Motor Weishi rocket engine three-view PD-3S rocket passive propeller power generation system and method

Abstract

The invention relates to the technical field of spaceflight rockets, in particular to a motor Weishi rocket engine three-view PD-3S rocket passive propeller power generation system and method, by arranging the passive propeller power generation system, a large amount of residual energy generated in the rocket launching process can be effectively recycled, and then the energy utilization efficiency is improved; in addition, due to the fact that the passive propeller power generation system does not need extra fuel, resources can be saved, environmental pollution can be reduced, the concept of sustainable development is met, meanwhile, the passive propeller power generation system has the advantages of being simple in structure, high in reliability, long in service life and the like, and therefore the passive propeller power generation system can work in various environments and has wide application prospects. In addition, the passive propeller power generation system can also be applied to other fields such as wind power generation and hydroelectric generation, jet flow energy of a rocket engine is used for driving a wind power generator or a hydroelectric generator to rotate, and energy conversion and utilization are achieved.

Description

Technical Field

[0001] This invention relates to the field of aerospace rocket technology, and in particular to a passive propeller power generation system and method for a Motor Sich rocket engine-based three-view PD-3S rocket. Background Technology

[0002] Human exploration of outer space and the strategic needs of various countries have driven the rapid development of aerospace vehicles. With the continuous development of science and technology, manned rocket technology has made great breakthroughs. Currently, manned rockets are usually used to transport astronauts to planetary orbits so that they can reach space.

[0003] Rocket engines are jet engines that utilize the impulse principle, carry their own propellant, and do not rely on external air. The most significant characteristic of rocket engines is that they carry both fuel and oxidizer, relying on the oxidizer for combustion. They do not need to draw oxygen from the surrounding atmosphere, so they can operate not only within the atmosphere but also in the vacuum of outer space. Currently, the propulsion devices used in artificial satellites, lunar spacecraft, and various spacecraft are all rocket engines.

[0004] Existing manned rockets generate a large amount of residual energy during launch, which is not recovered and utilized, thus reducing the energy efficiency of manned rockets. Therefore, it is necessary to develop a new type of passive propeller power generation system and method for rockets, so as to effectively recover and utilize the large amount of residual energy generated during rocket launch, thereby improving energy efficiency and having high practical application value. Summary of the Invention

[0005] The purpose of this invention is to provide a three-view Yao PD-3S rocket passive propeller power generation system and method for Motor Sich rocket engine, which solves the technical problem that existing manned rockets generate a large amount of residual energy during launch, which is not recovered and utilized, thereby reducing the energy utilization efficiency of manned rockets.

[0006] To achieve the above objectives, the present invention provides a passive propeller power generation system for the Motor Sich rocket engine's three-view PD-3S rocket, including a propeller, an intelligent control device, an energy storage device, a numerical simulation device, and a power generation device. The intelligent control device is used for real-time monitoring and precise control of each component of the system. The energy storage device is connected to the propeller and the intelligent control device, and is used to store and release residual energy. The numerical simulation device is connected to the intelligent control device, and is used to perform detailed modeling and analysis of the system. The power generation device is connected to the energy storage device and the intelligent control device, and is used to convert the kinetic energy of the propeller into electrical energy.

[0007] The Motor Sich rocket engine three-view PD-3S rocket passive propeller power generation system also includes an air intake pipe and an air exhaust pipe, which are respectively located at the front and rear of the power generation device. The propeller is connected to the power generation system via the energy storage device and the air intake pipe.

[0008] The air intake pipe and the air outlet pipe are both inclined, and the inclination angles of the air intake pipe and the air outlet pipe are the same.

[0009] The propeller is made of high-strength, lightweight materials or wear-resistant and high-temperature resistant materials.

[0010] The intelligent control device includes sensors and actuators. The sensors are used to monitor the various components of the system in real time, and the actuators are used to precisely control the various components of the system.

[0011] The power generation device includes an impeller, which is arranged in an arc-shaped plate.

[0012] This invention also provides a method for generating electricity using the passive propeller of a Motor Sich rocket engine with a three-view PD-3S rocket, comprising the following steps:

[0013] During rocket launch, the rocket jet generates a large amount of residual energy, which drives the propeller to rotate.

[0014] During the rotation of the propeller, the kinetic energy generated by the propeller is transferred to the energy storage device and stored therein.

