Machine body structure of inspection robot

Abstract

The utility model provides an inspection robot body structure which comprises a body, a guide face corresponding to an illuminating lamp of an inspection channel is arranged on the junction between the advancing side of the body and one of the left side and the right side of the body, a guide plate is arranged at the upper end of the body, and the body is cylindrical. The edge of the front side of the guide plate is a guide edge corresponding to the guide face, and a folded edge is arranged on the edge of the guide plate. The ceiling lamp guiding device is reasonable in design, ceiling lamps on a henhouse corridor can be stably moved away through the guiding face, the situation that the ceiling lamps are damaged due to direct contact between the machine body and the ceiling lamps and chicken flock stress reactions caused by violent activities or sudden damage of the ceiling lamps are avoided, meanwhile, the guiding range of the ceiling lamps is enlarged through the effect of the guiding plate, and the service life of the ceiling lamps is prolonged. Specialized and automatic poultry breeding is facilitated.

Description

Technical Field

[0001] The utility model relates to a body structure of an inspection robot. Background Art

[0002] At present, in the process of poultry farming, lighting is an indispensable part, which can directly affect the growth, maturity and egg production of poultry (such as chickens). Therefore, it is necessary to arrange a corresponding lighting control system to control the lighting in the chicken house. The executive components of the lighting control system of a conventional chicken house are realized by using a number of chandeliers installed on the passages beside the chicken house. On the other hand, the existing inspection robots are widely used in inspection, security, alarm and other tasks in various complex environments such as logistics centers, factories, airports, and substations. In the process of existing large-scale automated poultry farming, most of them also adopt When using inspection robots to inspect poultry houses, the moving channel of the inspection robots is generally set next to the poultry houses, so the inspection robots sometimes interfere with the chandeliers. For example, the "A kind of automatic inspection robot for abnormal chicken behavior in chicken houses" disclosed with application number: CN202121286871.6 adopts a column-type body. Therefore, during the movement of the inspection robot, the inspection robot body is prone to hit the chandelier, causing damage to the chandelier and stress response of the chickens caused by the violent activity or sudden damage of the chandelier, affecting the growth of the chickens. Summary of the Invention

[0003] In view of this, the purpose of the present invention is to overcome the deficiencies in the above-mentioned prior art and to provide a patrol robot body structure, which can smoothly move away from the chandelier on the corridor of the chicken house through the guide surface, avoiding direct contact between the body and the chandelier, resulting in damage to the chandelier and stress response of the chickens caused by violent movement or sudden damage of the chandelier. At the same time, the guide plate is used to expand the guidance range of the chandelier, thereby facilitating professional and automated poultry farming.

[0004] The utility model is implemented by the following scheme: a patrol robot fuselage structure: including a fuselage main body, a guide surface is provided on the intersection between the forward side of the fuselage main body and the left and right sides of the fuselage main body corresponding to the lighting lamp of the patrol channel, and a guide plate is provided on the upper end of the fuselage main body.

[0005] Furthermore, the fuselage body is a columnar body, the front edge of the guide plate is provided with a guide edge corresponding to the guide surface, and a folded edge is provided on the edge of the guide plate.

[0006] Furthermore, the fuselage body is a telescopic shell, and the fuselage body is composed of at least two telescopic kits that are sequentially connected from the inside to the outside. A push rod mechanism for driving the fuselage body to be telescopic is vertically installed in the fuselage body, and the telescopic end of the push rod mechanism is fixed on the innermost telescopic kit.

[0007] Furthermore, the telescopic kit is a hollow column, and a chamfered surface is provided at the junction between the forward side of the telescopic kit and the left and right sides thereof, and the chamfered surfaces of each telescopic kit constitute a guide surface.

[0008] Furthermore, a monitoring device is installed in the fuselage body, which is retractable and retractable as the fuselage body is retracted and retracted. A clearance groove is provided on the middle part of one side of the left and right sides of the telescopic kit that is not connected to the chamfered surface, corresponding to the monitoring device. The upper and lower ends of the clearance groove pass through the side panel of the telescopic kit.

[0009] Furthermore, an inspection base is provided under the main body of the machine, the outermost telescopic kit is fixed on the inspection base, and the push rod mechanism and the monitoring device are both installed on the inspection base.

[0010] Furthermore, the upper end of the innermost telescopic kit is closed by a cover plate, and the monitoring device includes a plurality of monitoring components from top to bottom, and two adjacent monitoring components are movably connected. The upper end of the monitoring device is fixed under the cover plate, the telescopic end of the push rod mechanism is fixed under the cover plate, and the guide plate is fixed on the cover plate; a folded edge is provided on the front edge of the guide plate and the edge of the guide plate away from the clearance groove.

