High pressure test tank structure
By designing a detachable sealing device and a high-strength, corrosion-resistant tank, combined with a servo motor and cylinder-driven opening assembly, the problems of complex sealing and insufficient temperature control in traditional high-pressure testing equipment have been solved. This has enabled rapid propeller replacement and improved the accuracy of test data, thus extending the equipment's lifespan.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- ZHEJIANG HANTEBO TECH CO LTD
- Filing Date
- 2025-05-21
- Publication Date
- 2026-06-05
AI Technical Summary
Traditional high-pressure testing equipment has a complex sealing structure, cumbersome propeller replacement operation, low testing efficiency, lack of efficient temperature control system, and is prone to tank damage due to temperature rise in high-pressure water environment.
The design incorporates a detachable sealing device and a high-strength, corrosion-resistant tank. Combined with a servo motor-driven upper opening assembly and a cylinder-driven lower opening assembly, it enables rapid opening, closing, and sealing of the tank. Built-in cooling pipes and a dual-channel pressure monitoring system ensure accurate temperature control and pressure data.
It enables rapid propeller replacement and improves testing flexibility, ensures sealing reliability and test data accuracy under high-pressure environments, and extends the continuous operating life of the equipment.
Smart Images

Figure CN224327890U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of propeller performance testing technology, specifically the structure of a high-pressure test tank. Background Technology
[0002] Propeller performance testing is a crucial step in evaluating key parameters such as efficiency, thrust, and torque of propellers under different operating conditions. It is widely used in aviation, shipbuilding, drones, and wind power generation. However, traditional high-pressure testing equipment has the following shortcomings in the field of propeller performance testing: 1) The sealing device has a complex structure, making propeller replacement cumbersome and resulting in low testing efficiency; 2) It lacks an efficient temperature control system, and the tank is prone to damage due to temperature rise under high-pressure water conditions. Utility Model Content
[0003] The purpose of this invention is to provide a high-pressure test tank structure to solve the problems mentioned in the background art.
[0004] To solve the above-mentioned technical problems, this utility model provides the following technical solution: a high-pressure test tank structure, comprising:
[0005] The tank is used to house the propeller to be tested and to provide a high-pressure water environment.
[0006] A detachable sealing device is located at the upper and lower ends of the tank to seal the tank and allow repeated opening and closing to allow for testing with different types of propellers. It includes an upper opening assembly and a lower opening assembly.
[0007] The upper opening assembly includes a housing, a servo motor is fixedly connected to the top of the housing, a turbine is fixedly connected to the output shaft of the servo motor, a worm gear is rotatably connected inside the housing, and an opening frame is fixedly connected to one end of the worm gear.
[0008] The lower opening assembly includes a lower bracket, on which a cylinder is fixedly connected. A sealing shell is fixedly connected to the right side of the cylinder. A limit plate is fixedly connected to the lower bracket, and a limit rod is slidably inserted into the limit plate. The right side of the limit rod is fixedly connected to the sealing shell.
[0009] Preferably, a sealing cap is provided at the right end of the tank body, the sealing cap is matched with the opening shape of the tank body, the top of the lower support is fixedly connected to the tank body, the bottom of the outer shell is fixedly connected to the tank body, and one end of the opening bracket is fixedly connected to the sealing cap.
[0010] Preferably, the tank is made of high-strength, corrosion-resistant material to withstand the pressure in a high-pressure water environment and to prevent corrosion.
[0011] Preferably, the interior of the tank is surrounded by cooling pipes, and the bottom of the tank is equipped with cooling water inlet and outlet valves that communicate with the cooling pipes.
[0012] Preferably, the bottom of the tank is fixedly connected to a support leg, and the bottom of the tank is equipped with an inlet and outlet.
[0013] Preferably, an automatic exhaust port is installed on the top of the tank, and a temperature measuring gauge is installed on the top of the tank.
[0014] Preferably, a local pressure gauge is installed on the top of the tank, and a remote pressure gauge is also installed on the top of the tank.
[0015] Compared with the prior art, the beneficial effects achieved by this utility model are:
[0016] First, this utility model, through the combination structure of a detachable sealing device and a matching sealing cap, enables the rapid opening and closing of the tank and reliable sealing, supports the efficient replacement of multiple propeller models, improves the flexibility of testing, and meets the sealing requirements of high-pressure environments.
[0017] Secondly, this utility model adopts a surrounding cooling pipeline and dual-channel pressure monitoring (local pressure gauge + remote pressure transmission gauge), combined with automatic exhaust and temperature sensing modules, which can realize dual redundant monitoring of temperature control accuracy and pressure data, ensuring the accuracy of test data under extreme working conditions and extending the continuous operating life of the equipment. Attached Figure Description
[0018] Figure 1 This is a schematic diagram of the main structure of this utility model;
[0019] Figure 2 This is a schematic diagram of the rear side view of the present invention;
[0020] Figure 3 This is an enlarged structural diagram of point A in this utility model.
