CN210618461U - Unmanned aerial vehicle capable of being anchored on cliff - Google Patents
Unmanned aerial vehicle capable of being anchored on cliff Download PDFInfo
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- CN210618461U CN210618461U CN201921416965.3U CN201921416965U CN210618461U CN 210618461 U CN210618461 U CN 210618461U CN 201921416965 U CN201921416965 U CN 201921416965U CN 210618461 U CN210618461 U CN 210618461U
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Abstract
The utility model discloses an unmanned aerial vehicle capable of being stationed on cliff, including unmanned aerial vehicle main part, linking arm, rotor installation mechanism and a plurality of unmanned aerial vehicle stabilizer blade, rotor installation mechanism includes rotor base and rotor retaining ring, and the unmanned aerial vehicle stabilizer blade includes axis of rotation, kink, plane connecting plate, driving motor and conical bit, and axis of rotation and kink fixed connection, plane connecting plate, driving motor are fixed in the kink, and driving motor and conical bit fixed connection drive conical bit to rotate; the axis of rotation is rotated through a rotation motor and is installed in the linking arm, can camp on the unmanned aerial vehicle of cliff and fly to the appointed point in high altitude after, adjust the angle of unmanned aerial vehicle stabilizer blade for the foot point through rotating the motor, drive conical bit through driving motor and bore into the cliff and fix to the fixed point is shot. The power of wing stops earlier, then carries out and shoots the order, ensures to shoot for a long time, solves the long-time problem of shooing of cliff, makes unmanned aerial vehicle shoot for a long time to the place that the mankind is difficult to reach.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field especially relates to an unmanned aerial vehicle that can camp on cliff.
Background
Currently, an unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by means of a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
However, the existing unmanned aerial vehicle has the following defects:
1. if the unmanned aerial vehicle needs to shoot on the rock wall for a long time or on a high-altitude cliff in the field, on one hand, the wing power of the existing unmanned aerial vehicle needs to be shot simultaneously, and the consumption is large;
2. when the device flies to a place which is difficult to reach by human beings, if fixed-point shooting is needed, the base is not provided with a mechanism for penetrating into soil or rock walls.
SUMMERY OF THE UTILITY MODEL
In order to overcome the not enough of prior art, one of the purposes of the utility model is to provide a can camp on unmanned aerial vehicle of cliff, its problem that can solve the long-time shooting of cliff.
The utility model discloses an one of the purpose adopts following technical scheme to realize:
an unmanned aerial vehicle capable of being anchored on cliff comprises an unmanned aerial vehicle main body, 4 connecting arms, 4 rotor wing mounting mechanisms and 4 unmanned aerial vehicle supporting legs, wherein the connecting arms are mounted on the outer side of the unmanned aerial vehicle main body, the connecting arms are distributed around the unmanned aerial vehicle main body, the rotor wing mounting mechanisms are mounted at the end parts of the connecting arms, and the connecting arms are located between the unmanned aerial vehicle main body and the rotor wing mounting mechanisms;
the rotor wing installation mechanism comprises a rotor wing base and a rotor wing retaining ring, the rotor wing base is in a cross shape, the outer side of the rotor wing base is connected with the rotor wing retaining ring, the rotor wing base is located in the rotor wing retaining ring, and an unmanned aerial vehicle rotor wing is installed on the rotor wing base;
the unmanned aerial vehicle support leg comprises a rotating shaft, a bent part, a plane connecting plate, a driving motor and a conical drill bit, wherein the rotating shaft is fixedly connected with the bent part, the plane connecting plate and the driving motor are fixed on the bent part, and the driving motor is fixedly connected with the conical drill bit and drives the conical drill bit to rotate; the rotating shaft is rotatably mounted on the connecting arm through a rotating motor, after the unmanned aerial vehicle capable of being anchored on a cliff flies to a designated high-altitude point, the rotating motor is used for adjusting the angle of the unmanned aerial vehicle stand bar relative to a foot landing point, and the driving motor is used for driving the conical drill bit to drill into a rock wall for fixing, so that fixed-point shooting is realized;
the rotor base includes support arm and three and strengthens the arm, support arm and three it is the cross form to strengthen the arm, unmanned aerial vehicle rotor install in the support arm.
