CN211766344U - Unmanned aerial vehicle with adjustable illumination angle - Google Patents
Unmanned aerial vehicle with adjustable illumination angle Download PDFInfo
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- CN211766344U CN211766344U CN201922293475.5U CN201922293475U CN211766344U CN 211766344 U CN211766344 U CN 211766344U CN 201922293475 U CN201922293475 U CN 201922293475U CN 211766344 U CN211766344 U CN 211766344U
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Abstract
The utility model discloses an unmanned aerial vehicle of adjustable illumination angle, including the unmanned aerial vehicle body, the first electric telescopic handle of bottom fixedly connected with of unmanned aerial vehicle body, first electric telescopic handle's bottom fixedly connected with casing, the top fixedly connected with motor of casing inner chamber, motor shaft's bottom fixedly connected with mounting panel, the bottom of mounting panel is seted up flutedly, and the bottom of casing is run through and is provided with the montant. The utility model provides a current unmanned aerial vehicle's light illumination angle be not convenient for adjust to because sheltering from of unmanned aerial vehicle landing leg when adjusting, and then the light is easy to be sheltered from and causes great area shadow, if the light is less than the position of unmanned aerial vehicle landing leg, the light easily causes the damage with ground contact when unmanned aerial vehicle descends, the person of not being convenient for uses at night, and unmanned aerial vehicle can not carry out the shock attenuation buffering at the in-process of descending, produce the impact force and conduct the problem that easily causes unmanned aerial vehicle to damage on the unmanned aerial vehicle skeleton.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle of adjustable illumination angle.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by using a radio remote control device and a self-contained program control device, the unmanned aerial vehicle is a general name of the unmanned aerial vehicle in reality, compared with manned aircraft, it has the advantages of small volume, low cost, convenient use, low requirement on the operation environment, strong battlefield viability and the like, and in order to facilitate the night flight of the unmanned aerial vehicle, the lighting device is required to be arranged on the unmanned aerial vehicle, however, the illumination angle of the illuminating lamp of the existing unmanned aerial vehicle is inconvenient to adjust, and due to the shielding of the supporting legs of the unmanned aerial vehicle during adjustment, further, the light rays are easy to be shielded to cause larger area shadow, if the illuminating lamp is lower than the position of the support legs of the unmanned aerial vehicle, when the unmanned aerial vehicle lands, the lighting lamp is easy to be damaged when contacting with the ground, is inconvenient for a user to use at night, and unmanned aerial vehicle can not carry out the shock attenuation buffering at the in-process that descends, produces the impact force and conducts and easily cause unmanned aerial vehicle to damage on the unmanned aerial vehicle skeleton.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle of adjustable illumination angle, possess the illumination angle and be convenient for adjust and the advantage of shock attenuation buffering, the illumination angle of the light of having solved current unmanned aerial vehicle is not convenient for adjust, and because sheltering from of unmanned aerial vehicle landing leg when adjusting, and then light is easy to be sheltered from and causes great area shadow, if the light is less than the position of unmanned aerial vehicle landing leg, light and ground contact easily cause the damage when unmanned aerial vehicle descends, the person of not being convenient for uses at night, and unmanned aerial vehicle can not carry out the shock attenuation buffering at the in-process of descending, produce the impact force and conduct and easily cause the problem that unmanned aerial vehicle damaged on the unmanned.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle with adjustable illumination angle comprises an unmanned aerial vehicle body, wherein the bottom of the unmanned aerial vehicle body is fixedly connected with a first electric telescopic rod, the bottom of the first electric telescopic rod is fixedly connected with a shell, the top of an inner cavity of the shell is fixedly connected with a motor, the bottom of a rotating shaft of the motor is fixedly connected with a mounting plate, the bottom of the mounting plate is provided with a groove, the bottom of the shell is provided with a vertical rod in a penetrating manner, the top of the vertical rod penetrates through the shell and extends to the inner cavity of the groove, the top of the right side of the vertical rod is provided with a clamping groove, the right side of the mounting plate is provided with a clamping rod in a penetrating manner, the left end of the clamping rod penetrates through the mounting plate and extends to the inner cavity of the clamping groove, the surface of the right end of the clamping rod, the right-hand member of first spring and the left side fixed connection of connecting plate, there is the light bottom of montant through pivot swing joint, there is second electric telescopic handle at the positive top of montant through pivot swing joint, the one end that the montant was kept away from to second electric telescopic handle and the front side swing joint at light top, there is the chamber door on the right side of casing through hinge swing joint, the equal fixedly connected with second spring in four corners of unmanned aerial vehicle body bottom, the bottom fixedly connected with landing leg of second spring.
