Propeller blade angle feedback arrangement and method
Propeller blade angle feedback arrangement and method
- New search for: MARONE JOSEPH ERNESTO
- New search for: YAKOBOV ELLA
- New search for: FARRELL IAN
- New search for: BASSE OLIVIER
- New search for: DOBSON MARTIN
- New search for: CLERMONT MARTIN
- New search for: LAVOIE MARC
- New search for: MARONE JOSEPH ERNESTO
- New search for: YAKOBOV ELLA
- New search for: FARRELL IAN
- New search for: BASSE OLIVIER
- New search for: DOBSON MARTIN
- New search for: CLERMONT MARTIN
- New search for: LAVOIE MARC
There is provided a blade angle feedback assembly for a propeller of an aircraft engine. The propeller is rotatable about an axis and has propeller blades rotatable about respective spanwise axes to adjust a blade angle thereof. The blade angle feedback assembly comprises a feedback ring having a plurality of position markers disposed thereon, at least one sensor configured to provide feedback on the blade angle of the propeller blades by detecting a relative movement between the feedback ring and the at least one sensor, and at least one shielding element provided between the feedback ring and the propeller, the at least one shielding element configured to shield the feedback ring from electromagnetism.
Document information
Propeller blade angle feedback arrangement and method
2023-10-10
Patent
Electronic Resource
English