A manned rocket composite energy harvesting and power generation system and method

Abstract

This invention relates to the field of rocket composite energy harvesting technology, specifically to a manned rocket composite energy harvesting and power generation system and method, including a harvesting module, a conversion module, a storage module, and a distribution module. During rocket launch, the harvesting module collects various forms of energy, the conversion module converts them into electrical energy, which is then stored in the storage module. The distribution module distributes the stored electrical energy to various systems or equipment of the rocket. By harvesting various forms of energy during rocket launch and converting them into electrical energy, energy utilization efficiency can be greatly improved and energy waste reduced. Utilizing the energy during rocket launch can reduce dependence on traditional energy sources, thereby reducing the cost of rocket launch. Compared to traditional rocket propulsion methods, manned rocket composite energy harvesting and power generation technology can reduce dependence on propellants, thereby reducing safety risks during rocket launch.

Description

Technical Field

[0001] This invention relates to the field of rocket composite energy harvesting technology, and in particular to a manned rocket composite energy harvesting and power generation system and method. Background Technology

[0002] A manned rocket is a type of rocket capable of sending humans into space and is an important tool for achieving manned spaceflight. Manned rockets typically consist of multiple stages that separate sequentially during launch and deliver the spacecraft into space upon reaching a predetermined altitude.

[0003] The propulsion of a manned rocket primarily relies on the thrust generated by its rocket engine. The rocket engine uses the reaction force of the high-speed ejected fuel to propel the rocket into the air. When the rocket fuel burns in the combustion chamber, it produces a large amount of high-temperature, high-pressure gas. This gas is ejected downwards through nozzles, generating a reaction force in the opposite direction of the gas ejection, thus providing the rocket with forward propulsion.

[0004] However, rockets require a large amount of fuel during launch and generate a large amount of heat and potential energy. The heat and potential energy generated by traditional rockets cannot be collected and utilized, resulting in energy waste. Summary of the Invention

[0005] The purpose of this invention is to provide a composite energy harvesting and power generation system and method for manned rockets, which solves the problem that the heat and potential energy generated by traditional rockets cannot be harvested and utilized, resulting in energy waste.

[0006] To achieve the above objectives, the present invention provides a manned rocket composite energy harvesting and power generation system, comprising a harvesting module, a conversion module, a storage module, and a distribution module, wherein the harvesting module is connected to the conversion module, the storage module is connected to the conversion module, and the distribution module is connected to the storage module; The collection module is used to collect various forms of energy during rocket launch; The conversion module is used to convert the collected energy into electrical energy; The storage module is used to store the converted electrical energy; The distribution module is used to distribute the stored electrical energy.

[0007] The manned rocket composite energy harvesting and power generation system also includes a management module, which is connected to the harvesting module, the conversion module, the storage module and the distribution module respectively. The management module is used to monitor, analyze and control the rocket's energy usage in real time, and to schedule and optimize energy according to actual needs.

[0008] The collection module includes a solar energy collection unit and a chemical energy collection unit. The solar energy collection unit is connected to the conversion module, and the chemical energy collection unit is connected to the conversion module. The solar energy collection unit is used to install solar panels on the outer surface of the rocket, collect solar energy during the rocket launch, and convert it into electrical energy through the conversion module. The chemical energy harvesting unit uses a fuel cell and converts chemical energy into electrical energy through the conversion module.

[0009] The collection module further includes a thermal energy acquisition unit, which is connected to the conversion module. The thermal energy harvesting unit is used to collect the thermal energy generated by burning propellant and the thermal energy generated by the operation of the fuel cell, and converts it into electrical energy through the conversion module.

[0010] The collection module further includes a motion mechanical energy acquisition unit, which is connected to the conversion module. The motion mechanical energy acquisition unit is used to collect the triboelectric and electrostatic induction effects generated by the surrounding environment and human movement, and convert them into electrical energy through the conversion module.

[0011] The collection module further includes a potential energy acquisition unit, which is connected to the conversion module. The potential energy harvesting unit is used to recover the potential energy of the rocket during launch and convert it into electrical energy through the conversion module.

[0012] A method for harvesting and generating electricity from composite energy in a manned rocket includes the following steps: During rocket launch, various forms of energy are collected; The collected energy is converted into electrical energy. The converted electrical energy is stored; The stored electrical energy is rationally allocated and transmitted to various systems or equipment of the rocket; The rocket's energy usage is monitored, analyzed, and controlled in real time, and energy is scheduled and optimized according to actual needs.