Further, the linking arm is equipped with the rotation mounting groove, rotate the mounting groove with the plane connecting plate size is corresponding, it drives to rotate the motor when the unmanned aerial vehicle stabilizer blade rotates, the plane connecting plate accomodate in it makes to rotate the mounting groove the plane connecting plate with the terminal surface parallel and level of linking arm.
Further, the linking arm still includes the link, link demountable installation in rotor installation mechanism.
Furthermore, state the linking arm and still include the link, the link is equipped with guide way and a plurality of fixed orifices, rotor installation mechanism install in the guide way to can dismantle through the screw and be fixed in the fixed orifices.
Further, the rotor base includes support arm and three enhancement arm, support arm and three it is the cross form to strengthen the arm, the unmanned aerial vehicle rotor install in the support arm.
Further, the support arm includes the mount table, the mount table is discoid, and the unmanned aerial vehicle rotor install in the mount table, the cross-sectional width of support arm is greater than the cross-sectional width of strengthening the arm.
Further, the unmanned aerial vehicle main part is equipped with the middle part and puts the thing groove, the middle part is put the thing groove and is located the middle part of unmanned aerial vehicle main part.
Furthermore, the middle storage groove is provided with a plurality of air quality collection bottles, each air quality collection bottle comprises a bottle opening piston, each bottle opening piston is connected with a control motor, and the control motors are fixedly connected with the bottle opening pistons and drive the bottle opening pistons to move so as to control the opening and closing of the air quality collection bottles.
Further, the extension direction of the conical drill is the same as that of the plane connecting plate.
Compared with the prior art, the beneficial effects of the utility model reside in that:
the unmanned aerial vehicle support leg comprises a rotating shaft, a bent part, a plane connecting plate, a driving motor and a conical drill bit, wherein the rotating shaft is fixedly connected with the bent part, the plane connecting plate and the driving motor are fixed on the bent part, and the driving motor is fixedly connected with the conical drill bit and drives the conical drill bit to rotate; the rotating shaft is rotatably installed on the connecting arm through a rotating motor, after the unmanned aerial vehicle capable of being anchored on the cliff flies to a designated high-altitude point, the angle of the unmanned aerial vehicle supporting legs relative to a foothold is adjusted through the rotating motor, and the conical drill bit is driven by the driving motor to drill into the rock wall to be fixed, so that fixed-point shooting is achieved. The power of wing stops earlier, then carries out and shoots the order, ensures to shoot for a long time, solves the long-time problem of shooing of cliff, makes unmanned aerial vehicle shoot for a long time to the place that the mankind is difficult to reach.
The foregoing description is only an overview of the technical solutions of the present invention, and in order to make the technical means of the present invention more clearly understood, the present invention may be implemented according to the content of the description, and in order to make the above and other objects, features, and advantages of the present invention more obvious and understandable, the following preferred embodiments are described in detail with reference to the accompanying drawings.
Drawings
FIG. 1 is a perspective view of a preferred embodiment of an unmanned aerial vehicle capable of being anchored to a cliff;
FIG. 2 is a partial perspective view of the drone of FIG. 1 that may be anchored to a cliff;
FIG. 3 is a side perspective view of the drone of FIG. 1 that may be anchored to a cliff;
FIG. 4 is a top perspective view of the drone of FIG. 1 that may be anchored to a cliff;
FIG. 5 is another perspective view of the drone of FIG. 1 that may be anchored to a cliff;
FIG. 6 is another partial perspective view of the drone of FIG. 1 that may be anchored to a cliff;
FIG. 7 is a partial enlarged view of the unmanned aerial vehicle shown in FIG. 6 that may be anchored to a cliff at A;
FIG. 8 is a perspective view of an unmanned aerial vehicle of FIG. 1 that may be anchored to a cliff.
