Resilient protection systems for hybrid electric propulsion applications

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Title
Resilient protection systems for hybrid electric propulsion applications

CoPED ID
26d65276-6dd8-443a-b994-c775da485628

Status
Active

Funders

Value
No funds listed.

Start Date
Sept. 30, 2018

End Date
Sept. 29, 2022

Description

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Hybrid Electric Propulsion for aerospace offers the potential to deliver improved efficiency and reduced emissions and is a key part of the transition to low carbon propulsion. The proposed PhD will investigate viable grounding and protection solutions for resilient hybrid electric propulsion, and includes the study of hybrid electric propulsion architectures and solutions. Key areas of investigation include fault characterization and analysis, fault detection and location, fault management, and protection solutions supporting resilient system reconfiguration. This study will incorporate the influence of multiple power electronics and energy storage devices, higher voltage levels, DC power distribution, and novel composite material in the hybrid propulsion applications.

Patrick Norman SUPER_PER
Euan Reid STUDENT_PER

Subjects by relevance
  1. Emissions
  2. Power electronics
  3. Motors and engines
  4. Architecture
  5. Propellers
  6. Hybrid cars

Extracted key phrases
  1. Resilient hybrid electric propulsion
  2. Hybrid electric propulsion application
  3. Hybrid electric propulsion architecture
  4. Resilient protection system
  5. Hybrid propulsion application
  6. Resilient system reconfiguration
  7. Protection solution
  8. Low carbon propulsion
  9. Hybrid Electric Propulsion
  10. Fault management
  11. Fault detection
  12. Fault characterization
  13. Multiple power electronic
  14. DC power distribution

Related Pages

UKRI project entry

UK Project Locations
200 km
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