CN210707932U

CN210707932U - Unmanned aerial vehicle zooms searchlight structure

Info

Publication number: CN210707932U
Application number: CN201921782509.0U
Authority: CN
Inventors: 刘春燕
Original assignee: Fuzhou Haohai Communication Technology Co Ltd
Current assignee: Fuzhou Haohai Communication Technology Co Ltd
Priority date: 2019-10-23
Filing date: 2019-10-23
Publication date: 2020-06-09
Anticipated expiration: 2029-10-23

Abstract

The utility model discloses an unmanned aerial vehicle searchlight structure that zooms, including a lamp body section of thick bamboo, central knob, complementary unit, main knob, the circle cover, become the focal plate, searchlight wick, zoom the ring, integrative shell, bracket and thread bush, this unmanned aerial vehicle zooms searchlight structure has set up complementary unit through optimizing, slide double hook piece into install into corresponding supporting trench on, the first tripod of double hook piece bottom, second tripod and internals, the fitting piece carries out normal running fit, the spring in the central outer pole can carry out the motion of zooming in the certain limit, even double hook piece cooperation internals on the mounted position of searchlight place, the swing range of less range appears in the fitting piece, increase the reply scope of searchlight limit end, nimble installation when the installation, the spring has certain slow-pressing effect.

Description

Unmanned aerial vehicle zooms searchlight structure

Technical Field

The utility model relates to an unmanned aerial vehicle field of being correlated with specifically is an unmanned aerial vehicle searchlight structure that zooms.

Background

The unmanned aerial vehicle is an unmanned aerial vehicle operated by a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, and the unmanned aerial vehicle zoom searchlight is a volume lamp body for searchlighting.

When using at unmanned aerial vehicle installation, the searchlight on the unmanned aerial vehicle generally need adjust the back that targets in place at illumination angle, sets for certain direction of use, and the spacing effect of the mode that adopts the screw fixation is limited, and the adaptation clearance is fixed on the installation position, is difficult to nimble installation when the installation, increases the reply scope of searchlight limit end simultaneously, has certain slow-pressing effect.

Disclosure of Invention

Therefore, in order to solve the above insufficiency, the utility model provides an unmanned aerial vehicle searchlight structure that zooms here.

The utility model discloses a realize like this, construct an unmanned aerial vehicle zooms searchlight structure, the device includes a lamp body section of thick bamboo, central knob, complementary unit, main knob, circle cover, zoom piece, searchlight wick, zoom ring, an organic whole shell, bracket and thread bush, the screw bush is installed to lamp body section of thick bamboo right side screw thread, central knob and bracket clearance fit, main knob surface embedding is installed on the circle cover, the zoom piece is installed on zoom ring, searchlight wick fixed mounting is in zoom ring inboard, an organic whole shell and thread bush fixed connection, complementary unit is located lamp body section of thick bamboo side, complementary unit includes double hook piece, central outer pole, first tripod, side knob, internals, fixed piece, fitting piece, second tripod, spring and interior pole, double hook bottom welded fastening has first tripod, second tripod, central outer pole side embedding is installed the side knob, the outer side surface of the inner part is attached to the inner side surface of the first tripod, the inner part is fixedly installed on the lamp body barrel, the inner part and the matching part are of an integrated forming structure, the outer side surface of the matching part is attached to the second tripod, the left side end and the right side end of the spring are elastically abutted to the inner surface of the central outer rod, and the inner rod is installed in the center of the spring in a rotating mode.

Preferably, the central outer rod is of a hollow cylindrical structure, and the central knob is of a flat cylindrical structure.

Preferably, the first tripod and the second tripod are the same in structure and size.

Preferably, a power supply battery is installed inside the lamp body cylinder.

Preferably, the number of the side knobs is two.

Preferably, the double hook is of a U-like structure.

Preferably, the distance between the zoom lens and the right end of the zoom ring is two centimeters.

Preferably, the center of the zoom lens and the searchlight are positioned on the same central line.

Preferably, the main knob is made of plastic, and has light weight and high hardness.

Preferably, the spring is made of spring steel, and the elastic potential energy is large.

