CN219545078U

CN219545078U - Camera holder for aircraft

Info

Publication number: CN219545078U
Application number: CN202321234735.1U
Authority: CN
Inventors: 颜小童; 张波; 金历群; 徐鸣
Original assignee: Galaxy Aerospace Technology Nantong Co ltd
Current assignee: Galaxy Aerospace Technology Nantong Co ltd
Priority date: 2023-05-22
Filing date: 2023-05-22
Publication date: 2023-08-18
Anticipated expiration: 2033-05-22

Abstract

The utility model relates to the technical field of camera holders, in particular to a camera holder for an aircraft, which comprises a mounting plate main body, wherein a rotating structure is fixedly arranged at the bottom end of the mounting plate main body, one end of the rotating structure is connected with a movable frame, a mounting frame is fixedly arranged on a base surface of the movable frame, a second motor is arranged on a base surface of the mounting frame, the output end of the second motor is connected with a transmission shaft through a coupling, a rotating block is fixedly connected with the outer side of the transmission shaft, a camera is arranged on the inner side of the mounting frame, an electric signal receiving emitter is arranged on the back surface of the movable frame, a storage battery is arranged at one side, close to the rotating structure, of the bottom end of the mounting plate main body, and a positioning hole is formed in the top end of the mounting plate main body.

Description

Camera holder for aircraft

Technical Field

The utility model relates to the technical field of camera holders, in particular to a camera holder for an aircraft.

Background

The camera holder is a mounting platform of the camera and can move horizontally and vertically, but note that the holder is different from a holder in a photographic apparatus, the holder of the photographic apparatus is generally only a tripod, the direction of the camera holder can be adjusted only by hands, and the holder of the monitoring system can be controlled remotely by a control system to rotate and move.

Through retrieving, just mention the cloud platform camera at published application number CN202222158083.X, including camera mechanism, camera mechanism's rear side is provided with adjustment mechanism, camera mechanism includes camera and solar charging panel, solar charging panel's downside is provided with the linking bridge, one side of linking bridge is provided with the installing support, the camera includes the camera body, the upside of camera body is provided with the shell body. According to the utility model, the limiting stop rod and the spring can move, the limiting stop ring and the spring enable the spring to be compressed by the second limiting block, the limiting slide block slides to enable the limiting slide block to move up and down on the front side of the mounting plate, when the limiting stop rod reaches a designated height, the handle is released to enable the spring to push the limiting stop ring to move, and the limiting stop ring moves to enable the limiting stop rod to be clamped and embedded on the mounting plate, so that a worker can fix the position of the camera shooting mechanism, and the height adjustment of the camera shooting mechanism by the worker is greatly facilitated.

The above solution, although solving the problems set forth in the background art, still has the following drawbacks: when the position of the image pickup mechanism is adjusted, the camera is not flexible enough, and multi-angle shooting is difficult to carry out.

Disclosure of Invention

The present utility model is directed to a camera pan-tilt for an aircraft, which solves the above-mentioned problems.

In order to achieve the above purpose, the present utility model provides the following technical solutions:

the camera cradle head for the aircraft comprises a mounting plate main body, a rotating structure is fixedly arranged at the bottom end of the mounting plate main body, a movable frame is connected with one end of the rotating structure, a mounting frame is fixedly arranged on a base surface of the movable frame, a second motor is arranged on the base surface of the mounting frame, the output end of the second motor is connected with a transmission shaft through a coupling, a rotating block is fixedly connected to the outer side of the transmission shaft, one end of the rotating block is connected with an electric telescopic rod, one end of the electric telescopic rod is connected with a fixing frame, a camera is arranged on the inner side of the fixing frame, an electric signal receiving emitter is arranged on the back surface of the movable frame, a storage battery is arranged on one side, close to the rotating structure, of the bottom end of the mounting plate main body, and a positioning hole is formed in the top end of the mounting plate main body;

the rotary structure comprises a limiting frame fixedly installed at the bottom end of the mounting plate main body, a rotating shaft is arranged at the bottom end of the inner wall of the limiting frame through a rotating bearing, and the output end of the rotating shaft is connected with a first motor through a coupling.

