Pitch variation control device for the blades of a turbomachine rotor and method of operating the device

• US 5,595,474 A
• Filed: 04/04/1996
• Issued: 01/21/1997
• Est. Priority Date: 11/10/1993
• Status: Expired due to Fees

• Current Assignee: Hispano Suiza SA (Safran SA)
• Original Assignee: Hispano Suiza SA (Safran SA)
• Inventors: Girard, Francis
• Primary Examiner(s): Larson, James
• Application Number:
  US08/627,394
• Time in Patent Office: 292 Days
• Field of Search: 416/1, 416/46, 416/47, 416/48, 416/152, 416/153, 416/155, 416/162
• US Class Current: 416/1
• CPC Class Codes: B64C 11/44 electric
• CPC Class Codes: F01D 7/00 Rotors with blades adjustable in operation; Control thereof for reversing F01D1/30
• CPC Class Codes: F05D 2220/36 specially adapted for the fan of turbofan engines
• CPC Class Codes: F05D 2260/74 by turning around an axis perpendicular the rotor centre line
• CPC Class Codes: F05D 2260/76 the adjusting mechanism using auxiliary power sources
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A device for controlling the pitch of the blades of a turbomachine rotor includes an electric motor having a stator which is stationary and a rotor, preferably of the permanent magnet or asynchronous kind, which is mounted on the turbomachine shaft and is rigidly secured to a toothed wheel meshing with pinion sectors rigidly secured to the roots of the blades, and a mechanism for locking the blade roots in position which includes an electromechanical actuator rigidly secured to the shaft and electrically powered by a rotary transformer.

Claims

1. A pitch variation control device for blades of a turbomachine having a rotor wherein said blades are mounted on a disc rotated by a shaft of the turbomachine and each of said blades has a longitudinal axis and a root by which said blade is pivotable about its longitudinal axis, said control device comprising:

actuating means for changing the pitch of said blades and locking means for locking said roots of said blades, said actuating means including an electric motor having a stationary stator winding and a rotor which is secured to said turbomachine shaft and has no electrical connection to the stator,

a toothed wheel which is rigidly secured to said rotor of said electric motor, and pinion sectors rigidly secured to said roots of said blades and meshing with said toothed wheel, said locking means including an electromechanical actuator which is rigidly secured to said turbomachine shaft, and a rotary transformer electrically powering said actuator.

2. A device according to claim 1, which comprises fixed stops respectively corresponding to two extreme blade positions, said fixed stops defining maximum angular movement of an assembly formed by said pinion sectors, said toothed wheel and said rotor of said electric motor.

3. A device according to claim 2, which comprises at least one movable stop corresponding to at least one intermediate blade position between said two extreme positions.

4. A device according to claim 3, wherein said movable stop comprises an electromagnet powered by a rotary transformer.

5. A device according to claim 4, wherein said electromagnet comprises a winding in a casing rigidly secured to said turbomachine shaft and a first metal rod which is movable longitudinally in said winding.

6. A device according to claim 5, which comprises a return spring mounted around said rod.

7. A device according to claim 5, wherein said electromechanical actuator actuates a bolt retaining said blade roots in a predetermined position and includes a winding which is housed in a casing rigidly secured to said turbomachine shaft and within which a second metal rod is disposed for longitudinal movement, said second metal rod being rigidly secured to said bolt.

8. A device according to claim 7, which comprises a mechanism monitoring the position of the first rod of said electromagnet forming said movable stop and a mechanism monitoring the position of the rod of the bolt actuator, the position-monitoring mechanism for said first and second rod comprising a position detector and a position monitor electrically energized by at least one rotary transformer.

9. A device according to claim 8, wherein said position detector comprises an end of stroke contact.

10. A device according to claim 9, wherein said position monitor is electrically powered by first and second rotary transformers, wherein the first rotary transformer comprises a fixed primary winding connected to an electrical power supply and a secondary winding secured to said turbomachine shaft and the second rotary transformer comprises a primary winding secured to said turbomachine shaft and connected by said position detector to said secondary winding of said first rotary transformer and a secondary winding connected to said position monitor.

11. A device according to claim 9, wherein said position monitor is electrically powered by a single rotary transformer having first and second independent sets of windings, the first set of windings including a primary winding connected to an electrical power supply and a secondary winding connected to an oscillator by said position detector, and the second set of windings having a plurality of turns and includes a primary winding connected to the oscillator and a secondary winding connected to said position monitor.

