Self-protection equipment of water spraying noise reduction system
By designing a water storage tank and water spray pipeline in the water spray noise reduction system, and utilizing cooling water injection and water curtain protection valves, the self-protection problem of the water spray noise reduction system during rocket launch was solved, thus achieving system safety and extending service life.
Patent Information
- Application Number
- CN202520269706.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-02-20
- Publication Date
- 2025-12-12
- Estimated Expiration
- 2035-02-20
AI Technical Summary
The valves and other components of the water spray noise reduction system are easily burned and blown away by the rocket's exhaust flow during rocket launch, lacking self-protection.
A self-protection device for a water spray noise reduction system was designed, including a water tank, main pipeline, water spray pipeline and protective water spray supply pipeline. Cooling water is sprayed through secondary nozzles to cool down and form a water curtain to protect valves and other components. The protective water spray supply pipeline protects the system.
It effectively protects the valves and other components of the water spray noise reduction system, preventing them from burning and being blown away, extending the system's service life, while achieving cooling and noise reduction effects.
Smart Images
Figure CN223665178U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to rocket launching technology field, especially relate to a self -protection equipment of water spray noise reduction system. BACKGROUND
[0002] In the process of launching rocket ignition, the high temperature and high pressure gas flow produced by rocket will cause great damage to launching platform and surrounding launching facilities, and the noise produced by launching will also cause damage to satellite, in order to solve these problems, the launching site is equipped with water spray noise reduction system, reduces the temperature and noise when launching, to protect the safety of launching facilities and satellite products.
[0003] However, the water spray noise reduction system solves the protection safety of other systems, however, the valve and other parts of its own system are in the launching environment, easy to be ablated and blown by rocket gas flow, the self-protection problem of water spray noise reduction system has not been solved. Therefore, a self-protection equipment of water spray noise reduction system for solving the above problems is proposed. UTILITY MODEL CONTENT
[0004] The utility model discloses a self-protection equipment of water spray noise reduction system, solve the valve and other parts of water spray noise reduction system's own system are in the launching environment, easy to be ablated and blown by rocket gas flow technical problem.
[0005] In order to achieve the above object, the utility model provides a self-protection equipment of water spray noise reduction system, comprising:
[0006] Launching platform;
[0007] Water accumulator, set up in the circumferential outside of launching platform, the top surface of water accumulator array is equipped with several secondary nozzles, and the secondary nozzles are used to spray cooling water to launching platform;
[0008] Main pipeline, set up below water accumulator, and the main pipeline is connected with water accumulator through several secondary water supply pipelines;
[0009] Water spray pipeline is connected with main pipeline through protection water spray water supply pipeline, and the water spray pipeline is horizontally arranged on the upper part of secondary water supply pipeline.
[0010] Preferably, the lower part of the secondary water supply pipeline is provided with a first control valve and a valve actuator, and the first control valve and the valve actuator are arranged below the water spray pipeline.
[0011] Preferably, a second control valve is arranged on the main pipeline, and the second control valve is used to control the on-off of the main pipeline.
[0012] Preferably, a third control valve is arranged on the protective water spraying water supply pipeline, and the third control valve is used for controlling the opening and closing of the protective water spraying water supply pipeline.
[0013] Preferably, a plurality of protective water spraying nozzles are arranged below the water spraying pipeline, and the protective water spraying nozzles are used for downwardly scattering water.
[0014] Preferably, a flow sensor is arranged in the secondary water supply pipeline and below the water spraying pipeline.
[0015] Preferably, a filter is arranged at a connection position of the secondary water supply pipeline and the water accumulator.
[0016] Preferably, a liquid level sensor is arranged in the water accumulator.
[0017] With respect to the above background, the self-protection device of the water spraying noise reduction system has the following beneficial effects: after the rocket ignition signal is sent, the water accumulator sprays cooling water to the launching platform through the secondary nozzle, the cooling water cools the high-temperature and high-pressure gas flow generated during the rocket launching, the vaporized water vapor molecules block the propagation of noise, and the purpose of noise reduction is achieved. At the same time, the water spraying pipeline sprays water for protection, isolates the high-temperature and high-pressure gas flow generated during the rocket launching, protects the valves and other components on the secondary water supply pipeline, prevents the water spraying noise reduction system from being ablated and blown out, achieves the purpose of protecting the water spraying noise reduction system, ensures the safety of the water spraying noise reduction system, and further prolongs the service life of the water spraying noise reduction system. BRIEF DESCRIPTION OF DRAWINGS
[0018] In order to more clearly illustrate the technical solutions in the embodiments of the present application or the prior art, the following will briefly introduce the drawings needed to be used in the embodiments or the prior art description. Obviously, the drawings in the following description are only embodiments of the present application, and other drawings can be obtained by those skilled in the art without creative labor on the basis of the provided drawings.