[0021] The components include: 1. Tank body; 2. Sealing cover; 11. Outer shell; 12. Servo motor; 13. Turbine; 14. Worm gear; 15. Opening frame; 16. Lower support; 17. Cylinder; 18. Sealing shell; 19. Limit rod; 4. Cooling pipe; 5. Cooling water inlet and outlet valves; 6. Support leg; 7. Inlet and outlet; 8. Automatic exhaust port; 9. Temperature gauge; 10. Local pressure gauge; 3. Remote pressure gauge. Detailed Implementation
[0022] 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.
[0023] This utility model provides the following technical solution:
[0024] Please see Figure 1 , Figure 2 and Figure 3 The high-pressure test tank structure includes:
[0025] Tank 1 is used to house the propeller to be tested and provide a high-pressure water environment;
[0026] A detachable sealing device is provided at the upper and lower ends of the tank body 1 to seal the tank body and allow repeated opening and closing to allow for testing of different types of propellers, including an upper opening assembly and a lower opening assembly;
[0027] The upper opening assembly includes a housing 11, a servo motor 12 is fixedly connected to the top of the housing 11, a turbine 13 is fixedly connected to the output shaft of the servo motor 12, a worm gear 14 is rotatably connected inside the housing 11, and an opening frame 15 is fixedly connected to one end of the worm gear 14.
[0028] The lower opening assembly includes a lower bracket 16, a cylinder 17 is fixedly connected to the lower bracket 16, a sealing shell 18 is fixedly connected to the right side of the cylinder 17, a limit plate is fixedly connected to the lower bracket 16, a limit rod 19 is slidably inserted into the limit plate, and the right side of the limit rod 19 is fixedly connected to the sealing shell 18.
[0029] Through the above technical solution, the tank body 1 is the core component, used to accommodate the propeller to be tested and provide a high-pressure water environment to simulate actual working conditions. The high-pressure test tank consists of the tank body 1 and a detachable sealing device. The sealing device is divided into upper and lower parts. The upper opening component drives the turbine 13 and worm gear 14 mechanism through the servo motor 12, which drives the opening frame 15 to realize the automatic opening and closing of the sealing cover 2. The lower opening component pushes the sealing shell 18 to move horizontally through the cylinder 17. With the help of the limit rod 19 and the limit plate, the sealing shell 18 is accurately aligned with the sealing cover 2, ensuring the stability of the sealing cover 2. The upper and lower double opening design enables quick propeller replacement and improves test efficiency. The turbine 13 and worm gear 14 mechanism has a self-locking function, which can accurately control the opening and closing position of the sealing cover. The cylinder 17 drives the sealing shell 18 in combination with the limit structure to ensure the sealing reliability of the sealing cover 2 under high pressure.
[0030] A sealing cap 2 is provided at the right end of the tank body 1. The sealing cap 2 matches the shape of the opening of the tank body 1. The top of the lower bracket 16 is fixedly connected to the tank body 1. The bottom of the outer shell 11 is fixedly connected to the tank body 1. One end of the opening bracket 15 is fixedly connected to the sealing cap 2.
[0031] Through the above technical solution, a sealing cover 2 is provided at the right end of the tank body 1, the shape of which matches the opening of the tank body 1. The lower bracket 16 and the outer shell 11 are both fixed to the opening frame 15 of the tank body 1 and directly connected to the sealing cover 2. The matching design of the sealing cover 2 and the opening of the tank body 1 ensures that the high-pressure water does not leak. The fixed connection method ensures the overall rigidity of the sealing device and the tank body 1, avoiding deformation under high pressure. The rigid connection between the opening frame 15 and the sealing cover 2 realizes the direct transmission of power and reduces transmission error.
[0032] Tank 1 is made of high-strength, corrosion-resistant materials to withstand the pressure of a high-pressure water environment and prevent corrosion.
[0033] Through the above technical solution, the tank body 1 is made of high-strength material that can withstand the pressure in a high-pressure water environment, preventing the tank body 1 from deforming or cracking. The corrosion-resistant material can prevent the tank body from being corroded in a high-pressure water environment, extending the service life of the tank body 1 and ensuring the stability and safety of the tank body 1 in a high-pressure water environment, while also extending the service life of the tank body 1.
[0034] The interior of the tank 1 is surrounded by cooling pipes 4, and the bottom of the tank 1 is equipped with cooling water inlet and outlet valves 5 that are connected to the cooling pipes 4.