[0013] This invention discloses a manned rocket composite energy harvesting and power generation system and method. During rocket launch, the harvesting module collects various forms of energy, the conversion module converts them into electrical energy, which is then stored in the storage module. The distribution module distributes the stored electrical energy to various systems or equipment within the rocket. By harvesting various forms of energy during rocket launch and converting them into electrical energy, energy utilization efficiency can be greatly improved, and energy waste can be reduced. Utilizing energy during rocket launch reduces reliance on traditional energy sources, thereby lowering rocket launch costs. Compared to traditional rocket propulsion methods, manned rocket composite energy harvesting and power generation technology reduces reliance on propellants, thus lowering safety risks during rocket launch. It also allows the rocket to retain a certain amount of energy after launch, making it easier to achieve reusability. This contributes to reducing the cost of space exploration and improving its sustainability. Attached Figure Description

[0014] 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.

[0015] Figure 1 This is a structural block diagram of the manned rocket composite energy harvesting and power generation system according to the first embodiment of the present invention.

[0016] Figure 2 This is a structural block diagram of the collection module in the first embodiment of the present invention.

[0017] Figure 3 This is a flowchart illustrating the steps of a manned rocket composite energy harvesting and power generation method according to the second embodiment of the present invention.

[0018] In the diagram: 101-Collection module, 102-Conversion module, 103-Storage module, 104-Distribution module, 105-Management module, 106-Solar energy collection unit, 107-Chemical energy collection unit, 108-Thermal energy collection unit, 109-Motion mechanical energy collection unit, 110-Potential energy collection unit. Detailed Implementation

[0020] 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.

[0021] The first embodiment of this application is as follows: Please see Figure 1 and Figure 2 ,in, Figure 1This is a structural block diagram of the manned rocket composite energy harvesting and power generation system according to the first embodiment of the present invention. Figure 2 This is a structural block diagram of the collection module 101 according to the first embodiment of the present invention. The present invention provides a manned rocket composite energy collection and power generation system: including a collection module 101, a conversion module 102, a storage module 103, a distribution module 104, and a management module 105. The collection module 101 includes a solar energy collection unit 106, a chemical energy collection unit 107, a thermal energy collection unit 108, a kinetic mechanical energy collection unit 109, and a potential energy collection unit 110.

[0022] In this specific embodiment, the collection module 101 is connected to the conversion module 102, the storage module 103 is connected to the conversion module 102, and the allocation module 104 is connected to the storage module 103; The collection module 101 is used to collect various forms of energy during rocket launch; The conversion module 102 is used to convert the collected energy into electrical energy; The storage module 103 is used to store the converted electrical energy; The distribution module 104 is used to distribute the stored electrical energy.

[0023] During rocket launch, the collection module 101 collects various forms of energy, including heat energy generated by burning propellant, potential energy generated when the rocket reaches high speed, solar energy collected by solar panels, and chemical energy generated by fuel cells. The conversion module 102 converts the collected energy into electrical energy, including heat energy converted into electrical energy through a thermoelectric converter or thermal power generation system, solar panels converting solar energy into direct current, and fuel cells generating electrical energy through chemical reactions. The storage module 103 stores the converted electrical energy for subsequent use. The storage devices include batteries, supercapacitors, etc., and an appropriate storage method is selected according to the specific needs of the rocket. The distribution module 104 rationally distributes the stored electrical energy to various systems or equipment of the rocket, ensuring the safe, reliable, and efficient transmission of electrical energy to meet the needs of various rocket systems.

[0024] The management module 105 is connected to the collection module 101, the conversion module 102, the storage module 103 and the allocation module 104 respectively. The management module 105 is used to monitor, analyze and control the rocket's energy usage in real time, and to schedule and optimize energy according to actual needs.

[0025] The management module 105 monitors, analyzes, and controls the rocket's energy usage in real time, and schedules and optimizes energy according to actual needs to improve energy utilization and reliability.

[0026] Secondly, the solar energy collection unit 106 is connected to the conversion module 102, and the chemical energy collection unit 107 is connected to the conversion module 102; The solar energy collection unit 106 is used to install solar panels on the outer surface of the rocket, collect solar energy during the rocket launch process, and convert it into electrical energy through the conversion module 102. The chemical energy harvesting unit 107 uses a fuel cell and converts chemical energy into electrical energy through the conversion module 102.