12. A method of operating a pitch variation control device for blades of a turbomachine having a rotor wherein said blades are mounted on a disc rotated by a shaft of the turbomachine and each of said blades has a longitudinal axis and a root by which said blade is pivotable about its longitudinal axis, said control device including actuating means for changing the pitch of the blades and locking means for locking said roots of the blades, the actuating means including an electric motor having a stationary stator winding and a rotor which is secured to said turbomachine shaft and which has no electrical connection to the stator, a toothed wheel which is rigidly secured to the rotor of the electric motor, and pinion sectors rigidly secured to the roots of the blades and meshing with the toothed wheel, the locking means including an electromechanical actuator which is rigidly secured to the turbomachine shaft and a rotary transformer electrically powering the actuator;

the control device also including first stops respectively corresponding to two extreme blade positions, the first stops defining maximum angular movement of an assembly formed by said pinion sectors, said toothed wheel and said rotor of said electric motor;

a movable stop corresponding to at least one intermediate blade position between the two extreme positions, the movable stop comprising an electromagnet powered by a rotary transformer, wherein said electromagnet comprises a winding in a casing rigidly secured to the turbomachine shaft and a metal rod which is movable longitudinally in said winding, said electromechanical actuator actuates a bolt retaining the blade roots in a predetermined position and including a winding which is housed in a casing rigidly secured to the turbomachine shaft and within which a metal rod is disposed for a longitudinal movement, the metal rod of said electromechanical actuator being rigidly secured to the bolt;

means for monitoring the position of the rod of the electromagnet forming the movable stop and means for monitoring the position of the rod of the electromechanical actuator, the position-monitoring means for each of said rods comprising a position detector associated with a position monitor electrically energized by at least one rotary transformer when the rod is in a retracted position, the pitch variation control device changing over from a locked position against one of said first stops to a locked position against a second stop of said first stops, comprising the steps of;

measuring the speed of rotation of said turbomachine shaft and monitoring the position of said bolt;

powering said electric motor;

producing a rotating magnetic field between the stator and the rotor of said electric motor such that the magnetic field rotates at a different speed from said turbomachine shaft to produce a magnetic torque to clamp said blades in position against one of said first stops to facilitate unlocking of said blade roots and to retain said blades in said position during the unlocking operation;

supplying power to said electromechanical actuator to release said blade roots;

altering the speed of said rotating magnetic field so that the direction of the magnetic torque is reversed and said blades are rotated around their longitudinal axes from said one of said first stops as far as said second stop;

cutting off the power supply to lock said blade roots against said second stop; and

cutting off the power supply to said electric motor.

13. A method according to claim 12, wherein upon changing from a locked position against said one of said first stops to a locked position against the second stop, a position of said movable stop is monitored before powering said electric motor, the electromagnet of said movable stop is powered before powering said electromechanical actuator of said bolt, and the power supply to said electromagnet of said movable stop is cut off after rotation of said blades into position against said second stop so as to prevent accidental return of said blades to an initial position.

14. A method according to claim 13, which comprises, in the event of simultaneous malfunctioning of said bolt and of said movable stop, supplying power to said electric motor to produce a rotating magnetic field.

15. A pitch variation control device for blades of a turbomachine having a rotor wherein said blades are mounted on a disc rotated by a shaft of the turbomachine and each of said blades has a longitudinal axis and a root by which said blades are each pivotable about the longitudinal axes thereof, said control device comprising:

an actuator changing the pitch of said blades and a lock locking said roots of the blade, said actuator including an electric motor having a stationary stator winding and a rotor which is secured to said turbomachine shaft and has no electrical connection to the stator;

a toothed wheel which is rigidly secured to said rotor of said electric motor, and

pinion sectors rigidly secured to said roots of said blades and meshing with said toothed wheel, said lock including an electromechanical actuator which is rigidly secured to said turbomachine shaft, and a rotary transformer electrically powering said actuator.

16. A device according to claim 15, which comprises fixed stops respectively corresponding to two extreme blade positions, said fixed stops defining maximum angular movement of an assembly formed by said pinion sectors, said toothed wheel and said rotor of said electric motor.

17. A device according to claim 16, which comprises at least one movable stop corresponding to at least one intermediate blade position between said two extreme blade positions.

18. A device according to claim 17, wherein said movable stop comprises an electromagnet powered by a rotary transformer.

19. A device according to claim 18, wherein said electromagnet comprises a winding in a casing rigidly secured to said turbomachine shaft and a first metal rod which is movable longitudinally in said winding.

