CN212099341U - Foldable many rotors rescue unmanned aerial vehicle - Google Patents
Foldable many rotors rescue unmanned aerial vehicle Download PDFInfo
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- CN212099341U CN212099341U CN202020445697.4U CN202020445697U CN212099341U CN 212099341 U CN212099341 U CN 212099341U CN 202020445697 U CN202020445697 U CN 202020445697U CN 212099341 U CN212099341 U CN 212099341U
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Abstract
The utility model discloses a foldable many rotors rescue unmanned aerial vehicle, wherein, foldable many rotors rescue unmanned aerial vehicle includes: a body; the power device comprises a plurality of machine arms, a power device and a control device, wherein one end of each machine arm is rotatably connected with the side surface of the machine body, and the other end of each machine arm is connected with a bearing part and the power device arranged on the bearing part; the side surface of the machine body is provided with a containing groove for containing the machine arm, and the side surface of the machine body is also provided with a containing space for containing the bearing part. The utility model provides a foldable many rotors rescue unmanned aerial vehicle, this foldable many rotors rescue unmanned aerial vehicle simple structure is compact, and the horn can be folded, has reduced unmanned aerial vehicle's whole volume during fold condition, is convenient for accomodate and carry.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to foldable many rotors rescue unmanned aerial vehicle.
Background
The unmanned aircraft is called an unmanned aerial vehicle for short, and called a UAV in English for short, and is an unmanned aircraft operated by using a radio remote control device and a self-contained program control device, and the definition of the technology can be divided into: unmanned fixed wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned paravane aircraft, and the like.
The unmanned aerial vehicle is a new-concept unmanned aerial vehicle which is rapidly developed in the current society, and has the advantages of flexibility, rapid response, long control distance, simplicity in operation and the like. The unmanned aerial vehicle can carry various loads to complete various complex tasks, the unmanned aerial vehicle is widely applied to civil aspects, and the existing unmanned aerial vehicle has wide application in various civil fields such as aerial photography, agriculture, plant protection, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, electric power inspection, disaster relief, movie and television shooting, pesticide spraying, fire prevention and relief, communication, drug enforcement and the like. However, most of the existing unmanned aerial vehicles are complex in structure, large in overall size and not foldable, and are troublesome to store.
Thus, there is a need for improvements and enhancements in the art.
SUMMERY OF THE UTILITY MODEL
In view of the weak point of above-mentioned prior art, the utility model aims at providing a foldable many rotors rescue unmanned aerial vehicle aims at solving the problem that current unmanned aerial vehicle is bulky, can not fold, be difficult to accomodate.
In order to achieve the purpose, the utility model adopts the following technical proposal:
a foldable many rotors rescue unmanned aerial vehicle, wherein, foldable many rotors rescue unmanned aerial vehicle includes:
a body;
the power device comprises a plurality of machine arms, a power device and a control device, wherein one end of each machine arm is rotatably connected with the side surface of the machine body, and the other end of each machine arm is connected with a bearing part and the power device arranged on the bearing part;
the side surface of the machine body is provided with a containing groove for containing the machine arm, and the side surface of the machine body is also provided with a containing space for containing the bearing part.
The folding multi-rotor rescue unmanned aerial vehicle is characterized in that the rotation direction of each arm is the same when the arm is folded.
Foldable many rotors rescue unmanned aerial vehicle, wherein, the horn with the organism is articulated, just the horn with organism articulated department is provided with the electro-magnet device that is used for spacing and cooperation locking.
Foldable many rotors rescue unmanned aerial vehicle, wherein, the horn with holding tank looks adaptation, bearing part with accommodation space looks adaptation, bearing part bottom still is provided with the foot rest.
The foldable multi-rotor rescue unmanned aerial vehicle is characterized in that the body is circular, the joint of each arm and the body is arranged at the equal division point of the circular body, and the arms are arc-shaped.
Foldable many rotors rescue unmanned aerial vehicle, wherein, the quantity of horn is four.
Foldable many rotors rescue unmanned aerial vehicle, wherein, the direction of rotation when every horn is folded is clockwise.
Foldable many rotors rescue unmanned aerial vehicle, wherein, power device is in including setting up motor and setting in the portion of bearing are in screw on the motor, the screw is for dismantling and folding screw.
Foldable many rotors rescue unmanned aerial vehicle, wherein, bottom of the body is provided with the infrared thermal imaging camera of connecting through electronic cloud platform.
