Fuselage Battery Support Structure for Crash Load Dispersion

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Solution Overview

Problem

Urban air mobility vehicles face safety concerns due to significant collision loads applied to the occupant space during crashes, which existing structures fail to adequately disperse, compromising occupant safety.

Innovation Solution

A battery load support structure is implemented, featuring a battery mount support mounted on the fuselage's floor frame, with a joint unit connecting to multiple framework members, including a front, center, and rear bulkheads, to enhance load dispersion and structural reinforcement.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a battery mount support is mounted on the floor frame with a simple structure, then the device complexity is reduced, but the load supporting performance deteriorates under collision loads

Engineering Contradiction:
Improvestructure complexityVSAvoidload supporting performance
Core Design Contradiction:
Device complexityVSStrength

Solution Approach 1:

The battery mount support is divided into multiple segments including a support body, front joint, center joint, and rear joint. Each segment connects to different bulkheads (front bulkhead, center bulkhead, rear bulkhead) to distribute collision loads across multiple attachment points rather than concentrating them at a single location, thereby improving load supporting performance while maintaining reasonable structural complexity

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The battery mount support extends in the longitudinal direction of the fuselage, utilizing the longitudinal dimension to span across multiple bulkheads. This dimensional extension allows the support structure to engage with multiple framework members along the length of the fuselage, distributing loads across a greater spatial extent and improving overall structural strength

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Ease of manufacture

If the battery unit is fastened to a single location on the floor frame, then the ease of manufacture is improved, but the stability deteriorates during collision

Engineering Contradiction:
Improveassembly simplicityVSAvoidoccupant space stability
Core Design Contradiction:
Ease of manufactureVSStability of the object's composition

Solution Approach 1:

The fastening system is segmented into multiple attachment points located at the front joint, center joint, and rear joint of the battery mount support. Each joint connects to a separate bulkhead, creating multiple fastening locations that work together to stabilize the battery unit and occupant space during collision, rather than relying on a single fastening point

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The battery mount support merges multiple functional elements including the support body, front joint, center joint, and rear joint into a single integrated structure. This merged structure provides multiple fastening locations simultaneously, achieving both manufacturing efficiency (as a single component) and enhanced stability (through multiple attachment points)

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentUS12388144B2Battery load support structure of fuselage
Publication Date: 2025.08.12 HYUNDAI MOTOR CO LTD
  • US12388144B2 patent drawing
  • US12388144B2 patent drawing
  • US12388144B2 patent drawing

AI summary

The present disclosure provides a battery load support structure of a fuselage, the battery load support structure including a battery mount support formed in a longitudinal direction of a floor frame of the fuselage, a battery unit inputted into an opened lower side of the floor frame and fastened to the battery mount support, and a joint unit configured to support the battery mount support and connected to a plurality of framework members that constitutes the floor frame.