Hyundai motor company (20240339711). DETACHABLE BATTERY STRUCTURE OF FUSELAGE simplified abstract
Contents
DETACHABLE BATTERY STRUCTURE OF FUSELAGE
Organization Name
Inventor(s)
Won Ki Song of Seongnam-si (KR)
DETACHABLE BATTERY STRUCTURE OF FUSELAGE - A simplified explanation of the abstract
This abstract first appeared for US patent application 20240339711 titled 'DETACHABLE BATTERY STRUCTURE OF FUSELAGE
The abstract describes a detachable battery structure for a fuselage, designed to withstand frontal collisions and ensure the safety of the battery unit.
- Floor unit positioned on the fuselage
- Battery unit fastened to the floor unit, capable of receiving a load during a frontal collision
- Battery unit extension fastened to a window frame, transmitting the load to the battery unit
- Crash unit positioned in front of the window frame
- Dash reinforcement assembly fastened to the window frame, moving backward in a collision to detach the battery unit from the floor unit
Potential Applications: - Aviation industry for aircraft safety - Automotive industry for vehicle safety in frontal collisions
Problems Solved: - Ensures battery safety in the event of a frontal collision - Prevents damage to the battery unit and surrounding structures
Benefits: - Enhanced safety measures for passengers and crew - Minimizes the risk of fire or explosion in the battery unit during a collision
Commercial Applications: - Aircraft manufacturers - Automotive companies focused on safety features
Questions about the technology: 1. How does the detachable battery structure improve safety in frontal collisions? 2. What materials are used in the construction of the battery unit for optimal performance?
Frequently Updated Research: - Ongoing studies on battery safety in transportation vehicles and aircraft.
Original Abstract Submitted
a detachable battery structure of a fuselage including a floor unit positioned on a fuselage, a battery unit fastened to the floor unit and configured to receive a load in the event of a frontal collision of the fuselage, a battery unit extension fastened to a window frame of the fuselage and configured to transmit the load to the battery unit in the event of the frontal collision of the fuselage, a crash unit positioned in front of the window frame, and a dash reinforcement assembly fastened to the window frame and positioned on a rear surface of the crash unit, wherein the dash reinforcement assembly moves backward in the event of the frontal collision of the fuselage so that the battery unit extension moves in a longitudinal direction, and the battery unit is configured to move backward to be detached from the floor unit.
