Modular Aircraft Server Cluster for Cross-Fleet Blade Scalability

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Solution Overview

Problem

Existing in-flight entertainment systems face challenges in quantifying passenger engagement, managing multimedia content costs, and accommodating varying aircraft configurations, leading to inefficiencies in resource utilization and maintenance costs.

Innovation Solution

A scalable and modular aircraft server design with interchangeable compute and storage blades, allowing for flexible configurations, redundancy, and compatibility with different aircraft types, along with integrated AI capabilities for data analysis.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Volume of moving object

If existing servers are used for in-flight entertainment systems, then they can provide basic entertainment functionality, but they consume excessive physical space and computational resources

Engineering Contradiction:
Improvephysical size of serverVSAvoidcomputational performance
Core Design Contradiction:
Volume of moving objectVSPower

Solution Approach 1:

The server is divided into separate functional modules: a chassis providing structural support and interconnectivity, and interchangeable blades providing compute, storage, or AI functions. This segmentation allows the system to achieve high computational performance in a compact form factor by optimizing each module independently while maintaining a unified architecture.

Inventive Principle:
Principle #1Segmentation

2Adaptability or versatility

If servers are designed to be compatible with multiple aircraft types, then adaptability improves, but device complexity increases

Engineering Contradiction:
Improvecompatibility with aircraft typesVSAvoidsystem configuration complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The chassis is designed with universal interfaces and standardized connection protocols that work across multiple aircraft types and generations. The modular blade architecture further enhances universality by allowing the same chassis to accommodate different functional blades (compute, storage, AI) depending on the specific aircraft configuration requirements, thereby achieving multi-functionality without proportionally increasing complexity.

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

Solution Approach 2:

The system employs dynamic configuration capabilities where blades can be added, removed, or swapped based on the specific aircraft type and operational requirements. This dynamic adaptability allows a single server platform to serve multiple aircraft types efficiently, with the system reconfiguring itself rather than requiring hardware changes for different platforms.

Inventive Principle:
Principle #15Dynamics

3Reliability

If redundant servers are deployed to ensure reliability, then system reliability improves, but loss of substance increases

Engineering Contradiction:
Improvesystem availabilityVSAvoidresource consumption
Core Design Contradiction:
ReliabilityVSLoss of substance

Solution Approach 1:

By segmenting the server into a reusable chassis and interchangeable blades, the system can achieve reliability through blade redundancy without proportionally increasing overall resource consumption. The shared chassis infrastructure (power supply, cooling, interconnectivity) is utilized efficiently across multiple blade configurations, reducing the total substance required compared to deploying complete redundant servers.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The modular architecture enables selective replacement of individual blades without discarding the entire server system. When a blade fails or becomes obsolete, only that specific blade is replaced while the chassis and other functional blades continue to operate, thereby reducing resource waste compared to replacing entire servers.

Inventive Principle:
Principle #34Discarding and recovering

Data Source

PatentUS20260075739A1Scalable and modular aircraft server cluster implementation
Publication Date: 2026.03.12 PANASONIC AVIONICS CORP
  • US20260075739A1 patent drawing
  • US20260075739A1 patent drawing
  • US20260075739A1 patent drawing

AI summary

Scalable and modular aircraft servers for aircraft and associated systems, devices, and methods are disclosed herein. A headend server can include a chassis meeting a 6 Modular Concept Unit (MCU) size requirement, a pair of modules insertable into and removable from the chassis, one or more electronic blades, an I/O interface module housed in the chassis, and a power supply integrated in the chassis. Each module can include a plurality of slots, and the one or more electronic blades can be shaped and sized to fit in corresponding ones of the plurality of slots. Each of the headend server and the pair of modules can be a Line Replacement Unit (LRU). The headend server can be configured to provide a common operational interface between multiple types of aircrafts and the one or more electronic blades.