[0027] The solar energy collection unit 106 is composed of solar panels. Solar panels are installed on the outer surface of the rocket to collect solar energy during rocket launch. The conversion module 102 converts solar energy into direct current. The chemical energy collection unit 107 is composed of fuel cells to convert chemical energy into electrical energy. During rocket launch, the fuel cells serve as auxiliary energy sources, providing continuous power support.

[0028] Meanwhile, the thermal energy acquisition unit 108 is connected to the conversion module 102; The thermal energy acquisition unit 108 is used to collect the thermal energy generated by burning propellant and the thermal energy generated by the operation of fuel cell, and convert it into electrical energy through the conversion module 102.

[0029] The thermal energy collection unit 108 includes a thermal energy collector. During rocket launch, thermal energy is collected by the collector and then converted into electrical energy by the thermal energy converter of the conversion module 102. This electrical energy is stored for later use.

[0030] In addition, the motion mechanical energy acquisition unit 109 is connected to the conversion module 102; The motion mechanical energy acquisition unit 109 is used to collect the triboelectric and electrostatic induction effects generated by the surrounding environment and human movement, and convert them into electrical energy through the conversion module 102.

[0031] The motion mechanical acquisition unit collects energy based on triboelectric nanogenerators, mainly through contact electrification and electrostatic induction. Specifically, when two materials with different electronegativity come into contact, electrostatic induction occurs due to the transfer of electrons during the contact or separation process. This process can collect a wide range of minute mechanical energy from the surrounding environment, such as the flow of air or water, the rotation of an engine, and subtle changes in pressure at a certain point in the human body. These minute mechanical energies are converted into electrical energy through triboelectric nanogenerators.

[0032] Finally, the potential energy acquisition unit 110 is connected to the conversion module 102; The potential energy harvesting unit 110 is used to recover the potential energy of the rocket during the launch process and convert it into electrical energy through the conversion module 102.

[0033] During launch, a rocket accumulates a significant amount of potential energy as its altitude increases. This potential energy primarily originates from the rocket's vertical position and the Earth's gravitational field. When the rocket reaches its predetermined altitude, the potential energy is converted into electrical energy by the potential energy harvesting unit 110. This unit 110 is a thermal energy converter. During ascent, the waste heat generated by the rocket's engines can be collected and converted into electrical energy. This conversion typically involves the thermoelectric effect, where a current is generated when two different conductors are connected with a temperature difference between their ends. Alternatively, it can utilize pressure difference to generate electricity. As the rocket ascends, its external pressure gradually decreases while its internal pressure remains relatively high. This pressure difference can be used to drive a turbine or piston engine, thereby converting potential energy into mechanical or electrical energy.

[0034] This embodiment of a manned rocket hybrid energy harvesting and power generation system collects various energy sources, including solar energy, chemical energy, thermal energy, potential energy, triboelectric induction, and electrostatic induction, through a collection module 101. These are then converted into electrical energy by a conversion module 102 and stored in a storage module 103. A distribution module 104 distributes the stored electrical energy to various systems or equipment within the rocket. By collecting various forms of energy during rocket launch and converting them into electrical energy, energy utilization efficiency is significantly improved, and energy waste is reduced. Utilizing the energy generated during rocket launch reduces reliance on traditional energy sources, thereby lowering launch costs. Compared to traditional rocket propulsion methods, manned rocket hybrid energy harvesting and power generation technology reduces propellant dependence, thus lowering safety risks during launch. It also allows the rocket to retain some energy after launch, making it more reusable. This contributes to reducing the cost of space exploration and improving its sustainability.

[0035] The second embodiment of this application is as follows: Based on the first embodiment, please refer to Figure 3 ,in, Figure 3 This is a flowchart illustrating the steps of a manned rocket hybrid energy harvesting and power generation method according to a second embodiment of the present invention. This embodiment of a manned rocket hybrid energy harvesting and power generation method includes the following steps: S201: Collects various forms of energy during rocket launch; S202: Convert the collected energy into electrical energy; S203: Store the converted electrical energy; S204: To rationally distribute the stored electrical energy and transmit it to the various systems or equipment of the rocket; S205: Real-time monitoring, analysis, and control of rocket energy usage, and energy scheduling and optimization based on actual needs.

