Flight control actuator drive

Patent metadata

Field	Value
Publication number	US-9701397-B2
Application number	US-201514639255-A
Country	US
Kind code	B2
Filing date	Mar 5, 2015
Priority date	Mar 5, 2014
Publication date	Jul 11, 2017
Grant date	Jul 11, 2017

Abstract

A flight control actuator drive including a first motor for providing a first rotational input, a second motor for providing a second rotational input and a speed summing device for combining the first and second rotational inputs into a rotational output for controlling an actuator. The speed summing device comprises first and second input gears to which the first and second motors are connected via first and second irreversible gears so that the first and second input gears can each transmit power in one direction only. The speed summing device may be a planetary gear assembly.

First claim

The invention claimed is:

1. A speed summing device for driving an actuator, the speed summing device comprising:
a first ring gear arranged to rotate about a central axis (X);
a second ring gear arranged to rotate about the central axis (X);
a plurality of pairs of planet gears, each pair comprising a first planet gear driveably connected to the first ring gear and a second planet gear driveably connected to the second ring gear, wherein the first and second planet gears of each pair are driveably connected to each other; and
a planet carrier providing a rotary output for controlling an actuator, the planet carrier being driveably connected to the planet gears such that movement of the planet gears around the central axis (X) causes the planet carrier to rotate but rotation of the planet gears about their own axes does not cause the planet carrier to rotate.

2. The speed summing device of claim 1 , wherein the planet carrier comprises a rotary output shaft for connection to an actuator.

3. The speed summing device of claim 1 , wherein the planet carrier comprises first and second plates and each of the planet gears is driveably connected to the first and second plates.

4. The speed summing device of claim 3 , wherein the first and second plates are spaced apart along the axial direction, with the first and second ring gears being positioned at axial positions between the first and second plates.

5. The speed summing device of claim 1 , wherein the first and second ring gears each comprise a row of internal teeth on their inner circumferential surfaces and a row of external teeth on their outer circumferential surfaces and the first and second planet gears engage the internal teeth of the first and second ring gears respectively.

6. The speed summing device of claim 1 , wherein the first and second planet gears of each pair are directly engaged with each other.

7. The speed summing device of claim 1 , wherein the first planet gears do not directly engage the second ring gear and the second ring gears do not directly engage the first ring gear.

8. The speed summing device of claim 7 , wherein the first and second planet gears each have an enlarged cross-section portion for engaging the internal teeth of the first and second ring gears respectively and a reduced cross-section portion, wherein the reduced cross-section portions of the first and second planet gears are aligned in the radial direction, relative to the central axis, with the second and first ring gears respectively.

9. The speed summing device of claim 8 , wherein the enlarged cross-section portions of each first planet gear engages directly with the enlarged cross-section portion of the second planet gear of the same pair.

10. The speed summing device of claim 1 , comprising two or more pairs of planet gears.

11. A flight control actuator drive comprising:
the speed summing device of claim 1 ;
a first motor driveably connected to the first ring gear via a first irreversible gear so that the first ring gear can transmit power in one direction only; and
a second motor driveably connected to the second ring gear via a second irreversible gear so that the second ring gear can transmit power in one direction only.

12. The flight control device actuator drive of claim 11 , wherein the first and second irreversible gears each comprise a worm gear.

13. A flight control actuator drive comprising:
a first motor for providing a first rotational input;
a second motor for providing a second rotational input; and
a speed summing device for combining the first and second rotational inputs into a rotational output for controlling an actuator, wherein the speed summing device comprises first and second input gears and the first and second motors are connected to the first and second input gears via first and second irreversible gears so that the first and second input gears can each transmit power in one direction only.

14. The flight control actuator drive of claim 13 , wherein the speed summing device comprises:
a first ring gear arranged to rotate about a central axis (X);
a second ring gear arranged to rotate about the central axis (X);
a plurality of pairs of planet gears, each pair comprising a first planet gear driveably connected to the first ring gear and a second planet gear driveably connected to the second ring gear, wherein the first and second planet gears of each pair are driveably connected to each other; and
a planet carrier providing a rotary output for controlling an actuator, the planet carrier being driveably connected to the planet gears such that movement of the planet gears around the central axis (X) causes the planet carrier to rotate but rotation of the planet gears about their own axes does not cause the planet carrier to rotate.

15. The flight control device actuator drive of claim 13 , wherein the first and second irreversible gears each comprise a worm gear.

16. The flight control device actuator drive of claim 14 , wherein the first and second irreversible gears each comprise a worm gear.

Assignees

• Goodrich Actuation Systems Sas

Inventors

• Grand Serge

Classifications

• B64C13/505

  having duplication or stand-by provisions · CPC title

• B64C13/341 Primary

  having duplication or stand-by provisions · CPC title

• F16H37/0826

  with only one output shaft · CPC title

• F16H1/36

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

• B64C13/50

  using electrical energy · CPC title