Preferably, the equal fixedly connected with quarter butt in four corners of unmanned aerial vehicle body bottom, the bottom cover on quarter butt surface is equipped with the sleeve pipe, the top fixed connection of sheathed tube bottom and landing leg, quarter butt and sleeve pipe all are located the inner chamber of second spring.
Preferably, the bottom of the shell is provided with a first through hole matched with the vertical rod, and the diameter of the vertical rod is smaller than that of the first through hole.
Preferably, the right side of the mounting plate is provided with a second through hole matched with the clamping rod, and the diameter of the clamping rod is smaller than that of the second through hole.
Preferably, the right side of the connecting plate is fixedly connected with a pull ring, and the pull ring is circular in shape.
Preferably, the bottom on the right side of the box door is fixedly connected with a handle, and the left end of the clamping rod is designed to be an inclined plane.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses an unmanned aerial vehicle body, first electric telescopic handle, a housing, including a motor, an end cap, a controller, and a cover plate, the mounting panel, a groove, the draw-in groove, the kelly, first spring, the connecting plate, the light, second electric telescopic handle, the chamber door, second spring and landing leg cooperate, possess the angle of illumination and be convenient for adjust and the advantage of shock attenuation buffering, the illumination angle of the light of having solved current unmanned aerial vehicle is not convenient for adjust, and because sheltering from of unmanned aerial vehicle landing leg when adjusting, and then the light is easy to be sheltered from and causes great area shadow, if the light is less than the position of unmanned aerial vehicle landing leg, the light easily causes the damage with the ground contact when unmanned aerial vehicle descends, the person of not facilitating the use uses at night, and unmanned aerial vehicle can not carry out the shock attenuation.
2. The utility model discloses a set up quarter butt and sleeve pipe, prevent that the second spring from can't supporting unmanned aerial vehicle at shock attenuation time deformation, cause unmanned aerial vehicle's damage, through setting up first through-hole, the montant of being convenient for does not receive the influence of casing when rotating, and the pivoted is more smooth and easy, through setting up the second through-hole, makes more smooth of kelly when removing, through setting up the pull ring, the kelly of being convenient for is removed in the pulling pull ring, through setting up the handle, the opening of the chamber door of being convenient for.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a right-side view schematically illustrating the connection between the second electric telescopic rod and the lighting lamp according to the present invention;
fig. 3 is an enlarged schematic view of a in fig. 1 according to the present invention.
In the figure: 1 unmanned aerial vehicle body, 2 first electric telescopic handle, 3 casings, 4 motors, 5 mounting panels, 6 recesses, 7 montants, 8 draw-in grooves, 9 kellies, 10 first springs, 11 connecting plates, 12 light, 13 second electric telescopic handle, 14 chamber doors, 15 second springs, 16 landing legs, 17 quarter butt, 18 sleeve pipes, 19 pull rings.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end", 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 element to be referred must have a specific orientation, be constructed in a specific orientation, and be operated, 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", "provided", "connected", and the like are to be construed broadly, such as "connected", which may be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The utility model discloses an unmanned aerial vehicle body 1, first electric telescopic handle 2, casing 3, motor 4, mounting panel 5, recess 6, montant 7, draw-in groove 8, kelly 9, first spring 10, connecting plate 11, light 12, second electric telescopic handle 13, chamber door 14, second spring 15, landing leg 16, quarter butt 17, sleeve pipe 18 and pull ring 19 part are the general standard or the part that technical personnel in the field know, its structure and principle all are that this technical personnel all can learn through the technical manual or learn through conventional experimental method.
