Double-shaft double-aviation-plug tilt angle sensor

Abstract

The utility model provides a double-shaft double-aviation-plug tilt angle sensor which comprises an upper shell and a rear buckle, and the left side and the right side of the upper end of the upper shell are each provided with a set of upper buckles used for limiting the position of the upper shell; the upper end of the upper shell is provided with two sets of indicator lamps used for prompting the inclination angle, and the left side and the right side of the upper shell are each provided with a set of side shells used for sealing and attaching the upper shell. A group of inner cavities for storing the tilt angle sensor are formed in the side shell, two groups of front shells for protecting the front ends of the inner cavities are arranged at the front end of the side shell, and a group of buckles for positioning and connecting the front shells are arranged on the left side and the right side of each front shell; the upper shell and the front shell can be limited, connected and fixed by using the buckles and the upper buckles. The upper shell and the front shell are limited, connected and fixed through the buckles and the upper buckles, and the outer sides of the upper ends of the transverse shaft rod and the longitudinal shaft rod are limited through the seat shell.

Description

Technical Field

[0001] The utility model belongs to the technical field of inclination sensors and relates to a biaxial double aviation plug inclination sensor. Background Art

[0002] The biaxial double aviation plug inclination sensor is an advanced measuring tool that combines biaxial measurement technology and double aviation plug design to provide more accurate and stable inclination measurement data. This kind of sensor has a wide range of applications in many fields, such as industrial automation, bridge construction, railway laying, aviation and navigation, etc. As an important measuring device, the biaxial double aviation plug inclination sensor is widely used in various industrial automation systems to monitor and feedback the inclination angle of an object in real time. When this kind of sensor fails, if it cannot be disassembled and repaired quickly, a series of problems will be caused.

[0003] The inclination sensor is a key component in the automatic control of the production line. Once it fails, the production line may not be able to accurately obtain the inclination state of the object, resulting in the interruption of the production process or the decline of product quality. If the faulty sensor cannot be quickly replaced or repaired, the enterprise may need to invest more manpower and material resources in troubleshooting and maintenance. Therefore, there is an urgent need for a biaxial double aviation plug inclination sensor to solve the above problems. Content of the Utility Model

[0004] Aiming at the deficiencies of the existing technology, the purpose of the utility model is to provide a biaxial double aviation plug inclination sensor to solve the problems put forward in the above background art.

[0005] The utility model is realized through the following technical solutions: A biaxial double aviation plug inclination sensor includes: an upper shell and a rear buckle, and a set of upper buckles for limiting the position of the upper shell are arranged on the left and right sides of the upper end of the upper shell;

[0006] Two groups of indicator lights for prompting the inclination angle are arranged at the upper end of the upper shell, and a set of side shells for hermetically fitting the upper shell are arranged on the left and right sides of the upper shell;

[0007] A set of inner cavities for storing the inclination sensor are arranged inside the side shells, and two groups of front shells for protecting the front end of the inner cavities are arranged at the front ends of the side shells. A set of buckles for positioning and connecting the front shells are arranged on the left and right sides of the front shells, and the upper shell and the front shell can be limited, connected and fixed by using the buckles and the upper buckles.

[0008] As a preferred embodiment, a set of display screens for displaying the data of the inclination sensor are arranged inside the front shells, a set of inner grooves for mutually fitting with a seat shell are arranged at the rear sides of the side shells, and a set of rear buckles for positioning the seat shell are arranged on the left and right sides of the inner grooves.

[0009] As a preferred embodiment, a set of seat shells for limiting the outer sides of the upper ends of the transverse shaft rod and the longitudinal shaft rod are provided at the lower end of the side shell. Four sets of fixing bolts for connecting and fixing the seat shell to the lower shell are provided on the outer side of the upper end of the seat shell. The outer sides of the upper ends of the transverse shaft rod and the longitudinal shaft rod can be limited by using the seat shell.

[0010] As a preferred embodiment, a lower shell for limiting the outer sides of the lower ends of the transverse shaft rod and the longitudinal shaft rod is provided at the lower end of the seat shell. A transverse shaft rod for detecting the transverse inclination angle is provided inside the lower shell. The transverse inclination angle can be detected by using the transverse shaft rod.

[0011] As a preferred embodiment, a longitudinal shaft rod for detecting the longitudinal inclination angle is provided inside the lower shell. A set of inner slots for fitting and connecting with an external data wire harness are provided inside each of the aviation sockets. The longitudinal inclination angle can be detected by using the longitudinal shaft rod.

[0012] As a preferred embodiment, both of the two aviation sockets are electrically connected to an inclination sensor. The inclination sensor is connected to a display screen and two indicator lights through wires. The two indicator lights respectively indicate the predetermined angles in the longitudinal and transverse directions. The predetermined angles in the longitudinal and transverse directions can be respectively indicated by using the indicator lights.

[0013] As a preferred embodiment, the two upper buckles are connected and fixed to the upper shell by bolts. The front shell is connected and fixed to the two buckles by bolts. The rear side of the seat shell is hermetically fitted and connected to the inner groove, and the two rear buckles are connected and fixed to the seat shell by external bolts.