As a preferable scheme of the utility model, a control panel is arranged at one side of the bottom end of the mounting plate main body, which is close to the storage battery, and the control panel is electrically connected with the first motor, the second motor, the electric telescopic rod, the camera, the electric signal receiving and emitting device and the storage battery.

As a preferable scheme of the utility model, the limiting frame is provided with a connecting block for connecting the first motor.

As a preferable scheme of the utility model, the mounting frame is made of metal.

As a preferable scheme of the utility model, one end of the transmission shaft is connected with one end of the inner wall of the mounting frame through a bearing.

As a preferable scheme of the utility model, the number of the positioning holes is four.

Compared with the prior art, the utility model has the beneficial effects that:

according to the utility model, the rotating structure, the mounting frame, the second motor, the transmission shaft, the rotating block, the electric telescopic rod, the camera and the electric signal receiving and transmitting device are arranged in the camera cradle head for the aircraft, so that shooting can be carried out at multiple angles under the cooperation of the rotating structure, the mounting frame, the second motor, the transmission shaft, the rotating block, the electric telescopic rod, the camera and the electric signal receiving and transmitting device, and the camera cradle head has a rotation function.

Drawings

Some specific embodiments of the utility model will be described in detail hereinafter by way of example and not by way of limitation with reference to the accompanying drawings. The same reference numbers will be used throughout the drawings to refer to the same or like parts or portions. It will be appreciated by those skilled in the art that the drawings are not necessarily drawn to scale. In the accompanying drawings:

FIG. 1 is a schematic diagram of the overall structure of the present utility model;

FIG. 2 is a schematic diagram of a rotating structure according to the present utility model;

fig. 3 is a schematic view of the structure of the mounting frame, the second motor and the transmission shaft of the present utility model.

In the figure: 1. a mounting plate body; 2. a rotating structure; 201. a limiting frame; 202. a rotating shaft; 203. a first motor; 204. a sliding block; 3. a movable frame; 4. a mounting frame; 5. a second motor; 6. a transmission shaft; 7. a rotating block; 8. an electric telescopic rod; 9. a fixing frame; 10. a camera; 11. an electric signal receiving transmitter; 12. a storage battery; 13. positioning holes; 14. and a control panel.

Detailed Description

It should be noted that, without conflict, the embodiments of the present utility model and features of the embodiments may be combined with each other. The utility model will be described in detail below with reference to the drawings in connection with embodiments.

In order that those skilled in the art will better understand the present utility model, a technical solution in the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in which it is apparent that the described embodiments are only some embodiments of the present utility model, not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the present utility model without making any inventive effort, shall fall within the scope of the present utility model.

It should be noted that the terms "first," "second," and the like in the description and the claims of the present utility model and the above figures are used for distinguishing between similar objects and not necessarily for describing a particular sequential or chronological order. It is to be understood that the terms so used are interchangeable under appropriate circumstances such that the embodiments of the utility model described herein are, for example, capable of operation in other environments. Furthermore, the terms "comprises," "comprising," and "having," and any variations thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or apparatus that comprises a list of steps or elements is not necessarily limited to those steps or elements expressly listed but may include other steps or elements not expressly listed or inherent to such process, method, article, or apparatus.

It is noted that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of exemplary embodiments according to the present utility model. As used herein, the singular is also intended to include the plural unless the context clearly indicates otherwise, and furthermore, it is to be understood that the terms "comprises" and/or "comprising" when used in this specification are taken to specify the presence of stated features, steps, operations, devices, components, and/or combinations thereof.

The technical solutions of the embodiments of the present utility model will be clearly and completely described below in conjunction with the embodiments of the present utility model, and it is apparent that the described embodiments are only some embodiments of the present utility model, but not all embodiments, and all other embodiments obtained by those skilled in the art without making any inventive effort based on the embodiments of the present utility model are within the scope of protection of the present utility model.

In order that the utility model may be readily understood, a more complete description of the utility model will be rendered by reference to the appended drawings. Several embodiments of the utility model are presented. This utility model may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.

It will be understood that when an element is referred to as being "mounted" on another element, it can be directly on the other element or intervening elements may also be present. When an element 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 terms "vertical," "horizontal," "left," "right," and the like are used herein 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 utility model belongs. The terminology used herein in the description of the utility model is for the purpose of describing particular embodiments only and is not intended to be limiting of the utility model. The term "and/or" as used herein includes any and all combinations of one or more of the associated listed items.