Referring to fig. 1-3, an unmanned aerial vehicle with adjustable illumination angle comprises an unmanned aerial vehicle body 1, a first electric telescopic rod 2 is fixedly connected to the bottom of the unmanned aerial vehicle body 1, a housing 3 is fixedly connected to the bottom of the first electric telescopic rod 2, a motor 4 is fixedly connected to the top of the inner cavity of the housing 3, a mounting plate 5 is fixedly connected to the bottom of the rotating shaft of the motor 4, a groove 6 is formed in the bottom of the mounting plate 5, a vertical rod 7 is arranged at the bottom of the housing 3 in a penetrating manner, the top of the vertical rod 7 penetrates through the housing 3 and extends to the inner cavity of the groove 6, a clamping groove 8 is formed in the top of the right side of the vertical rod 7, a clamping rod 9 is arranged at the right side of the mounting plate 5 in a penetrating manner, the left end of the clamping rod 9 penetrates through the mounting plate 5 and extends to the inner cavity of the clamping groove 8, a first spring, the right end of the first spring 10 is fixedly connected with the left side of the connecting plate 11, the bottom of the vertical rod 7 is movably connected with an illuminating lamp 12 through a rotating shaft, the front top of the vertical rod 7 is movably connected with a second electric telescopic rod 13 through a rotating shaft, one end, far away from the vertical rod 7, of the second electric telescopic rod 13 is movably connected with the front side of the top of the illuminating lamp 12, the right side of the shell 3 is movably connected with a box door 14 through a hinge, four corners of the bottom of the unmanned aerial vehicle body 1 are fixedly connected with second springs 15, supporting legs 16 are fixedly connected with the bottom of the second spring 15, short rods 17 are fixedly connected with four corners of the bottom of the unmanned aerial vehicle body 1, sleeves 18 are sleeved on the surfaces of the short rods 17, the bottoms of the sleeves 18 are fixedly connected with the tops of the supporting legs 16, the short rods 17 and the sleeves 18 are both located in the inner cavities of the second springs, cause unmanned aerial vehicle's damage, the first through-hole with montant 7 looks adaptation is seted up to the bottom of casing 3, the diameter of montant 7 is less than the diameter of first through-hole, through setting up first through-hole, be convenient for montant 7 does not receive the influence of casing 3 when rotating, it is more smooth and easy to rotate, the second through-hole with kelly 9 looks adaptation is seted up on the right side of mounting panel 5, the diameter of kelly 9 is less than the diameter of second through-hole, through setting up the second through-hole, make kelly 9 more smooth when moving, the right side fixedly connected with pull ring 19 of connecting plate 11, the shape of pull ring 19 is circular, through setting up pull ring 19, pulling pull ring 19 is convenient for kelly 9 to remove, the bottom fixedly connected with handle on chamber door 14 right side, the left end of kelly 9 is the inclined plane design, through setting up the handle, be convenient for opening of chamber door 14, through unmanned, Motor 4, mounting panel 5, recess 6, montant 7, draw-in groove 8, kelly 9, first spring 10, connecting plate 11, light 12, second electric telescopic handle 13, chamber door 14, second spring 15 and landing leg 16 cooperate, possess the angle of illumination and be convenient for adjust and the advantage of shock attenuation buffering, the 12 illumination angles of light of having solved current unmanned aerial vehicle are not convenient for adjust, and because sheltering from of unmanned aerial vehicle landing leg 16 when adjusting, and then light is easy to be sheltered from and causes great area shadow, if light 12 is less than the position of unmanned aerial vehicle landing leg 16, light 12 easily causes the damage with ground contact when unmanned aerial vehicle descends, the person of not facilitating the use uses at night, and unmanned aerial vehicle can not carry out the shock attenuation buffering at the in-process of descending, produce the problem that the impact force conducts and easily causes unmanned aerial vehicle to damage on the unmanned.
