Anti-shock pressure gauge with remote transmission function

CN224802585UActive Publication Date: 2026-09-25浙江中恒仪器仪表有限公司
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Patent Information

Application Number
CN202522605907.7
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-12-09
Publication Date
2026-09-25
Estimated Expiration
2035-12-09

AI Technical Summary

Technical Problem

[0003]在石油、煤炭、地质等部门的钻井设备作业过程中,抗震压力表是测量高粘度介质中必不可少的,然而,现在常用的抗震压力表都有一个缺点是,需要工作人员到现场近距离观测油路压力,使用起来较为不便,难以同时观测多个压力表数据,因此,针对上述问题提出一种带远传功能的抗震压力表

Benefits of technology

1、本实用新型中,通过设置的传动机构、传感器支架、磁头、角度传感器、度盘组件、指针组件和航空插度等构件,角度传感器安装到机芯组件后端,中心齿轮轴后端装有磁头,磁头带动角度传感器内部芯片,通过角度传感器内部主板处理后输出电流信号,通电压输入12-24VDC,表内机芯带动角度传感器,通过数据电缆传输至数字显示表或数据终端,也可通过无线传速至电脑和手机直接观测实时压力,可以从一个屏幕上同时查看多组抗震压力表的数据,从而解决了在石油、煤炭、地质等部门的钻井设备作业过程中,抗震压力表是测量高粘度介质中必不可少的,然而,现在常用的抗震压力表都有一个缺点是,需要工作人员到现场近距离观测油路压力,使用起来较为不便,难以同时观测多个压力表数据的问题;

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to pressure measuring instrument technical field especially is an anti -shock pressure gauge with remote transmission function, including hexagonal joint subassembly and shell subassembly, the top fixedly connected with shell subassembly of hexagonal joint subassembly, the inside of hexagonal joint subassembly is equipped with the cover, the inside fixedly connected with the sealing washer of cover outside of hexagonal joint subassembly, the inside of hexagonal joint subassembly is equipped with the damping assembly of sealing washer and cover top, in the utility model, angle sensor installs to the back end of movement subassembly, the back end of central gear shaft is equipped with magnetic head, and magnetic head drives angle sensor internal chip, and the current signal is exported after through angle sensor internal mainboard processing, voltage input 12 24VDC, and the movement in the meter drives angle sensor, and through data cable transmission to digital display meter or data terminal, also can be through wireless transmission to computer and mobile phone direct observation real -time pressure, can view simultaneously multiple anti -shock pressure gauge's data from one screen.
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Description

Technical Field

[0001] This utility model relates to the field of pressure measuring instrument technology, specifically to a shock-resistant pressure gauge with remote transmission function. Background Technology

[0002] Vibration-resistant pressure gauges (also known as shock-resistant pressure gauges) are specialized instruments designed for complex working conditions such as vibration, shock, and pulsating pressure in the field of industrial pressure measurement. Their core is to solve the pain points of decreased measurement accuracy, pointer jitter, and easy damage of components under vibration environment by optimizing the structure and protective design on the basis of ordinary pressure gauges, so as to ensure stable and reliable pressure data.

[0003] In the drilling operations of petroleum, coal, and geological sectors, anti-vibration pressure gauges are essential for measuring high-viscosity media. However, commonly used anti-vibration pressure gauges have a drawback: they require personnel to be on-site to observe the oil pressure at close range, which is inconvenient and makes it difficult to observe data from multiple pressure gauges simultaneously. Therefore, to address these issues, an anti-vibration pressure gauge with remote transmission function is proposed. Utility Model Content

[0004] The purpose of this invention is to provide a shock-resistant pressure gauge with remote transmission function to solve the problems mentioned in the background art.

[0005] To achieve the above objectives, this utility model provides the following technical solution: A shock-resistant pressure gauge with remote transmission function includes a hexagonal connector assembly and a housing assembly. The housing assembly is fixedly connected to the top of the hexagonal connector assembly. A protective cover is provided on the inner side of the hexagonal connector assembly. A sealing gasket located on the outer side of the protective cover is fixedly connected to the inner side of the hexagonal connector assembly. A damping assembly located on the inner side of the hexagonal connector assembly is provided at the top of the sealing gasket and the protective cover. A sealing gasket is fixedly connected to the top of the damping assembly. A diaphragm is fixedly connected to the top of the sealing gasket. A push rod penetrating the diaphragm is fixedly connected to the top of the sealing gasket. A fork spring is provided at the top of the push rod. A transmission mechanism located on the inner side of the housing assembly is provided at the top of the fork spring. A sensor bracket is fixedly connected to the rear side of the transmission mechanism. A magnetic head located inside the sensor bracket is provided on the rear side of the transmission mechanism. An angle sensor is fixedly connected to the side of the sensor bracket away from the transmission mechanism. A dial assembly is provided on the front side of the transmission mechanism. A pointer assembly penetrating the dial assembly is fixedly connected to the front side of the transmission mechanism. An aviation scale is fixedly connected to the outer side of the housing assembly.