[0011] Furthermore, the monitoring assembly includes a vertically arranged fixing plate, a monitor is fixed on the plate body on the side of the fixing plate facing the clearance slot, and two adjacent fixing plates are connected by an accordion-type protective cover.

[0012] Furthermore, an auxiliary guide rail assembly for assisting the extension and retraction of the monitoring device is symmetrically arranged on the left and right sides of the fuselage body. The auxiliary guide rail assembly is composed of a number of auxiliary guide rails corresponding to the monitoring assemblies and arranged in parallel. The plane formed by each auxiliary guide rail is parallel to the plane of the fixed plate body. Adjacent auxiliary guide rails are vertically slidably connected. The auxiliary guide rail on one edge of the same auxiliary guide rail assembly is fixed on the inspection base, and the auxiliary guide rail on the other edge is fixed under the cover plate. A vertical auxiliary slide groove is provided on the front side of each auxiliary guide rail, and a slider that cooperates with the corresponding auxiliary slide groove is installed on each fixed plate.

[0013] Furthermore, vertical lifting guide rails are installed on the inner walls of the telescopic kits except the innermost telescopic kit, guide wheel assemblies are provided on the outer walls of the telescopic kits except the outermost telescopic kit corresponding to the lifting guide rails on the inner walls of the telescopic kits of the outer layer, and limiting plates are provided on the upper ends of the telescopic kits except the innermost telescopic kit corresponding to the guide wheel assemblies on the telescopic kits of the inner layer.

[0014] Compared with the existing technology, the utility model has the following beneficial effects: reasonable design, the chandelier on the corridor of the chicken house can be smoothly moved away through the guide surface, avoiding direct contact between the main body of the machine and the chandelier, which may cause damage to the chandelier and stress reaction of the chickens due to violent movement or sudden damage of the chandelier. At the same time, the guide plate is used to expand the guidance range of the chandelier, which facilitates professional and automated poultry farming. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 The structure of the embodiment of the utility model is shown in FIG. Figure 1 (Remove the guide plate);

[0016] Figure 2 The structure of the embodiment of the utility model is shown in FIG. Figure 2 (Remove the guide plate);

[0017] Figure 3 This is a schematic diagram of the top view of the structure of an embodiment of the utility model (the guide plate moves in translation);

[0018] Figure 4 This is a schematic diagram of the main structure of an embodiment of the utility model;

[0019] Figure 5 for Figure 4 Schematic diagram of the partially enlarged structure;

[0020] Figure 6 This is a schematic side sectional structural diagram of an embodiment of the present utility model;

[0021] Figure 7 for Figure 6 The enlarged structural diagram at B in the middle;

[0022] Figure 8 This is a schematic structural diagram of an embodiment of the utility model after the telescopic kit is removed;

[0023] Figure 9 for Figure 8 Enlarged structural diagram at point A in the middle.

[0024] In the figure: 1- fuselage body; 2- guide surface; 3- guide plate; 4- chandelier; 5- guide edge; 6- folding edge; 7- telescopic kit; 8- push rod mechanism; 9- chamfered surface; 10- clearance slot; 11- inspection base; 12- cover plate; 13- monitoring assembly; 14- fixed plate; 15- monitor; 16- accordion protective cover; 17- auxiliary guide rail assembly; 18- auxiliary guide rail; 19- guide rail slide; 20- guide rail slider; 21- monitoring device; 22- auxiliary slide; 23- slider; 24- lifting guide rail; 25- guide wheel assembly; 26- limit plate; 27- chandelier wire. DETAILED DESCRIPTION

[0025] The present invention will be further described below with reference to the accompanying drawings and embodiments.

[0026] It should be noted that the following detailed descriptions are exemplary and are intended to provide further explanation of the present application. Unless otherwise specified, all technical and scientific terms used herein have the same meaning as commonly understood by those skilled in the art to which the present application belongs.

[0027] It should be noted that the terms used herein are only for describing specific embodiments and are not intended to limit the exemplary embodiments according to the present application. As used herein, unless the context clearly indicates otherwise, the singular form is also intended to include the plural form. In addition, it should be understood that when the terms "comprise" and / or "include" are used in this specification, they indicate the presence of features, steps, operations, devices, components and / or combinations thereof.