The utility model has the advantages of as follows: the utility model discloses an improve and provide an unmanned aerial vehicle searchlight structure that zooms here, compare with the equipment of the same type, have following improvement:

the advantages are that: an unmanned aerial vehicle searchlight structure that zooms has set up complementary unit through optimizing, slide into the installation with the hook piece on corresponding supporting trench, the first tripod of hook piece bottom, second tripod and internals, the fitting piece carries out normal running fit, the motion of zooming in the certain limit can be carried out to the spring in the outer pole of center, even the hook piece cooperation internals on searchlight place mounted position, the swing range of less range appears in the fitting piece, increase the reply scope of searchlight limit, when the installation nimble installation, the spring has certain slow-pressing effect.

Drawings

FIG. 1 is a schematic structural view of the present invention;

fig. 2 is a top view of the present invention;

FIG. 3 is a schematic structural view of the auxiliary mechanism of the present invention;

fig. 4 is a partial enlarged view of fig. 3B according to the present invention;

fig. 5 is a partial enlarged view of a portion a of fig. 1 according to the present invention;

fig. 6 is a schematic view of the spring structure of the present invention.

Wherein: the lamp body comprises a lamp body barrel-1, a central knob-2, an auxiliary mechanism-3, a main knob-4, a round sleeve-5, a zoom lens-6, a searchlight core-7, a zoom ring-8, an integrated shell-9, a bracket-10, a threaded sleeve-11, a double hook-31, a central outer rod-32, a first tripod-33, a side rotating knob-34, an inner part-35, a fixed part-36, a matching part-37, a second tripod-38, a spring-39 and an inner rod-310.

Detailed Description

The present invention will be described in detail with reference to the accompanying fig. 1-6, and the technical solutions in the embodiments of the present invention will be clearly and completely described, 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.

The utility model provides an unmanned aerial vehicle zooms searchlight structure here through the improvement, including a lamp body section of thick bamboo 1, center knob 2, complementary unit 3, main knob 4, the round cover 5, zoom lens 6, searchlight wick 7, zoom ring 8, integrative shell 9, bracket 10 and thread bush 11, lamp body section of thick bamboo 1 right side screw thread mounting has thread bush 11, center knob 2 and bracket 10 clearance fit, main knob 4 surface embedding is installed on round cover 5, zoom lens 6 is installed on zoom ring 8, searchlight wick 7 fixed mounting is inboard in zoom ring 8, integrative shell 9 and thread bush 11 fixed connection, complementary unit 3 is located lamp body section of thick bamboo 1 side, complementary unit 3 includes double hook piece 31, central outer pole 32, first tripod 33, side knob 34, internals 35, the piece 36, the fitting piece 37, second tripod 38, spring 39 and interior pole 310, double hook piece 31 bottom welded fastening has first tripod 33, the tripod 33, In the second tripod 38, a side rotating button 34 is embedded in the side end of the central outer rod 32, the outer side surface of the inner member 35 is attached to the inner side surface of the first tripod 33, the inner member 35 is fixedly mounted on the lamp barrel 1, the fixed member 36 and the fitting member 37 are of an integrated molding structure, the outer side surface of the fitting member 37 is attached to the second tripod 38, the left and right side ends of the spring 39 are elastically abutted to the inner surface of the central outer rod 32, and the inner rod 310 is rotatably mounted in the center of the spring 39.

Further, the central outer rod 32 is a hollow cylinder structure, and the central knob 2 is a flat cylinder structure.

Further, the first tripod 33 and the second tripod 38 are identical in structure and size.

Further, a power supply battery is installed inside the lamp body tube 1.

Furthermore, two side rotating buttons 34 are provided, so as to facilitate the rotation fit.

Further, the double hook 31 has a U-like structure.

Further, the distance between the zoom lens 6 and the right end of the zoom ring 8 is two centimeters.

Furthermore, the center of the zoom lens 6 and the searchlight 7 are positioned on the same central line.

Furthermore, the main knob 4 is made of plastic, and has light weight and high hardness.

Further, the spring 39 is made of spring steel, and has large elastic potential energy.

According to the above table, the spring 39 is made of spring steel, and has a large elastic potential.

The utility model provides an unmanned aerial vehicle zooming searchlight structure through improvement, and the working principle is as follows;

firstly, before the searchlight is installed and used, the integrity of the searchlight is checked, and when the searchlight is intact and not damaged, the searchlight can be used;

secondly, when in use, the integral shell 9 can rotate around the central knob 2, and the tablet mark of the zoom ring 8 can be horizontally adjusted through the matching of the main knob 4 and the round sleeve 5.