When the unmanned aerial vehicle is used, the first electric telescopic rod 2, the motor 4 and the second electric telescopic rod 13 are connected with the remote control end and controlled by remote control, when the unmanned aerial vehicle is lifted off and needs to be irradiated for angle adjustment, the extension of the first electric telescopic rod 2 is controlled by remote control, the extension of the first electric telescopic rod 2 drives the shell 3 and the vertical rod 7 to move downwards, the height of the illuminating lamp 12 is lower than the bottom of the supporting leg 16, the supporting leg 16 is prevented from blocking the illumination of the illuminating lamp 12 to form a shadow, when the longitudinal angle is required to be adjusted, the extension of the second electric telescopic rod 13 is controlled by remote control, the extension of the second electric telescopic rod 13 drives the illuminating lamp 12 to rotate by taking the bottom of the vertical rod 7 as the circle center, so as to adjust the longitudinal angle, when the horizontal angle is required to rotate, the operation of the rotating shaft of the motor 4 is controlled by remote control, the rotation, the rotation of the vertical rod 7 drives the horizontal direction of the illuminating lamp 12 to rotate for illumination, so that the illumination angle of the illuminating lamp 12 is adjusted, when the unmanned aerial vehicle is about to fall to the ground, the contraction of the first electric telescopic rod 2 is controlled by remote control, the contraction of the first electric telescopic rod 2 drives the shell 3 and the vertical rod 7 to move upwards, the height of the illuminating lamp 12 is higher than the bottom of the supporting leg 16, the illuminating lamp 12 is prevented from being easily damaged due to contact with the ground when the unmanned aerial vehicle descends, the unmanned aerial vehicle can be subjected to shock absorption and buffering by arranging the second spring 15, the generated impact force is reduced and transmitted to the framework of the unmanned aerial vehicle, the descending is more stable, when the illuminating lamp 12 needs to be disassembled for maintenance or replacement, the box door 14 is opened, the clamping rod 9 is separated from the clamping groove 8 by pulling the pull ring 19, the illuminating lamp 12 can be disassembled, when the illuminating lamp 12 needs, due to the inclined plane design of the clamping rod 9, the vertical rod 7 extrudes the clamping rod 9, the left end of the clamping rod 9 is moved into the second through hole, the vertical rod 7 is rotated when the top of the vertical rod 7 is in contact with the top of the inner cavity of the groove 6, when the clamping groove 8 is aligned with the clamping rod 9, the clamping rod 9 is fixed in the clamping groove 8 due to the fact that the elastic force of the first spring 10 drives the left end of the clamping rod 9 to insert, and therefore the illuminating lamp 12 is fixed.
In summary, the following steps: the unmanned aerial vehicle with the adjustable illumination angle has the advantages that the illumination angle is convenient to adjust and shock-absorbing and buffering effects are achieved through the cooperation of the unmanned aerial vehicle body 1, the first electric telescopic rod 2, the shell 3, the motor 4, the mounting plate 5, the groove 6, the vertical rod 7, the clamping groove 8, the clamping rod 9, the first spring 10, the connecting plate 11, the illuminating lamp 12, the second electric telescopic rod 13, the box door 14, the second spring 15 and the supporting legs 16, the problem that the illumination angle of the existing unmanned aerial vehicle is inconvenient to adjust is solved, and due to the fact that the supporting legs of the unmanned aerial vehicle are shielded during adjustment, further, the light rays are easy to be shielded to cause larger area shadow, if the illuminating lamp is lower than the position of the support legs of the unmanned aerial vehicle, when the unmanned aerial vehicle lands, the lighting lamp is easy to be damaged when contacting with the ground, is inconvenient for a user to use at night, and unmanned aerial vehicle can not carry out the shock attenuation buffering at the in-process that descends, produces the impact force and conducts and easily cause the problem of unmanned aerial vehicle damage on the unmanned aerial vehicle skeleton.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an unmanned aerial vehicle of adjustable illumination angle, includes unmanned aerial vehicle body (1), its characterized in that: the unmanned aerial vehicle is characterized in that a first electric telescopic rod (2) is fixedly connected to the bottom of the unmanned aerial vehicle body (1), a shell (3) is fixedly connected to the bottom of the first electric telescopic rod (2), a motor (4) is fixedly connected to the top of an inner cavity of the shell (3), a mounting plate (5) is fixedly connected to the bottom of a rotating shaft of the motor (4), a groove (6) is formed in the bottom of the mounting plate (5), a vertical rod (7) penetrates through the bottom of the shell (3), the top of the vertical rod (7) penetrates through the shell (3) and extends to the inner cavity of the groove (6), a clamping groove (8) is formed in the top of the right side of the vertical rod (7), a clamping rod (9) penetrates through the right side of the mounting plate (5), the left end of the clamping rod (9) penetrates through the mounting plate (5) and extends to the inner cavity of the clamping groove (8), the right-hand member fixedly connected with connecting plate (11) of kelly (9), the left end of first spring (10) and the right side fixed connection of mounting panel (5), the right-hand member of first spring (10) and the left side fixed connection of connecting plate (11), there is light (12) bottom of montant (7) through pivot swing joint, there is second electric telescopic handle (13) through pivot swing joint in the positive top of montant (7), the one end that montant (7) were kept away from in second electric telescopic handle (13) and the front side swing joint at light (12) top, there is chamber door (14) on the right side of casing (3) through hinge swing joint, the equal fixedly connected with second spring in four corners (15) of unmanned aerial vehicle body (1) bottom, the bottom fixedly connected with landing leg (16) of second spring (15).