In the figure: 100. an unmanned aerial vehicle capable of being anchored on a cliff; 10. an unmanned aerial vehicle main body; 11. a middle storage groove; 20. a connecting arm; 21. rotating the mounting groove; 22. a connecting end; 221. a guide groove; 222. a fixing hole; 30. a rotor wing mounting mechanism; 31. a rotor base; 311. a support arm; 3111. An installation table; 312. a reinforcing arm; 32. a rotor wing shroud ring; 321. a side edge; 322. a connecting portion; 40. unmanned aerial vehicle support legs; 41. a rotating shaft; 42. a bending section; 43. a planar connecting plate; 44. a drive motor; 45. a cone drill bit.
Detailed Description
The present invention will be further described with reference to the accompanying drawings and the detailed description, and it should be noted that the embodiments or technical features described below can be arbitrarily combined to form a new embodiment without conflict.
It will be understood that when an element is referred to as being "secured to" 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 component, it can be directly connected to the other component or intervening components may also be present. When a component is referred to as being "disposed on" another component, it can be directly on the other component or intervening components may also be present. The terms "vertical," "horizontal," "left," "right," and the like as used herein are for illustrative purposes only.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
Referring to fig. 1 to 8, an unmanned aerial vehicle 100 capable of being anchored on a cliff includes an unmanned aerial vehicle main body 10, 4 connecting arms 20, 4 rotor wing mounting mechanisms 30, and 4 unmanned aerial vehicle legs 40, wherein the connecting arms 20 are mounted on the outer side of the unmanned aerial vehicle main body 10, the connecting arms 20 are distributed around the unmanned aerial vehicle main body 10, the rotor wing mounting mechanisms 30 are mounted on the end portions of the connecting arms 20, and the connecting arms 20 are located between the unmanned aerial vehicle main body 10 and the rotor wing mounting mechanisms 30. Rotor installation mechanism 30 includes rotor base 31 and rotor retaining ring 32, rotor base 31 is the cross form, rotor base 31 the outside with rotor retaining ring 32 links up, rotor base 31 is located in rotor retaining ring 32, the unmanned aerial vehicle rotor install in rotor base 31. The inboard unmanned aerial vehicle rotor is protected by rotor shroud 32.
Specifically, in this embodiment, the rotor of the unmanned aerial vehicle is driven by a rotating motor, the rotating motor is fixedly connected through a lifting motor, and when the unmanned aerial vehicle is in a rest state, the wings are accommodated in the protective sleeve under the action of the lifting motor; when the aircraft is in a state of waiting for flying, the wings move out of the protective sleeves under the action of the lifting motor. The problem of conventional state touch unmanned aerial vehicle rotor easily is solved.
The unmanned aerial vehicle support leg 40 comprises a rotating shaft 41, a bent part 42, a plane connecting plate 43, a driving motor 44 and a conical drill bit 45, wherein the rotating shaft 41 is fixedly connected with the bent part 42, the plane connecting plate 43 and the driving motor 44 are fixed on the bent part 42, and the driving motor 44 is fixedly connected with the conical drill bit 45 and drives the conical drill bit 45 to rotate; the rotating shaft 41 is rotatably mounted on the connecting arm 20 through a rotating motor, after the unmanned aerial vehicle 100 capable of being anchored on a cliff flies to a designated high-altitude point, the rotating motor adjusts the angle of the unmanned aerial vehicle support leg 40 relative to a foot-falling point, and the driving motor 44 drives the conical drill bit 45 to drill into a rock wall for fixing, so that fixed-point shooting is realized. The power of wing stops earlier, then carries out and shoots the order, ensures to shoot for a long time, solves the long-time problem of shooing of cliff, makes unmanned aerial vehicle shoot for a long time to the place that the mankind is difficult to reach.