[0014] After adopting the above technical solutions, the beneficial effects of the present utility model are as follows: The upper shell and the front shell are limited, connected and fixed by using the buckles and the upper buckles. The outer sides of the upper ends of the transverse shaft rod and the longitudinal shaft rod are limited by using the seat shell. The transverse inclination angle is detected by using the transverse shaft rod. The longitudinal inclination angle is detected by using the longitudinal shaft rod. The predetermined angles in the longitudinal and transverse directions are respectively indicated by using the indicator lights. Description of the Drawings

[0015] In order to more clearly illustrate the technical solutions in the embodiments of the present utility model or the prior art, the following will briefly introduce the drawings required for use in the description of the embodiments or the prior art. Obviously, the following drawings are only some embodiments of the present utility model. For those of ordinary skill in the art, other drawings can be obtained based on these drawings without creative efforts.

[0016] Figure 1Schematic diagram of the front right oblique top view of a dual-axis dual-aerial plug inclinometer sensor of the present utility model;

[0017] Figure 2 Schematic diagram of the rear right oblique top view of a dual-axis dual-aerial plug inclinometer sensor of the present utility model;

[0018] Figure 3 Schematic diagram of the front right oblique top view of the display screen in a dual-axis dual-aerial plug inclinometer sensor of the present utility model;

[0019] In the figure: 100 - upper shell, 110 - upper buckle, 120 - aviation socket, 130 - side shell, 140 - front shell, 150 - display screen, 160 - base shell, 170 - lower shell, 180 - horizontal shaft rod, 190 - vertical shaft rod, 200 - fixing bolt, 210 - indicator light, 220 - inner slot, 230 - rear buckle. Specific embodiments

[0020] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments. Based on the embodiments in the present utility model, all other embodiments obtained by those of ordinary skill in the art without making creative efforts shall fall within the protection scope of the present utility model.

[0021] Please refer to Figures 1 - 3 , a dual-axis dual-aerial plug inclinometer sensor, including: an upper shell 100, a display screen 150, an inner slot 220, and a rear buckle 230. On both the left and right sides of the upper end of the upper shell 100, a set of upper buckles 110 for limiting the position of the upper shell 100 are provided;

[0022] On the upper end of the upper shell 100, two sets of indicator lights 210 for indicating the inclination angle are provided. On both the left and right sides of the upper shell 100, a set of side shells 130 for hermetically fitting the upper shell 100 are provided;

[0023] Inside the side shell 130, a set of inner cavities for storing the inclinometer sensor are provided. At the front end of the side shell 130, two sets of front shells 140 for protecting the front end of the inner cavity are provided. On both the left and right sides of the front shell 140, a set of buckles for positioning and connecting the front shell 140 are provided, and the upper shell 100 and the front shell 140 can be limited and connected and fixed by using the buckles and the upper buckles 110.

[0024] Inside the front shell 140, a set of display screens 150 for displaying the data of the inclinometer sensor are provided. At the rear side of the side shell 130, a set of inner grooves for mutually fitting with the base shell 160 are provided. On both the left and right sides of the inner groove, a set of rear buckles 230 for positioning the base shell 160 are provided.

[0025] A set of seat shells 160 for limiting the outer sides of the upper ends of the transverse shaft rod 180 and the longitudinal shaft rod 190 are provided at the lower end of the side shell 130. Four sets of fixing bolts 200 for connecting and fixing the seat shell 160 to the lower shell 170 are provided on the outer side of the upper end of the seat shell 160. The outer sides of the upper ends of the transverse shaft rod 180 and the longitudinal shaft rod 190 can be limited by using the seat shell 160.

[0026] A lower shell 170 for limiting the outer sides of the lower ends of the transverse shaft rod 180 and the longitudinal shaft rod 190 is provided at the lower end of the seat shell 160. A transverse shaft rod 180 for detecting the transverse inclination angle is provided inside the lower shell 170. The transverse inclination angle can be detected by using the transverse shaft rod 180.

[0027] A longitudinal shaft rod 190 for detecting the longitudinal inclination angle is provided inside the lower shell 170. A set of inner slots 220 for engaging and connecting with an external data wire harness are provided inside each set of aviation sockets 120. The longitudinal inclination angle can be detected by using the longitudinal shaft rod 190.

[0028] Both sets of aviation sockets 120 are electrically connected to the inclination sensor. The inclination sensor is connected to the display screen 150 and the two sets of indicator lights 210 through wires. The two sets of indicator lights 210 respectively indicate the predetermined angles in the longitudinal and transverse directions. The predetermined angles in the longitudinal and transverse directions can be respectively indicated by using the indicator lights 210.

[0029] The two sets of upper buckles 110 are connected and fixed to the upper shell 100 by bolts. The front shell 140 is connected and fixed to the two sets of buckles by bolts. The rear side of the seat shell 160 is hermetically fitted and connected to the inner groove, and the two sets of rear buckles 230 are connected and fixed to the seat shell 160 by external bolts.

