DC Link Capacitor Isolation for Aircraft Fault Current Protection

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

The challenge of managing high fault currents resulting from the discharge of DC link capacitors in electrical power systems, particularly in electric and hybrid-electric aircraft, which can exceed component ratings and cause damage due to the collapse of voltage across the capacitor.

Innovation Solution

Incorporating a power semiconductor switch in series with the DC link capacitor and a control unit that responds to faults by opening the switch to prevent capacitor discharge, utilizing hardware-implemented control mechanisms and specific semiconductor devices like depletion-mode MOSFETs or JFETs, and employing a control unit with a potential divider and comparator to manage the switch state.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a DC link capacitor is used to maintain smooth DC output waveform, then power quality is improved, but fault current magnitude increases due to capacitor discharge

Engineering Contradiction:
Improvepower qualityVSAvoidfault current magnitude
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent extracts the harmful discharge path from the system by introducing a series switch between the DC link capacitor and the DC electrical network. This switch isolates the capacitor during faults, preventing the discharge current from flowing into the network while preserving the capacitor's voltage-smoothing function during normal operation.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The series switch acts as an intermediary element between the DC link capacitor and the DC electrical network. It mediates the connection by being normally closed to allow capacitor discharge for smoothing, but can open to block harmful fault currents while still permitting the capacitor to maintain voltage stability during normal conditions.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If traditional protection methods are used (turning on all transistors or adding parallel diode), then component protection is improved, but device complexity increases

Engineering Contradiction:
Improvecomponent protectionVSAvoidconverter complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent removes the need for complex protection circuits by extracting the protection function into a simple series switch with basic control logic. Instead of requiring all transistors to turn on or adding parallel diodes, the solution uses a single series switch that opens to block fault current, significantly reducing the complexity of the protection mechanism.

Inventive Principle:
Principle #2Taking out (Extraction)

3Object-affected harmful factors

If series switch is added to prevent capacitor discharge, then fault current is reduced, but device complexity increases

Engineering Contradiction:
Improvefault currentVSAvoidconverter structure
Core Design Contradiction:
Object-affected harmful factorsVSDevice complexity

Solution Approach 1:

The series switch serves multiple functions: it enables the DC link capacitor to provide voltage smoothing during normal operation by being closed, and it provides fault current protection by opening during faults. This multi-functionality justifies the addition of the switch while delivering both smoothing and protection benefits from a single component.

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

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

Effectively prevents damage to power converters by isolating the DC link capacitor during faults, ensuring faster response times and reducing component size and mass through targeted discharge management.

Implementation Method 1

a DC link capacitor connected between the first and second DC output terminals

Methodology Applied
Scientific EffectCapacitance: Capacitance

Data Source

PatentUS20250330014A1Electrical power system
Publication Date: 2025.10.23 ROLLS ROYCE PLC
  • US20250330014A1 patent drawing
  • US20250330014A1 patent drawing
  • US20250330014A1 patent drawing

AI summary

An electrical power system and an aircraft including an electrical power system are provided. The electrical power system includes: an electrical power source; a DC electrical network; a power converter including at least one input terminal and first and second DC output terminals, the at least one input terminal connected to the electrical power source, the first and second DC output terminals connected to the DC electrical network; a DC link capacitor connected between the first and second DC output terminals; a power semiconductor switch connected in series with the DC link capacitor between the first and second DC output terminals; and a control unit configured to respond to a fault in the DC electrical network by opening the power semiconductor switch, whereby discharge of the DC link capacitor is prevented.