20. A device according to claim 19, which comprises a return spring mounted around said rod.

21. A device according to claim 19, wherein said electromechanical actuator actuates a bolt retaining said blade roots in a predetermined position and includes a winding which is housed in a casing rigidly secured to said turbomachine shaft and within which a second metal rod is disposed for longitudinal movement, said second metal rod being rigidly secured to said bolt.

22. A device according to claim 21, which comprises a monitor monitoring the position of the first rod of said electromagnet forming said movable stop and a monitor monitoring the position of the rod of the actuator which actuates the bolt, the position-monitoring monitor for each of said first rod and said rod of the actuator comprising a position detector associated with a position monitor electrically energized by at least one rotary transformer when said first rod and said rod of the actuator are respectively in a retracted position.

23. A device according to claim 22, wherein said position detector comprises an end of stroke contact.

24. A device according to claim 23, wherein said position monitor is electrically powered by first and second rotary transformers wherein the first rotary transformer comprises a fixed primary winding connected to an electrical power supply and a secondary winding secured to said turbomachine shaft and the second rotary transformer comprises a primary winding secured to said turbomachine shaft and connected by said position detector to said secondary winding of said first rotary transformer and a secondary winding connected to said position monitor.

25. A device according to claim 22, wherein said position monitor is electrically powered by a single transformer having first and second independent sets of windings, the first set of windings including a primary winding connected to an electrical power supply and a secondary winding connected to an oscillator by said position detector, and the second set of windings have a plurality of turns and include a primary winding connected to the oscillator and a secondary winding connected to said position monitor.

26. A method of operating a pitch variation control device for blades of a turbomachine having a rotor wherein said blades are mounted on a disc rotated by a shaft of the turbomachine and each of said blades has a longitudinal axis and a root by which said blade is pivotable about its longitudinal axis, said control device including an actuator changing the pitch of the blades and a lock locking said roots of the blades, the actuator including an electric motor having a stationary stator winding and a rotor which is secured to said turbomachine shaft and has no electrical connection to the stator, a toothed wheel which is rigidly secured to the rotor of the electric motor, and pinion sectors rigidly secured to the roots of the blades and meshing with the toothed wheel, the lock including an electromechanical actuator which is rigidly secured to the turbomachine shaft and a transformer electrically powering the actuator and a first metal rod;

the control device also including fixed stops respectively corresponding to two extreme blade positions, the fixed stops defining maximum angular movement of an assembly formed by said pinion sectors, said toothed wheel and said rotor of said electric motor;

a movable stop corresponding to at least one intermediate blade positioned between the two extreme blade positions, the movable stop comprising an electromagnet powered by a rotary transformer, wherein said electromagnet comprises a winding in a casing rigidly secured to the turbomachine shaft and a second metal rod which is movable longitudinally in said winding and wherein said electromechanical actuator actuates a bolt retaining the blade roots in a predetermined position and includes a winding which is housed in a casing rigidly secured to the turbomachine shaft and within which the first metal rod is disposed for longitudinal movement, the first metal rod being rigidly secured to the bolt;

a monitor monitoring the position of the second rod of the electromagnet forming the movable stop and a monitor monitoring the position of the second rod of the electromagnet, the position monitor for the first rod comprisintg a position detector associated with a position monitor electrically energized by at least one rotary transformer when the first rodis in a retracted position,the pitch variation control device changing over from a locked position against one of the fixed stops to a locked position against a second stop of the fixed stops, the method comprising the steps of;

measuring the speed of rotation of said turbomachine shaft and monitoring the position of said bolt;

powering said electric motor;

producing a rotating magnetic field between the stator and the rotor of said electric motor such that the magnetic field rotates at a different speed from said turbomachine shaft to produce a magnetic torque to clamp said blades in position against said one of said first stops to facilitate unlocking of said blade roots and to retain said blades in said position during the unlocking operation;

supplying power to said electromechanical actuator to release said blade roots;

altering the speed of said rotating magnetic field so that the direction of rotation of the magnetic torque is reversed and said blades are rotated around their longitudinal axes as far as said second stop;

cutting off the power supply so as to lock said blade roots against said second stop; and

cutting off the power supply to said electric motor.

27. A method according to claim 26, wherein upon changing from a first locked position to a second locked position, a position of said movable stop is monitored before powering said electric motor, the actuator of said movable stop is powered before powering said electromechanical actuator, and the power supply to said movable stop actuator is cut off after rotation of said blades into position against said second stop so as to prevent accidental return of said blades to an initial position in the event of a malfunction of blade root locking.

28. A method according to claim 27, which comprises, in the event of simultaneous malfunctioning of said bolt and of said movable stop, supplying power to said electric motor to produce a rotating magnetic field.