eVTOL Casing Cooling With Embedded Pulsating Heat Pipes
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Solution Overview
Problem
Conventional cooling systems for electric aircraft are inefficient in heat spreading, leading to poor cooling effectiveness and reduced electronic functionality due to heat concentration near the heat source.
Innovation Solution
The integration of pulsating heat pipes (PHPs) within the casing of electric aircraft, in conjunction with a heat spreader casing, to enhance heat transfer capabilities and spread heat uniformly across the casing surface.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Temperature
If conventional cooling systems use the surface area of the casing to spread heat, then the structure is simple, but the heat spreading capability is poor and cooling effectiveness is low
Solution Approach 1:
The patent employs pulsating heat pipes that utilize phase transitions of the working fluid between liquid and vapor states to transport heat. The evaporator section converts liquid to vapor absorbing heat from electronics, the vapor travels to the condenser section where it condenses back to liquid releasing heat, and the liquid returns to the evaporator. This phase change mechanism enables efficient heat spreading throughout the casing surface while maintaining a relatively simple overall structure.
Solution Approach 2:
The pulsating heat pipe system uses fluid dynamics and pressure variations to drive the circulation of working fluid through the closed-loop channel. The pulsating flow of liquid and vapor creates pressure waves that propel the phase-change process, enabling passive heat transport without external pumps or complex control systems, thus achieving effective cooling with minimal structural complexity.
2Temperature
If conventional cooling systems are used, then the device structure is simple, but the heat remains concentrated near the heat source and does not spread to distant portions of the casing
Solution Approach 1:
The pulsating heat pipe acts as an intermediary heat transfer device between the heat source (electronic components) and the casing surface. The working fluid within the PHP serves as a mobile mediator that absorbs heat at the evaporator near the electronics and transports it through phase change to the condenser sections distributed across the casing surface, enabling uniform heat spreading without requiring direct thermal contact across the entire casing.
Solution Approach 2:
The patent transitions from two-dimensional heat conduction through the casing wall to three-dimensional heat transport by embedding the pulsating heat pipe channel within the casing structure. The PHP creates internal heat transport pathways that extend throughout the casing volume, allowing heat to be distributed across multiple dimensions of the casing surface rather than relying solely on surface conduction.
3Temperature
If more cooling capacity is added to meet the high heat generation of electric aircraft motors, then cooling effectiveness improves, but the device complexity and space requirements increase
Solution Approach 1:
The pulsating heat pipe integrates multiple heat transfer functions into a single unified component. The evaporator, condenser sections, and return channel are merged into one continuous closed-loop structure embedded within the casing. This consolidation provides high cooling capacity equivalent to multiple separate cooling devices while maintaining a simple integrated structure that utilizes the existing casing space efficiently.
Solution Approach 2:
The pulsating heat pipe performs multiple heat transfer functions simultaneously: heat absorption at the evaporator, heat transport through phase change, heat release at condenser sections, and fluid return. This multi-functionality allows a single component to replace what would traditionally require multiple separate cooling devices, achieving high cooling capacity without proportional increases in system complexity or space requirements.
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
This solution provides increased cooling capacity, efficient heat spreading, and improved electronic functionality by utilizing the full surface area of the casing, while also being resistant to g-forces and orientation changes.
Implementation Method 1
The refrigerant can travel between the evaporator section and condenser section, transforming between vapor phase and liquid phase. Such transformation can absorb and release heat
Implementation Method 2
The refrigerant can travel between the evaporator section and condenser section, transforming between vapor phase and liquid phase
Implementation Method 3
The refrigerant can travel between the evaporator section and condenser section, transforming between vapor phase and liquid phase
Implementation Method 4
This can provide the advantage of higher heat transfer capability, spreading of high heat flux
Implementation Method 5
heat being absorbed from the electronic devices and released into an airflow at an end of the fin a distance from the casing
Data Source
AI summary
The present disclosure is directed to systems for cooling an electric aircraft. The system comprises an electronic device, a casing, and at least one PHP. The electronic device can generate heat. The electronic device can be housed within the casing. The casing comprises a casing inner wall and a casing outer wall wherein a first casing width is between the casing outer wall and the casing inner wall, and at least one PHP embedded in the first casing width. The casing may also comprise a casing inner base and a casing outer base wherein a second casing width is between the casing inner base and the casing outer base. The first casing width and second with may comprise a single fluidly connected channel with a connecting point, and a PHP may be embedded into the single fluidly connected channel. The system may be configured for use on an eVTOL.