Referring to fig. 1-3, the present utility model provides a technical solution:

the camera cradle head for the aircraft comprises a mounting plate main body 1, wherein a rotating structure 2 is fixedly arranged at the bottom end of the mounting plate main body 1, one end of the rotating structure 2 is connected with a movable frame 3, a mounting frame 4 is fixedly arranged on a base surface of the movable frame 3, a second motor 5 is arranged on a base surface of the mounting frame 4, the output end of the second motor 5 is connected with a transmission shaft 6 through a coupling, a rotating block 7 is fixedly connected to the outer side of the transmission shaft 6, one end of the rotating block 7 is connected with an electric telescopic rod 8, one end of the electric telescopic rod 8 is connected with a fixing frame 9, a camera 10 is arranged on the inner side of the fixing frame 9, an electric signal receiving and emitting device 11 is arranged on the back surface of the movable frame 3, and a storage battery 12 is arranged on one side, close to the rotating structure 2, of the bottom end of the mounting plate main body 1;

the rotating structure 2 comprises a limiting frame 201 fixedly arranged at the bottom end of the mounting plate main body 1, the bottom end of the inner wall of the limiting frame 201 is connected with a rotating shaft 202 through a rotating bearing, the output end of the rotating shaft 202 is connected with a first motor 203 through a coupler, the bottom end of the first motor 203 is provided with a sliding block 204, the sliding block 204 is coupled with a sliding groove on the inner wall of the limiting frame 201 and can move along the sliding groove, so that a ground operator can remotely send out an operation signal through an electric signal receiving transmitter 11, the first motor 203 is driven to drive the rotating shaft 202 to rotate under the action of the coupler, the rotating bearing drives the camera 10 to horizontally rotate, the height of the camera 10 is further adjusted through an electric telescopic rod 8, the pitch angle of the camera 10 can be adjusted under the cooperation of the mounting frame 4, a second motor 5, a transmission shaft 6 and the rotating block 7, the camera 10 can be shot at multiple angles, and the rotating structure has a rotating function;

wherein control panel 14 is installed to one side that the bottom of mounting panel main part 1 is close to battery 12, and control panel 14 and first motor 203, second motor 5, electric telescopic handle 8, camera 10, electric signal receiving and transmitting device 11, electric connection between the battery 12, slider 204 is installed to the bottom of first motor 203, mounting bracket 4 is made for the metal, the one end of transmission shaft 6 passes through the bearing and connects in the inner wall one end of mounting bracket 4, thereby can remote signal transmission through electric signal receiving and transmitting device 11, the operating signal that ground operating personnel can send remotely, drive first motor 203, drive pivot 202 rotation under the effect of shaft coupling, drive the horizontal rotation of camera 10 through swivel bearing, and further adjust the height of camera 10 through electric telescopic handle 8, drive second motor 5, drive transmission shaft 6 under the effect of shaft coupling, rotatory piece 7 and camera 10 rotate, adjust the pitch angle of camera 10, be convenient for take photograph in the multiple angles, moreover have the gyration function, play fixed action to second motor 5 through mounting bracket 4.

In this embodiment, referring to fig. 1, a positioning hole 13 is formed at the top end of the mounting plate main body 1, so as to adapt to different mounting sizes through the positioning hole 13;

the number of the positioning holes 13 is four, so that the positioning holes 13 adapt to different installation sizes under the action of the positioning holes, and the practicability is enhanced.

The working flow of the utility model is as follows: during the use, inspection equipment outward appearance is damaged, after the inspection, adapt to different installation dimensions under the effect of locating hole 13, power by battery 12, can long-range signal transmission through signal reception transmitter 11, ground operating personnel can long-range operating signal who sends, drive first motor 203, drive pivot 202 rotation under the effect of shaft coupling, drive the horizontal rotation of camera 10 through the swivel bearing, and further adjust the height of camera 10 through electric telescopic handle 8, drive second motor 5, drive transmission shaft 6 under the effect of shaft coupling, rotatory 7 and the camera 10 rotation of rotatory, adjust the pitch angle of camera 10, be convenient for the multi-angle take photograph, moreover have the gyration function, play the fixed action to second motor 5 through mounting bracket 4, have spreading value.