[0028] like Figure 1-9 As shown, a patrol robot body structure comprises a body body 1, a guide surface 2 is provided on the boundary between the forward side of the body body and the left and right sides thereof, corresponding to the lighting lamp of the patrol channel, that is, a guide surface is provided on the boundary between the forward side of the body body and the side of the body body away from the chicken house, a guide plate 3 is provided on the upper end of the body body, when the body body walks on the chicken house corridor, the chandelier 4 on the chicken house corridor can be smoothly moved away through the guide surface, avoiding direct contact between the body body and the chandelier, resulting in damage to the chandelier and stress reaction of the chickens due to violent activity or sudden damage of the chandelier, the function of the guide plate is to expand the guiding range of the chandelier, that is, the range of the guide surface is limited. In order to expand the guiding range, the guide plate on the upper end of the body body expands the range of contact with the chandelier or the chandelier wire 27.

[0029] In this embodiment, in order to design reasonably and realize the guide plate to expand the guiding range of the chandelier, the fuselage body is a columnar body, and the front edge of the guide plate is provided with a guide edge 5 corresponding to the guide surface, that is, compared with the guide surface on the fuselage body connecting the front and side sides of the fuselage body, the front edge of the guide plate is directly the guide edge that cooperates with the guide surface, so that a part of the guide surface exceeds the forward side of the fuselage body, thereby expanding the guiding range of the chandelier. Specifically, in this embodiment, the guide plate is a right-angled trapezoid, and the edge of the non-right-angled side is the guide edge. A folded edge 6 is provided on the edge of the guide plate, which can be upward or downward. The purpose of setting the folded edge is that when the fuselage body moves forward, the chandelier will move along the guide surface. At this time, the chandelier will have an inclination angle, and the chandelier wire will abut against the guide edge of the guide plate and move along the guide plate. Once the number of times is too many, it is easy to cause the wire to wear, and then damage the chandelier, causing a stress response in the chicken flock, so by setting the folded edge, The possibility of cutting the chandelier wires is reduced and the service life of the chandelier is increased. At the same time, the main body structure of the fuselage matched with the guide plate is as follows: the fuselage main body is a telescopic shell, and the fuselage main body is composed of at least two telescopic kits 7 that are sequentially sleeved from the inside to the outside. This embodiment uses 3 telescopic kits, and other numbers are also possible, mainly to adapt to the height of the chicken house. A push rod mechanism 8 for driving the fuselage main body to be telescopic is vertically installed in the fuselage main body. The telescopic end of the push rod mechanism is fixed on the innermost telescopic kit. The push rod mechanism can be an existing multi-stage electric push rod, and of course other existing telescopic rod mechanisms can be used, as long as it can drive the fuselage main body to be telescopic and lifted. More specifically: the telescopic kit is a hollow column, and the junction between the forward side of the telescopic kit and its left and right sides is provided with a chamfered surface 9. The chamfered surfaces of each telescopic kit constitute a guide surface, that is, the cross section of the telescopic kit is a rectangle with a missing corner, and the guide edge of the guide plate coincides with the missing corner.

[0030] In this embodiment, in order to enable the fuselage body to monitor the situation of the chicken house, a monitoring device 21 that can be extended and retracted as the fuselage body is extended and retracted is installed in the fuselage body. A clearance groove 10 is provided on the middle part of one side that is not connected to the chamfered surface on the left and right sides of the telescopic kit, corresponding to the monitoring device. The upper and lower ends of the clearance groove pass through the side panels of the telescopic kit, that is, the telescopic kit is provided with a clearance groove on the side facing the chicken house. Each clearance groove forms a channel for the monitoring device to extend, which is convenient for chicken house monitoring. At the same time, each clearance groove can form a channel for the monitoring device to extend after extension as each telescopic kit rises and falls, which is convenient for the monitoring device to adapt to chicken houses of different heights.

[0031] In this embodiment, in order to realize the movement of the fuselage body, an inspection base 11 is provided under the fuselage body. The inspection base can be an existing movable base. Since it is not the invention point of the present device, it will not be described in detail. The outermost telescopic kit is fixed on the inspection base, so that the internal telescopic kit can be raised and lowered in sequence under the action of the push rod mechanism. The push rod mechanism and the monitoring device are both installed on the inspection base. More specifically: the upper end of the innermost telescopic kit is closed by a cover plate 12, and the monitoring device includes a plurality of monitoring components 13 from top to bottom, and the two adjacent monitoring components are movably connected, which can be: the monitoring component includes a vertically arranged fixed plate 14, and the fixed plate is fixed with a monitor on the side of the plate facing the clearance slot. 15. The two adjacent fixed plates are connected by an existing accordion-type protective cover 16, and the connection method can be a threaded connection. The device realizes the extension and retraction of the monitoring device through the accordion-type protective cover. Of course, other existing methods can also be used for connection, as long as the extension and retraction of the monitoring device can be realized. At the same time, the monitoring components located at the upper and lower ends can be respectively connected to the cover plate and the inspection base through the accordion-type protective cover, or can be directly screwed to the cover plate and the inspection base. The upper end of the monitoring device is fixed under the cover plate, the telescopic end of the push rod mechanism is fixed under the cover plate, and the guide plate is fixed on the cover plate; a folding edge is set on the front edge of the guide plate and the edge of the guide plate away from the clearance groove, that is, a folding edge is set only on the contact edge of the chandelier wire and the guide plate.

