CRASH LOAD DISTRIBUTION STRUCTURE OF FUSELAGE

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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.

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 could be used in the aerospace industry for improving crash safety in aircraft fuselages.

Problems Solved: This technology addresses the need for effective crash load distribution in fuselages during oblique crashes.

Benefits:

Enhanced crash safety in aircraft
Improved structural integrity during oblique crashes

Commercial Applications: Potential commercial applications include aircraft manufacturing companies looking to enhance the safety features of their aircraft.

Prior Art: Readers can start their search for prior art related to crash load distribution structures in aircraft fuselages by looking into existing patents in the aerospace industry.

Frequently Updated Research: There may be ongoing research in the aerospace industry related to crash safety technologies and innovations in fuselage structures.

Questions about Crash Load Distribution Structures in Fuselages: 1. What are the key components of a crash load distribution structure in a fuselage? 2. How does the crash box in this technology selectively 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.