
Madial wall is provided with the hook being used cooperatively with cone groove, and hooking in cone groove makes tail be fixedly connected with empennage, described empennage
Top be provided with cover on erecting bed with hook plate on the outside of connection shell；
Two groups of described advancing slip wheel carriers set up separately has bent rod and support bar, bent rod in the both sides of fuselage, advancing slip wheel carrier
One end be connected on fuselage, the other end is connected on two wheels, and one end of support bar is connected to the bottom of fuselage, and its is another
End is connected with wheel；
Described rear wheel frame sets up separately in the both sides of drive end unit, and rear wheel frame has pole, and one end of pole is arranged on machine
On the bottom surface of body afterbody, the other end is connected on two other wheel.
At least two groups of described hook plate.
Be provided with described tail fixed cover can 360 ° rotation knobs.
Described connection shell is provided with mounting blocks, and the other end of mounting blocks extends to the lateral surface of empennage, opened in mounting blocks
There is screwed hole, being inserted by bolt in screwed hole, which makes tail be reinforced with empennage, connects.
The beneficial effects of the utility model are that of the present utility model simple in construction, easy to operate, empennage is downward, can avoid
Empennage is collided after unmanned plane drops to ground, while all parts are reasonable in design, and unmanned plane body weight is lighter, volume is smaller.
Brief description of the drawings
The utility model is further illustrated with reference to the accompanying drawings and examples.
Fig. 1 is overall structure diagram of the present utility model.
Fig. 2 is structural representation of the present utility model.
Fig. 3 is side view of the present utility model.
Fig. 4 is the utility model empennage and the structural representation after fuselage installation.
Fig. 5 is the structural representation of the utility model empennage and fuselage.
In figure：1st, head, 2, wing, 3, fuselage, 31, upper lid, 32, first chamber, 33, second chamber, the 34, the 3rd chamber
Room, 4, tail, 41, erecting bed, 411, cone groove, 5, empennage, 51, hook plate, 511, hook, 6, connection shell, 61, mounting blocks, 7,
Advancing slip wheel carrier, 71, bent rod, 72, support bar, 8, rear wheel frame, 81, pole, 9, wheel, 10, knob.
Embodiment
The utility model is described in further detail presently in connection with accompanying drawing.These accompanying drawings are simplified schematic diagram,
Only illustrate basic structure of the present utility model in a schematic way, therefore it only shows the composition relevant with the utility model.
As Figure 1-Figure 5, during installation, upper lid 31 is opened, battery and flight controller are put into first chamber 32, phase
Machine is put into second chamber 33, data radio station is put into the 3rd chamber 34, then changes upper lid 31, Turning knob 10, in fixation
Lid 31；When assembling empennage 5, two hook plates 51 are blocked into the both sides to erecting bed 41, hook 511 hooks cone groove 411, then passed through
Bolt inserts the screwed hole of mounting blocks 61, tightens screw bolt reinforcing empennage 5 and tail 4, while by bent rod 71 and support bar 72
One end is connected on the axle of wheel 9, and the other end of bent rod 71 and support bar 72 is separately fixed on fuselage 3, by pole
81 one end is fixed on the wheel 9 of end, and the other end is connected on fuselage 3, can both complete to install.
Using it is above-mentioned according to desirable embodiment of the present utility model as enlightenment, pass through above-mentioned description, related work people
Member can carry out various changes and amendments in the range of without departing from this item utility model technological thought completely.This item is real
The content being not limited to new technical scope on specification, it is necessary to which its technology is determined according to right
Property scope.
Claims (4)
- The unmanned plane 1. one kind is taken photo by plane, including head (1), two wings (2), fuselage (3), tail (4), two empennages (5), two groups Advancing slip wheel carrier (7), two groups of rear wheel framves (8) and four wheels (9), head (1) are arranged on the head of fuselage (3), wing (2) position In the both sides of fuselage (3), empennage (5) is arranged on the both sides of tail (4), it is characterized in that：Described fuselage (3) has upper lid (31), the first chamber of placing battery and flight controller (32), the second chamber (33) of placement camera and placement data radio station The 3rd chamber (34)；The empennage (5) of described tail (4) both sides is in splayed downwards, and the side of described tail (4) is provided with outwardly Erecting bed (41), two sides of erecting bed (41) are provided with inside cone groove (411), and the top of described empennage (5) is provided with two Plate (51) is hooked, the madial wall for hooking the top of plate (51) is provided with the hook (511) being used cooperatively with cone groove (411), hook (511) hooking in cone groove (411) makes tail (4) be fixedly connected with empennage (5), and the top of described empennage (5), which is provided with, covers on peace Platform (41) is filled with hooking the connection shell (6) on the outside of plate (51)；Two groups of described advancing slip wheel carriers (7) are set up separately has bent rod (71) and support in the both sides of fuselage (3), advancing slip wheel carrier (7) Bar (72), one end of bent rod (71) are connected on fuselage (3), and the other end is connected on two wheels (9), support bar (72) One end is connected to the bottom of fuselage (3), and its other end is connected with wheel (9)；Described rear wheel frame (8) sets up separately has pole (81), pole (81) in the both sides of fuselage (3) afterbody, rear wheel frame (8) One end be arranged on fuselage (3) afterbody bottom surface on, the other end is connected on two other wheel (9).
- 2. unmanned plane according to claim 1 of taking photo by plane, it is characterized in that：At least two groups of described hook plate (51).
- 3. unmanned plane according to claim 1 of taking photo by plane, it is characterized in that：Fixed cover is provided with described tail (4) (31) can 360 ° rotation knobs (10).
- 4. unmanned plane according to claim 1 of taking photo by plane, it is characterized in that：Described connection shell (6) is provided with mounting blocks (61), The other end of mounting blocks (61) extends to the lateral surface of empennage, is provided with screwed hole in mounting blocks (61), screw thread is inserted by bolt Make tail (4) reinforce with empennage (5) in hole to connect.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720645054.2U CN207015575U (en) | 2017-06-05 | 2017-06-05 | Take photo by plane unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720645054.2U CN207015575U (en) | 2017-06-05 | 2017-06-05 | Take photo by plane unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207015575U true CN207015575U (en) | 2018-02-16 |
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ID=61484873
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720645054.2U Active CN207015575U (en) | 2017-06-05 | 2017-06-05 | Take photo by plane unmanned plane |
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| Country | Link |
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| CN (1) | CN207015575U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108759793A (en) * | 2018-03-13 | 2018-11-06 | 清远市巨劲科技有限公司 | A kind of mapping unmanned plane convenient for angular adjustment |
| CN112278313A (en) * | 2020-11-05 | 2021-01-29 | 湖南浩天翼航空技术有限公司 | Landing arresting rope mechanism of sliding unmanned aerial vehicle |
-
2017
- 2017-06-05 CN CN201720645054.2U patent/CN207015575U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108759793A (en) * | 2018-03-13 | 2018-11-06 | 清远市巨劲科技有限公司 | A kind of mapping unmanned plane convenient for angular adjustment |
| CN112278313A (en) * | 2020-11-05 | 2021-01-29 | 湖南浩天翼航空技术有限公司 | Landing arresting rope mechanism of sliding unmanned aerial vehicle |
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