18156522. FUEL COOLING SYSTEM simplified abstract (General Electric Company)
Contents
FUEL COOLING SYSTEM
Organization Name
Inventor(s)
Brian Magann Rush of Niskayuna NY (US)
Constantinos Minas of Slingerlands NY (US)
William Morton of Schenectady NY (US)
FUEL COOLING SYSTEM - A simplified explanation of the abstract
This abstract first appeared for US patent application 18156522 titled 'FUEL COOLING SYSTEM
- Simplified Explanation:**
The patent application describes a fuel system with a fuel tank and a fuel cooling system that cools the fuel before returning it to the tank.
- Key Features and Innovation:**
- Fuel system includes a fuel tank, fuel cooling system fuel line, fuel cooling system heat exchangers, and a fuel cooling system fuel pump.
- Fuel is pumped from the tank through the cooling system to absorb heat from aircraft components.
- Heated fuel is then returned to the tank for storage.
- Potential Applications:**
This technology could be used in aircraft fuel systems to prevent overheating and maintain optimal fuel temperature during flight.
- Problems Solved:**
The technology addresses the issue of fuel overheating in aircraft, which can lead to performance issues and safety concerns.
- Benefits:**
- Improved fuel efficiency and performance.
- Enhanced safety and reliability of aircraft systems.
- Extended lifespan of fuel components.
- Commercial Applications:**
Potential commercial applications include aviation industry for commercial airlines, private aircraft, and military aviation.
- Prior Art:**
Readers can explore prior patents related to aircraft fuel systems, heat exchangers, and fuel cooling technologies.
- Frequently Updated Research:**
Stay informed about advancements in fuel cooling systems, aircraft technology, and aviation safety protocols.
- Questions about Fuel Cooling Systems:**
1. How does the fuel cooling system in aircraft contribute to overall safety and performance? 2. What are the key considerations when designing and implementing a fuel cooling system in aircraft?
Original Abstract Submitted
A fuel system includes a fuel tank that stores fuel therein, and a fuel cooling system. The fuel cooling system includes a fuel cooling system fuel line in fluid communication with the fuel tank, one or more fuel cooling system heat exchangers in fluid communication with the fuel cooling system fuel line, and a fuel cooling system fuel pump. The fuel cooling system fuel pump pumps the fuel from the fuel tank such that the fuel flows through the fuel cooling system fuel line and into the one or more fuel cooling system heat exchangers to absorb heat from one or more aircraft components to become heated fuel. The heated fuel is returned and stored in the fuel tank.
