Device for shifting a propeller into reverse, comprising an actuator acting on a crank pin

Patent metadata

Field	Value
Publication number	US-9366147-B2
Application number	US-201113885133-A
Country	US
Kind code	B2
Filing date	Nov 16, 2011
Priority date	Nov 16, 2010
Publication date	Jun 14, 2016
Grant date	Jun 14, 2016

Abstract

A device controlling shifting of a propeller turbine engine into reverse mode, by acting on a shaft for controlling pitch of propellers. The device includes: at least one centrifugal weight arranged to drive the propellers into a flag position thereof under action of the centrifugal force; and an actuator that can rotate the control shaft to shift the pitch of the propellers from a traction mode to a reverse mode, passing through a zero pitch position. The centrifugal weight is in an unstable equilibrium position in relation to action of the centrifugal force when the control shaft shifts the pitch of the propellers through the zero pitch position. Further, an actuation mechanism exerts a torque on the control shaft when the centrifugal weight is in the unstable equilibrium position, to prevent it from staying in this position.

First claim

The invention claimed is:

1. A device for controlling a shift into reverse of a propeller-type turbomachine, through action on a pitch control spindle that controls a pitch of propellers, the device comprising:
at least one bob weight mounted on and so as to project in cantilevered manner beyond the control spindle and configured to drive the propellers toward their feathered position under action of centrifugal force generated by rotation of the turbomachine;
an actuator configured to cause the control spindle to turn to shift the pitch of the propellers from a traction mode to a reverse mode, passing via a zero-pitch position; and
an actuating means that applies a torque to the control spindle when the control spindle turns to shift the pitch of the blades via a zero-pitch position, so as to prevent the control spindle from remaining in that position.

2. The device as claimed in claim 1 , wherein the bob weight is in a position of unstable equilibrium with respect to the action of the centrifugal force when the control spindle causes the pitch of the propellers to pass via the zero-pitch position.

3. The device as claimed in claim 1 , wherein the actuating means applies a torque to the control spindle both during the shift from the traction mode to the reverse mode and during a return from the reverse mode to the traction mode.

4. The device as claimed in claim 1 , wherein the actuator applies no torque to the control spindle when the bob weights are in the position of unstable equilibrium.

5. The device as claimed in claim 1 , wherein the actuating means applies its torque to the control spindle via a crank pin mounted with freedom to rotate via one of its ends on the bob weight.

6. The device as claimed in claim 5 , wherein the actuating means is held at one of its ends by a pivot spindle offset parallel to the control spindle and is returned in rotation about the pivot spindle, toward the crank pin, via a mechanism that creates a return torque.

7. The device as claimed in claim 6 , wherein the crank pin at its free end bears a transfer means for collaborating with the actuating means so as to transfer the torque supplied by the actuating means to the control spindle.

8. The device as claimed in claim 7 , wherein the actuating means includes a tongue and the transfer means includes a rod configured to slide along the tongue during the shift into reverse.

9. The device as claimed in claim 8 , wherein the tongue at its free end comprises a retaining means for limiting the sliding of the rod along the tongue during the shift into reverse, so as to provide a purchase for the crank pin.

10. The device as claimed in claim 9 , wherein the rod is in abutment against the retaining means before the bob weight reaches its position of unstable equilibrium.

11. The device as claimed in claim 10 , wherein the bob weight enters its position of unstable equilibrium, the rod is in abutment against the retaining means and the crank pin is oriented to push the bob weight beyond the unstable position.

12. A control device comprising:
the device of claim 1 ;
said actuating means comprises two actuating means;
a first means applying a torque to the crank pin for a shift from a position of use to the reverse position; and
second means applying a torque to the crank pin for return to the position of use.

13. A turbomachine propeller comprising a blade root including a device for controlling the shift into reverse as claimed in claim 1 .

14. A turbomachine comprising at least one propeller as claimed in claim 13 .

Assignees

• Gallet Francois
• Snecma

Inventors

• Gallet Francois

Classifications

• B64D2027/005

  Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR] · CPC title

• B64C11/48

  Units of two or more coaxial propellers · CPC title

• B64C11/346

  actuated by the centrifugal force or the aerodynamic drag acting on auxiliary masses or surfaces · CPC title

• F01D7/00 Primary

  Rotors with blades adjustable in operation; Control thereof (for reversing F01D1/30) · CPC title

• B64C11/325 Primary

  comprising feathering, braking or stopping systems · CPC title