[0006] Preferably, the outer diameter of the sealing gasket matches the inner diameter of the hexagonal connector assembly, and the inner diameter of the sealing gasket matches the outer diameter of the cover.

[0007] Preferably, the shape of the sealing gasket matches the shape of the diaphragm, both being disc-shaped, and the diameter of the sealing gasket matches the diameter of the diaphragm.

[0008] Preferably, the dial assembly is disc-shaped, and the diameter of the dial assembly is larger than the diameter of the protective glass portion of the outer casing assembly.

[0009] Preferably, the push rod and the fork spring are connected by a hexagonal thread and a spring washer, with the push rod located directly below the fork spring.

[0010] Compared with the prior art, the beneficial effects of this utility model are: 1. In this utility model, through the setting of transmission mechanism, sensor bracket, magnetic head, angle sensor, dial assembly, pointer assembly and aviation scale, etc., the angle sensor is installed at the rear end of the mechanism assembly, and the magnetic head is installed at the rear end of the central gear shaft. The magnetic head drives the internal chip of the angle sensor, and after processing by the internal motherboard of the angle sensor, it outputs a current signal. The voltage input is 12-24VDC. The internal mechanism drives the angle sensor and transmits it to the digital display meter or data terminal through the data cable. It can also be transmitted wirelessly to the computer and mobile phone to directly observe the real-time pressure. The data of multiple anti-vibration pressure gauges can be viewed on one screen at the same time. This solves the problem that anti-vibration pressure gauges are essential for measuring high viscosity media in the drilling equipment operation of petroleum, coal, geology and other departments. However, the commonly used anti-vibration pressure gauges have a disadvantage: the staff needs to observe the oil pressure at close range on site, which is inconvenient to use and makes it difficult to observe the data of multiple pressure gauges at the same time. 2. In this utility model, through the damping components, diaphragm, push rod and fork spring, the damping mechanism inside the instrument controls the pulsation throughout the entire pressure range. No adjustment is required during use. This structure can not only measure the pressure of violent pulsation, but also withstand instantaneous pressure shocks (such as sudden pressure relief). The diaphragm, push rod and fork spring can ensure "precise force transmission", further ensuring the accuracy of measurement. Attached Figure Description

[0011] Figure 1 This is a schematic diagram of the overall structure of this utility model; Figure 2 This utility model Figure 1 A schematic diagram of the side view cross-sectional structure.

[0012] In the diagram: 1. Hexagonal connector assembly; 2. Housing assembly; 3. Protective cover; 4. Sealing gasket; 5. Damping assembly; 6. Sealing gasket; 7. Diaphragm; 8. Top rod; 9. Fork spring; 10. Transmission mechanism; 11. Sensor bracket; 12. Magnetic head; 13. Angle sensor; 14. Dial assembly; 15. Pointer assembly; 16. Aviation scale. Detailed Implementation

[0013] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0014] It should be noted that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to limit the exemplary embodiments according to this application. As used herein, the singular form is intended to include the plural form as well, unless the context clearly indicates otherwise. Furthermore, it should be understood that when the terms "comprising" and / or "including" are used in this specification, they indicate the presence of features, steps, operations, devices, components, and / or combinations thereof.

[0015] Furthermore, it should be noted that the use of terms such as "first" and "second" to define components is merely for the purpose of distinguishing the corresponding components. Unless otherwise stated, the above terms have no special meaning and therefore should not be construed as limiting the scope of protection of this invention.

[0016] Please see Figure 1-2 This utility model provides a technical solution: A shock-resistant pressure gauge with remote transmission function includes a hexagonal connector assembly 1 and a housing assembly 2. The housing assembly 2 is fixedly connected to the top of the hexagonal connector assembly 1. A cover 3 is provided on the inner side of the hexagonal connector assembly 1. A sealing gasket 4 located outside the cover 3 is fixedly connected to the inner side of the hexagonal connector assembly 1. A damping assembly 5 located inside the hexagonal connector assembly 1 is provided at the top of the sealing gasket 4 and the cover 3. A sealing gasket 6 is fixedly connected to the top of the damping assembly 5. A diaphragm 7 is fixedly connected to the top of the sealing gasket 6. A push rod 8 penetrating the diaphragm 7 is fixedly connected to the top of the sealing gasket 6. A fork spring 9 is provided at the top of the rod 8. A transmission mechanism 10 is provided at the top of the fork spring 9 and located inside the housing assembly 2. A sensor bracket 11 is fixedly connected to the rear side of the transmission mechanism 10. A magnetic head 12 is provided inside the sensor bracket 11 and located at the rear side of the transmission mechanism 10. An angle sensor 13 is fixedly connected to the side of the sensor bracket 11 away from the transmission mechanism 10. A dial assembly 14 is provided at the front side of the transmission mechanism 10. A pointer assembly 15 is fixedly connected to the front side of the transmission mechanism 10 and located through the dial assembly 14. An aviation connector 16 is fixedly connected to the outer side of the housing assembly 2.

