Rotary Engine Modular Sleeve and Crossover Seal System

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Solution Overview

Problem

Existing rotary internal combustion engines face inefficiencies due to poor sealing capabilities, suboptimal combustion, lower torque, and RPM limitations, primarily attributed to mechanical configurations and cam follower issues.

Innovation Solution

A rotary internal combustion engine design featuring a power module with all moving parts enclosed within a housing, utilizing a sleeve with integrated intake and exhaust, and a crossover seal system with spring-activated seals to maintain constant combustion chamber pressures and prevent leakage.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional rotary engine designs are used, then the engine structure is simpler, but sealing capabilities are insufficient and combustion chamber pressures cannot be maintained

Engineering Contradiction:
Improvesealing capabilityVSAvoidmechanical configuration complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The engine is divided into modular components including a rotor assembly with multiple arms, a stator with separate intake and exhaust sections, and individual combustion chambers. This segmentation allows each component to be optimized for its specific function while maintaining overall sealing integrity through precise mating surfaces and seals at the interfaces between segments.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Seal elements are introduced as intermediary components between moving and stationary parts. These seals act as mediators that transfer the sealing function from the mechanical configuration itself to dedicated sealing components, thereby maintaining combustion chamber pressure while allowing the necessary relative motion between rotor and stator components.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Speed

If cam follower mechanical configurations are used, then valve actuation is achieved, but RPM is limited due to floating mechanisms

Engineering Contradiction:
ImproveRPM capabilityVSAvoidvalve actuation stability
Core Design Contradiction:
SpeedVSReliability

Solution Approach 1:

The conventional cam follower mechanism is replaced with a direct-actuation system where rotor arms directly control valve timing and lift through their rotational motion. This substitution eliminates the floating cam follower mechanism and its associated inertia limitations, enabling higher RPM operation while maintaining precise valve actuation control through the rotor's rotational position.

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

3Use of energy by moving object

If conventional combustion chamber designs are used, then engine construction is simpler, but combustion burn is suboptimal resulting in high temperatures and poor fuel economy

Engineering Contradiction:
Improvefuel economyVSAvoidcombustion chamber configuration
Core Design Contradiction:
Use of energy by moving objectVSDevice complexity

Solution Approach 1:

The combustion chamber design incorporates local quality variations through specifically shaped chamber volumes, strategically positioned spark plugs, and targeted fuel injection points. These localized optimizations create ideal combustion conditions in each chamber, improving burn efficiency and reducing peak temperatures while maintaining overall engine design simplicity.

Inventive Principle:
Principle #3Local quality

4Force

If conventional rotary engine designs are used, then engine mass is reduced, but torque output is lower than desired

Engineering Contradiction:
Improvetorque outputVSAvoidengine mass
Core Design Contradiction:
ForceVSWeight of moving object

Solution Approach 1:

Multiple combustion chambers are merged into a single rotor assembly, allowing multiple power strokes to occur simultaneously or in rapid succession. This merging of combustion events within a compact rotor-stator configuration increases total torque output while maintaining the lightweight rotary engine architecture, as the combined force from multiple chambers acts on the same rotational mechanism.

Inventive Principle:
Principle #5Merging (Combining)

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 design enhances sealing efficiency, maintains constant combustion pressures, and improves torque and RPM capabilities, leading to increased engine performance and fuel economy.

Implementation Method 1

a crossover seal system with spring-activated seals to maintain constant combustion chamber pressures and prevent leakage

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

rotary internal combustion engine design featuring a power module with all moving parts enclosed within a housing

Methodology Applied
Scientific EffectCombustion: Combustion

Data Source

PatentUS9714574B2Rotary internal combustion engine, gas compressor, and liquid pump
Publication Date: 2017.07.25 GOTEK ENERGY INC
  • US9714574B2 patent drawing
  • US9714574B2 patent drawing
  • US9714574B2 patent drawing

AI summary

A rotatory internal combustion engine includes a power module, a housing configured to retain the power module and including an intake and an exhaust, and a first sleeve including a sleeve intake, a sleeve exhaust, and an injector port. The first sleeve is removably coupleable within the housing to form an intake flow path between the housing intake and the sleeve intake, and an exhaust flow path between the housing exhaust and the sleeve exhaust. The first sleeve is interchangeable with a second sleeve that has at least one of a sleeve intake, a sleeve exhaust, and an injector port different than the corresponding sleeve intake, sleeve exhaust, and injector port of the first sleeve, and that is configured to modify at least one of a torque output of the engine, a power output of the engine, and a fuel timing of the engine, compared to the first sleeve.