CN215245516U - High-protection micro unmanned aerial vehicle for optical and radar detection - Google Patents
High-protection micro unmanned aerial vehicle for optical and radar detection Download PDFInfo
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- CN215245516U CN215245516U CN202120498311.0U CN202120498311U CN215245516U CN 215245516 U CN215245516 U CN 215245516U CN 202120498311 U CN202120498311 U CN 202120498311U CN 215245516 U CN215245516 U CN 215245516U
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Abstract
The utility model discloses a high-protection micro unmanned aerial vehicle for optical and radar detection, which comprises a micro unmanned aerial vehicle body, wherein the micro unmanned aerial vehicle body is provided with a peripheral protective frame connected with a vehicle body through a connecting rod, and the whole micro unmanned aerial vehicle body is positioned in the peripheral protective frame; the bottom of the body of the micro unmanned aerial vehicle body is provided with a groove and supporting legs, an optical probe and a detection radar are arranged in the groove, and a groove door is arranged on the groove opening of the groove in a matched manner; every rotor of miniature unmanned aerial vehicle body all has the rotor screen panel, rotor screen panel cage rotor, and the rotor screen panel all can be dismantled with the rotor arm of peripheral protective frame and miniature unmanned aerial vehicle body and be connected. The utility model provides a pair of miniature unmanned aerial vehicle of high protection that optics and radar were listened can carry out comparatively comprehensive protection to unmanned aerial vehicle, reduces its damage degree and the cost of maintenance that takes place the crash accident.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, especially, relate to a high protection micro unmanned aerial vehicle that optics and radar were listened.
Background
Present unmanned aerial vehicle is equipped with protector for unmanned aerial vehicle mostly in order to reduce damage degree and the cost of maintenance that the crash accident caused, and folding is a more common protection mode, but the protecting effect is not fine, and parachute protection mode application is also more in addition, but more troublesome, still can cause rubbish to pollute. In order to solve the problem, the utility model discloses a high protection micro unmanned aerial vehicle that optics and radar were listened can carry out comparatively comprehensive protection to unmanned aerial vehicle, reduces its damage degree and the cost of maintenance that takes place the air crash accident.
Disclosure of Invention
The purpose of the invention is as follows: in order to overcome the not enough that exists among the prior art, the utility model provides a high protection micro unmanned aerial vehicle that optics and radar were listened can carry out comparatively comprehensive protection to unmanned aerial vehicle, reduces its damage degree and the cost of maintenance that takes place the crash accident.
The technical scheme is as follows: in order to achieve the purpose, the high-protection micro unmanned aerial vehicle for optical and radar detection comprises a micro unmanned aerial vehicle body, wherein the micro unmanned aerial vehicle body is provided with a peripheral protection frame connected with a machine body through a connecting rod, and the whole micro unmanned aerial vehicle body is positioned in the peripheral protection frame;
the bottom of the body of the micro unmanned aerial vehicle body is provided with a groove and supporting legs, an optical probe and a detection radar are arranged in the groove, and a groove door is arranged on a groove opening of the groove in a matched manner;
every rotor of miniature unmanned aerial vehicle body all has the rotor screen panel, rotor screen panel cage the rotor, and the rotor arm of rotor screen panel and peripheral protective frame and miniature unmanned aerial vehicle body all can be dismantled and be connected.
Further, the peripheral protective frame is of a circular ring structure.
Furthermore, the slot door is composed of a plurality of door plates hinged with the machine body, a miniature electric push rod is movably connected between the inner side of each door plate and the bottom of the inner groove of each groove, and the slot door can be opened and closed by pushing and pulling the door plates through the miniature electric push rods.
Further, the door panel is of a transparent plate structure.
Furthermore, the support legs are arranged on the outer back face of the door plate and close to the hinged connection of the door plate.
