Novel Electric Field Sensors for Advanced Aero-Engine Monitoring

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Title
Novel Electric Field Sensors for Advanced Aero-Engine Monitoring

CoPED ID
858f2002-8949-4f06-9056-cbafeb096f7f

Status
Closed


Value
£1,045,026

Start Date
Jan. 1, 2013

End Date
July 30, 2015

Description

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This project is developing a novel electric potential sensing technique for use in gas turbine engine monitoring. Specifically the project seeks to optimise the sensor for measurement of ultra-high temperature. This could lead to an industry first of measuring combustion exit temperature, which would have a significant impact on engine efficiency, fuel consumption and emissions. However, as a second objective, the sensor will then be optimised to allow measurement of high temperature blade tip clearance and corollary parameters such as rotational speed. In this case, the technology could displace several existing techniques and improve current temperature limitations. The project will develop the sensors, electronics and associated packaging demonstrators for proof-of-concept tests via a range of laboratory and small engine trials. The project team consists of Meggitt (Lead), the University of Sussex, and Plessey Semiconductors.

Mark Langley PM_PER

Subjects by relevance
  1. Measurement
  2. Temperature
  3. Emissions
  4. Optimisation
  5. Gas turbines
  6. Sensors
  7. Combustion engines
  8. Gas engine

Extracted key phrases
  1. Novel Electric Field Sensors
  2. Gas turbine engine monitoring
  3. Engine monitoring
  4. Novel electric potential sensing technique
  5. High temperature blade tip clearance
  6. Advanced Aero
  7. Project team
  8. Current temperature limitation
  9. Combustion exit temperature
  10. Small engine trial
  11. Engine efficiency
  12. Sensor
  13. Packaging demonstrator
  14. Concept test
  15. Measurement

Related Pages

UKRI project entry

UK Project Locations