Honda motor co., ltd. (20240327020). AIRCRAFT simplified abstract
Contents
AIRCRAFT
Organization Name
Inventor(s)
Azuki Ichikawa of Wako-shi (JP)
Yuichi Fukuchi of Wako-shi (JP)
Hikari Hirayanagi of Wako-shi (JP)
Takuya Kubota of Wako-shi (JP)
AIRCRAFT - A simplified explanation of the abstract
This abstract first appeared for US patent application 20240327020 titled 'AIRCRAFT
Simplified Explanation: The patent application describes an aircraft with a cooling unit that includes radiators and cooling fans to regulate the temperature inside the fuselage.
Key Features and Innovation:
- Aircraft with a cooling unit including first and second radiators and cooling fans.
- Cooling unit positioned forward of the engine in the fuselage.
- Exhaust orifice located rearward of the engine in the fuselage for discharging air.
Potential Applications: This technology can be applied in various aircraft models to improve cooling efficiency and maintain optimal temperatures inside the fuselage.
Problems Solved: The technology addresses the need for effective cooling systems in aircraft to prevent overheating and ensure passenger comfort.
Benefits:
- Enhanced cooling capabilities.
- Improved temperature regulation.
- Increased passenger comfort during flights.
Commercial Applications: The technology can be utilized in commercial airlines, private jets, and military aircraft to enhance overall performance and passenger experience.
Prior Art: Readers can explore prior patents related to aircraft cooling systems and ventilation to understand the evolution of this technology.
Frequently Updated Research: Stay updated on advancements in aircraft cooling systems and related technologies to ensure the latest innovations are incorporated into future designs.
Questions about Aircraft Cooling Systems: 1. How does the positioning of the cooling unit impact the overall efficiency of the system? 2. What are the potential challenges in integrating this cooling technology into different types of aircraft?
Original Abstract Submitted
an aircraft including a fuselage with a cooling unit including a first radiator, a second radiator, a first cooling fan and a second cooling fan for taking air outside the fuselage into the fuselage and supplying air to the first radiator and the second radiator. the aircraft has an exhaust orifice for discharging air delivered into the interior of the fuselage, the cooling unit is arranged forward of the engine in the fuselage, and the exhaust orifice is positioned rearward of the engine in the fuselage.