[0019] Figure 1 The working principle diagram of the self-protection device of the water spraying noise reduction system provided by the embodiments of the present application.
[0020] Specifically, 1 is a water accumulator, 2 is a secondary nozzle, 3 is a main pipeline, 4 is a secondary water supply pipeline, 401 is a first control valve, 402 is a first valve actuator, 5 is a water spraying pipeline, 6 is a protective water spraying water supply pipeline, 601 is a third control valve, 602 is a second valve actuator, 7 is a protective water spraying nozzle, 8 is a first pressure sensor, 9 is a second pressure sensor, and 10 is a third pressure sensor. DETAILED DESCRIPTION
[0021] With reference to the drawings of the embodiments of the present application, the technical solutions in the embodiments of the present application will be described clearly and completely. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all the embodiments. Based on the embodiments of the present application, all other embodiments obtained by those skilled in the art without creative work are within the scope of the present application.
[0022] In order for those skilled in the art to better understand the technical solutions of the present application, the present application will be further described in detail below with reference to the drawings and specific embodiments.
[0023] As Figure 1 shown, in order to achieve the above-mentioned purpose, the present application provides a self-protection equipment of a water-spraying noise reduction system, comprising: a water accumulator 1, a main pipeline 3 and a water-spraying pipeline 5.
[0024] The water accumulator 1 is arranged on the circumferential outer side of a launching platform (not shown in the figure), a certain amount of cooling water is stored in the water accumulator 1, and a plurality of secondary nozzles 2 are arranged on the top surface of the water accumulator 1, the secondary nozzles 2 are directed to the launching platform, and the cooling water is sprayed to the launching platform through the secondary nozzles 2, so as to reduce the temperature and noise during the launching of the rocket.
[0025] The main pipeline 3 is arranged below the water accumulator 1, the main pipeline 3 is connected to the water accumulator 1 through a plurality of secondary water supply pipelines 4, preferably, four secondary water supply pipelines 4 are arranged, and the main pipeline 3 supplies water to the water accumulator 1 through the secondary water supply pipelines 4. It should be noted that before the launching of the rocket, the inside of the water accumulator 1 is in a full water state, at this time, the main pipeline 3 stops supplying water to the water accumulator 1.
[0026] The water-spraying pipeline 5 is connected to the main pipeline 3 through a protection water-spraying water supply pipeline 6, the water-spraying pipeline 5 is horizontally arranged on the upper part of the secondary water supply pipeline 4, after the rocket ignition signal is sent, the cooling water in the main pipeline 3 is delivered to the water-spraying pipeline 5 through the protection water-spraying water supply pipeline 6, the protection water-spraying is carried out through the water-spraying pipeline 5, the valve and other components on the secondary water supply pipeline 4 are protected, and the safety of the water-spraying noise reduction system is ensured.
[0027] In use, in the initial state, the main pipeline 3 is in the closed state, after the rocket ignition signal is sent, the main pipeline 3 is controlled to be opened, under the action of the pressure of the main pipeline 3, the water accumulator 1 sprays cooling water to the launching platform through the secondary nozzle 2, the cooling water cools the high-temperature and high-pressure gas flow generated during the launching of the rocket, the water vapor molecules of the gasified water block the propagation of the noise, so that the purpose of noise reduction is achieved, at the same time, the main pipeline 3 supplies water to the water spraying pipeline 5 through the protective water spraying supply pipeline 6, the water spraying pipeline 5 sprays water to protect the water spraying noise reduction system, and the valve and other components on the secondary water supply pipeline 4 are protected, while the water spraying noise reduction system reduces the temperature and noise during the launching of the rocket, the water spraying noise reduction system can be protected, the safety of the water spraying noise reduction system is ensured, and the service life of the water spraying noise reduction system is prolonged.
[0028] In one embodiment of the utility model, the lower part of the secondary water supply pipeline 4 is equipped with a first control valve 401 and a first valve actuator 402, the first control valve 401 can control the on-off of the secondary water supply pipeline 4, and the first valve actuator 402 can control the opening of the first control valve 401, both the first control valve 401 and the first valve actuator 402 are arranged below the water spraying pipeline 5, so as to facilitate manual control and maintenance by the staff.