Foldable many rotors rescue unmanned aerial vehicle, wherein, still be provided with GPS module and artificial intelligence module in the organism.
Compared with the prior art, the utility model provides a folding multi-rotor rescue unmanned aerial vehicle, which is provided with a body; the power device comprises a plurality of machine arms, a power device and a control device, wherein one end of each machine arm is rotatably connected with the side surface of the machine body, and the other end of each machine arm is connected with a bearing part and the power device arranged on the bearing part; the side surface of the machine body is provided with a containing groove for containing the machine arm, and the side surface of the machine body is also provided with a containing space for containing the bearing part. The horn has development condition and folded condition, the horn can rotate relatively the organism, makes the horn switches between development condition and folded condition. When the folding multi-rotor rescue unmanned aerial vehicle is in a flying state, the horn is unfolded relative to the body and is in an unfolded state; when the foldable multi-rotor rescue unmanned aerial vehicle is in a non-flight state, the horn is folded in the accommodating groove of the body and is in a folded state; this foldable many rotors rescue unmanned aerial vehicle simple structure is compact, and the horn can be folded, has reduced unmanned aerial vehicle's whole volume during fold condition, is convenient for accomodate and carry.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments described in the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
Fig. 1 is the embodiment of the utility model provides a foldable many rotors rescue unmanned aerial vehicle expandes the structural schematic diagram of state.
Fig. 2 is the embodiment of the utility model provides a foldable many rotors rescue unmanned aerial vehicle fold condition's structural schematic.
Fig. 3 is the embodiment of the utility model provides a foldable many rotors rescue unmanned aerial vehicle expandes the elevation view of state.
Fig. 4 is the embodiment of the utility model provides a folded state's of foldable many rotors rescue unmanned aerial vehicle elevation.
Reference numerals: 1. the infrared thermal imaging camera comprises a body, 11, a containing groove, 12, a containing space, 13, an infrared thermal imaging camera, 2, a machine arm, 3, a bearing part, 4 and a foot rest.
Detailed Description
In order to make the objects, technical solutions and effects of the present invention clearer and clearer, the following description of the present invention will refer to the accompanying drawings and illustrate embodiments. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the invention.
In the description of the present invention, it should be understood that the terms "center", "upper", "lower", "front", "rear", "left", "right", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or assembly referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may for example be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; the two components can be directly connected or indirectly connected through an intermediate medium, and the two components can be communicated with each other. When an element is referred to as being "secured to" or "disposed on" another element, it can be directly on the other element or intervening elements may also be present. When a component is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. The specific meaning of the above terms in the present invention can be understood in specific cases for those skilled in the art.
In the description of the present invention, the terms "comprising," "including," "having," "containing," and the like, as used herein, are open-ended terms that mean including, but not limited to. Reference to the description of the terms "one embodiment," "a particular embodiment," "some embodiments," "for example," etc., means that a particular feature, structure, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the application. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. The sequence of steps involved in the embodiments is for illustrative purposes to illustrate the implementation of the present application, and the sequence of steps is not limited and can be adjusted as needed.
Various non-limiting embodiments of the present invention are described in detail below with reference to the accompanying drawings.
Referring to fig. 1-4, the utility model provides a pair of foldable many rotors rescue unmanned aerial vehicle, wherein, foldable many rotors rescue unmanned aerial vehicle includes:
a machine body 1;
the device comprises a plurality of machine arms 2, wherein one end of each machine arm 2 is rotatably connected with the side surface of the machine body 1, and the other end of each machine arm 2 is connected with a bearing part 3 and a power device arranged on the bearing part 3;
the side surface of the machine body 1 is provided with a containing groove 11 for containing the machine arm 2, and the side surface of the machine body 1 is also provided with a containing space 12 for containing the bearing part 3.
Specifically, the horn 2 has an unfolded state and a folded state, and the horn 2 can rotate relative to the machine body 1, so that the horn 2 is switched between the unfolded state and the folded state. When the folding multi-rotor rescue unmanned aerial vehicle is in a flying state, the horn 2 is unfolded relative to the body 1 and is in an unfolded state; when this foldable many rotors rescue unmanned aerial vehicle is in non-flight state, horn 2 draw in organism 1 in the storage tank 11, be fold condition.
Specifically, the plurality of booms 2 refers to two or more, the booms 2 and the bearing part 3 may be of an integral structure, so that the production process may be simplified, and the stability between the booms 2 and the bearing part 3 may be improved, and the power device includes a motor (not shown in the drawings) disposed on the bearing part 3 and a propeller (not shown in the drawings) disposed on the motor.
