Electric Vacuum Jet Engine Counter-Rotating Propellers

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Solution Overview

Problem

Traditional gas-fueled jet engines are inefficient and environmentally harmful due to their weight and high fuel consumption, while current eco-friendly alternatives fail to match the thrust and efficiency of traditional engines.

Innovation Solution

An electric vacuum jet engine with a series of counter-rotating propeller assemblies within a tubular housing, generating thrust by increasing air flow velocity through the creation of pressure differentials, using a vacuum effect to exhaust air flow at high velocity, resulting in a more efficient and eco-friendly propulsion system.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Power

If traditional gas-fueled jet engines are used, then thrust is generated effectively, but weight increases and fuel consumption rises

Engineering Contradiction:
ImprovethrustVSAvoidengine weight
Core Design Contradiction:
PowerVSWeight of moving object

Solution Approach 1:

The engine is divided into multiple independent propeller assemblies arranged in series within the tubular housing. Each propeller assembly functions as a separate thrust-generating unit, allowing the system to achieve total thrust through cumulative effect of multiple lighter components rather than relying on a single heavy gas turbine engine

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent replaces the traditional gas-fueled combustion-based mechanical system with an electrically-driven propeller system. Electric motors drive the propeller assemblies, substituting the heavy gas turbine machinery with lighter electric propulsion components that achieve similar or superior thrust output

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Power

If traditional gas-fueled jet engines are used, then thrust is generated, but fuel consumption increases and environmental impact worsens

Engineering Contradiction:
ImprovethrustVSAvoidfuel consumption
Core Design Contradiction:
PowerVSUse of energy by moving object

Solution Approach 1:

The patent substitutes the fuel-consuming combustion system with an electric propulsion system. Electric motors power the propeller assemblies, eliminating the need for traditional jet fuel and the associated high energy consumption and environmental pollution while maintaining effective thrust generation

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The counter-rotating propeller assemblies create periodic vacuum and pressure cycles that enhance air flow velocity. This periodic action allows the system to extract more energy from each unit of electrical power input, improving overall energy efficiency compared to continuous combustion

Inventive Principle:
Principle #19Periodic action

3Speed

If counter-rotating propeller assemblies are used to generate vacuum, then air flow velocity increases, but device complexity increases

Engineering Contradiction:
Improveair flow velocityVSAvoidpropeller assembly complexity
Core Design Contradiction:
SpeedVSDevice complexity

Solution Approach 1:

Multiple propeller assemblies are merged within a single tubular housing structure, sharing common support frameworks and electrical power systems. This integration reduces the overall complexity that would result from having separate units, while maintaining the velocity-multiplying effect of the counter-rotating configuration

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The counter-rotating propeller assemblies serve multiple functions simultaneously: they generate thrust, create vacuum cycles to accelerate air flow, and control directional airflow. This multi-functionality reduces the need for additional separate components, thereby managing system complexity while achieving superior performance

Inventive Principle:
Principle #6Universality (Multi-functionality)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The electric vacuum jet engine achieves the same or higher thrust as traditional gas-fueled engines while reducing weight and environmental impact, with air flow velocity increasing five times at each iteration, enhancing energy efficiency and reducing fuel consumption.

Implementation Method 1

the vacuum force can become evident at the moment that air is extracted out of a sealed bottle by a pneumatic mechanism. When a pump, for instance, extracts air out of the bottle, the extraction results in a vacuum

Methodology Applied
Scientific EffectVacuum: Vacuum

Implementation Method 2

generate thrust by generating a pressure differential using one or more vacuums within the jet engine to exhaust air flow from the jet engine at a high velocity

Methodology Applied
Scientific EffectPressure differential: Pressure Gradient

Data Source

PatentUS11613371B1Electric vacuum jet engine
Publication Date: 2023.03.28 ROMO JOHN DANIEL
  • US11613371B1 patent drawing
  • US11613371B1 patent drawing
  • US11613371B1 patent drawing

AI summary

An electric vacuum jet engine is a more ecofriendly alternative to gas-fueled jet engines that generates the same or higher thrust than traditional gas-fueled jet engines. The jet engine includes a tubular housing, at least one first propeller assembly, and at least one second propeller assembly. The tubular housing accommodates an alternating of series of propeller assemblies formed by the at least one first propeller assembly and the at least one second propeller assembly. Together, the at least one first propeller assembly and the at least one second propeller assembly generate several vacuums along the tubular housing that increase the velocity of air flow through the tubular housing to generate the thrust necessary to propel the desired aircraft. The tubular housing also includes a housing inlet and a housing outlet corresponding to the open ends of the tubular housing through which air flow enters and exits the tubular housing, respectively.