System and method for propeller feedback ring position detection
AssigneePratt & Whitney Canada Corp.
InventorsJoseph Ernesto Marone, Ian Farrell
Life of this patent
Estimating the term…
Loading patent…
AssigneePratt & Whitney Canada Corp.
InventorsJoseph Ernesto Marone, Ian Farrell
Estimating the term…
A system and method for determining a position of a feedback ring of a propeller of an aircraft engine are provided. The feedback ring is coupled to the propeller to rotate with the propeller and to be displaced along a longitudinal axis with adjustment of a blade angle. An engagement member is configured to engage the feedback ring and to be displaced along a longitudinal direction substantially parallel to the longitudinal axis with displacement of the feedback ring. A sensor comprises a first member coupled to the engine and a second member coupled to the engagement member. The second member is moveable relative to the first member along the longitudinal direction as the engagement member is displaced. The sensor generates a signal indicative of a longitudinal position of the second member relative to the first member. A controller determines an axial position of the feedback ring from the sensor signal.
A feedback ring position detection system for a propeller of an aircraft engine, the propeller rotatable about a longitudinal axis and having an adjustable blade angle, the system comprising:
An aircraft engine comprising:
A method for determining an axial position of a feedback ring of a propeller of an aircraft engine, the propeller rotatable about a longitudinal axis and having an adjustable blade angle and the feedback ring rotatable with the propeller, the method comprising:
Dependencies are inferred from the claim text.