18375137. DETACHABLE BATTERY STRUCTURE OF FUSELAGE simplified abstract (Hyundai Motor Company)
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 18375137 titled 'DETACHABLE BATTERY STRUCTURE OF FUSELAGE
Simplified Explanation: The patent application describes a detachable battery structure for a fuselage that is designed to detach in the event of a frontal collision, enhancing safety.
Key Features and Innovation:
- Floor unit positioned on the fuselage
- Battery unit fastened to the floor unit to receive load in a collision
- Battery unit extension fastened to a window frame to transmit load to the battery unit
- Crash unit positioned in front of the window frame
- Dash reinforcement assembly fastened to the window frame to move backward in a collision, detaching the battery unit
Potential Applications: This technology could be used in various transportation vehicles to improve safety in the event of collisions.
Problems Solved: The detachable battery structure addresses the need for enhanced safety measures in the event of frontal collisions.
Benefits:
- Improved safety in collisions
- Detachable battery for easy maintenance and replacement
Commercial Applications: The technology could be applied in the automotive industry for vehicles requiring detachable battery structures for safety purposes.
Prior Art: Research existing patents related to detachable battery structures in transportation vehicles for further information.
Frequently Updated Research: Stay updated on advancements in detachable battery structures for fuselages in transportation vehicles for the latest safety features.
Questions about Detachable Battery Structure for Fuselage: 1. How does the detachable battery structure enhance safety in a frontal collision? 2. What are the potential applications of this technology in the automotive industry?
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.