[0036] Specifically, during rocket launch, various forms of energy are collected, including heat energy generated by propellant combustion, potential energy generated when the rocket reaches high speed, solar energy collected by solar panels, and chemical energy generated by fuel cells. The collected energy undergoes a conversion process to become electrical energy. This includes converting heat energy into electricity via thermoelectric converters or thermal power generation systems, solar panels converting solar energy into direct current, and fuel cells generating electricity through chemical reactions. The converted electrical energy needs to be stored for later use. Storage devices may include batteries, supercapacitors, etc., with appropriate storage methods selected based on the specific needs of the rocket. The stored electrical energy is then rationally allocated and transmitted to various systems or equipment within the rocket, ensuring safe, reliable, and efficient transmission to meet the needs of each system. To ensure the effective utilization and optimized management of composite energy, the management module 105 monitors, analyzes, and controls the rocket's energy usage in real time, scheduling and optimizing energy according to actual needs to improve energy utilization and reliability. By collecting heat energy, potential energy, and chemical energy during rocket launch and converting them into electrical energy, energy utilization efficiency can be greatly improved, and energy waste reduced. This helps reduce the cost of rocket launches and decreases reliance on traditional energy sources, aligning with sustainable development requirements. Utilizing clean energy sources such as solar power and fuel cells as a hybrid energy source can reduce the negative environmental impact of rocket launches, enhancing their environmental friendliness. Simultaneously, reducing reliance on propellants lowers safety risks and improves safety. Harvesting hybrid energy sources also makes rockets more reusable. After launch, residual energy can be recovered and stored for reuse in subsequent launches. This helps reduce the cost of space exploration and improve its sustainability.

[0037] 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 manned rocket composite energy harvesting and power generation system, characterized in that, It includes a collection module, a conversion module, a storage module, and an allocation module. The collection module is connected to the conversion module, the storage module is connected to the conversion module, and the allocation module is connected to the storage module. The collection module is used to collect various forms of energy during rocket launch; The conversion module is used to convert the collected energy into electrical energy; The storage module is used to store the converted electrical energy; The distribution module is used to distribute the stored electrical energy.

2. The manned rocket composite energy harvesting and power generation system as described in claim 1, characterized in that, The manned rocket composite energy harvesting and power generation system also includes a management module, which is connected to the harvesting module, the conversion module, the storage module and the distribution module respectively; The management module is used to monitor, analyze and control the rocket's energy usage in real time, and to schedule and optimize energy according to actual needs.

3. The manned rocket composite energy harvesting and power generation system as described in claim 1, characterized in that, The collection module includes a solar energy collection unit and a chemical energy collection unit. The solar energy collection unit is connected to the conversion module, and the chemical energy collection unit is connected to the conversion module. The solar energy collection unit is used to install solar panels on the outer surface of the rocket, collect solar energy during the rocket launch, and convert it into electrical energy through the conversion module. The chemical energy harvesting unit uses a fuel cell and converts chemical energy into electrical energy through the conversion module.

4. The manned rocket composite energy harvesting and power generation system as described in claim 3, characterized in that, The collection module further includes a thermal energy acquisition unit, which is connected to the conversion module. The thermal energy harvesting unit is used to collect the thermal energy generated by burning propellant and the thermal energy generated by the operation of the fuel cell, and converts it into electrical energy through the conversion module.

5. The manned rocket composite energy harvesting and power generation system as described in claim 1, characterized in that, The collection module further includes a motion mechanical energy acquisition unit, which is connected to the conversion module; The motion mechanical energy acquisition unit is used to collect the triboelectric and electrostatic induction effects generated by the surrounding environment and human movement, and convert them into electrical energy through the conversion module.

6. The manned rocket composite energy harvesting and power generation system as described in claim 1, characterized in that, The collection module further includes a potential energy acquisition unit, which is connected to the conversion module. The potential energy harvesting unit is used to recover the potential energy of the rocket during launch and convert it into electrical energy through the conversion module.

7. A method for harvesting and generating electricity from a manned rocket's composite energy, applicable to the manned rocket composite energy harvesting and power generation system as described in claim 1, characterized in that, Includes the following steps: During rocket launch, various forms of energy are collected; The collected energy is converted into electrical energy. The converted electrical energy is stored; The stored electrical energy is rationally allocated and transmitted to various systems or equipment of the rocket; The rocket's energy usage is monitored, analyzed, and controlled in real time, and energy is scheduled and optimized according to actual needs.

Images