Marine ternary solid-liquid propellant rocket protection equipment
A protective equipment and propellant technology, which is applied in the direction of mechanical equipment, jet propulsion devices, rocket engine devices, etc., can solve problems such as lack, and achieve the effect of improving energy characteristics and high safety factor
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0015] Example 1: Such as figure 1 As shown, a marine ternary solid-liquid propellant rocket protection device with protection function includes an injector 1, a combustion chamber 2, a control system 3, a supply system 4, a nozzle 5, and a storage tank 6, and is characterized in that: The injector 1 is connected to the combustion chamber 2 and the storage tank 6, the combustion chamber 2 is filled with solid fuel, the control system 3 is connected to the control system of the ship's cab and has a wire connection to the supply system 4, and the supply system 4 is connected to the storage tank. Box 6, the nozzle pipe 5 leads to the outside from the combustion chamber, the nozzle of the nozzle pipe 5 is perpendicular to the water surface, and the storage tank 6 contains liquid oxidant and liquid hydrogen respectively.
Embodiment 2
[0016] Example 2: Such as figure 1 As shown, a marine ternary solid-liquid propellant rocket protection device with protection function includes an injector 1, a combustion chamber 2, a control system 3, a supply system 4, a nozzle 5, and a storage tank 6, and is characterized in that: The injector 1 is connected to the combustion chamber 2 and the storage tank 6, the combustion chamber 2 is filled with solid fuel, the control system 3 is connected to the control system of the ship's cab and has a wire connection to the supply system 4, and the supply system 4 is connected to the storage tank. Box 6, the supply system 4 includes a pressurized gas cylinder and a pressure reducer start valve, the nozzle 5 leads to the outside from the combustion chamber, the nozzle of the nozzle 5 is in a vertical direction with the water surface, and the storage tanks 6 are respectively filled with liquid oxidants and liquid hydrogen.
Embodiment 3
[0017] Example 3: A marine ternary solid-liquid propellant rocket protection device with protection function, comprising injector 1, combustion chamber 2, control system 3, supply system 4, nozzle 5, storage tank 6, parachute 7, is characterized in that: The injector 1 is connected to the combustion chamber 2 and the storage tank 6, the combustion chamber 2 is filled with solid fuel, the control system 3 is connected to the control system of the ship's cab and has a wire connection to the supply system 4, and the supply system 4 is connected to the storage tank. Box 6, the nozzle 5 leads to the outside from the combustion chamber, the nozzle of the nozzle 5 is in a vertical direction with the water surface, the storage tank 6 holds liquid oxidant and liquid hydrogen respectively, and the parachute 7 is installed on the top of the ship and has a wire Connect the control system 3.
PUM
Abstract
Description
Claims
Application Information
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com