Preferably, the connecting arm 20 is equipped with rotation mounting groove 21, rotate mounting groove 21 with the size of plane connecting plate 43 is corresponding, it drives to rotate the motor when unmanned aerial vehicle stabilizer blade 40 rotates, plane connecting plate 43 take in it makes to rotate mounting groove 21 plane connecting plate 43 with the terminal surface parallel and level of connecting arm 20. Both can ensure the flexibility ratio and adjust the angle of falling to the ground, can ensure the outward appearance again, need during the function of unmanned aerial vehicle stabilizer blade 40, the retractable is inside, reduces flight resistance on the one hand, and on the other hand controls the convenience.
Preferably, the connecting arm 20 further comprises a connecting end 22, and the connecting end 22 is detachably mounted to the rotor mounting mechanism 30. Specifically, the connecting arm 20 further includes a connecting end 22, the connecting end 22 is provided with a guide groove 221 and a plurality of fixing holes 222, and the rotor wing mounting mechanism 30 is mounted in the guide groove 221 and detachably fixed to the fixing holes 222 through screws. Through demountable installation's mode, realize the change of unmanned aerial vehicle wing subassembly, it is simple and convenient.
Preferably, unmanned aerial vehicle main part 10 is equipped with middle part and puts thing groove 11, middle part is put thing groove 11 and is located the middle part of unmanned aerial vehicle main part 10. The middle storage groove 11 is provided with a plurality of air quality collection bottles, each air quality collection bottle comprises a bottle opening piston, each bottle opening piston is connected with a control motor, and the control motors are fixedly connected with the bottle opening pistons and drive the bottle opening pistons to move so as to control the opening and closing of the air quality collection bottles. In the implementation of the sampling task, the sampling can be carried out once every 2h interval, which is not separated from our main body, and if the wing power is stopped without fixed point, the battery supply cannot guarantee long-time sampling.
Preferably, the extension direction of the cone bit 45 is the same as the extension direction of the plane connection plate 43. Novel structure, the suitability is strong, the facilitate promotion.
Preferably, rotor shroud ring 32 includes two lateral part borders 321 and connecting portion 322, connecting portion 322 both ends respectively with two lateral part borders 321 fixed connection, protect effectually.
The above embodiments are only preferred embodiments of the present invention, and the protection scope of the present invention cannot be limited thereby, and any insubstantial changes and substitutions made by those skilled in the art based on the present invention are all within the protection scope of the present invention.
Claims (8)
1. An unmanned aerial vehicle that can camp on cliff which characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle main body, 4 connecting arms, 4 rotor wing mounting mechanisms and 4 unmanned aerial vehicle supporting legs, wherein the connecting arms are mounted on the outer side of the unmanned aerial vehicle main body, the connecting arms are distributed around the unmanned aerial vehicle main body, the rotor wing mounting mechanisms are mounted at the end parts of the connecting arms, and the connecting arms are located between the unmanned aerial vehicle main body and the rotor wing mounting mechanisms;
the rotor wing installation mechanism comprises a rotor wing base and a rotor wing retaining ring, the rotor wing base is in a cross shape, the outer side of the rotor wing base is connected with the rotor wing retaining ring, the rotor wing base is located in the rotor wing retaining ring, and an unmanned aerial vehicle rotor wing is installed on the rotor wing base;
the unmanned aerial vehicle support leg comprises a rotating shaft, a bent part, a plane connecting plate, a driving motor and a conical drill bit, wherein the rotating shaft is fixedly connected with the bent part, the plane connecting plate and the driving motor are fixed on the bent part, and the driving motor is fixedly connected with the conical drill bit and drives the conical drill bit to rotate; the rotating shaft is rotatably mounted on the connecting arm through a rotating motor, after the unmanned aerial vehicle capable of being anchored on a cliff flies to a designated high-altitude point, the rotating motor is used for adjusting the angle of the unmanned aerial vehicle stand bar relative to a foot landing point, and the driving motor is used for driving the conical drill bit to drill into a rock wall for fixing, so that fixed-point shooting is realized;
the rotor base includes support arm and three and strengthens the arm, support arm and three it is the cross form to strengthen the arm, unmanned aerial vehicle rotor install in the support arm.
