Monoblock Battery Hot-Swap Control With Dual Power Paths

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Solution Overview

Problem

Existing aircraft battery systems lack efficient hot-swappable solutions that allow for the addition or removal of battery modules without disrupting the power supply, posing safety hazards and inefficiencies in weight management and electrical capacity adjustments.

Innovation Solution

A hot-swappable battery system featuring a monoblock with a solid-state relay printed circuit board (SSR PCB) and a control system that manages power paths to enable seamless connection and disconnection of battery modules, using a low-power path for control and monitoring, and a high-power path for primary power delivery, with automatic deactivation and activation mechanisms to prevent safety hazards.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If battery modules are connected or disconnected in existing aircraft battery systems, then the power supply is disrupted and safety hazards occur, but the ability to adjust weight and electrical capacity is limited

Engineering Contradiction:
Improveability to adjust weight and electrical capacityVSAvoidpower supply continuity
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The control system detects the connection status of battery modules through the second power path and initiates deactivation of the first power path before physical connection or disconnection occurs. This preliminary detection and deactivation sequence prevents power disruption while enabling module adjustment.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The second power path serves as an intermediary control path that provides power to the control system independently of the first power path. This intermediary path enables the control system to monitor and manage the first power path's activation state, facilitating safe hot-swapping operations.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Weight of moving object

If battery modules are removed to reduce weight, then weight management improves, but the power supply must be shut down causing operational inefficiency

Engineering Contradiction:
Improveaircraft weightVSAvoidoperational efficiency
Core Design Contradiction:
Weight of moving objectVSProductivity

Solution Approach 1:

The second power path maintains continuous power supply to the control system throughout the battery module replacement process. This continuity enables the control system to remain operational and manage the first power path's activation state, allowing weight adjustment without interrupting aircraft operations.

Inventive Principle:
Principle #20Continuity of useful action

3Ease of operation

If battery modules are added or removed without control mechanisms, then operational flexibility improves, but safety hazards increase due to uncontrolled power path activation

Engineering Contradiction:
Improveease of battery module replacementVSAvoidsafety hazards from power path activation
Core Design Contradiction:
Ease of operationVSObject-affected harmful factors

Solution Approach 1:

The control system continuously monitors the connection status of battery modules through the second power path and provides feedback control of the first power path's activation state. When modules are detected as connected or disconnected, the control system automatically adjusts the first power path accordingly, preventing unsafe activation states.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system automatically detects battery module connection status and controls the switching device to activate or deactivate the first power path without requiring manual intervention. This self-service mechanism ensures safety while maintaining ease of operation for battery module replacement.

Inventive Principle:
Principle #25Self-service

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Enables efficient and safe addition or removal of battery modules without powering down the system, allowing for real-time adjustments in weight and electrical capacity without interrupting aircraft operations, thereby enhancing operational efficiency and safety.

Implementation Method 1

a solid-state relay printed circuit board (SSR PCB) that includes a switching device coupled to the first power path and configured to open and to close the first circuit thereof

Methodology Applied
Scientific EffectSolid-state relay switching: Relay

Implementation Method 2

a second power path electrically coupled to the monoblock and configured to form a second circuit and to provide power to the control system

Methodology Applied
Scientific EffectElectrical conduction: Conduction (electrical)

Data Source

PatentUS20240421592A1Hot Swappable Monoblock Battery
Publication Date: 2024.12.19 TEXTRON INNOVATIONS INC
  • US20240421592A1 patent drawing
  • US20240421592A1 patent drawing
  • US20240421592A1 patent drawing

AI summary

A battery module includes a monoblock comprising one or more battery cells, a first power path electrically coupled to the monoblock and electrically couplable to one or more terminals, a switching device coupled to the first power path and configured to open and to close a circuit thereof, a control system that controls the switching device, and a second power path electrically coupled to the monoblock. The second power path is configured to provide power to the control system. An absence of a voltage signal from the second power path detected by the control system causes the switching device to open to electrically disconnect the one or more terminals of the first power path. Detection of the voltage signal from the second power path by the control system may cause the switching device to close to electrically connect the one or more terminals of the first power path.