[0029] In addition, a second control valve (not shown in the figure) is arranged on the main pipeline 3, the second control valve can control the on-off of the main pipeline 3, wherein the second control valve adopts a pneumatic butterfly valve, the valve stem is driven by compressed air through the pneumatic butterfly valve, and the on-off can be completed by controlling the rotation of the butterfly plate by 90 degrees, so that the on-off of the main pipeline 3 can be accurately controlled.
[0030] In one embodiment of the utility model, a plurality of protective water spraying nozzles 7 are arranged in an array below the water spraying pipeline 5, the protective water spraying nozzles 7 scatter water downward, and the cooling water after being sprayed forms a downward water curtain, isolates the high-temperature and high-pressure gas flow generated during the launching of the rocket, protects the valve and other components on the secondary water supply pipeline 4, prevents the water spraying noise reduction system from being ablated and blown out, and further enhances the protection effect of the water spraying noise reduction system itself.
[0031] At the same time, a flow sensor is arranged in the secondary water supply pipeline 4, the flow sensor is arranged below the water spraying pipeline 5, the water flow in the secondary water supply pipeline 4 can be monitored in real time through the flow sensor, so that the opening of the first control valve 401 is adjusted by the first valve actuator 402 according to the demand, so that the water accumulator 1 can continuously supply water to the secondary nozzle 2, and the continuous cooling and noise reduction effect of the water spraying noise reduction system is ensured.
[0032] The third control valve 601 is arranged on the protective water spraying water supply pipeline 6, and the third control valve 601 can control the opening and closing of the protective water spraying water supply pipeline 6. In the initial state, the third control valve 601 is in the closed state. When the rocket is not launched, the main pipeline 3 supplies water to the water accumulator 1 through the secondary water supply pipeline 4, and the protective water spraying water supply pipeline 6 does not supply water to the water spraying pipeline 5. To ensure that the water spraying pipeline 5 can normally supply water to the water spraying pipeline 5 when the rocket is launched, the second valve actuator 602 is arranged in the protective water spraying water supply pipeline 6. When the rocket ignition signal is sent, the second valve actuator 602 controls the third control valve 601 to open, the protective water spraying water supply pipeline 6 supplies water to the protective water spraying nozzle 7, and the water curtain is formed by the downward scattering of the water through the protective water spraying nozzle 7, so as to achieve the purpose of isolating the high-temperature and high-pressure gas flow generated when the rocket is launched. In addition, after the water spraying pipeline 5 continuously sprays cooling water through the protective water spraying nozzle 7 for a certain period of time, the rocket flies away from the launch area, and then the third control valve 601 is controlled to be closed by the second valve actuator 602, so that the protective function of the water spraying noise reduction system is no longer needed.
[0033] To ensure that the cooling water in the water accumulator 1 can be smoothly sprayed from the secondary nozzle 2, a filter is arranged at the connection position of the secondary water supply pipeline 4 and the water accumulator 1. Before the cooling water in the secondary water supply pipeline 4 enters the water accumulator 1, the filter can filter the impurities in the cooling water, so as to avoid that the impurities in the secondary water supply pipeline 4 or the main pipeline 3 are brought into the inside of the water accumulator 1 by the cooling water, thereby preventing the secondary nozzle 2 from being blocked due to long-term deposition of the impurities, and further ensuring that the cooling water in the water accumulator 1 can be smoothly sprayed from the secondary nozzle 2.
[0034] It should be noted that, to further ensure that the water accumulator 1 can continuously supply water to the secondary nozzle 2, a liquid level sensor is arranged in the inside of the water accumulator 1. The liquid level sensor can monitor the liquid level of the cooling water in the water accumulator 1 in real time. Meanwhile, a water inflow level line and a water stop level line are preset in the water accumulator 1. When the liquid level of the cooling water in the water accumulator 1 is lower than the water inflow level line, the cooling water is added to the water accumulator 1 through the water supply pipeline, so as to avoid interruption of the water spraying of the secondary nozzle 2 at the moment of launching the rocket, and ensure the noise reduction effect when the rocket is launched. When the liquid level of the cooling water in the water accumulator 1 is higher than the water stop level line, the cooling water is stopped from being added to the water accumulator 1 through the water supply pipeline, so as to prevent the cooling water in the water accumulator 1 from overflowing.
