CN211869681U - Unmanned aerial vehicle flight anti-collision device - Google Patents
Unmanned aerial vehicle flight anti-collision device Download PDFInfo
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- CN211869681U CN211869681U CN202020239629.2U CN202020239629U CN211869681U CN 211869681 U CN211869681 U CN 211869681U CN 202020239629 U CN202020239629 U CN 202020239629U CN 211869681 U CN211869681 U CN 211869681U
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- aerial vehicle
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Abstract
The utility model relates to the technical field of unmanned aerial vehicle devices, in particular to an anti-collision device for unmanned aerial vehicle flight, which comprises an unmanned aerial vehicle body, an induction device and a protective device, wherein the induction device comprises a lifting device and an inductor body, the lifting device comprises an installation rod, a slide rod and a power mechanism, the installation rod is arranged on the unmanned aerial vehicle body, the slide rod is arranged at the side part of the installation rod in a sliding way, the power mechanism is fixedly arranged on the installation rod, the protective device comprises a protective mechanism arranged around the unmanned aerial vehicle body, the protective mechanism comprises an arc-shaped base, a first electric push rod, a baffle plate and a second electric push rod arranged around the unmanned aerial vehicle body, the arc-shaped base is fixedly connected with the output end of the second electric push rod, a mounting groove is arranged on the arc-shaped base, the second electric push rod is arranged in, baffle and second electric putter's output fixed connection, the device can protect unmanned aerial vehicle to receive the striking to lead to damaging.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle device technical field, concretely relates to unmanned aerial vehicle is buffer stop for flight.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, and has wide application fields, such as power inspection, agricultural insurance, environmental survey, movie and television series shooting and the like. It mainly comprises organism and a plurality of rotor, all does not set up any protector on traditional unmanned aerial vehicle's the rotor, consequently when indoor outer flight, especially when in the city that the environment is comparatively complicated, the operation is improper and lead to unmanned aerial vehicle to collide with the object in the environment, causes great damage to unmanned aerial vehicle's rotor, probably leads to the condition that the organism is out of control or falls, for this reason, we propose an unmanned aerial vehicle collision avoidance device for flight.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle is buffer stop for flight.
To achieve the purpose, the utility model adopts the following technical proposal:
the utility model provides an unmanned aerial vehicle flight anti-collision device, which comprises an unmanned aerial vehicle body, a sensing device and a protective device, wherein the bottom of the unmanned aerial vehicle body is provided with a landing support frame, the sensing device comprises a lifting device and an inductor body, the lifting device comprises an installation rod, a slide rod and a power mechanism for driving the slide rod to slide along the installation rod, the installation rod is fixedly arranged on the unmanned aerial vehicle body, the installation rod is vertically arranged, the slide rod is arranged at the side part of the installation rod in a sliding manner, the power mechanism is fixedly arranged on the installation rod, the output end of the power mechanism is connected with the slide rod, the protective device comprises a protective mechanism uniformly arranged around the unmanned aerial vehicle body, the protective mechanism comprises an arc-shaped base, a first electric push rod, a baffle and a second electric push rod detachably arranged around the unmanned aerial vehicle body, the arc-shaped base is fixedly connected with the output, the arc-shaped base is provided with a mounting groove, the second electric push rod is fixedly mounted in the mounting groove, and the baffle is fixedly connected with the output end of the second electric push rod.
As unmanned aerial vehicle for flight buffer stop's an preferred scheme, power unit is including micro motor, micro gear and mount pad, the mount pad is fixed to be set up on the installation pole, and micro motor fixed mounting is on the mount pad, micro gear and micro motor's output fixed connection, the lateral part of slide bar is provided with the tooth's socket, micro gear is connected with the slide bar meshing.
As an unmanned aerial vehicle for flight buffer stop's an preferred scheme, one side that the slide bar is close to the installation pole is provided with the draw runner, it is provided with the spout to correspond on the installation pole, the draw runner slides and sets up in the spout.
As an unmanned aerial vehicle for flight buffer stop's an preferred scheme, second electric putter's bottom is provided with the thread installation department, the lateral part of unmanned aerial vehicle body is provided with connecting portion, be provided with the thread groove on the connecting portion, thread installation department threaded connection is in the thread groove.
As an unmanned aerial vehicle for flight buffer stop's an preferred scheme, the baffle is kept away from one side of unmanned aerial vehicle body and is provided with the buckle, the buckle inside callipers are equipped with buffer gear.
As an optimal scheme of the collision avoidance device for unmanned aerial vehicle flight, the buffer mechanism is a rubber buffer pad.
As an unmanned aerial vehicle for the flight collision avoidance system an optimal selection scheme, the outside of unmanned aerial vehicle body still overlaps and is equipped with the bradyseism layer.
The utility model has the advantages that:
1. this unmanned aerial vehicle is buffer stop for flight, the design has the installation pole, the inductor body, the slide bar, micro motor, micro gear, the mount pad, the arc base, first electric putter, the baffle with can dismantle the setting at unmanned aerial vehicle body second electric putter all around, there is or not the barrier at the in-process that unmanned aerial vehicle body flies through inductor response the place ahead, when sensing the barrier, first electric putter just can release the arc base with the baffle, protect all around the unmanned aerial vehicle body.