In some embodiments, the folding multi-rotor rescue drone has the same rotation direction when each of the arms 2 is folded.
Specifically, the rotation direction of each of the arms 2 during folding may be clockwise rotation or counterclockwise rotation.
In some embodiments, the folding multi-rotor rescue unmanned aerial vehicle comprises a body 1, and the joint between the arm 2 and the body 1 is provided with an electromagnet device for limiting and matching locking.
Specifically, the electromagnet device is mainly used for fixing the horn 2 by the magnetic force of the electromagnet device when the horn 2 is in the unfolded state.
In some embodiments, the folding multi-rotor rescue unmanned aerial vehicle includes a horn 2 adapted to the accommodating groove 11, a bearing portion 3 adapted to the accommodating space 12, and a foot rest 4 disposed at the bottom of the bearing portion 3.
Specifically, every 3 bottoms in bearing part all are provided with foot rest 4 plays the support balanced effect to this foldable many rotor wing rescue unmanned aerial vehicle.
In some embodiments, the foldable multi-rotor rescue drone is characterized in that the body 1 is circular, the connection point of each horn 2 and the body 1 is arranged on a bisector of the circular body 1, and the horns 2 are arc-shaped.
Specifically, the connection point of each of the arms 2 and the machine body 1 is not limited to be disposed on the outer circle of the circular machine body 1, and may be on the line of a concentric circle of the machine body 1 smaller than the outer circle of the machine body 1.
In some embodiments, the folding multi-rotor rescue drone has four arms 2.
In some embodiments, the folding multi-rotor rescue drone has a clockwise direction of rotation when each of the arms 2 is folded.
In particular, in some embodiments, the rotation direction of each of the arms 2 when folded may also be counterclockwise.
In some embodiments, the folding multi-rotor rescue drone includes a motor (not shown in the drawings) disposed on the carrying portion 3, and a propeller (not shown in the drawings) disposed on the motor, wherein the propeller is a detachable and foldable propeller.
Specifically, because the paddle of screw is generally longer, in order to further reduce this foldable many rotors rescue unmanned aerial vehicle whole volume under the non-flight state, can with the screw design can dismantle the screw that can fold simultaneously.
In some embodiments, the folding multi-rotor rescue unmanned aerial vehicle is provided with an infrared thermal imaging camera 13 connected through an electric pan-tilt head at the bottom of the machine body 1.
Specifically, the electric pan-tilt is used for mounting a camera, and horizontally and vertically rotates under the action of control voltage (voltage output by a pan-tilt controller), so that the camera can be aligned and shoot a required observation target in a large range, and the electric pan-tilt and the camera are matched for use, so that the shooting range can be expanded, and the use value of the camera is improved; carry on the electronic cloud platform infrared thermal imaging camera 13 can carry out life detection, has improved this foldable many rotor rescue unmanned aerial vehicle's search and rescue ability.
In some embodiments, the folding multi-rotor rescue unmanned aerial vehicle further includes a GPS module and an artificial intelligence module disposed in the body 1.
Specifically, through appointing this foldable many rotor rescue unmanned aerial vehicle flight waypoint at ground control center, this unmanned aerial vehicle carries out the flight independently according to generating the orbit according to waypoint automatic generation flight orbit, this unmanned aerial vehicle of whole flight process obtains real-time positional information according to GPS satellite signal, constantly revises the position in order to keep flying on predetermineeing the orbit. Constantly send real-time position information and infrared thermal imaging image data back to ground control center through wireless data transmission and wireless picture transmission at the flight in-process, improved this foldable many rotors rescue unmanned aerial vehicle's search and rescue efficiency.
Further, set up artificial intelligence module, this unmanned aerial vehicle just can independently discern the rescue target like this, can high efficiency discernment be rescued the target in natural disasters such as earthquake, mud-rock flow, conflagration, strive for valuable rescue time to improve the survival rate of calamity people, have high social civilian value.
