Hyundai motor company (20240317383). Crash Load Distribution Structure of Fuselage simplified abstract

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Crash Load Distribution Structure of Fuselage

Organization Name

hyundai motor company

Inventor(s)

Won Ki Song of Seongnam-si (KR)

Crash Load Distribution Structure of Fuselage - A simplified explanation of the abstract

This abstract first appeared for US patent application 20240317383 titled 'Crash Load Distribution Structure of Fuselage

The abstract describes a crash load distribution structure for a fuselage, including a front fuselage frame, a crash unit, an extension frame, and a battery unit.

  • Front fuselage frame surrounds the front surface of the fuselage
  • Crash unit is located at the front end of the front fuselage frame
  • Extension frame is connected to the crash unit and extends to a floor frame
  • Battery unit is positioned under the floor frame and connected to a portion of the floor frame
  • Battery unit can be separated from the floor frame in case of a crash load transmission

Potential Applications: - Aircraft manufacturing - Aerospace industry - Safety engineering

Problems Solved: - Efficient distribution of crash loads - Enhanced safety measures in case of impact

Benefits: - Improved crash resistance - Enhanced structural integrity - Potential weight reduction

Commercial Applications: Title: "Innovative Fuselage Crash Load Distribution Structure for Enhanced Safety" This technology can be used in the aviation industry to improve aircraft safety and crash resistance, potentially attracting interest from aircraft manufacturers and safety regulators.

Questions about the technology: 1. How does the crash unit function in distributing crash loads effectively? 2. What are the advantages of having a battery unit that is separable from the floor frame in case of a crash?


Original Abstract Submitted

a crash load distribution structure of a fuselage may include a front fuselage frame surrounding a front surface of the fuselage, a crash unit disposed at the front end of the front fuselage frame, an extension frame coupled to the crash unit and extending to a floor frame, and a battery unit disposed under the floor frame and coupled to a portion of the floor frame constituting the floor frame. the battery unit may be selectively separable from the portion of the floor frame, e.g., if a crash load is transmitted from the extension frame.