Furthermore, the rotor screen cover is formed by arranging a plurality of arc-shaped rods in a circumferential array, the rod ends of the arc-shaped rods are gathered at the same point to form a co-junction body, the bottom of each co-junction body is connected with a plug, and the two plugs are respectively inserted into the jacks formed in the peripheral protective frame and the rotor arm.
Further, optical probe, detection radar, miniature electric putter are connected with the flight control system signal transmission of miniature unmanned aerial vehicle body respectively.
Has the advantages that: the utility model discloses a high protection micro unmanned aerial vehicle that optics and radar were listened, beneficial effect is: the whole body of the micro unmanned aerial vehicle is positioned in the peripheral protective frame, so that the whole body of the micro unmanned aerial vehicle is protected, the peripheral protective frame is of a circular structure, the impact damage rate is lower, and the protection effect is better; in addition, the optical probe and the detection radar are both hidden in the groove with the slot door, so that the probability of damage to the optical probe and the detection radar when the optical probe and the detection radar touch the ground can be greatly reduced under the crash fault; moreover, carry out the cage protection to the rotor through the rotor screen panel, avoid the rotor to receive the impact damage.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of the overall structure of the present invention;
fig. 3 is a schematic structural view of the rotor mesh enclosure in a disassembled state.
Detailed Description
The present invention will be further described with reference to the accompanying drawings.
As shown in fig. 1 and fig. 2, a high protection micro unmanned aerial vehicle that optics and radar were listened, including micro unmanned aerial vehicle body 1, micro unmanned aerial vehicle body 1 has the peripheral protective frame 2 of connecting fuselage 10 through connecting rod 20, and is whole micro unmanned aerial vehicle body 1 is located in peripheral protective frame 2 to protect whole micro unmanned aerial vehicle body 1, it is more specific, peripheral protective frame 2 is the ring column structure, and the striking spoilage is lower, and the protective effect is better.
The bottom of the body 10 of the unmanned aerial vehicle body 1 is provided with a groove 101 and supporting legs 102, the groove 101 is internally provided with an optical probe 3 and a detection radar 4, and a groove door 5 is arranged on the groove opening of the groove 101 in a matched manner. The optical probe 3 and the detection radar 4 are both hidden in the groove 101 with the slot door 5, and the probability of damage to the optical probe 3 and the detection radar 4 due to contact with the ground can be greatly reduced under the condition of crash failure.
Every rotor 11 of miniature unmanned aerial vehicle body 1 all has rotor screen panel 6, rotor screen panel 6 covers rotor 11, and rotor screen panel 6 all can be dismantled with peripheral protective frame 2 and miniature unmanned aerial vehicle body 1's rotor arm 12 and be connected. Carry out the cage protection through rotor screen panel 6 to rotor 11, avoid rotor 11 to receive to hit to damage.
The slot door 5 is composed of a plurality of door plates 51 hinged with the body 10, a micro electric push rod 52 is movably connected between the inner surface of each door plate 51 and the inner slot bottom of the groove 101, and the slot door 5 pushes and pulls the door plates 51 through the micro electric push rods 52 to realize door opening and door closing actions. Notably, the door panel 51 is a transparent plate structure. The optical detection and the radar detection cannot be influenced in the door closing state, and the optical detection effect is better in the door opening state.
The supporting legs 102 are disposed on the outer back of the door panel 51, and the supporting legs 102 are close to the hinged joint of the door panel 51, so as to avoid affecting optical detection and radar detection.
As shown in fig. 3, the rotor mesh enclosure 6 is formed by arranging a plurality of arc-shaped rods 61 in a circumferential array, the rod ends of each arc-shaped rod 61 are gathered at the same point to form a union 62, the bottom of each union 62 is connected with a plug 63, and the two plugs 63 are respectively inserted into the jacks 13 formed in the peripheral protective frame 2 and the rotor arm 12. The rotor mesh enclosure 6 is convenient and quick to mount and dismount.
More specifically, optical probe 3, listen radar 4, miniature electric putter 52 are connected with the flight control system signal transmission of miniature unmanned aerial vehicle body 1 respectively, and the ground staff of being convenient for controls.