[0030] Please refer to Figures 1 - 3, as the first embodiment of the present utility model: To solve the problem that the inclination sensor is a key component in the automatic control of the production line. Once a failure occurs, the production line may not be able to accurately obtain the inclination state of the object, resulting in the interruption of the production process or the decline of product quality. If the faulty sensor cannot be quickly replaced or repaired, the enterprise may need to invest more manpower and material resources for troubleshooting and maintenance. First, when a failure occurs during the process of using the present utility model to measure the inclination angle of the equipment, since a set of upper buckles 110 for limiting the position of the upper shell 100 are provided on the left and right sides of the upper end of the upper shell 100, a set of buckles for positioning and connecting the front shell 140 are provided on the left and right sides of the front shell 140, and a set of inner grooves for engaging with the seat shell 160 are provided on the rear side of the side shell 130. A set of rear buckles 230 for positioning the seat shell 160 are provided on the left and right sides of the inner groove. The staff can choose to disassemble the whole or part of the front shell 140, the upper shell 100, and the side shell 130 according to the specific position to be troubleshot, so as to carry out targeted maintenance, thereby reducing the working time of equipment disassembly.

[0031] Please refer to Figures 1 - 3 , as the second embodiment of the present utility model: Based on the description in the above embodiment, further, since a set of transverse shaft rods 180 for detecting the transverse inclination are provided inside the lower shell 170, and a set of longitudinal shaft rods 190 for detecting the longitudinal inclination are provided inside the lower shell 170. By using the transverse shaft rods 180 and the longitudinal shaft rods 190, the inclination angle can be detected in a fitting manner, and two groups of indicator lights 210 are used to respectively indicate the longitudinal and transverse predetermined angles, so that the staff can directly observe the situation where the transverse shaft rods 180 and the longitudinal shaft rods 190 exceed the inclination pre-set range.

[0032] The above are only the preferred embodiments of the present utility model and are not intended to limit the present utility model. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present utility model shall be included in the protection scope of the present utility model.

Claims

1. A dual-axis dual-pilot inclination sensor, comprising: An upper shell (100), a display screen (150), an inner slot (220) and a rear buckle (230), characterized in that: a group of upper buckles (110) for limiting the position of the upper shell (100) are provided on both left and right sides of the upper end of the upper shell (100); Two groups of indicator lights (210) for indicating the tilt angle are provided at the upper end of the upper shell (100), and a group of side shells (130) for sealing and fitting the upper shell (100) are provided on both the left and right sides of the upper shell (100); A group of inner cavities for storing the inclination sensor are provided inside the side shell (130), two groups of front shells (140) for protecting the front ends of the inner cavities are provided at the front ends of the side shells (130), and a group of buckles for positioning and connecting the front shells (140) are provided on both left and right sides of the front shells (140).

2. A dual-axis dual-air insertion inclination sensor according to claim 1, characterized in that: A display screen (150) for displaying tilt sensor data is provided inside the front shell (140), a group of inner grooves for interlocking with the seat shell (160) are provided on the rear side of the side shell (130), and a group of rear buckles (230) for positioning the seat shell (160) are provided on both left and right sides of the inner groove.

3. A dual-axis dual-air insertion inclination sensor according to claim 2, characterized in that: A group of seat shells (160) for limiting the outer sides of the upper ends of the transverse shaft rod (180) and the longitudinal shaft rod (190) are provided at the lower ends of the side shells (130), and four groups of fixing bolts (200) for connecting and fixing the seat shells (160) and the lower shell (170) are provided at the outer sides of the upper ends of the seat shells (160).

4. A dual-axis dual-air insertion inclination sensor according to claim 3, characterized in that: A group of lower shells (170) for limiting the outer sides of the lower ends of the transverse shaft rod (180) and the longitudinal shaft rod (190) are provided at the lower end of the seat shell (160), and a group of transverse shaft rods (180) for detecting the transverse inclination angle are provided inside the lower shell (170).

5. A dual-axis dual-air insertion inclination sensor according to claim 4, characterized in that: A group of longitudinal shaft rods (190) for detecting longitudinal inclination angles are provided inside the lower shell (170), and a group of inner slots (220) for engaging and connecting with an external data harness are provided inside each group of aviation sockets (120).

6. A dual-axis dual-air insertion inclination sensor according to claim 5, characterized in that: The two groups of aviation sockets (120) are both electrically connected to the inclination sensor, and the inclination sensor is connected to the display screen (150) and the two groups of indicator lights (210) via wires, and the two groups of indicator lights (210) respectively indicate predetermined longitudinal and transverse angles.

7. The dual-axis dual-air insertion inclination sensor according to claim 1, characterized in that: The two groups of upper buckles (110) are fixed to the upper shell (100) by bolts, the front shell (140) is fixed to the two groups of buckles by bolts, the rear side of the seat shell (160) is sealed and engaged with the inner groove, and the two groups of rear buckles (230) are fixed to the seat shell (160) by external bolts.

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