[0015] Simultaneously with the rocket launch, sensors monitor the various components of the system in real time and transmit the monitoring results to a numerical simulation device.

[0016] The monitoring results are numerically simulated using the numerical simulation device to achieve detailed modeling and analysis of the system.

[0017] After analysis, the numerical simulation device transmits the analysis results to the actuator, allowing the actuator to precisely control each component of the system.

[0018] When electrical energy is needed, the energy stored in the energy storage device is transferred to the power generation device, which then converts the kinetic energy into electrical energy, thereby realizing the recovery and utilization of the remaining energy.

[0019] This invention discloses a passive propeller power generation system and method for the Motor Sich PD-3S rocket with a three-view design. By incorporating this passive propeller power generation system, the invention effectively recovers and utilizes the large amount of residual energy generated during rocket launch, thereby improving energy efficiency and demonstrating high practical application value. Furthermore, since the passive propeller power generation system does not require additional fuel, it saves resources, reduces environmental pollution, and aligns with the concept of sustainable development. Simultaneously, the passive propeller power generation system possesses advantages such as simple structure, high reliability, and long lifespan, enabling it to operate in various environments, including extreme conditions such as high and low temperatures and strong radiation. In addition, the passive propeller power generation system can also be applied to other fields, such as wind power generation and hydropower generation, utilizing the jet energy of the rocket engine to drive the rotation of wind or hydro generators, achieving energy conversion and utilization. Attached Figure Description

[0020] To more clearly illustrate the technical solutions in the embodiments of this application or the prior art, the accompanying drawings used in the description of the embodiments or the prior art will be briefly introduced below.

[0021] Figure 1 This is a schematic diagram of the overall structure of the Motor Sich rocket engine three-view PD-3S rocket passive propeller power generation system according to the first embodiment of the present invention.

[0022] Figure 2 This is a schematic diagram of the propeller blades of the first embodiment of the present invention.

[0023] Figure 3 This is a control principle diagram of the three-view Yao PD-3S rocket passive propeller power generation system of the Motor Sich rocket engine according to the first embodiment of the present invention.

[0024] Figure 4 This is a flowchart illustrating the power generation method of the three-view PD-3S rocket passive propeller of the Motor Sich rocket engine according to the second embodiment of the present invention.

[0025] In the diagram: 101-propeller, 102-intelligent control device, 103-energy storage device, 104-numerical simulation device, 105-power generation device, 106-intake pipe, 107-outtake pipe, 108-sensor, 109-actuator, 110-blade, 111-impeller, 112-hyperbolic convex guide edge, 113-hyperbolic concave follow edge, 114-circumferential arc edge. Detailed Implementation

[0026] The embodiments of the present invention are described in detail below. Examples of the embodiments are shown in the accompanying drawings. The embodiments described below with reference to the accompanying drawings are exemplary and intended to explain the present invention, but should not be construed as limiting the present invention.

[0027] First embodiment:

[0028] Please see Figures 1 to 3 ,in Figure 1 This is a schematic diagram of the overall structure of the Motor Sich rocket engine three-view Yao PD-3S rocket passive propeller power generation system according to the first embodiment of the present invention. Figure 2 This is a schematic diagram of the structure of the blade 110 of the propeller 101 according to the first embodiment of the present invention. Figure 3 This is a control principle diagram of the passive propeller power generation system of the Motor Sich rocket engine three-view PD-3S rocket according to the first embodiment of the present invention. The present invention provides a passive propeller power generation system of the Motor Sich rocket engine three-view PD-3S rocket, including a propeller 101, an intelligent control device 102, an energy storage device 103, a numerical simulation device 104, a power generation device 105, an air intake pipe 106, and an air exhaust pipe 107.

[0029] In this embodiment, the present invention effectively recovers and utilizes the large amount of residual energy generated during rocket launch by setting up a passive propeller power generation system, thereby improving energy utilization efficiency and having high practical application value. In addition, since the passive propeller power generation system does not require additional fuel, it can save resources, reduce environmental pollution, and conform to the concept of sustainable development. At the same time, the passive propeller power generation system has the advantages of simple structure, high reliability, and long service life, so it can work in various environments, including extreme conditions such as high and low temperatures and strong radiation. In addition, the passive propeller power generation system can also be applied to other fields, such as wind power generation and hydropower generation, using the jet energy of the rocket engine to drive the rotation of wind or hydro generators to realize energy conversion and utilization.