[0032] In this embodiment, in order to assist the up and down movement of each monitoring device, auxiliary guide rail assemblies 17 for assisting the extension and retraction of the monitoring device are symmetrically arranged in the left and right sides of the fuselage main body. The auxiliary guide rail assembly is composed of a number of auxiliary guide rails 18 corresponding to the monitoring assemblies and arranged in parallel. The plane formed by each auxiliary guide rail is parallel to the plane of the fixed plate body, that is, the auxiliary guide rails on one side are distributed along the length direction of the fixed plate body, and the adjacent auxiliary guide rails are vertically slidably connected, so that the auxiliary guide rails in the same auxiliary guide rail assembly form multi-level slide rails, and different heights correspond to different levels of slide rails. At the same time, the adjacent auxiliary guide rails can be provided with a guide rail groove 19 on one guide rail and a guide rail slider 20 that cooperates with the guide rail groove on the other guide rail, so as to achieve Lifting and lowering, both ends of the guide rail slide are provided with limiting blocks for limiting the guide rail slider from dislodging, the auxiliary guide rail on one edge of the same auxiliary guide rail assembly is fixed on the inspection base, and the auxiliary guide rail on the other edge is fixed under the cover plate, that is, the edge guide rails on both sides of the auxiliary guide rail on the same auxiliary guide rail assembly are respectively connected to the inspection base or the cover plate, so that the overall auxiliary guide rail assembly can be lifted and lowered with the extension and contraction of the fuselage body, and each auxiliary guide rail is provided with a vertical auxiliary slide groove 22 on the front side surface, and each fixed plate is equipped with a slider 23 that cooperates with the corresponding auxiliary slide groove, that is, the auxiliary slide grooves of the two auxiliary guide rails corresponding to the same height level on the auxiliary slide groove are both provided with sliders, and limit blocks can be provided on both ends of the auxiliary slide groove corresponding to the slider to prevent the slider from dislodging.

[0033] In this embodiment, in order to realize the sliding of each telescopic kit, vertical lifting guide rails 24 are installed on the inner walls of the telescopic kits except the innermost telescopic kit, and guide wheel assemblies 25 are provided on the outer walls of the telescopic kits except the outermost telescopic kit, corresponding to the lifting guide rails on the inner walls of the telescopic kits of the outer layer. The guide wheel assemblies can be existing rollers, and limiting plates 26 are provided on the upper ends of the telescopic kits except the innermost telescopic kit, corresponding to the guide wheel assemblies on the telescopic kits of the inner layer.

[0034] Unless otherwise stated, any numerical range disclosed for any technical solution disclosed in the present invention is a preferred numerical range. Those skilled in the art should understand that a preferred numerical range is merely a numerical range that provides a more significant or representative technical effect among a wide range of practicable values. Due to the large number of numerical values, it is impossible to enumerate them exhaustively. Therefore, only some numerical values ​​are disclosed in the present invention to illustrate the technical solution of the present invention. Furthermore, the numerical values ​​listed above should not be construed as limiting the scope of protection of the present invention.

[0035] If words such as "first" and "second" are used in this document to limit components, those skilled in the art should know that the use of "first" and "second" is only for the convenience of description to distinguish between components. Unless otherwise stated, the above words have no special meaning.

[0036] If the present invention discloses or involves components or structural parts that are fixedly connected to each other, then, unless otherwise stated, the fixed connection can be understood as: a detachable fixed connection (for example, connection using bolts or screws), and can also be understood as: a non-detachable fixed connection (for example, riveting, welding). Of course, the mutual fixed connection can also be replaced by an integrated structure (for example, manufactured by integral molding using a casting process) (except where it is obviously not possible to use an integrated molding process).

[0037] In addition, the orientations or positional relationships indicated by terms such as "longitudinal", "transverse", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", and "outside" used in any of the technical solutions disclosed in the above-mentioned utility model are based on the orientations or positional relationships shown in the accompanying drawings, and are only for the convenience of describing this patent, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation. Therefore, they cannot be understood as limitations on this patent. Unless otherwise stated, the terms used to indicate shapes used in any of the technical solutions disclosed in the above-mentioned utility model include shapes that are approximate, similar, or close to them.

