Airframe-Integrated Optical Midplane for High-Bandwidth Connectivity

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Solution Overview

Problem

Existing modular computing systems face limitations in optical connectivity due to space constraints on the midplane, restricting bandwidth and redundancy, especially as emerging applications require data rates exceeding 56 Gbps per lane.

Innovation Solution

An optical midplane is introduced that utilizes the airframe to optimize airflow and includes optical connectors interconnected by fibers within structural cavities, enabling optical connectivity between modules across hemispheres and within the same hemisphere, thereby increasing bandwidth and flexibility.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If optical connectors are placed on the midplane to provide optical connectivity, then bandwidth and connectivity are improved, but space constraints on the midplane limit the number of connectors and their locations

Engineering Contradiction:
Improveoptical connectivityVSAvoidmidplane space
Core Design Contradiction:
ReliabilityVSArea of stationary object

Solution Approach 1:

The patent moves optical connectors from the traditional midplane location to the airframe structure itself, utilizing the three-dimensional space within the airframe cavities. This dimensional shift allows optical connectivity without consuming midplane area, resolving the space constraint problem while maintaining improved optical connectivity.

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

2Productivity

If electrical connectivity is used to connect modules, then system simplicity is maintained, but bandwidth is insufficient for emerging applications requiring data rates exceeding 56 Gbps per lane

Engineering Contradiction:
Improvedata rateVSAvoidconnectivity infrastructure
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The patent replaces electrical connectivity infrastructure with optical connectivity infrastructure. By substituting electrical signals with optical signals through fiber optic connectors, the system achieves the required high data rates for emerging applications while the airframe integration keeps the overall system design manageable.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

3Adaptability or versatility

If optical connectors are integrated into the airframe structure, then space utilization is improved and connectivity is enhanced, but manufacturing complexity increases

Engineering Contradiction:
Improveoptical connectivity flexibilityVSAvoidairframe integration
Core Design Contradiction:
Adaptability or versatilityVSEase of manufacture

Solution Approach 1:

The patent merges the optical connector mounting function with the airframe structure by integrating connectors into the airframe cavities. This consolidation allows the airframe to serve dual purposes: providing structural support and housing optical connectivity infrastructure, thereby improving space utilization and connectivity flexibility while managing manufacturing complexity through functional integration.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentUS11442231B2Airframe-integrated optical midplane
Publication Date: 2022.09.13 HEWLETT PACKARD ENTERPRISE DEV LP
  • US11442231B2 patent drawing
  • US11442231B2 patent drawing
  • US11442231B2 patent drawing

AI summary

An optical midplane includes an airframe having a first side on which first modules are disposed and a second side on which second modules are disposed. The airframe is to provide for optimized airflow through the first modules disposed on the first side. A plurality of optical connectors are disposed at respective locations on the airframe to provide optical connectivity. Optical connectivity is provided between at least one of any first module disposed on the first side of the airframe and any second module disposed on the second side of the airframe, any first modules disposed on the first side of the airframe, and any second modules disposed on the second side of the airframe.