Granted Patent B2

US 12,291,321 · App. 17/988,325 · Granted May 6, 2025

Inventors: Thibaut Marger (Beduer, FR); Romain Bouloc (Saint-Félix, FR)

Assignee: RATIER-FIGEAC SAS

B64C11/38B64C27/64

Abstract

Claims (60)

1. A pitch change actuation system for varying a propeller blade pitch, the pitch change actuation system comprising:

an actuator body defining an interior volume; and

a chamber separator located within the interior volume of the actuator body and dividing the interior volume into a first chamber and a second chamber, the two chambers being fluidly separated by the chamber separator;

wherein the first and second chambers are configured to receive hydraulic fluid;

wherein the actuator body is configured to translate relative to the chamber separator in response to a difference in hydraulic pressure between the first chamber and second chamber; and

wherein the translation of the actuator body is configured to effect a change in propeller blade pitch;

the pitch change actuation system further comprising:

a transfer tube, wherein the transfer tube is coupled to the actuator body; and

a shaft extending axially from the chamber separator and wherein the actuator body is configured to translate with respect to the shaft;

wherein the actuator body is slidably mounted on the shaft such that the actuator body may slidably translate along the shaft with respect to the chamber separator;

wherein a portion of the transfer tube is received within the actuator body;

wherein the transfer tube is configured to provide hydraulic fluid to the first and second chambers;

wherein the actuator body comprises a fluid passageway that extends from the transfer tube to the first or second chamber such that the transfer tube and the first or second chamber are in fluid communication.

2. The pitch change actuation system of claim 1 , wherein

the actuator body comprises an aperture at an end of the actuator body and the shaft extends through the aperture.

3. The pitch change actuation system of claim 1 , wherein

the shaft is configured to abut or otherwise engage with a propeller hub cover at an axially forward end of the shaft.

4. The pitch change actuation system of claim 1 , wherein:

the actuator body is configured to engage with a propeller blade pitch kinematic; the actuator body comprises a flange extending radially outwards of an outer surface of the actuator body; and

the flange is configured for mechanically coupling the actuator body to the propeller blade pitch kinematic.

5. The pitch change actuation system of claim 1 , wherein:

the actuator body comprises a first actuator body portion and a second actuator body portion coupled together to define the interior volume; and

the first and second actuator body portions each comprise a flange and the first actuator body portion and the second actuator body portion are fastened to one another via at least one fastener extending through the flanges of the first and second actuator body portions.

6. A pitch change actuation system for varying a propeller blade pitch, the pitch change actuation system comprising:

an actuator body defining an interior volume; and

a chamber separator located within the interior volume of the actuator body and dividing the interior volume into a first chamber and a second chamber, the two chambers being fluidly separated by the chamber separator;

wherein the first and second chambers are configured to receive hydraulic fluid;

wherein the actuator body is configured to translate relative to the chamber separator in response to a difference in hydraulic pressure between the first chamber and second chamber; and

wherein the translation of the actuator body is configured to effect a change in propeller blade pitch;

pitch change actuation system further comprising:

a shaft extending axially from the chamber separator and wherein the actuator body is configured to translate with respect to the shaft;

wherein the actuator body is slidably mounted on the shaft such that the actuator body may slidably translate along the shaft with respect to the chamber separator;

wherein the pitch change actuation system further comprises:

a transfer tube, wherein the transfer tube is coupled to the actuator body, wherein a portion of the transfer tube is received within the actuator body and the transfer tube is configured to provide hydraulic fluid to the first and second chambers; and

wherein the actuator body comprises a coupling that connects the transfer tube to the actuator body,

wherein the coupling is configured to prevent relative axial displacement between the actuator body and transfer tube and prevent relative rotation between the actuator body and the transfer tube about a longitudinal axis of the pitch change actuation system, and allow relative rotation of the transfer tube with respect to the actuator body about axes perpendicular to the longitudinal axis.

7. The pitch change actuation system of claim 6 , wherein

the shaft comprises an interior fluid passageway configured to fluidly couple at least one of the first and second chambers to the transfer tube;

wherein the shaft comprises fluid outlets to provide fluid from the interior fluid passageway to at least one of the first and second chambers.

8. A propeller assembly comprising:

a propeller hub;

a propeller blade mounted to the propeller hub; and

the pitch change actuation system of claim 6 .

9. A propeller assembly as claimed in claim 8 , wherein the actuator body intersects a plane of the propeller blade.

10. A method of controlling the propeller assembly of claim 8 , the method comprising:

varying the difference in hydraulic pressure acting on either side of the chamber separator such that the actuator body enclosing the chamber separator translates relative to the chamber separator,

wherein the translation of the actuator body effects a change in propeller blade pitch.

11. A method of installing a pitch change actuation system as claimed in claim 6 , in a propeller assembly, comprising inserting the pitch change actuation system into a propeller hub.

12. The pitch change actuation system of claim 6 , wherein the shaft comprises an interior fluid passageway configured to fluidly couple at least one of the first and second chambers to the transfer tube; and

wherein the shaft comprises fluid outlets to provide fluid from the interior fluid passageway to at least one of the first and second chambers.

13. The pitch change actuation system of claim 6 , wherein

the actuator body comprises an aperture at an end of the actuator body and the shaft extends through the aperture.

14. The pitch change actuation system of claim 6 , wherein

the shaft is configured to abut or otherwise engage with a propeller hub cover at an axially forward end of the shaft.

15. The pitch change actuation system of claim 6 , wherein:

the actuator body is configured to engage with a propeller blade pitch kinematic; the actuator body comprises a flange extending radially outwards of an outer surface of the actuator body; and

the flange is configured for mechanically coupling the actuator body to the propeller blade pitch kinematic.

16. The pitch change actuation system of claim 6 , wherein:

the actuator body comprises a first actuator body portion and a second actuator body portion coupled together to define the interior volume; and

the first and second actuator body portions each comprise a flange and the first actuator body portion and the second actuator body portion are fastened to one another via at least one fastener extending through the flanges of the first and second actuator body portions.

Assignments (1)

Priority Claims (1)

Continuity (1)

References Cited (10)