Decentralized Power Distribution Node for Aircraft Transient Loads

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Solution Overview

Problem

Aircraft power distribution systems face challenges in efficiently managing power distribution to electrical loads during transient periods when the primary power sources, such as generators, cannot meet peak demands, leading to potential power shortages and system instability.

Innovation Solution

The implementation of a power distribution node architecture that includes microgenerators and power storage devices, strategically located proximate to electrical loads, which can supplement power through a common power distribution bus, enabling selective energization and conversion of power as needed, managed by a controller module to address transient power demands.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Power

If a centralized power distribution system is used with primary generators, then power can be generated and distributed to electrical loads, but the system cannot meet peak power demands during transient periods leading to power shortages

Engineering Contradiction:
Improvepower supply capabilityVSAvoidsystem stability
Core Design Contradiction:
PowerVSReliability

Solution Approach 1:

The patent divides the centralized power system into distributed power distribution nodes throughout the aircraft. Each node includes local power storage devices and microgenerators that can independently supplement power locally, eliminating the single-point failure problem and enabling peak demand to be met through distributed supplementation.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Power storage devices are pre-charged during normal operation when power demand is low. During transient peak demands, these pre-charged storage devices immediately supplement power without waiting for primary generators to respond, thus preventing power shortages before they occur.

Inventive Principle:
Principle #10Preliminary action

2Power

If power distribution nodes are dispersed throughout the aircraft, then localized power supplementation can meet peak demands, but the wiring infrastructure becomes more complex

Engineering Contradiction:
Improvelocalized power supplementationVSAvoidwiring infrastructure
Core Design Contradiction:
PowerVSDevice complexity

Solution Approach 1:

The patent combines multiple functions into integrated power distribution nodes that include power storage devices, microgenerators, and distribution controls in single modular units. This merging reduces the overall wiring complexity compared to separate centralized systems while maintaining localized power supplementation capability.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

Each power distribution node is designed as a universal module that can perform multiple functions: storing power, generating power locally, and distributing power to connected loads. This multi-functionality reduces the need for specialized wiring for different functions, simplifying the overall infrastructure.

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

3Reliability

If microgenerators are deployed at power distribution nodes, then redundant power sources enhance reliability, but the device complexity increases

Engineering Contradiction:
Improveredundant power sourcesVSAvoidnode complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The control systems in power distribution nodes dynamically manage the operation of microgenerators and power storage devices based on real-time power demand and availability. This dynamic control allows the system to activate redundant power sources only when needed, reducing operational complexity while maintaining reliability.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system incorporates feedback mechanisms that continuously monitor power demand, storage levels, and generator status. This feedback enables automatic coordination between multiple power sources at each node, simplifying the control of redundant systems by allowing them to self-regulate based on system conditions.

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS11342759B2Power distribution node for a power architecture
Publication Date: 2022.05.24 GE AVIATION SYST LTD
  • US11342759B2 patent drawing
  • US11342759B2 patent drawing
  • US11342759B2 patent drawing

AI summary

A power distribution node for a power architecture, and method for operating, includes a microgenerator configured to generate a supply of electrical power, and a power distribution unit connected with a power supply bus and the microgenerator and configured to selectively energize at least a subset of electrical loads disposed proximately to the power distribution node. The energizing power is operably supplied by at least one of the power supply bus or the microgenerator.