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 maintaining compatibility across different aircraft configurations, leading to inefficiencies in resource utilization and maintenance.
Innovation Solution
A scalable and modular aircraft server design with interchangeable blades and standardized chassis, supporting compute and storage modules, along with AI capabilities, to enhance performance, reduce redundancy, and improve compatibility.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Volume of moving object
If existing servers are used for in-flight entertainment systems, then they can provide basic functionality, but they occupy excessive physical space and reduce scalability
Solution Approach 1:
The server is divided into modular blades (compute blades, storage blades, AI blades) that can be independently selected and combined. This segmentation allows the system to achieve high performance through selective module deployment while minimizing physical footprint by only including necessary components for each specific application workload.
Solution Approach 2:
A universal chassis design with standardized interfaces accepts multiple types of blades (compute, storage, AI, networking) through a common slot architecture. This multi-functional platform enables high performance for diverse in-flight entertainment workloads while maintaining a compact form factor through shared infrastructure.
2Adaptability or versatility
If multiple server configurations are maintained for different aircraft types, then compatibility is achieved, but device complexity and maintenance burden increase
Solution Approach 1:
A single universal chassis design with standardized mechanical and electrical interfaces accommodates all aircraft types through interchangeable blade modules. This eliminates the need for aircraft-type-specific server configurations, reducing complexity while maintaining broad compatibility across different aircraft platforms.
Solution Approach 2:
The system enables dynamic reconfiguration of server functionality by allowing operators to select and swap different blade combinations based on specific aircraft types and workload requirements. This dynamic adaptability maintains compatibility without requiring permanent complex configurations for each aircraft type.
3Reliability
If redundant servers are deployed to ensure high availability, then reliability is improved, but hardware redundancy and resource waste increase
Solution Approach 1:
The modular blade architecture enables selective redundancy where only critical components are duplicated based on availability requirements. Operators can configure minimal necessary redundancy (e.g., only storage blades or only compute blades) rather than redundant copies of entire servers, reducing hardware waste while maintaining required reliability levels.
Solution Approach 2:
The standardized blade design allows for easy replacement and recycling of individual failing components without replacing the entire server. When a blade fails, only that specific blade is removed and replaced, minimizing hardware waste and reducing the quantity of redundant components needed for maintenance purposes.
Data Source
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.