2. This anti-collision device is used in unmanned aerial vehicle flight, the design has second electric putter, screw thread installation department and connecting portion, and when not having the barrier, second electric putter is in the shrink state, can receive the house type base and transfer at the unmanned aerial vehicle body, reduces the resistance of unmanned aerial vehicle body, and screw thread installation department and connecting portion have made things convenient for protector's dismantlement.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings required to be used in the embodiments of the present invention will be briefly described below. It is obvious that the drawings described below are only some embodiments of the invention, and that for a person skilled in the art, other drawings can be obtained from these drawings without inventive effort.
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a schematic view of the split structure of the present invention.
Fig. 3 is a schematic structural diagram of the lifting device of the present invention.
In the figure: unmanned aerial vehicle body 1, descending support frame 2, elevating gear 3, inductor body 4, installation pole 5, slide bar 6, power unit 7, protection machanism 8, arc base 9, first electric putter 10, baffle 11, second electric putter 12, mounting groove 13, micro motor 14, micro gear 15, mount pad 16, threaded mounting portion 17, connecting portion 18, thread groove 19, buckle 20, rubber buffer 21.
Detailed Description
The technical solution of the present invention is further explained by the following embodiments with reference to the accompanying drawings.
Wherein the showings are for the purpose of illustration only and are shown by way of illustration only and not in actual form, and are not to be construed as limiting the present patent; for a better understanding of the embodiments of the present invention, some parts of the drawings may be omitted, enlarged or reduced, and do not represent the size of an actual product; it will be understood by those skilled in the art that certain well-known structures in the drawings and descriptions thereof may be omitted.
The same or similar reference numerals in the drawings of the embodiments of the present invention correspond to the same or similar parts; in the description of the present invention, it should be understood that if the terms "upper", "lower", "left", "right", "inner", "outer", etc. are used to indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, it is only for convenience of description and simplification of description, but it is not indicated or implied that the device or element referred to must have a specific orientation, be constructed in a specific orientation, and be operated, and therefore, the terms describing the positional relationship in the drawings are used only for illustrative purposes and are not to be construed as limiting the present patent, and the specific meaning of the terms will be understood by those skilled in the art according to the specific circumstances.
In the description of the present invention, unless otherwise explicitly specified or limited, the term "connected" or the like, if appearing to indicate a connection relationship between the components, is to be understood broadly, for example, as being either a fixed connection, a detachable connection, or an integral part; can be mechanically or electrically connected; they may be directly connected or indirectly connected through intervening media, or may be connected through one or more other components or may be in an interactive relationship with one another. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1 to 3, shown collision avoidance device is used in unmanned aerial vehicle flight, including unmanned aerial vehicle body 1, induction system and protector, the bottom of unmanned aerial vehicle body 1 is provided with descending support frame 2, induction system is including elevating gear 3 and inductor body 4, elevating gear 3 is including installation pole 5, slide bar 6 and drive slide bar 6 along the gliding power unit 7 of installation pole 5, installation pole 5 is fixed to be set up on unmanned aerial vehicle body 1 to installation pole 5 vertical setting, slide bar 6 slides and sets up the lateral part at installation pole 5, power unit 7 fixed mounting is on installation pole 5, and power unit 7's output is connected with slide bar 6, protector is including evenly setting up protection machanism 8 around unmanned aerial vehicle body 1, protection machanism 8 is including arc base 9, first electric putter 10, Baffle 11 with can dismantle the setting at unmanned aerial vehicle body 1 second electric putter 12 all around, the arc base 9 is fixed with the output fixed connection of second electric putter 12, is provided with mounting groove 13 on the arc base 9, second electric putter 12 fixed mounting is in mounting groove 13, baffle 11 and second electric putter 12's output fixed connection. When using, at first install protector on unmanned aerial vehicle body 1, at the flight in-process, can drive elevating gear 3's rising observe more distant barrier, after sensing the barrier, drive second electric putter 12 pushes away arc-shaped base 9, then first electric putter 10 just can release arc-shaped base 9 with baffle 11, protects all around unmanned aerial vehicle body 1.
The power mechanism 7 comprises a micro motor 14, a micro gear 15 and a mounting seat 16, the mounting seat 16 is fixedly arranged on the mounting rod 5, the micro motor 14 is fixedly arranged on the mounting seat 16, the micro gear 15 is fixedly connected with the output end of the micro motor 14, a tooth groove is formed in the side portion of the sliding rod 6, and the micro gear 15 is meshed with the sliding rod 6. When the inductor is lifted, the micro motor 14 drives the micro gear 15 to rotate, and the sliding rod 6 meshed with the micro gear 15 can ascend along the mounting rod 5, so that the purpose of lifting the inductor is achieved.
One side of the sliding rod 6, which is close to the mounting rod 5, is provided with a sliding strip, a sliding groove is correspondingly arranged on the mounting rod 5, and the sliding strip is arranged in the sliding groove in a sliding manner.
