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Hybrid Jet and Electric Engine System

[Category : - DESIGN PATENTS]
[Viewed 38 times]

Overview:The invention pertains to a Hybrid Jet and Electric Engine System designed to revolutionize aircraft propulsion and operational efficiency. This system integrates hybrid electric jet engines that can switch between conventional fuel and electric power. It features a distributed engine layout, a blended wing body design, advanced control systems with AI assistance, and enhanced emergency capabilities. The system aims to improve fuel efficiency, environmental impact, and overall aircraft safety.Problem Addressed:Fuel Consumption and Emissions: Traditional jet engines are heavily reliant on fossil fuels, contributing to high fuel consumption and significant carbon emissions. The need for more sustainable and efficient aviation technologies is pressing.Engine Failure and Stability: Aircraft with multiple engines often face stability issues during engine failure. Traditional configurations may not provide optimal balance and control in such scenarios.Aerodynamic Efficiency: Conventional aircraft designs may not fully utilize aerodynamic principles to enhance fuel efficiency and performance.Emergency Response: Aircraft require rapid and reliable emergency response capabilities, particularly for rescue missions and medical evacuations.Benefits Compared to Existing Technologies:Enhanced Fuel Efficiency and Reduced Emissions: The hybrid jet/electric engine system offers the flexibility to switch between conventional fuel and electric power, optimizing fuel consumption and reducing emissions. The potential use of hydrogen fuel cells or sustainable aviation fuel (SAF) further enhances environmental benefits.Improved Stability and Control: The distributed engine layout ensures even thrust distribution, enhancing stability and control, especially during engine failure. Electric engines contribute to balance control and maneuverability, providing additional reliability in emergencies.Superior Aerodynamic Efficiency: The blended wing body design reduces drag and improves lift, leading to better fuel efficiency and a more spacious design for engines and equipment. This design also supports better weight distribution, crucial for accommodating additional engines.Advanced Control and Safety Features: The integration of a fly-by-wire system with AI-assisted balancing enables automatic adjustments to engine thrust, enhancing stability and safety. The predictive crash detection systems and smart auto-retraction wings further contribute to reducing crash risk and improving emergency response capabilities.Versatile Emergency Capabilities: The inclusion of Vertical Takeoff and Landing (VTOL) capabilities allows for quick takeoff and landing in constrained or remote locations, making the aircraft highly versatile for rescue missions, medical evacuations, and military operations.Overall, this invention represents a significant advancement in aircraft technology, addressing critical issues related to fuel efficiency, environmental impact, stability, and emergency response while offering a more versatile and safe flying experience.

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miracleeeee (Nigeria)

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