[0030] The intelligent control device 102 is used to monitor and precisely control the various components of the system in real time. The energy storage device 103 is connected to the propeller 101 and the intelligent control device 102, and is used to store and release the remaining energy. The numerical simulation device 104 is connected to the intelligent control device 102, and is used to perform detailed modeling and analysis of the system. The power generation device 105 is connected to the energy storage device 103 and the intelligent control device 102, and is used to convert the kinetic energy of the propeller 101 into electrical energy.

[0031] Secondly, the Motor Sich rocket engine three-view PD-3S rocket passive propeller power generation system also includes an air intake pipe 106 and an air exhaust pipe 107. The air intake pipe 106 and the air exhaust pipe 107 are respectively arranged at the front and rear of the power generation device 105. The propeller 101 is connected to the power generation system via the energy storage device 103 and the air intake pipe 106. The air intake pipe 106 and the air exhaust pipe 107 are both inclined, and the inclination angles of the air intake pipe 106 and the air exhaust pipe 107 are the same. This allows the kinetic energy generated by the propeller 101 to be transferred to the energy storage device 103, and then from the energy storage device 103 and the air intake pipe 106 to the power generation system for power generation.

[0032] Furthermore, the propeller 101 is made of high-strength lightweight materials or wear-resistant and high-temperature resistant materials. At the same time, the power generation system is also made of high-strength lightweight materials or wear-resistant and high-temperature resistant materials, which enables it to withstand the high temperature and high pressure environment of the rocket jet, thereby improving the performance and lifespan of the system.

[0033] Meanwhile, the propeller 101 has blades 110. The blade surface profile of the blade 110 is formed by a hyperbolic convex guide edge 112, a hyperbolic concave follow edge 113, and a circumferential arc edge 114. The inner cross-section of the blade 110 is circular, and the outer cross-section is an ellipse with a gradually increasing major axis and a gradually decreasing minor axis. The blade surface profile of the propeller 101 is formed by a hyperbolic convex guide edge 112, a hyperbolic concave follow edge 113, and a circumferential arc edge 114. The inner cross-section of the blade 110 is circular, and the outer cross-section is an ellipse with a gradually increasing major axis and a gradually decreasing minor axis. The inner cross-section is circular, while the outer cross-section is an ellipse with the major axis gradually increasing and the minor axis gradually decreasing. The short chord length design on the inner side allows the blade 110 of the propeller 101 to have a slightly wider width, thereby ensuring smooth air intake and exhaust, preventing vortices, and reducing cavitation formation. By increasing the arc chord length on the outer side of the propeller 101, the disk area of ​​the propeller 101 can be increased without increasing the diameter of the propeller 101, which in turn helps to improve the efficiency of the propeller 101.

[0034] In addition, the intelligent control device 102 includes a sensor 108 and an actuator 109. The sensor 108 is used to monitor the various components of the system in real time, and the actuator 109 is used to precisely control the various components of the system.

[0035] Finally, the power generation device 105 is equipped with an impeller 111, which is arranged in an arc-shaped plate to increase the kinetic energy generated by the impeller 111. The power generation device 105 is connected to an electric motor, which can convert the kinetic energy generated by the impeller 111 into electrical energy.

[0036] When using the Motor Sich rocket engine three-view Yao PD-3S rocket passive propeller power generation system of this embodiment, during rocket launch, the rocket generates a large amount of residual energy during the jet stream. This residual energy drives the propeller 101 to rotate. During the rotation of the propeller 101, the kinetic energy generated by the propeller 101 is transferred to the energy storage device 103 and stored there. At the same time as the rocket launch, the sensors 108 monitor the various components of the system in real time and transmit the monitoring results to the numerical simulation. The device 104 then performs numerical simulation on the monitoring results, thereby enabling detailed modeling and analysis of the system. After analysis, the numerical simulation device 104 transmits the analysis results to the actuator 109, allowing the actuator 109 to precisely control each component of the system. When electrical energy is needed, the energy stored in the energy storage device 103 is transmitted to the power generation device 105, enabling the power generation device 105 to gradually convert kinetic energy into electrical energy, thereby realizing the recovery and utilization of a large amount of residual energy generated by the rocket during the jet.

[0037] This invention utilizes the proprietary algorithm of Motor Sich Hubei Sanshi Yao PD-3S rocket engine to establish an advanced power generation system for a rocket passive propeller. The method includes: intelligent control technology, energy storage technology, materials science, numerical simulation and system integration, reliability technology, etc.