2. The unmanned aerial vehicle of claim 1, wherein the lighting angle is adjustable by: the equal fixedly connected with quarter butt (17) in four corners of unmanned aerial vehicle body (1) bottom, the bottom cover on quarter butt (17) surface is equipped with sleeve pipe (18), the top fixed connection of the bottom of sleeve pipe (18) and landing leg (16), quarter butt (17) and sleeve pipe (18) all are located the inner chamber of second spring (15).
3. The unmanned aerial vehicle of claim 1, wherein the lighting angle is adjustable by: the bottom of the shell (3) is provided with a first through hole matched with the vertical rod (7), and the diameter of the vertical rod (7) is smaller than that of the first through hole.
4. The unmanned aerial vehicle of claim 1, wherein the lighting angle is adjustable by: the second through-hole with kelly (9) looks adaptation is seted up on the right side of mounting panel (5), the diameter of kelly (9) is less than the diameter of second through-hole.
5. The unmanned aerial vehicle of claim 1, wherein the lighting angle is adjustable by: the right side of the connecting plate (11) is fixedly connected with a pull ring (19), and the pull ring (19) is circular.
6. The unmanned aerial vehicle of claim 1, wherein the lighting angle is adjustable by: the bottom on the right side of the box door (14) is fixedly connected with a handle, and the left end of the clamping rod (9) is designed to be an inclined surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922293475.5U CN211766344U (en) | 2019-12-18 | 2019-12-18 | Unmanned aerial vehicle with adjustable illumination angle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922293475.5U CN211766344U (en) | 2019-12-18 | 2019-12-18 | Unmanned aerial vehicle with adjustable illumination angle |
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| Publication Number | Publication Date |
|---|---|
| CN211766344U true CN211766344U (en) | 2020-10-27 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922293475.5U Active CN211766344U (en) | 2019-12-18 | 2019-12-18 | Unmanned aerial vehicle with adjustable illumination angle |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113879553A (en) * | 2021-11-03 | 2022-01-04 | 国网辽宁省电力有限公司铁岭供电公司 | Unmanned aerial vehicle night illumination mounting device for power inspection |
| CN115675953A (en) * | 2022-12-29 | 2023-02-03 | 北京熙捷科技有限公司 | Unmanned aerial vehicle device for night illumination |
-
2019
- 2019-12-18 CN CN201922293475.5U patent/CN211766344U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113879553A (en) * | 2021-11-03 | 2022-01-04 | 国网辽宁省电力有限公司铁岭供电公司 | Unmanned aerial vehicle night illumination mounting device for power inspection |
| CN115675953A (en) * | 2022-12-29 | 2023-02-03 | 北京熙捷科技有限公司 | Unmanned aerial vehicle device for night illumination |
| CN115675953B (en) * | 2022-12-29 | 2023-11-03 | 北京熙捷科技有限公司 | Unmanned aerial vehicle device for night illumination |
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Effective date of registration: 20230720 Address after: 430000 Room B1-13, 3rd Floor, Building S5-1, Block B, Wanda Plaza, Wuhan Economic and Technological Development Zone, Wuhan, Hubei Province Patentee after: Wuhan Miaobimeng Cultural Media Co.,Ltd. Address before: Room 1406, 14 / F, unit 1, building 5, No. 366, Ronghua South Road, high tech Zone, Chengdu, Sichuan 610000 Patentee before: Sichuan qiyibiao Information Technology Co.,Ltd. |