Routable Backup Power Control Units for Aircraft Ice Protection

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Solution Overview

Problem

Safety critical systems, such as aircraft ice protection systems, require redundant power control, but the need for a dedicated backup power control unit for each primary unit increases system size, weight, and complexity.

Innovation Solution

A redundant power control system that includes multiple primary power control circuits and at least one secondary power control circuit, where the secondary circuit can connect to multiple primary power input lines via a switch circuit, allowing it to assume control in case of a fault, thereby reducing the number of required backup units.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a dedicated backup power control unit is provided for each primary power control unit, then system reliability is improved, but system size, weight, and complexity increase

Engineering Contradiction:
Improvesystem reliabilityVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The backup power control unit is designed to serve multiple primary power control units simultaneously. The single backup unit can assume control of any failed primary unit through a switch circuit that allows it to connect to multiple load power input lines, making the backup unit universal rather than dedicated to a single primary unit.

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

Solution Approach 2:

Multiple backup functions are merged into a single backup power control unit. Instead of having separate backup units for each primary unit, the invention combines the backup capability into one shared unit that can replace any failed primary unit through control channel switching and load power input line connection.

Inventive Principle:
Principle #5Merging (Combining)

2Reliability

If a dedicated backup power control unit is provided for each primary power control unit, then system reliability is improved, but system weight increases

Engineering Contradiction:
Improvesystem reliabilityVSAvoidsystem weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The backup power control unit is designed to serve multiple primary power control units simultaneously. The single backup unit can assume control of any failed primary unit through a switch circuit that allows it to connect to multiple load power input lines, making the backup unit universal rather than dedicated to a single primary unit.

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

Solution Approach 2:

Multiple backup functions are merged into a single backup power control unit. Instead of having separate backup units for each primary unit, the invention combines the backup capability into one shared unit that can replace any failed primary unit through control channel switching and load power input line connection.

Inventive Principle:
Principle #5Merging (Combining)

3Reliability

If a dedicated backup power control unit is provided for each primary power control unit, then system reliability is improved, but system size increases

Engineering Contradiction:
Improvesystem reliabilityVSAvoidsystem size
Core Design Contradiction:
ReliabilityVSVolume of moving object

Solution Approach 1:

The backup power control unit is designed to serve multiple primary power control units simultaneously. The single backup unit can assume control of any failed primary unit through a switch circuit that allows it to connect to multiple load power input lines, making the backup unit universal rather than dedicated to a single primary unit.

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

Solution Approach 2:

Multiple backup functions are merged into a single backup power control unit. Instead of having separate backup units for each primary unit, the invention combines the backup capability into one shared unit that can replace any failed primary unit through control channel switching and load power input line connection.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentEP3498607B1Routable backup power control units
Publication Date: 2022.03.16 ROSEMOUNT AEROSPACE INC
  • EP3498607B1 patent drawingFigure 1
  • EP3498607B1 patent drawingFigure 2
  • EP3498607B1 patent drawingFigure 3

AI summary

A system and method for controlling power includes a power source, a plurality of primary control circuits (20a - 20n), a load, at least one secondary control circuit (22a - 22n), a switch circuit (24), and a control channel. The plurality of primary control circuits (20a - 20n) are connected to control load power from the power source to respective ones of a plurality of load power inputs. The load is configured to receive power from the plurality of load power inputs. The at least one secondary control circuit (22a - 22n) is connected to the power source, and the switch circuit (24) is connected between the at least one secondary control circuit (22a - 22n) and the plurality of load power inputs. The control channel is configured to control the switch circuit (24) to connect the at least one secondary control circuit (22a - 22n) to a selected one of the plurality of load power inputs.