Staggered Seating and Cargo Access in Small Aircraft

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Solution Overview

Problem

In small aircraft with a cargo area behind passengers, passengers in the closest row face challenges accessing multiple luggage items stored in the cargo hold, as existing designs do not effectively separate passenger and cargo areas, leading to potential interference and inefficiencies in access and turnaround times.

Innovation Solution

The design incorporates forward and aft doors that open simultaneously or independently, with a pivotable shelf in the cargo hold to create separate storage sections and a divider that prevents passengers from accessing the cargo hold, while angled seating and asymmetrical seating arrangements optimize passenger access and reduce line of sight and knee interference, allowing for efficient access and egress.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If passengers are seated in rows directly behind the cargo hold, then passenger access to luggage becomes difficult, but this arrangement increases turnaround time and reduces operational efficiency

Engineering Contradiction:
Improvepassenger access to luggageVSAvoidturnaround time
Core Design Contradiction:
Ease of operationVSLoss of time

Solution Approach 1:

The cargo hold is divided into multiple sections with staggered access points at different rows. The cargo compartments are segmented so that luggage is distributed across multiple accessible locations, allowing passengers in different rows to access their own luggage without blocking others.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Instead of a single-row access design, the patent introduces multi-dimensional access by positioning cargo compartments at different depths and heights, with access points available from multiple row positions. This allows passengers to access luggage from their respective seating positions without requiring others to move.

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

2Productivity

If a single door is used for passenger entry, then the aircraft structure is simpler, but passenger access to both passenger and cargo zones requires multiple door operations increasing turnaround time

Engineering Contradiction:
Improveturnaround timeVSAvoiddoor configuration
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The single door is designed to serve multiple functions: it provides access to both the passenger cabin and the cargo hold. The door system includes a door assembly that can open to reveal both passenger entry and cargo access points, eliminating the need for separate doors while maintaining streamlined operations.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The passenger door and cargo door functions are merged into a single integrated door assembly. This unified door structure allows simultaneous or sequential access to both passenger and cargo areas through one door opening, reducing the number of door operations required during boarding and unloading.

Inventive Principle:
Principle #5Merging (Combining)

3Ease of operation

If symmetric seating arrangement is used, then manufacturing is simpler, but knee interference and line of sight blockage reduce passenger comfort

Engineering Contradiction:
Improvepassenger comfortVSAvoidseating arrangement
Core Design Contradiction:
Ease of operationVSEase of manufacture

Solution Approach 1:

The seating arrangement uses asymmetric positioning where seats in adjacent rows are offset from each other. The first row seats are positioned at different longitudinal locations compared to the second row seats, creating a staggered configuration that eliminates knee interference and improves line of sight while maintaining manufacturing feasibility through modular seat units.

Inventive Principle:
Principle #4Asymmetry

Data Source

PatentEP3873809B1Aircraft with staggered seating arrangement
Publication Date: 2024.09.11 SAFRAN CABIN INC
  • EP3873809B1 patent drawingFigure 1~2
  • EP3873809B1 patent drawingFigure 3
  • EP3873809B1 patent drawingFigure 4

AI summary

An aircraft that includes a cabin interior that is bifurcated into first and second sides and includes a pilot zone and a passenger zone aft of the pilot zone, a pilot seat positioned in the pilot zone and on a first side of the cabin interior, and first and second rows positioned in the passenger zone. The front row includes first and second front seats positioned on first and second sides of the cabin interior, respectively. The first and second front seats are angled away from one another and the second front seat is positioned forwardly of the first front seat. The back row includes first and second back seats positioned on first and second sides of the cabin interior, respectively.