Propeller blade pitch angle feedback from actuator rotation

Patent metadata

Field	Value
Publication number	US-11479339-B2
Application number	US-202016732726-A
Country	US
Kind code	B2
Filing date	Jan 2, 2020
Priority date	Jan 2, 2020
Publication date	Oct 25, 2022
Grant date	Oct 25, 2022

Abstract

A propeller control system for controlling a blade pitch angle including: a propeller blade extending from a blade base, the propeller blade being configured to rotate around a longitudinal axis to generate thrust for the propeller blade and rotate around a pitch change axis to adjust the blade pitch angle, wherein the pitch change axis extends through a center point of the blade base; a trunnion pin operably connected to the blade base at a location offset from the center point; a yoke plate operably connected to the trunnion pin; an actuator configured to move the yoke plate linearly along the longitudinal axis to rotate the trunnion pin and the propeller blade around the pitch change axis; and a transfer tube operably connected to the yoke plate, the transfer tube being free to rotate around the longitudinal axis as the actuator moves the yoke plate linearly along the longitudinal axis.

First claim

What is claimed is:

1. A propeller control system for controlling a blade pitch angle, the propeller control system comprising:
a propeller hub;
a propeller blade extending from a blade base, the propeller blade attached to the propeller hub and being configured to rotate around a longitudinal axis to generate thrust for the propeller blade and rotate around a pitch change axis to adjust the blade pitch angle of the propeller blade, wherein the pitch change axis extends through a center point of the blade base;
a trunnion pin operably connected to the blade base at a location offset from the center point of the blade base;
a yoke plate operably connected to the trunnion pin;
an actuator configured to move the yoke plate linearly along the longitudinal axis of the propeller blade to rotate the trunnion pin and the propeller blade around the pitch change axis;
a transfer tube operably connected to the yoke plate, the transfer tube being free to rotate around the longitudinal axis as the actuator moves the yoke plate linearly along the longitudinal axis; and
a blade angle sensing system configured to determine the blade pitch angle in response to a rotational direction and a rotational magnitude of the transfer tube relative to the propeller hub.

2. The propeller control system of claim 1 , wherein the blade angle sensing system further comprises:
a differential rotation sensor configured to detect the rotational direction and the rotational magnitude of the transfer tube relative to the propeller hub.

3. The propeller control system of claim 1 , wherein the blade angle sensing system further comprises:
a differential rotation sensor configured to detect the rotational velocity of the differential gear train output shaft.

4. The propeller control system of claim 1 , wherein the actuator is a hydraulic actuator, and wherein the transfer tube is configured to deliver hydraulic fluid through the transfer tube to the actuator.

5. A propeller control system for controlling a blade pitch angle, the propeller control system comprising:
a propeller blade extending from a blade base, the propeller blade being configured to rotate around a longitudinal axis to generate thrust for the propeller blade and rotate around a pitch change axis to adjust the blade pitch angle of the propeller blade, wherein the pitch change axis extends through a center point of the blade base;
a trunnion pin operably connected to the blade base at a location offset from the center point of the blade base;
a yoke plate operably connected to the trunnion pin;
an actuator configured to move the yoke plate linearly along the longitudinal axis of the propeller blade to rotate the trunnion pin and the propeller blade around the pitch change axis;
a transfer tube operably connected to the yoke plate, the transfer tube being free to rotate around the longitudinal axis as the actuator moves the yoke plate linearly along the longitudinal axis; and
a differential gear train mechanically connected to the transfer tube.

6. The propeller control system of claim 5 , further comprising:
a propeller hub, wherein the differential gear train is mechanically connected to the propeller hub.

7. The propeller control system of claim 6 , wherein the differential gear train further comprises:
a first input, the propeller hub mechanically connects to the differential gear train at the first input and is configured to rotate the first input at a first rotational velocity;
a second input, the transfer tube mechanically connects to the differential gear train at the second input and is configured to rotate the second input at a second rotational velocity; and
a differential gear train output shaft rotates in a first direction or a second direction with a rotational velocity proportional to the difference between the first rotational velocity and the second rotational velocity.

8. A method for controlling a blade pitch angle of a propeller blade, the method comprising:
activating an actuator operably connected to a yoke plate;
translating, using the actuator, the yoke plate along a longitudinal axis when the actuator is activated, the yoke plate being operably connected to a trunnion pin;
rotating, using the yoke plate, the trunnion pin around a pitch change axis of the propeller blade when the yoke plate is translated, the trunnion pin being operably connected to a blade base of the propeller blade at a location offset from a center point of the blade base;
rotating, using the trunnion pin, the blade base around the pitch change axis when the trunnion pin is rotated, wherein the pitch change axis extending through the center point of the blade base and the propeller blade extending from the blade base;
rotating, using the blade base, the propeller blade around the pitch change axis to adjust the blade pitch angle of the propeller blade when the blade base is rotated; and
rotating, using the yoke plate, a transfer tube around the longitudinal axis of when the yoke plate is translated, the propeller blade being configured to rotate around the longitudinal axis to generate thrust for the propeller blade; and
rotating a differential gear train using the transfer tube, the differential gear train being mechanically connecting the transfer tube.

9. The method of claim 8 , further comprising:
rotating the differential gear train using a propeller hub, wherein the differential gear train is mechanically connected to the propeller hub.

10. The method of claim 9 , further comprising:
rotating a first input of the differential gear train at a first rotational velocity, the propeller hub mechanically connects to the differential gear train at the first input; and
rotating a second input of the differential gear train at a second rotational velocity, the transfer tube mechanically connects to the differential gear train at the second input,
wherein a differential gear train output shaft of the differential gear train rotates in a first direction or a second direction with a rotational velocity proportional to the difference between the first rotational velocity and the second rotational velocity.

11. The method of claim 10 , further comprising:
detecting, using a differential rotation sensor, the rotational velocity of the differential gear train output shaft.

12. The method of claim 10 , further comprising:
rotating the differential gear train output shaft in a first direction when the first rotational velocity is greater than the second rotational velocity.

13. The method of claim 12 , further comprising:
rotating the differential gear train output shaft in a second direction when the first rotational velocity is less than the second rotational velocity, the second direction being opposite the first direction.

14. The method of claim 13 , further comprising:
maintaining the differential gear train output shaft rotationally stationary when the first rotational velocity is equal to the second rotational velocity.

15. A method for controlling a blade pitch angle of a propeller blade, the method comprising:
activating an actuator operably connected to a yoke plate;
translating, using the actuator, the yoke plate along a longitudinal axis when the actuator is activated, the yoke plate being operably connected to a trunnion pin;
rotating, using the yoke plate, the trunnion pin around a pitch change axis of the propeller blade when the yoke plate is translated, the trunnion pin being operably connected to a blade base of the propeller blade at a location offset from a center point of the blade base;
rotating, using the trunnion pin, the blade ba

Assignees

• Hamilton Sundstrand Corp

Inventors

• Danielson David R

Classifications

• B64C11/44

  electric · CPC title

• B64C11/301 Primary

  characterised by blade position indicating means · CPC title

• B64C11/42 Primary

  non-automatic · CPC title

• B64C11/303

  characterised by comprising a governor · CPC title

• B64C11/30

  Blade pitch-changing mechanisms · CPC title