[0038] With the development of artificial intelligence and sensor 108 technology, through intelligent control technology and proprietary algorithms, as well as the installation of advanced sensors 108 and actuators 109, real-time monitoring and precise control of various components of the system can be achieved, thereby improving the stability and efficiency of the system. Ultimately, remote monitoring and management of the power generation system of the rocket's passive propeller can be realized, thereby improving the system's operating efficiency and safety.

[0039] With the development of energy storage technologies such as batteries and supercapacitors, they have become one of the important technologies in rocket passive propeller power generation systems. By selecting efficient energy storage technologies, the storage and release of surplus energy can be realized, thereby improving energy utilization efficiency.

[0040] The development of materials science has provided new solutions for the power generation system of rocket passive propellers. By developing high-temperature and high-strength materials, it is possible to withstand the high-temperature and high-pressure environment of rocket jets. At the same time, the manufacturing process is also very advanced. By adopting new materials such as high-strength lightweight materials and wear-resistant and high-temperature resistant materials, the performance and life of the system have been improved.

[0041] The development of numerical simulation technology has provided strong support for the design and optimization of the power generation system of rocket passive propellers. Through numerical simulation, detailed modeling and analysis of the system have been achieved, the performance and behavior of the system can be accurately predicted, and the quality and efficiency of the design can be improved. At the same time, through in-depth research on the integration and verification of the rocket passive propeller power generation system, a complete testing and verification process has been developed to verify the performance, reliability and safety of the system.

[0042] With the increasing application of rocket passive propeller power generation systems under extreme conditions, reliability technology has become one of the key technologies. By adopting highly reliable materials and devices and formulating reasonable maintenance and repair strategies, the reliability and lifespan of the system can be improved. Through in-depth research on the reliability and maintenance of rocket passive propeller power generation systems, the developed maintenance strategies and reliability technologies can ensure the long-term stable operation of the system.

[0043] This invention utilizes the three-system coordinates of the Motor Sich rocket engine on the PD-3S rocket, along with technologies such as rocket jet energy-driven generator sets, passive propeller 101 technology, and efficient energy conversion and storage technology, to provide efficient, environmentally friendly, and reliable power resources. This provides the thrust required for rocket attitude adjustment and orbital maneuvering, as well as other uses, and has significant practical significance and application value.

[0044] In summary, this invention, by setting up a passive propeller power generation system, can effectively recover and utilize the large amount of residual energy generated during rocket launch, thereby improving energy utilization efficiency and possessing high practical application value. Furthermore, since the passive propeller power generation system does not require additional fuel, it can save resources, reduce environmental pollution, and align with the concept of sustainable development. Simultaneously, the passive propeller power generation system has advantages such as simple structure, high reliability, and long lifespan, allowing it to operate in various environments, including extreme conditions such as high and low temperatures and strong radiation. In addition, the passive propeller power generation system can also be applied to other fields, such as wind power generation and hydropower generation, utilizing the jet energy of the rocket engine to drive the rotation of wind or hydroelectric generators, achieving energy conversion and utilization.

[0045] Second embodiment:

[0046] Based on the first embodiment, please refer to Figure 4 , Figure 4 This is a flowchart illustrating the power generation method of the passive propeller of the Motor Sich rocket engine three-view Yao PD-3S rocket according to the second embodiment of the present invention. The present invention also provides a power generation method of the passive propeller of the Motor Sich rocket engine three-view Yao PD-3S rocket, comprising the following steps:

[0047] S101. During the rocket launch process, the rocket jet will generate a large amount of residual energy, which will drive the propeller 101 to rotate.

[0048] S102. During the rotation of the propeller 101, the kinetic energy generated by the propeller 101 is transferred to the energy storage device 103 and stored in the energy storage device 103.

[0049] S103. At the same time as the rocket is launched, the system components are monitored in real time by sensor 108 and the monitoring results are transmitted to numerical simulation device 104.

[0050] S104. The monitoring results are numerically simulated using the numerical simulation device 104 to achieve detailed modeling and analysis of the system;

[0051] S105. After analysis, the numerical simulation device 104 transmits the analysis results to the actuator 109, so that the actuator 109 can precisely control each component of the system.

