18221289. CRASH LOAD DISTRIBUTION STRUCTURE OF FUSELAGE simplified abstract (HYUNDAI MOTOR COMPANY)
Contents
CRASH LOAD DISTRIBUTION STRUCTURE OF FUSELAGE
Organization Name
Inventor(s)
Won Ki Song of Whasung-si (KR)
CRASH LOAD DISTRIBUTION STRUCTURE OF FUSELAGE - A simplified explanation of the abstract
This abstract first appeared for US patent application 18221289 titled 'CRASH LOAD DISTRIBUTION STRUCTURE OF FUSELAGE
Simplified Explanation:
This patent application describes a crash load distribution structure for a fuselage, which includes a floor frame, a skid member, and a crash box that deforms in a crash load direction during an oblique crash.
- The structure includes a floor frame that defines the fuselage floor.
- A skid member is fastened to the lower portion of the floor frame.
- A crash box is coupled to the skid member and extends to the lower portion of the floor frame.
- The crash box is designed to selectively deform in a crash load direction in the event of an oblique crash.
Key Features and Innovation:
- Floor frame defining fuselage floor
- Skid member fastened to lower portion of floor frame
- Crash box coupled to skid member and floor frame
- Crash box selectively deforms in crash load direction during oblique crash
Potential Applications:
This technology can be applied in the aerospace industry for enhancing crash safety in aircraft fuselages.
Problems Solved:
This technology addresses the need for improved crash load distribution in fuselages during oblique crashes.
Benefits:
- Enhanced crash safety in aircraft fuselages
- Improved structural integrity during oblique crashes
Commercial Applications:
Potential commercial applications include aircraft manufacturing companies, airlines, and other entities in the aerospace industry looking to enhance safety measures in aircraft design.
Prior Art:
Readers can start their search for prior art related to this technology by looking into patents and research papers on crash load distribution structures in aircraft fuselages.
Frequently Updated Research:
Stay updated on the latest research in crash safety technology for aircraft fuselages to ensure the most current information on advancements in the field.
Questions about Crash Load Distribution Structure for Fuselage:
1. What are the key components of a crash load distribution structure for a fuselage? 2. How does the crash box in this structure deform during an oblique crash?
Original Abstract Submitted
A crash load distribution structure of a fuselage, includes a floor frame defining a fuselage floor, a skid member fastened to the lower portion of the floor frame, and a crash box coupled to the skid member and extending to the lower portion of the floor frame, and configured to selectively deform in a crash load direction when an oblique crash occurs thereto.