[0035] Through the above technical solution, the cooling pipe 4 is used to cool the tank 1 to prevent the tank 1 from being damaged due to excessive temperature in a high-pressure water environment. The cooling water inlet and outlet valves 5 are used to control the inflow and outflow of cooling water and regulate the temperature of the tank. Through the cooling system, the temperature of the tank 1 can be effectively controlled to ensure the smooth progress of the test and improve the safety of the tank 1.
[0036] The bottom of the tank 1 is fixedly connected to a support leg 6, and the bottom of the tank 1 is equipped with an inlet and outlet 7.
[0037] Through the above technical solution, the support leg 6 is used to support the tank body 1 and ensure the stability of the tank body 1. The inlet and outlet 7 is used to control the inflow and outflow of water, which facilitates water filling before the test, drainage after the test, and water circulation during the test. The support leg improves the stability of the tank body, and the inlet and outlet 7 facilitates water control and management, thereby improving the convenience and efficiency of the test.
[0038] An automatic exhaust port 8 is installed on the top of tank 1, and a temperature measuring gauge 9 is installed on the top of tank 1.
[0039] Through the above technical solution, the automatic exhaust port 8 is used to automatically exhaust air when water is injected into the tank 1 to prevent air accumulation from affecting the test results. The thermometer 9 is used to measure the temperature inside the tank 1, so that the test personnel can understand the temperature inside the tank at any time. The automatic exhaust port 8 ensures the accuracy of the test, and the thermometer 9 facilitates the test personnel to monitor and manage the temperature inside the tank 1.
[0040] A local pressure gauge 10 is installed on the top of tank 1, and a remote pressure gauge 3 is installed on the top of tank 1.
[0041] Through the above technical solution, the local pressure gauge 10 is used to directly display the pressure value inside the tank 1, which is convenient for the test personnel to observe at any time. The pressure remote transmission gauge 3 is used to transmit the pressure value inside the tank 1 to the control system or monitoring room to realize remote monitoring and management. The local pressure gauge 10 facilitates the test personnel to monitor the pressure inside the tank 1 in real time, and the pressure remote transmission gauge 3 realizes remote monitoring and management, which improves the safety and convenience of the test.
[0042] 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 may be made to these embodiments without departing from the principles and spirit, the scope of which is defined by the appended claims and their equivalents.
Claims
1. A high-pressure test tank structure, characterized in that, include: Tank (1) is used to house the propeller to be tested and provide a high-pressure water environment; A detachable sealing device is provided at the upper and lower ends of the tank (1) to seal the tank and allow repeated opening and closing for testing with different types of propellers, including an upper opening assembly and a lower opening assembly; The upper opening assembly includes a housing (11), a servo motor (12) is fixedly connected to the top of the housing (11), a turbine (13) is fixedly connected to the output shaft of the servo motor (12), a worm gear (14) is rotatably connected inside the housing (11), and an opening frame (15) is fixedly connected to one end of the worm gear (14). The lower opening assembly includes a lower bracket (16), a cylinder (17) is fixedly connected to the lower bracket (16), a sealing shell (18) is fixedly connected to the right side of the cylinder (17), a limit plate is fixedly connected to the lower bracket (16), a limit rod (19) is slidably inserted into the limit plate, and the right side of the limit rod (19) is fixedly connected to the sealing shell (18).
2. The high-pressure test tank structure according to claim 1, characterized in that: A sealing cap (2) is provided at the right end of the tank (1). The sealing cap (2) matches the opening shape of the tank (1). The top of the lower bracket (16) is fixedly connected to the tank (1). The bottom of the outer shell (11) is fixedly connected to the tank (1). One end of the opening bracket (15) is fixedly connected to the sealing cap (2).
3. The high-pressure test vessel structure according to claim 1, characterized in that: The tank (1) is made of high-strength, corrosion-resistant material to withstand the pressure in a high-pressure water environment and to prevent corrosion.
4. The high-pressure test vessel structure according to claim 1, characterized in that: The tank (1) is surrounded by a cooling pipe (4), and the bottom of the tank (1) is equipped with a cooling water inlet and outlet valve (5) that communicates with the cooling pipe (4).
5. The high-pressure test vessel structure according to claim 1, characterized in that: The bottom of the tank (1) is fixedly connected to a support leg (6), and the bottom of the tank (1) is equipped with an inlet and outlet (7).
6. The high-pressure test tank structure according to claim 1, characterized in that: An automatic exhaust port (8) is installed on the top of the tank (1), and a thermometer (9) is installed on the top of the tank (1).
7. The high-pressure test vessel structure according to claim 1, characterized in that: A local pressure gauge (10) is installed on the top of the tank (1), and a remote pressure gauge (3) is installed on the top of the tank (1).