The above description is only a preferred embodiment of the present invention, and it should be noted that: for those skilled in the art, without departing from the principle of the present invention, several improvements and modifications can be made, and these improvements and modifications should also be considered as the protection scope of the present invention.
Claims (7)
1. The utility model provides a miniature unmanned aerial vehicle of high protection that optics and radar were listened which characterized in that: the unmanned aerial vehicle comprises a micro unmanned aerial vehicle body (1), wherein the micro unmanned aerial vehicle body (1) is provided with a peripheral protective frame (2) connected with a vehicle body (10) through a connecting rod (20), and the whole micro unmanned aerial vehicle body (1) is positioned in the peripheral protective frame (2);
the bottom of a body (10) of the unmanned aerial vehicle body (1) is provided with a groove (101) and supporting legs (102), an optical probe (3) and a detection radar (4) are arranged in the groove (101), and a groove door (5) is arranged on a groove opening of the groove (101) in a matched manner;
every rotor (11) of miniature unmanned aerial vehicle body (1) all has rotor screen panel (6), rotor screen panel (6) cage rotor (11), and rotor screen panel (6) all can be dismantled with rotor arm (12) of peripheral protective frame (2) and miniature unmanned aerial vehicle body (1) and be connected.
2. The micro drone of claim 1, wherein the micro drone further comprises: the peripheral protective frame (2) is of a circular ring structure.
3. The micro drone of claim 1, wherein the micro drone further comprises: the slot door (5) is composed of a plurality of door plates (51) hinged with the machine body (10), a micro electric push rod (52) is movably connected between the inner surface of each door plate (51) and the inner groove bottom of the groove (101), and the slot door (5) pushes and pulls the door plates (51) through the micro electric push rods (52) to realize door opening and door closing actions.
4. The micro unmanned aerial vehicle with high protection for optical and radar detection as claimed in claim 3, wherein: the door panel (51) is of a transparent plate structure.
5. The micro unmanned aerial vehicle with high protection for optical and radar detection as claimed in claim 3, wherein: the support legs (102) are arranged on the outer back of the door panel (51), and the support legs (102) are close to the hinged connection of the door panel (51).
6. The micro drone of claim 1, wherein the micro drone further comprises: rotor screen panel (6) have a plurality of arc poles (61) to be the circumference array and arrange and form, and the rod end of every arc pole (61) gathers in same point constitution coaptation body (62), every coaptation body (62) bottom all is connected with plug (63), two plug (63) insert respectively in jack (13) of seting up on peripheral protective frame (2) and rotor arm (12).
7. The micro unmanned aerial vehicle with high protection for optical and radar detection as claimed in claim 3, wherein: the optical probe (3), the detection radar (4) and the micro electric push rod (52) are respectively connected with a flight control system of the micro unmanned aerial vehicle body (1) in a signal transmission mode.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120498311.0U CN215245516U (en) | 2021-03-09 | 2021-03-09 | High-protection micro unmanned aerial vehicle for optical and radar detection |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120498311.0U CN215245516U (en) | 2021-03-09 | 2021-03-09 | High-protection micro unmanned aerial vehicle for optical and radar detection |
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| Publication Number | Publication Date |
|---|---|
| CN215245516U true CN215245516U (en) | 2021-12-21 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202120498311.0U Active CN215245516U (en) | 2021-03-09 | 2021-03-09 | High-protection micro unmanned aerial vehicle for optical and radar detection |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2792921C1 (en) * | 2022-06-14 | 2023-03-28 | Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации | Method for concealing the electrooptical means of the airborne electrooptical surveillance complex |
-
2021
- 2021-03-09 CN CN202120498311.0U patent/CN215245516U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2792921C1 (en) * | 2022-06-14 | 2023-03-28 | Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации | Method for concealing the electrooptical means of the airborne electrooptical surveillance complex |
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