[0017] The outer diameter of the sealing gasket 4 matches the inner diameter of the hexagonal connector assembly 1, and the inner diameter of the sealing gasket 4 matches the outer diameter of the cover 3, which can effectively ensure the sealing effect inside the pressure gauge; the shape of the sealing gasket 6 matches the shape of the diaphragm 7, both being disc-shaped, and the diameter of the sealing gasket 6 matches the diameter of the diaphragm 7, which can effectively improve the sealing effect at the diaphragm 7 and ensure the stability of pressure sensing and transmission of the diaphragm 7; the dial assembly 14 is disc-shaped, and the diameter of the dial assembly 14 is larger than the diameter of the protective glass part of the outer shell assembly 2, which can effectively ensure the viewing effect of the dial assembly 14 and avoid the phenomenon of bottom leakage; the push rod 8 and the fork spring 9 are connected by hexagonal threads and spring washers, and the push rod 8 is located directly below the fork spring 9, further ensuring the stability of pressure transmission.

[0018] Workflow: When a shock-resistant pressure gauge with remote transmission function is required, the entire system is powered externally. The measuring medium presses against the inner cover 3 of the hexagonal connector assembly 1 and transmits the signal to the damping assembly 5. The damping assembly 5 lifts the diaphragm 7 and the push rod 8, and the push rod 8 lifts the fork spring 9. At this time, the fork spring 9 deforms under force, causing the transmission mechanism 10 to move. Then, the transmission mechanism 10 drives the magnetic head 12 to rotate. The rotation of the magnetic head 12 causes the internal chip of the angle sensor 13 to work and output a 4-20mA current signal. The current signal is input to an external digital display, wireless transmission module, or data terminal through the aviation connector 16 and data cable. Data from multiple shock-resistant pressure gauges can then be easily viewed from a distance, making it more convenient.

[0019] Contents not described in detail in this specification are existing technologies known to those skilled in the art. Standard parts used in this invention can all be purchased commercially, and irregularly shaped parts can be custom-made according to the description and drawings. The specific connection methods for each part all employ conventional methods such as bolts, rivets, and welding, which are already mature technologies. The machinery, parts, and equipment all use conventional models from the prior art, and the circuit connections also employ conventional connection methods from the prior art, which will not be detailed here.

[0020] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A shock-resistant pressure gauge with remote transmission function, comprising a hexagonal connector assembly (1) and a housing assembly (2), characterized in that: The top of the hexagonal connector assembly (1) is fixedly connected to the outer shell assembly (2). A cover (3) is provided on the inner side of the hexagonal connector assembly (1). A sealing gasket (4) located outside the cover (3) is fixedly connected to the inner side of the hexagonal connector assembly (1). A damping assembly (5) located inside the hexagonal connector assembly (1) is provided at the top of the sealing gasket (4) and the cover (3). A sealing gasket (6) is fixedly connected to the top of the damping assembly (5). A diaphragm (7) is fixedly connected to the top of the sealing gasket (6). A push rod (8) penetrating the diaphragm (7) is fixedly connected to the top of the sealing gasket (6). A fork spring (9) is provided at the top of the push rod (8). The top of the fork spring (9) is provided with a transmission mechanism (10) located inside the housing assembly (2). A sensor bracket (11) is fixedly connected to the rear side of the transmission mechanism (10). A magnetic head (12) is located inside the sensor bracket (11) on the rear side of the transmission mechanism (10). An angle sensor (13) is fixedly connected to the side of the sensor bracket (11) away from the transmission mechanism (10). A dial assembly (14) is provided on the front side of the transmission mechanism (10). A pointer assembly (15) is fixedly connected to the front side of the transmission mechanism (10) and passes through the dial assembly (14). An aviation gauge (16) is fixedly connected to the outer side of the housing assembly (2).

2. The anti-vibration pressure gauge with remote transmission function according to claim 1, characterized in that: The outer diameter of the sealing gasket (4) matches the inner diameter of the hexagonal connector assembly (1), and the inner diameter of the sealing gasket (4) matches the outer diameter of the cover (3).

3. The anti-vibration pressure gauge with remote transmission function according to claim 1, characterized in that: The shape of the sealing gasket (6) matches the shape of the diaphragm (7), both being disc-shaped, and the diameter of the sealing gasket (6) matches the diameter of the diaphragm (7).

4. The anti-vibration pressure gauge with remote transmission function according to claim 1, characterized in that: The dial assembly (14) is disc-shaped, and the diameter of the dial assembly (14) is larger than the diameter of the protective glass portion of the outer shell assembly (2).

5. A shock-resistant pressure gauge with remote transmission function according to claim 1, characterized in that: The top rod (8) and the fork spring (9) are connected by a hexagonal thread and a spring washer, with the top rod (8) located directly below the fork spring (9).