The bottom of second electric putter 12 is provided with threaded mounting portion 17, the lateral part of unmanned aerial vehicle body 1 is provided with connecting portion 18, be provided with thread groove 19 on connecting portion 18, threaded mounting portion 17 threaded connection is in thread groove 19.
One side that unmanned aerial vehicle body 1 was kept away from to baffle 11 is provided with buckle 20, buckle 20 inside callipers are equipped with buffer gear.
The buffer mechanism is a rubber buffer 21.
The outside of unmanned aerial vehicle body 1 still overlaps and is equipped with the bradyseism layer.
The working principle is as follows: when using, at first install protector on unmanned aerial vehicle body 1, at the flight in-process, can drive elevating gear 3's rising observe more distant barrier, after sensing the barrier, drive second electric putter 12 pushes away arc-shaped base 9, then first electric putter 10 just can release arc-shaped base 9 with baffle 11, protects all around unmanned aerial vehicle body 1.
It should be understood that the above-described embodiments are merely illustrative of the preferred embodiments of the present invention and the technical principles thereof. It will be understood by those skilled in the art that various modifications, equivalents, changes, and the like can be made to the present invention. However, these modifications are within the scope of the present invention as long as they do not depart from the spirit of the present invention. In addition, certain terms used in the specification and claims of the present application are not limiting, but are used merely for convenience of description.
Claims (7)
1. The utility model provides an unmanned aerial vehicle is buffer stop for flight which characterized in that: including unmanned aerial vehicle body (1), induction system and protector, the bottom of unmanned aerial vehicle body (1) is provided with descending support frame (2), induction system is including elevating gear (3) and inductor body (4), elevating gear (3) are including installation pole (5), slide bar (6) and drive slide bar (6) along installation pole (5) gliding power unit (7), installation pole (5) are fixed to be set up on unmanned aerial vehicle body (1), and installation pole (5) vertical setting, slide bar (6) slide and set up the lateral part at installation pole (5), power unit (7) fixed mounting is on installation pole (5), and the output and the slide bar (6) of power unit (7) are connected, protector is including evenly setting up protection machanism (8) around unmanned aerial vehicle body (1), protection machanism (8) including arc base (9), first electric putter (10), baffle (11) and can dismantle and set up second electric putter (12) around unmanned aerial vehicle body (1), arc base (9) are fixed with the output fixed connection of second electric putter (12), are provided with mounting groove (13) on arc base (9), second electric putter (12) fixed mounting is in mounting groove (13), the output fixed connection of baffle (11) and second electric putter (12).
2. The unmanned aerial vehicle collision avoidance device for flight of claim 1, characterized in that: the power mechanism (7) comprises a micro motor (14), a micro gear (15) and a mounting seat (16), the mounting seat (16) is fixedly arranged on the mounting rod (5), the micro motor (14) is fixedly arranged on the mounting seat (16), the micro gear (15) is fixedly connected with the output end of the micro motor (14), a tooth groove is formed in the side portion of the sliding rod (6), and the micro gear (15) is meshed with the sliding rod (6) and is connected with the sliding rod.
3. The unmanned aerial vehicle collision avoidance device for flight of claim 2, characterized in that: one side of the sliding rod (6) close to the installation rod (5) is provided with a sliding strip, the installation rod (5) is correspondingly provided with a sliding groove, and the sliding strip is arranged in the sliding groove in a sliding mode.
4. The unmanned aerial vehicle collision avoidance device for flight of claim 3, characterized in that: the bottom of second electric putter (12) is provided with thread mounting portion (17), the lateral part of unmanned aerial vehicle body (1) is provided with connecting portion (18), be provided with thread groove (19) on connecting portion (18), thread mounting portion (17) threaded connection is in thread groove (19).
5. The unmanned aerial vehicle collision avoidance device for flight of claim 4, characterized in that: one side that unmanned aerial vehicle body (1) was kept away from in baffle (11) is provided with buckle (20), buckle (20) inside callipers are equipped with buffer gear.
6. The unmanned aerial vehicle collision avoidance device for flight of claim 5, characterized in that: the buffer mechanism is a rubber buffer (21).
7. The unmanned aerial vehicle collision avoidance device for flight of claim 6, characterized in that: the outside of unmanned aerial vehicle body (1) still overlaps and is equipped with the bradyseism layer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020239629.2U CN211869681U (en) | 2020-03-02 | 2020-03-02 | Unmanned aerial vehicle flight anti-collision device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020239629.2U CN211869681U (en) | 2020-03-02 | 2020-03-02 | Unmanned aerial vehicle flight anti-collision device |
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| CN211869681U true CN211869681U (en) | 2020-11-06 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114802783A (en) * | 2022-03-01 | 2022-07-29 | 东莞市酷得智能科技有限公司 | Intelligent anti-collision unmanned aerial vehicle |
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2020
- 2020-03-02 CN CN202020239629.2U patent/CN211869681U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114802783A (en) * | 2022-03-01 | 2022-07-29 | 东莞市酷得智能科技有限公司 | Intelligent anti-collision unmanned aerial vehicle |
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