Modular Actuation Device for an Aerodynamic Control Surface of a Missile

Patent metadata

Field	Value
Publication number	US-2016226338-A1
Application number	US-201414155088-A
Country	US
Kind code	A1
Filing date	Jan 14, 2014
Priority date	Jul 23, 2013
Publication date	Aug 4, 2016
Grant date	—

Abstract

A modular actuation device for an object, such as an aerodynamic control surface of a missile. The modular actuation device can include an outer support structure configured to couple with an external support member, such as a structural portion of a missile. The modular actuation device can also include an electric motor to provide an input torque and having an outer casing coupled to the outer support structure. The modular actuation device can further include an epicyclic gear train disposed within the outer support structure and operably coupled to the electric motor to receive the input torque. The epicyclic gear train can be configured to provide an output torque to move the object. In addition, the modular actuation device can include a torque output member disposed at least partially within the outer support structure and coupled to the epicyclic gear train to receive the output torque. The torque output member can be configured to couple with the object.

First claim

What is claimed is:

1 . A modular actuation device comprising:
an outer support structure; an electric motor to provide an input torque and having an outer casing coupled to the outer support structure; an epicyclic gear train disposed within the outer support structure and operably coupled to the electric motor to receive the input torque, wherein the epicyclic gear train is configured to provide an output torque to move an object; a torque output member disposed at least partially within the outer support structure and coupled to the epicyclic gear train to receive the output torque, wherein the torque output member is configured to couple with the object; and a first bearing and a second bearing disposed between the torque output member and the outer support structure, wherein the first and second bearings are of different types.

2 . The modular actuation device of claim 1 , wherein the epicyclic gear train comprises at least two-stages.

3 . The modular actuation device of claim 2 , wherein the at least two-stages comprises first stage components disposed between the electric motor and second stage components.

4 . The modular actuation device of claim 2 , wherein the at least two-stages comprises third stage components disposed between first stage components and second stage components.

5 . The modular actuation device of claim 1 , wherein the first bearing comprises a platform needle roller thrust bearing and the second bearing comprises a radial ball bearing.

6 . The modular actuation device of claim 1 , wherein the electric motor comprises a brushless or brushed DC motor.

7 . The modular actuation device of claim 1 , further comprising a position sensor associated with the electric motor.

8 . The modular actuation device of claim 1 , wherein the outer support structure and the outer casing of the electric motor are configured in a cylindrical form factor.

9 . The modular actuation device of claim 1 , wherein an output shaft of the electric motor is configured to transfer torque directly to a sun gear of the epicyclic gear train.

10 . The modular actuation device of claim 9 , wherein the sun gear and the output shaft are rotatable about a common axis.

11 . The modular actuation device of claim 9 , wherein a portion of the output shaft forms the sun gear.

12 . The modular actuation device of claim 1 , wherein the torque output member comprises a planetary gear carrier.

13 . The modular actuation device of claim 1 , wherein the epicyclic gear train comprises a ring gear that is integral with the outer support structure.

14 . The modular actuation device of claim 1 , wherein the outer support structure comprises an annular cap to secure the torque output member to the outer support structure and provide an opening to facilitate access to the torque output member for coupling with the object.

15 . The modular actuation device of claim 1 , wherein an axis of rotation of the electric motor is parallel to an axis of rotation of the torque output member.

16 . An actuation system comprising:
an external support member and an object moveable relative to the external support member; and a modular actuation device, having
an outer support structure coupled with the external support member,
an electric motor to provide an input torque and having an outer casing coupled to the outer support structure,
an epicyclic gear train disposed within the outer support structure and operably coupled to the electric motor to receive the input torque, wherein the epicyclic gear train is configured to provide an output torque to move the object, and
a torque output member disposed at least partially within the outer support structure and coupled to the epicyclic gear train to receive the output torque, wherein the torque output member is configured to couple with the object,
wherein the external support member comprises a cylindrical opening configured to receive at least a portion of the modular actuation device.

17 . The system of claim 16 , wherein the object comprises an aerodynamic control surface.

18 . (canceled)

19 . The system of claim 16 , wherein a longitudinal axis of the cylindrical opening is parallel to an axis of rotation of the electric motor.

20 . The system of claim 16 , wherein an axis of rotation of the electric motor is parallel to an axis of rotation of the torque output member.

21 . The system of claim 16 , wherein the outer support structure is coupled with the external support member via one or more fasteners.

22 . A method for facilitating actuation of an object, the method comprising:
providing a modular actuation device having
an outer support structure,
an electric motor to provide an input torque and having an outer casing coupled to the outer support structure,
an epicyclic gear train disposed within the outer support structure and operably coupled to the electric motor to receive the input torque, wherein the epicyclic gear train is configured to provide an output torque to move an object,
a torque output member disposed at least partially within the outer support structure and coupled to the epicyclic gear train to receive the output torque, and
a first bearing and a second bearing disposed between the torque output member and the outer support structure, wherein the first and second bearings are of different types;
facilitating coupling of the outer support structure with an external support member; and facilitating coupling of the torque output member with the object.

23 . The method of claim 22 , wherein the axis of rotation of the electric motor is coaxial to the axis of rotation of the torque output member.

Assignees

• Raytheon Co

Inventors

• Bugge John F

Classifications

• H02K7/116 Primary

  with gears · CPC title

• F42B14/00

  Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels · CPC title

• F41G3/00

  Aiming or laying means (sighting devices F41G1/00; determining direction, distance or velocity by use of radio or other waves G01S; computers G06; antennas H01Q) · CPC title

• F16H1/46

  Systems consisting of a plurality of gear trains each with orbital gears, {i.e. systems having three or more central gears} · CPC title

• F41A27/22

  Traversing gear (F41A27/18 takes precedence) · CPC title