2. The unmanned aerial vehicle stationed on a cliff of claim 1, wherein: the linking arm is equipped with the rotation mounting groove, rotate the mounting groove with the plane connecting plate size is corresponding, it drives to rotate the motor when the unmanned aerial vehicle stabilizer blade rotates, the plane connecting plate accomodate in it makes to rotate the mounting groove the plane connecting plate with the terminal surface parallel and level of linking arm.
3. The unmanned aerial vehicle stationed on a cliff of claim 1, wherein: the linking arm still includes the link, link demountable installation in rotor installation mechanism.
4. The unmanned aerial vehicle stationed on a cliff of claim 1, wherein: the linking arm still includes the link, the link is equipped with guide way and a plurality of fixed orifices, rotor installation mechanism install in the guide way to can dismantle through the screw and be fixed in the fixed orifices.
5. The unmanned aerial vehicle stationed on a cliff of claim 1, wherein: the support arm includes the mount table, the mount table is discoid, unmanned aerial vehicle rotor install in the mount table, the cross-sectional width of support arm is greater than the cross-sectional width of strengthening the arm.
6. The unmanned aerial vehicle stationed on a cliff of claim 1, wherein: the unmanned aerial vehicle main part is equipped with the middle part and puts the thing groove, the middle part is put the thing groove and is located the middle part of unmanned aerial vehicle main part.
7. The unmanned aerial vehicle capable of stationing on a cliff of claim 6, wherein: the middle storage groove is provided with a plurality of air quality collection bottles, each air quality collection bottle comprises a bottle opening piston, each bottle opening piston is connected with a control motor, and the control motors are fixedly connected with the bottle opening pistons and drive the bottle opening pistons to move so as to control the opening and closing of the air quality collection bottles.
8. The unmanned aerial vehicle stationed on a cliff of claim 1, wherein: the extension direction of the conical drill bit is the same as that of the plane connecting plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921416965.3U CN210618461U (en) | 2019-08-29 | 2019-08-29 | Unmanned aerial vehicle capable of being anchored on cliff |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921416965.3U CN210618461U (en) | 2019-08-29 | 2019-08-29 | Unmanned aerial vehicle capable of being anchored on cliff |
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| Publication Number | Publication Date |
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| CN210618461U true CN210618461U (en) | 2020-05-26 |
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| CN201921416965.3U Active CN210618461U (en) | 2019-08-29 | 2019-08-29 | Unmanned aerial vehicle capable of being anchored on cliff |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111773580A (en) * | 2020-07-02 | 2020-10-16 | 乐清市万正消防设备有限公司 | Intensive residential area unmanned aerial vehicle fire extinguishing device |
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2019
- 2019-08-29 CN CN201921416965.3U patent/CN210618461U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111773580A (en) * | 2020-07-02 | 2020-10-16 | 乐清市万正消防设备有限公司 | Intensive residential area unmanned aerial vehicle fire extinguishing device |
| CN111773580B (en) * | 2020-07-02 | 2021-06-29 | 乐清市万正消防设备有限公司 | Intensive residential area unmanned aerial vehicle fire extinguishing device |
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| TR01 | Transfer of patent right |
Effective date of registration: 20220822 Address after: North side of Chuangxin Road, Xuzhuang Street, Gaogang District, Taizhou City, Jiangsu Province 225324 Patentee after: Taizhou Zhongyi Marine Equipment Co.,Ltd. Address before: 225300 east side of Xingyuan Road, science and Technology Pioneer Park, Gao Gang, Taizhou, Jiangsu Patentee before: TAIZHOU KEPUNI COMMUNICATION EQUIPMENT Co.,Ltd. |
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