[0035] In one embodiment of the utility model, in order to ensure that the secondary nozzle 2 normally sprays cooling water, first pressure sensor 8 can be selected to be arranged in main pipeline 3, the water pressure at the position of main pipeline 3 is monitored in real time through first pressure sensor 8, when the water pressure of main pipeline 3 is too low to normally supply water, timely maintenance and processing can be carried out, to ensure that main pipeline 3 normally supplies water to water accumulator 1. Second pressure sensor 9 is arranged in the inside of water accumulator 1, the water pressure in water accumulator 1 is monitored in real time through second pressure sensor 9, to ensure that water accumulator 1 can normally supply water to secondary nozzle 2. Third pressure sensor 10 is arranged in secondary nozzle 2, the water pressure at the position of secondary nozzle 2 is monitored in real time through third pressure sensor 10, when secondary nozzle 2 is blocked, timely discovery and processing can be carried out, to ensure that secondary nozzle 2 normally sprays cooling water.
[0036] The utility model discloses a working principle: initial state, first control valve 401, second control valve and third control valve 601 are all in the closed state, after the rocket ignition signal is sent, control opens first control valve 401 and second control valve, under the pressure of main pipeline 3, water accumulator 1 sprays cooling water to the launching platform through secondary nozzle 2, and the cooling water is cooled to the high-temperature high-pressure gas flow generated by the rocket, and the water vapor molecule is blocked to the propagation of noise, to achieve the purpose of noise reduction, simultaneously, second valve actuator 602 controls and opens third control valve 601, and main pipeline 3 supplies water to water spraying pipeline 5 through protective water spraying water supply pipeline 6, and water spraying pipeline 5 scatters water downward through protective water spraying nozzle 7, and the cooling water after spraying forms a downward water curtain, and the high-temperature high-pressure gas flow generated during the rocket launching is isolated, and the valve and other parts on secondary water supply pipeline 4 are protected, to prevent the water spraying noise reduction system from being ablated and blown.
[0037] Summarizing above, when water accumulator 1 sprays cooling water to the launching platform through secondary nozzle 2, the temperature and noise during the rocket launching are reduced, and main pipeline 3 supplies water to water spraying pipeline 5 through protective water spraying water supply pipeline 6, to protect the water spraying noise reduction system itself, to ensure the safety of the water spraying noise reduction system, and to prolong the service life of the water spraying noise reduction system.
[0038] It should be noted that in the present specification, relational terms such as first and second are used solely to distinguish one entity from another entity, without necessarily requiring or implying any actual such relationship or order between such entities.
[0039] The principle and implementation mode of the present application are described by using specific examples in the present application, and the above examples are only used to help understand the method and core idea of the present application. It should be pointed out that, for ordinary skilled persons in the technical field, some improvements and modifications can be made to the present application without departing from the principle of the present application, and these improvements and modifications also fall within the protection scope of the present application.
Claims
1. A self-protection device for a water injection noise reduction system, characterized in that, The utility model relates to a kind of water conservancy facilities, including: Launch platform; Water reservoir is arranged in the circumferential outside of the launch platform, the top surface of the water reservoir is arrayed with several secondary nozzles, and the secondary nozzles are used to spray cooling water to the launch platform; Main pipeline is arranged below the water reservoir, and the main pipeline is connected with the water reservoir by several secondary water supply pipelines; Water spraying pipeline is connected with the main pipeline by protective water spraying water supply pipeline, and the water spraying pipeline is horizontally arranged in the upper portion of the secondary water supply pipeline.
2. A self-protection device for a water injection noise reduction system according to claim 1, characterized in that, The lower portion of the secondary water supply pipeline is provided with a first control valve and a valve actuator, and the first control valve and the valve actuator are arranged below the water spraying pipeline.
3. A self-protecting apparatus of a water-jet noise reduction system according to claim 2, wherein, A second control valve is arranged on the main pipeline, and the second control valve is used to control the on-off of the main pipeline.
4. A self-protecting apparatus of a water-jet noise reduction system according to claim 3, wherein, A third control valve is arranged on the protective water spraying water supply pipeline, and the third control valve is used to control the on-off of the protective water spraying water supply pipeline.
5. A self-protecting apparatus of a water-jet noise reduction system according to claim 2, wherein, Several protective water spraying nozzles are arranged below the water spraying pipeline, and the protective water spraying nozzles are used to scatter water downward.
6. A self-protecting apparatus of a water-jet noise reduction system according to claim 1, wherein, A flow sensor is arranged in the secondary water supply pipeline, and the flow sensor is arranged below the water spraying pipeline.
7. A self-protecting apparatus of a water-jet noise reduction system according to claim 1, wherein, A filter is arranged at the connection position of the secondary water supply pipeline and the water reservoir.
8. A self-protecting apparatus of a water-jet noise reduction system according to claim 1, wherein, A liquid level sensor is arranged in the water reservoir.