초록

A method of controlling a Counter-Rotating Open-Rotor (CROR) includes measuring a speed of a first rotor and deriving a speed of a second rotor and controlling a pitch of the first rotor and the second rotor.

대표청구항 ▼

1. A method of controlling a Counter-Rotating Open-Rotor (CROR) comprising: measuring a speed of a first rotor to obtain a measured first rotor speed;measuring a power turbine output speed to obtain a measured power turbine speed;indirectly deriving a speed of a second rotor as a function of the mea

1. A method of controlling a Counter-Rotating Open-Rotor (CROR) comprising: measuring a speed of a first rotor to obtain a measured first rotor speed;measuring a power turbine output speed to obtain a measured power turbine speed;indirectly deriving a speed of a second rotor as a function of the measured first rotor speed and the measured power turbine speed to obtain a derived second rotor speed; andcontrolling a pitch of the first rotor and a pitch of the second rotor in response to the measured first rotor speed and the derived second rotor speed. 2. The method as recited in claim 1, wherein the first rotor is a forward rotor and the second rotor is an aft rotor along a common axis of rotation. 3. The method as recited in claim 1, wherein a gear system which drives the first rotor and the second rotor axially is located between the first rotor and the second rotor. 4. The method as recited in claim 1, wherein deriving the speed of the second rotor occurs in all control modes. 5. The method as recited in claim 1, further comprising preventing the second rotor from entering a coefficient of power (CP) bucket. 6. The method as recited in claim 1, further comprising restricting the second rotor to a low pitch stop. 7. The method as recited in claim 1, further comprising mechanically holding the second rotor at a low pitch stop. 8. The method as recited in claim 1, further comprising at least one pitch lock which prevents travel in a low pitch direction below a predetermined point. 9. The method as recited in claim 1, further comprising holding the second rotor at a feather stop when the first rotor is in Reverse. 10. A Counter-Rotating Open-Rotor (CROR) comprising: a first rotor;a second rotor;a power turbine; anda rotor control configured to receive a measured speed of the first rotor, receive a measured speed of the power turbine, derive a speed of the second rotor as a function of the first rotor measured speed and the power turbine measured speed, and command a pitch angle of the second rotor in response to the derived speed of the second rotor. 11. The CROR as recited in claim 10 wherein the first rotor is a forward rotor and the second rotor is an aft rotor along a common axis of rotation. 12. The CROR as recited in claim 10 further comprising a gear system which drives said first rotor and said second rotor, said gear system axially between said first rotor and said second rotor. 13. The CROR as recited in claim 10 wherein said rotor control module receives a Blade Angle feedback (Beta2 Feedback) of said second rotor. 14. The CROR as recited in claim 10 wherein said second rotor is prevented from entering a coefficient of power (CP) bucket. 15. The CROR as recited in claim 10 wherein a pitch of said second rotor is restricted to a Low Pitch Stop. 16. The method as recited in claim 1, wherein the indirect deriving of the includes deriving without directly measuring the pitch angle of the second rotor. 17. The method as recited in claim 1, wherein the derived second rotor speed is equal to the measured speed of the power turbine multiplied by a gear constant of a gear system configured to drive the first and second rotor and the measured speed of the first rotor subtracted therefrom. 18. The CROR as recited in claim 10, wherein the rotor control module is configured to derive the speed of the second rotor and to command the pitch angle of the second rotor without receiving a second rotor pitch angle feedback. 19. The CROC as recited in claim 10, further comprising a gear system configured to drive the first rotor and the second rotor, wherein the derived speed of the second rotor is equal to the measured speed of the power turbine multiplied by a gear constant of the gear system and the measured speed of the first rotor subtracted therefrom. 20. The CROC as recited in claim 19, wherein the gear system is located axially between the first and second rotor. 21. A method of controlling a Counter-Rotating Open-Rotor (CROR) comprising: indirectly deriving a speed of a second rotor as a function of a first rotor speed of a first rotor and a power turbine speed of a power turbine to obtain a derived second rotor speed; andcontrolling a pitch of the first rotor and a pitch of the second rotor in response to the first rotor speed and the derived second rotor speed.