Thirdly, when the searchlight is integrally installed, the double-hook member 31 slides into the corresponding matching groove, the first tripod 33 and the second tripod 38 at the bottom end of the double-hook member 31 are in running fit with the internal member 35 and the matching member 37, and the spring 39 in the central outer rod 32 can perform zooming movement within a certain range, so that even if the double-hook member 31 at the installation position of the searchlight is matched with the internal member 35 and the matching member 37 to generate a smaller-amplitude swinging range, the restoring range of the edge end of the searchlight is enlarged.

The utility model discloses an improvement provides an unmanned aerial vehicle zooms searchlight structure, auxiliary mechanism 3 has been set up through optimizing, slide into double hook piece 31 and install on advancing corresponding supporting trench, the first tripod 33 of double hook piece 31 bottom, second tripod 38 and internals 35, cooperation piece 37 carries out normal running fit, spring 39 in the outer pole 32 in the center can carry out the zoom motion in the certain limit, even double hook piece 31 on the searchlight place mounted position cooperates internals 35, the swing range of less range appears in cooperation piece 37, increase the reply scope of searchlight limit, install in a flexible way when the installation, spring 39 has certain slow compression effect.

The basic principle and the main characteristics of the utility model and the advantages of the utility model have been shown and described above, and the utility model discloses the standard part that uses all can purchase from the market, and dysmorphism piece all can be customized according to the record of the description with the drawing, and the concrete connection mode of each part all adopts conventional means such as ripe bolt rivet among the prior art, welding, and machinery, part and equipment all adopt prior art, conventional model, and conventional connection mode in the prior art is adopted in addition to circuit connection, and the details are not repeated here.

The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.

Claims

1. An unmanned aerial vehicle zoom searchlight structure comprises a lamp body cylinder (1), a center knob (2), a main knob (4), a round sleeve (5), a zoom lens (6), a searchlight wick (7), a zoom ring (8), an integrated shell (9), a bracket (10) and a threaded sleeve (11), wherein the threaded sleeve (11) is installed on the right side of the lamp body cylinder (1) in a threaded mode, the center knob (2) is in clearance fit with the bracket (10), the outer surface of the main knob (4) is embedded and installed on the round sleeve (5), the zoom lens (6) is installed on the zoom ring (8), the searchlight wick (7) is fixedly installed on the inner side of the zoom ring (8), and the integrated shell (9) is fixedly connected with the threaded sleeve (11);

the method is characterized in that: the lamp body tube is characterized by further comprising an auxiliary mechanism (3), wherein the auxiliary mechanism (3) is located on the side face of the lamp body tube (1), the auxiliary mechanism (3) comprises a double-hook piece (31), a central outer rod (32), a first triangular frame (33), a side rotating button (34), an inner piece (35), a fixed piece (36), a matching piece (37), a second triangular frame (38), a spring (39) and an inner rod (310), the bottom end of the double-hook piece (31) is fixedly welded with the first triangular frame (33) and the second triangular frame (38), the side rotating button (34) is embedded in the central outer rod (32), the outer side face of the inner piece (35) is attached to the inner side face of the first triangular frame (33), the inner piece (35) is fixedly installed on the lamp body tube (1), the fixed piece (36) and the matching piece (37) are of an integrated molding structure, the outer side face of the matching piece (37), the left side end and the right side end of the spring (39) are elastically abutted to the inner surface of the central outer rod (32), and the inner rod (310) is rotatably installed in the center of the spring (39).

2. The zoom searchlight structure of unmanned aerial vehicle of claim 1, wherein: the central outer rod (32) is of a hollow cylindrical structure, and the central knob (2) is of a flat cylindrical structure.

3. The zoom searchlight structure of unmanned aerial vehicle of claim 1, wherein: the first tripod (33) and the second tripod (38) are the same in structure and size.

4. The zoom searchlight structure of unmanned aerial vehicle of claim 1, wherein: the lamp body barrel (1) is internally provided with a power supply battery.

5. The zoom searchlight structure of unmanned aerial vehicle of claim 1, wherein: the number of the side rotating buttons (34) is two.

6. The zoom searchlight structure of unmanned aerial vehicle of claim 1, wherein: the double hook piece (31) is of a U-like structure.

7. The zoom searchlight structure of unmanned aerial vehicle of claim 1, wherein: the distance between the zoom lens (6) and the right end of the zoom ring (8) is two centimeters.

8. The zoom searchlight structure of unmanned aerial vehicle of claim 1, wherein: the center of the zoom lens (6) and the searchlight (7) are positioned on the same central line.