[0038] Any component provided by the present invention can be assembled from multiple separate components, or can be a separate component manufactured by an integral forming process.

[0039] Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the utility model and not to limit it; although the utility model has been described in detail with reference to the preferred embodiments, ordinary technicians in the field should understand that the specific implementation methods of the utility model can still be modified or some technical features can be replaced by equivalents; without departing from the spirit of the technical solution of the utility model, they should all be included in the scope of the technical solution for which protection is requested in the utility model.

Claims

1. A patrol robot body structure, characterized by: It includes a fuselage main body, a guide surface is provided on the junction between the forward side of the fuselage main body and the left and right sides of the fuselage main body, and the lighting lamp corresponding to the inspection channel is provided with a guide surface, and the upper end of the fuselage main body is provided with a guide plate.

2. The inspection robot body structure according to claim 1, characterized in that: The fuselage body is a columnar body, the front edge of the guide plate is provided with a guide edge corresponding to the guide surface, and a folded edge is provided on the edge of the guide plate.

3. The inspection robot body structure according to claim 2, characterized in that: The fuselage body is a telescopic shell, and the fuselage body is composed of at least two telescopic kits that are sequentially connected from the inside to the outside. A push rod mechanism for driving the fuselage body to be telescopic is vertically installed in the fuselage body, and the telescopic end of the push rod mechanism is fixed to the innermost telescopic kit.

4. The inspection robot body structure according to claim 3, characterized in that: The telescopic kit is a hollow column, and the intersection between the forward side of the telescopic kit and the left and right sides thereof is provided with a chamfered surface, and the chamfered surface of each telescopic kit constitutes a guide surface.

5. The inspection robot body structure according to claim 3, characterized in that: A monitoring device is installed in the fuselage body and is retracted and retracted as the fuselage body retracts and retracts. A clearance groove is provided on the middle part of one of the left and right sides of the telescopic kit that is not connected to the chamfered surface, corresponding to the monitoring device. The upper and lower ends of the clearance groove pass through the side panel of the telescopic kit.

6. The inspection robot body structure according to claim 5, characterized in that: An inspection base is provided under the main body of the fuselage, the outermost telescopic kit is fixed on the inspection base, and the push rod mechanism and the monitoring device are both installed on the inspection base.

7. The inspection robot body structure according to claim 6, characterized in that: The upper end of the innermost telescopic kit is closed by a cover plate. The monitoring device includes several monitoring components from top to bottom, and two adjacent monitoring components are movably connected. The upper end of the monitoring device is fixed under the cover plate, the telescopic end of the push rod mechanism is fixed under the cover plate, and the guide plate is fixed on the cover plate; a folded edge is provided on the front edge of the guide plate and the edge of the guide plate away from the clearance groove.

8. The inspection robot body structure according to claim 7, characterized in that: The monitoring assembly includes a vertically arranged fixing plate, a monitor is fixed on the plate body on the side of the fixing plate facing the clearance slot, and two adjacent fixing plates are connected by an accordion-type protective cover.

9. The inspection robot body structure according to claim 8, characterized in that: An auxiliary guide rail assembly for assisting the extension and retraction of the monitoring device is symmetrically arranged in the left and right sides of the fuselage body. The auxiliary guide rail assembly consists of a number of auxiliary guide rails corresponding to the monitoring assemblies and arranged in parallel. The plane formed by each auxiliary guide rail is parallel to the plane of the fixed plate body. Adjacent auxiliary guide rails are vertically slidably connected. The auxiliary guide rail on one edge of the same auxiliary guide rail assembly is fixed on the inspection base, and the auxiliary guide rail on the other edge is fixed under the cover plate. A vertical auxiliary slide groove is provided on the front side of each auxiliary guide rail, and a slider that cooperates with the corresponding auxiliary slide groove is installed on each fixed plate.

10. The inspection robot body structure according to any one of claims 3 to 9, characterized in that: Vertical lifting guide rails are installed on the inner walls of the telescopic kits except the innermost telescopic kit, and guide wheel assemblies are set on the outer walls of the telescopic kits except the outermost telescopic kit, corresponding to the lifting guide rails on the inner walls of the telescopic kits of the outer layer. Limit plates are set on the upper ends of the telescopic kits except the innermost telescopic kit, corresponding to the guide wheel assemblies on the telescopic kits of the inner layer.

Images