In summary, the utility model provides a folding multi-rotor rescue unmanned aerial vehicle, which is provided with a body; the power device comprises a plurality of machine arms, a power device and a control device, wherein one end of each machine arm is rotatably connected with the side surface of the machine body, and the other end of each machine arm is connected with a bearing part and the power device arranged on the bearing part; the side surface of the machine body is provided with a containing groove for containing the machine arm, and the side surface of the machine body is also provided with a containing space for containing the bearing part. The horn has development condition and folded condition, the horn can rotate relatively the organism, makes the horn switches between development condition and folded condition. When the folding multi-rotor rescue unmanned aerial vehicle is in a flying state, the horn is unfolded relative to the body and is in an unfolded state; when the foldable multi-rotor rescue unmanned aerial vehicle is in a non-flight state, the horn is folded in the accommodating groove of the body and is in a folded state; this foldable many rotors rescue unmanned aerial vehicle simple structure is compact, and the horn can be folded, has reduced unmanned aerial vehicle's whole volume during fold condition, is convenient for accomodate and carry.
The technical features of the embodiments described above may be arbitrarily combined, and for the sake of brevity, all possible combinations of the technical features in the embodiments described above are not described, but should be considered as being within the scope of the present specification as long as there is no contradiction between the combinations of the technical features.
The above-mentioned embodiments only represent some embodiments of the present invention, and the description thereof is specific and detailed, but not to be construed as limiting the scope of the present invention. It is to be understood that the invention is not limited to the above-described embodiments, and that modifications and variations may be made by those skilled in the art in light of the above teachings, and all such modifications and variations are intended to be included within the scope of the invention as defined in the appended claims.
Claims (9)
1. The utility model provides a foldable many rotors rescue unmanned aerial vehicle, its characterized in that, foldable many rotors rescue unmanned aerial vehicle includes:
a body (1);
the device comprises a plurality of machine arms (2), wherein one end of each machine arm (2) is rotatably connected with the side surface of the machine body (1), and the other end of each machine arm (2) is connected with a bearing part (3) and a power device arranged on the bearing part (3);
a containing groove (11) for containing the machine arm (2) is formed in the side face of the machine body (1), and a containing space (12) for containing the bearing part (3) is further formed in the side face of the machine body (1);
the machine arm (2) is hinged with the machine body (1), and an electromagnet device used for limiting and matching locking is arranged at the hinged position of the machine arm (2) and the machine body (1).
2. Folding multi-rotor rescue drone according to claim 1, characterized in that the direction of rotation of each horn (2) when folded is the same.
3. The folding multi-rotor rescue unmanned aerial vehicle according to claim 1 or 2, wherein the horn (2) is adapted to the accommodating groove (11), the bearing part (3) is adapted to the accommodating space (12), and a foot rest (4) is further disposed at the bottom of the bearing part (3).
4. The unmanned folding multi-rotor rescue helicopter of claim 3, wherein the shape of the airframe (1) is circular, the connection of each horn (2) to the airframe (1) is arranged at the bisector of the circular airframe (1), and the horns (2) are arc-shaped.
5. Folding multi-rotor rescue drone according to claim 4, characterized in that the number of arms (2) is four.
6. Folding multi-rotor rescue drone according to claim 5, characterized in that each of the arms (2) rotates clockwise when folded.
7. Folding multi-rotor rescue drone according to claim 1 or 2, characterized in that the power means comprise an electric motor arranged on the carrying portion (3) and a propeller arranged on the electric motor, the propeller being a detachable and foldable propeller.
8. Folding multi-rotor rescue drone according to claim 1 or 2, characterized in that the bottom of the body (1) is provided with an infrared thermal imaging camera (13) connected by an electric cradle head.
9. The folding multi-rotor rescue unmanned aerial vehicle of claim 8, wherein a GPS module and an artificial intelligence module are further disposed in the body (1).
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| CN202020445697.4U CN212099341U (en) | 2020-03-31 | 2020-03-31 | Foldable many rotors rescue unmanned aerial vehicle |
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| CN202020445697.4U CN212099341U (en) | 2020-03-31 | 2020-03-31 | Foldable many rotors rescue unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113697119A (en) * | 2021-10-03 | 2021-11-26 | 广东技术师范大学 | Unmanned aerial vehicle inspection equipment for power transmission line |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113697119A (en) * | 2021-10-03 | 2021-11-26 | 广东技术师范大学 | Unmanned aerial vehicle inspection equipment for power transmission line |
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Address after: 518000 3113, block a, Zhongguan Times Square, 4168 Liuxian Avenue, Pingshan community, Taoyuan Street, Nanshan District, Shenzhen, Guangdong Patentee after: Shenzhen Aiquan Technology Co.,Ltd. Address before: 518100 Bantian Street Yangmei Shangpin Yayuan 3b403, Longgang District, Shenzhen City, Guangdong Province Patentee before: SHENZHEN SHUDAI TECHNOLOGY CO.,LTD. |
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