The relative arrangement of the components and steps, numerical expressions and numerical values set forth in these embodiments do not limit the scope of the present utility model unless it is specifically stated otherwise. Meanwhile, it should be understood that the sizes of the respective parts shown in the drawings are not drawn in actual scale for convenience of description. Techniques, methods, and apparatus known to one of ordinary skill in the relevant art may not be discussed in detail, but should be considered part of the specification where appropriate. In all examples shown and discussed herein, any specific values should be construed as merely illustrative, and not a limitation. Thus, other examples of the exemplary embodiments may have different values. It should be noted that: like reference numerals and letters denote like items in the following figures, and thus once an item is defined in one figure, no further discussion thereof is necessary in subsequent figures.

Spatially relative terms, such as "above … …," "above … …," "upper surface at … …," "above," and the like, may be used herein for ease of description to describe one device or feature's spatial location relative to another device or feature as illustrated in the figures. It will be understood that the spatially relative terms are intended to encompass different orientations in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, elements described as "above" or "over" other devices or structures would then be oriented "below" or "beneath" the other devices or structures. Thus, the exemplary term "above … …" may include both orientations of "above … …" and "below … …". The device may also be positioned in other different ways (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly.

In the description of the present utility model, it should be understood that the azimuth or positional relationships indicated by the azimuth terms such as "front, rear, upper, lower, left, right", "lateral, vertical, horizontal", and "top, bottom", etc., are generally based on the azimuth or positional relationships shown in the drawings, merely to facilitate description of the present utility model and simplify the description, and these azimuth terms do not indicate and imply that the apparatus or elements referred to must have a specific azimuth or be constructed and operated in a specific azimuth, and thus should not be construed as limiting the scope of protection of the present utility model; the orientation word "inner and outer" refers to inner and outer relative to the contour of the respective component itself.

The present utility model is not limited to the above-mentioned embodiments, and any changes or substitutions that can be easily understood by those skilled in the art within the technical scope of the present utility model are intended to be included in the scope of the present utility model. Therefore, the protection scope of the present utility model should be subject to the protection scope of the claims.

Claims

1. A camera cloud platform for aircraft, including mounting panel main part (1), its characterized in that: the novel electric power generation device comprises a mounting plate main body (1), wherein a rotating structure (2) is fixedly arranged at the bottom end of the mounting plate main body (1), a movable frame (3) is connected to one end of the rotating structure (2), a mounting frame (4) is fixedly arranged on a base surface of the movable frame (3), a second motor (5) is arranged on a base surface of the mounting frame (4), a transmission shaft (6) is connected to the output end of the second motor (5) through a coupling, a rotating block (7) is fixedly connected to the outer side of the transmission shaft (6), an electric telescopic rod (8) is connected to one end of the rotating block (7), a fixing frame (9) is connected to one end of the electric telescopic rod (8), a video camera (10) is arranged on the inner side of the fixing frame (9), an electric signal receiving and emitting device (11) is arranged on the back surface of the movable frame (3), a storage battery (12) is arranged on one side, close to the rotating structure (2), and a positioning hole (13) is formed in the top end of the mounting plate main body (1).

The rotary structure (2) comprises a limiting frame (201) fixedly installed at the bottom end of the mounting plate main body (1), a rotating shaft (202) is arranged at the bottom end of the inner wall of the limiting frame (201) through a rotary bearing, and a first motor (203) is connected to the output end of the rotating shaft (202) through a coupling.

2. The camera head for an aircraft of claim 1, wherein: a control panel (14) is arranged at one side, close to the storage battery (12), of the bottom end of the mounting plate main body (1), and the control panel (14) is electrically connected with the first motor (203), the second motor (5), the electric telescopic rod (8), the camera (10), the electric signal receiving and emitting device (11) and the storage battery (12).

3. The camera head for an aircraft of claim 1, wherein: the limiting frame (201) is provided with a connecting block (204) for connecting the first motor (203).

4. The camera head for an aircraft of claim 1, wherein: the mounting frame (4) is made of metal.

5. The camera head for an aircraft of claim 1, wherein: one end of the transmission shaft (6) is connected with one end of the inner wall of the mounting frame (4) through a bearing.

6. The camera head for an aircraft of claim 1, wherein: the number of the positioning holes (13) is four.