US Patent Application 17827162. INTEGRATED THERMAL MANAGEMENT APPARATUS simplified abstract
Contents
INTEGRATED THERMAL MANAGEMENT APPARATUS
Organization Name
Inventor(s)
Braedon Lohe of ESSEX JUNCTION VT (US)
Sean Donovan of RICHMOND VT (US)
Sarah Overfield of SOUTH BURLINGTON VT (US)
INTEGRATED THERMAL MANAGEMENT APPARATUS - A simplified explanation of the abstract
This abstract first appeared for US patent application 17827162 titled 'INTEGRATED THERMAL MANAGEMENT APPARATUS
Simplified Explanation
- The patent application is for an apparatus designed to manage the thermal energy of an electric aircraft energy source. - The apparatus includes fins that extend from the skin of the electric aircraft. - The energy source is positioned near or connected to the fins, allowing heat energy to dissipate through the fins and the aircraft's skin. - The apparatus also includes a coolant system, with channels located between the fins, allowing coolant to flow through them. - The purpose of the apparatus is to effectively dissipate heat from the energy source, preventing overheating and ensuring optimal performance of the electric aircraft.
Original Abstract Submitted
The present invention is directed to an apparatus for managing thermal energy of an electric aircraft energy source. Apparatus may include fins, which extend from a skin of electric aircraft. The energy source may bias or be adjacent to the fins so that heat energy may dissipate from the energy source and through the fins and, thus, the skin. A coolant may also be run through the apparatus, where the coolant may flow through channels that are disposed between the fins.
