Propeller pitch control system

Patent metadata

Field	Value
Publication number	US-10494084-B2
Application number	US-201715471185-A
Country	US
Kind code	B2
Filing date	Mar 28, 2017
Priority date	Mar 31, 2016
Publication date	Dec 3, 2019
Grant date	Dec 3, 2019

Abstract

A control system for controlling the pitch of a propeller, the system including a propeller shaft, a blade swivel device having a rotary control element suitable for placing the blades in an angular position corresponding to a desired propeller pitch, and a transmission presenting an outlet member coupled in rotation with the rotary control element of the blade swivel device. The transmission includes a variable speed drive having drive, control, and outlet rotors that are coupled in rotation respectively with the propeller shaft, with a control member, and with the outlet member of the transmission. With the variable speed drive, the speed of rotation of the outlet member of the transmission is a predetermined function of the speeds of rotation not only of the propeller shaft, but also of the control member.

First claim

The invention claimed is:

1. A control system for controlling pitch of a propeller, the propeller having blades designed to be driven in rotation by a propeller shaft, each blade being configured to pivot about a substantially radial axis of the blade, the system comprising:
the propeller shaft;
a blade swivel device comprising a rotary control element suitable for placing the blades in an angular position corresponding to a desired propeller pitch as a function of rotation of said rotary control element relative to the propeller shaft;
a transmission presenting an outlet member that is coupled to rotate with the rotary control element of the blade swivel device; and
a variable speed drive;
wherein
the variable speed drive has a drive rotor, a control rotor, and an outlet rotor;
said drive, control, and outlet rotors are coupled to rotate respectively with a drive member that is the propeller shaft, with a control member, and with the outlet member of the transmission, and consequently speeds of rotation of the drive, control, and outlet rotors are proportional respectively to the speeds of rotation of the drive, control, and said outlet members of the transmission;
the variable speed drive is configured to drive the outlet rotor in rotation at a speed that is a predetermined function of the speeds of rotation of the drive and control rotors; and
the outlet rotor is coupled to rotate with the outlet member via an epicyclic geartrain having two planet gears meshing with each other, carried by the propeller shaft, and meshing respectively with the outlet rotor of the variable speed drive and with the outlet member of the transmission.

2. The control system according to claim 1 , arranged in such a manner that the drive member and the rotary control element of the blade swivel device driven by the outlet member of the transmission necessarily rotate in the same direction.

3. The control system according to claim 1 , wherein the rotary control element of the blade swivel device is a wormscrew, and the blade swivel device further includes a nut arranged on the wormscrew.

4. The control system according to claim 3 , wherein the nut includes notches, each notch is configured to receive a blade attachment finger extending radially from a blade root along a radial attachment axis, and each attachment axis is offset relative to a radial opening for fastening the blade that is arranged in the periphery of the propeller shaft.

5. The control system according to claim 1 , wherein said rotary control element of the blade swivel device is a pitch adjustment rotor including one radial actuator rod for each blade, each actuator rod being configured to engage a blade and to impart a desired angular position thereto.

6. The control system according to claim 1 , wherein the transmission is arranged in such a manner that the speed of rotation of the outlet member is the sum of the speed of rotation of the drive member plus a value that is a function of the speed of rotation of the control member.

7. A propeller engine having a propeller and a control system according to claim 1 .

8. A control system for controlling pitch of a propeller, the propeller having blades designed to be driven in rotation by a propeller shaft, each blade being configured to pivot about a substantially radial axis of the blade, the system comprising:
the propeller shaft;
a blade swivel device comprising a rotary control element suitable for placing the blades in an angular position corresponding to a desired propeller pitch as a function of rotation of said rotary control element relative to the propeller shaft;
a transmission presenting an outlet member that is coupled to rotate with the rotary control element of the blade swivel device; and
a variable speed drive;
wherein
the variable speed drive has a drive rotor, a control rotor, and an outlet rotor;
said drive, control, and outlet rotors are coupled to rotate respectively with a drive member that is the propeller shaft, with a control member, and with the outlet member of the transmission, and consequently speeds of rotation of the drive, control, and outlet rotors are proportional respectively to the speeds of rotation of the drive, control, and outlet members of the transmission;
the variable speed drive is configured to drive the outlet rotor in rotation at a speed that is a predetermined function of the speeds of rotation of the drive and control rotors; and
the variable speed drive comprises a magnetic gear.

9. A propeller engine having a propeller and a control system according to claim 8 .

10. The control system according to claim 8 , wherein the rotary control element of the blade swivel device is a wormscrew, and the blade swivel device further includes a nut arranged on the wormscrew.

11. The control system according to claim 8 , wherein said rotary control element of the blade swivel device is a pitch adjustment rotor including one radial actuator rod for each blade, each actuator rod being configured to engage a blade and to impart a desired angular position thereto.

12. A control system for controlling pitch of a propeller, the propeller having blades designed to be driven in rotation by a propeller shaft, each blade being configured to pivot about a substantially radial axis of the blade, the system comprising:
the propeller shaft;
a blade swivel device comprising a rotary control element suitable for placing the blades in an angular position corresponding to a desired propeller pitch as a function of rotation of said rotary control element relative to the propeller shaft;
a transmission presenting an outlet member that is coupled to rotate with the rotary control element of the blade swivel device; and
a variable speed drive;
wherein
the variable speed drive has a drive rotor, a control rotor, and an outlet rotor;
said drive, control, and outlet rotors are coupled to rotate respectively with a drive member that is the propeller shaft, with a control member, and with the outlet member of the transmission, and consequently speeds of rotation of the drive, control, and outlet rotors are proportional respectively to the speeds of rotation of the drive, control, and outlet members of the transmission;
the variable speed drive is configured to drive the outlet rotor in rotation at a speed that is a predetermined function of the speeds of rotation of the drive and control rotors; and
said drive, control, and outlet rotors are coaxial, and of them, the control rotor, is an outer rotor.

13. The control system according to claim 12 , wherein the drive, control, and outlet rotors are coaxially arranged with the outlet rotor arranged between the control and drive rotors.

14. The control system according to claim 12 , wherein the drive, control, and outlet rotors are coaxially arranged with the drive rotor arranged between the control and outlet rotors.

15. A propeller engine having a propeller and a control system according to claim 12 .

16. The control system according to claim 12 , wherein the rotary control element of the blade swivel device is a wormscrew, and the blade swivel device further includes a nut arranged on the wormscrew.

17. The control system according to claim 12 , wherein said rotary control element of the blade swivel device is a pitch adjustment rotor including one radial actuator rod for each blade, each actuator rod being configured to engage a blade and to impart a desired angular position thereto.

Assignees

• Safran Aircraft Engines

Inventors

• Garassino Alain Pierre

Classifications

• H02K49/102

  Magnetic gearings, i.e. assembly of gears, linear or rotary, by which motion is magnetically transferred without physical contact (magnetized gearings with physical contact F16H13/12, F16H49/005) · CPC title

• F16H1/36

  with two central gears coupled by intermeshing orbital gears · CPC title

• F16H21/54

  for conveying or interconverting oscillating or reciprocating motions · CPC title

• B64C11/325

  comprising feathering, braking or stopping systems · CPC title

• B64C11/32 Primary

  mechanical · CPC title