[0052] S106. When electrical energy is needed, the energy stored in the energy storage device 103 is transferred to the power generation device 105, so that the power generation device 105 converts kinetic energy into electrical energy, thereby realizing the recycling of the remaining energy.

[0053] When using the passive propeller power generation method of the Motor Sich rocket engine three-view Yao PD-3S rocket according to this embodiment, during rocket launch, the rocket generates a large amount of residual energy during the jet. This residual energy drives the propeller 101 to rotate. During the rotation of the propeller 101, the kinetic energy generated by the propeller 101 is transferred to the energy storage device 103 and stored therein. At the same time as the rocket launch, the sensors 108 monitor the various components of the system in real time and transmit the monitoring results to the numerical simulation. The device 104 then performs numerical simulation on the monitoring results, thereby enabling detailed modeling and analysis of the system. After analysis, the numerical simulation device 104 transmits the analysis results to the actuator 109, allowing the actuator 109 to precisely control each component of the system. When electrical energy is needed, the energy stored in the energy storage device 103 is transmitted to the power generation device 105, enabling the power generation device 105 to gradually convert kinetic energy into electrical energy, thereby realizing the recovery and utilization of a large amount of residual energy generated by the rocket during the jet.

[0054] The above-disclosed embodiments are merely one or more preferred embodiments of this application and should not be construed as limiting the scope of this application. Those skilled in the art can understand that all or part of the processes for implementing the above embodiments and equivalent changes made in accordance with the claims of this application still fall within the scope of this application.

Claims

1. A passive propeller power generation system for a Motor Sich rocket engine-based three-view Yao PD-3S rocket, comprising a propeller, characterized in that, It also includes an intelligent control device, an energy storage device, a numerical simulation device, and a power generation device. The intelligent control device is used to monitor and precisely control each component of the system in real time. The energy storage device is connected to the propeller and the intelligent control device to store and release residual energy. The numerical simulation device is connected to the intelligent control device to perform detailed modeling and analysis of the system. The power generation device is connected to the energy storage device and the intelligent control device to convert the kinetic energy of the propeller into electrical energy.

2. The Motor Sich rocket engine three-view PD-3S rocket passive propeller power generation system as described in claim 1, characterized in that, The Motor Sich rocket engine three-view PD-3S rocket passive propeller power generation system also includes an air intake pipe and an air exhaust pipe, which are respectively located at the front and rear of the power generation device. The propeller is connected to the power generation system via the energy storage device and the air intake pipe.

3. The Motor Sich rocket engine three-view PD-3S rocket passive propeller power generation system as described in claim 2, characterized in that, Both the air intake pipe and the air outlet pipe are inclined, and the inclination angles of the air intake pipe and the air outlet pipe are the same.

4. The Motor Sich rocket engine three-view PD-3S rocket passive propeller power generation system as described in claim 1, characterized in that, The propeller is made of high-strength, lightweight materials or wear-resistant and high-temperature resistant materials.

5. The Motor Sich rocket engine three-view PD-3S rocket passive propeller power generation system as described in claim 1, characterized in that, The intelligent control device includes sensors and actuators. The sensors are used to monitor the various components of the system in real time, and the actuators are used to precisely control the various components of the system.

6. The Motor Sich rocket engine three-view Yao PD-3S rocket passive propeller power generation system as described in claim 1, characterized in that, The power generation device is equipped with an impeller, which is arranged in an arc-shaped plate.

7. A method for generating electricity using a passive propeller of a Motor Sich rocket engine-based three-view Yao PD-3S rocket, applied to the passive propeller power generation system of a Motor Sich rocket engine-based three-view Yao PD-3S rocket as described in any one of claims 1 to 6, characterized in that, Includes the following steps: During rocket launch, the rocket jet generates a large amount of residual energy, which drives the propeller to rotate. During the rotation of the propeller, the kinetic energy generated by the propeller is transferred to the energy storage device and stored therein. Simultaneously with the rocket launch, sensors monitor the various components of the system in real time and transmit the monitoring results to a numerical simulation device. The monitoring results are numerically simulated using the numerical simulation device to achieve detailed modeling and analysis of the system. After analysis, the numerical simulation device transmits the analysis results to the actuator, allowing the actuator to precisely control each component of the system. When electrical energy is needed, the energy stored in the energy storage device is transferred to the power generation device, which then converts the kinetic energy into electrical energy, thereby realizing the recovery and utilization of the remaining energy.

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