Tandem motor actuator

• US 7,255,304 B2
• Filed: 12/06/2004
• Issued: 08/14/2007
• Est. Priority Date: 12/08/2003
• Status: Expired due to Fees

• Current Assignee: General Dynamics Ordnance and Tactical Systems Incorporated (General Dynamics Corporation)
• Original Assignee: General Dynamics Ordnance and Tactical Systems Incorporated (General Dynamics Corporation)
• Inventors: May, Michael C., Ericson, Charles R.
• Primary Examiner(s): Collins; Timothy D.
• Application Number:
  US11/005,368
• Publication Number:
  US 20050150999A1
• Time in Patent Office: 981 Days
• Field of Search: 244/3.24, 244/3.28, 244/3.29
• US Class Current: 244/3.24
• CPC Class Codes: F42B 10/64 of fins

Abstract

The invention relates to an actuator system for a projectile having a first and second pair of opposing steering fins disposed in a transverse plane of the projectile. The first pair of opposing steering fins includes a first fin and second fin. The second pair of opposing steering fins includes a third fin and a fourth fin. The actuator system comprises a first motor assembly configured to control the position of the first pair of opposing steering fins, and a second motor assembly configured to control the position of the second pair of opposing steering fins. The first motor assembly and second motor assembly are mounted axially along an axis of the projectile such that a first portion of the first motor assembly is telescopically received within a second portion of the second motor assembly.

Claims

1. An actuator system for a projectile having a first and second pair of opposing steering fins disposed in a transverse plane of the projectile, the first pair of opposing steering fins including a first fin and second fin, the second pair of opposing steering fins including a third fin and a fourth fin, the actuator system comprising:

a first motor assembly configured to control the position of the first pair of opposing steering fins; and

a second motor assembly configured to control the position of the second pair of opposing steering fins,

wherein the first motor assembly and second motor assembly are mounted axially along an axis of the projectile such that a first portion of the first motor assembly is telescopically received within a second portion of the second motor assembly.

2. The actuator system of claim 1, wherein the first motor assembly is adapted to apply torque to a first output shaft coupled to the first fin and a second output shaft coupled to the second fin such that the first output shaft and the second output shaft rotate in a first rotational direction.

3. The actuator system of claim 2, wherein the first output shaft includes a first pinion gear, and the second output shaft includes a second pinion gear.

4. The actuator system of claim 3, wherein the first motor assembly comprises a first planetary gear system including a first gear member having

a first face gear for mating engagement with the first pinion gear and

a second face gear for mating engagement with the second pinion gear.

5. The actuator system of claim 4, wherein the first face gear is disposed forward of the first pinion gear, and the second face gear is disposed aft of the second pinion gear.

6. The actuator system of claim 4, wherein the first planetary gear system further includes:

a first ring gear coupled to the first gear member;

a first plurality of planetary gears for mating engagement with the first ring gear; and

a first motor adapted to drive the first plurality of planetary gears and cause the rotation of the first gear member.

7. The actuator system of claim 6, wherein the first planetary gear system further includes

a first central sun gear fixed to a housing of the projectile, the first plurality of planetary gears being adapted to revolve about the first central sun gear in mating engagement.

8. The actuator system of claim 2, wherein the second motor assembly is adapted to apply torque to a third output shaft coupled to the third fin and a fourth output shaft coupled to the fourth fin such that the third output shaft and the fourth output shaft rotate in a second rotational direction.

9. The actuator system of claim 8, wherein the second motor assembly comprises a second planetary gear system including a second gear member having

a third face gear for mating engagement with a third pinion gear of the third output shaft and

a fourth face gear for mating engagement with a fourth pinion gear of the fourth output shaft.

10. The actuator system of claim 9, wherein the third face gear is disposed forward of the third pinion gear, and the fourth face gear is disposed aft of the fourth pinion gear.

11. The actuator system of claim 10, wherein the second planetary gear system further includes:

a second ring gear coupled to the second gear member;

a second plurality of planetary gears for mating engagement with the second ring gear; and

a second motor adapted to drive the second plurality of planetary gears and cause the rotation of the second gear member.

12. The actuator system of claim 11, wherein the second planetary gear system further includes

a second central sun gear fixed to the first motor assembly, the second plurality of planetary gears being adapted to revolve about the second central sun gear in mating engagement.

13. The actuator system of claim 9, wherein the second portion of the second motor assembly comprises the second gear member.

14. The actuator system of claim 9, wherein the second gear member further includes a plurality of windows through which a plurality of motor mounts attach to a housing of the projectile.

15. In a projectile having a plurality of steering fins disposed in a first transverse plane of the projectile, the plurality of steering fins including a first fin opposing a second fin, and a third fin opposing a fourth fin, an actuator system for controlling the positioning of the plurality of steering fins comprising:

a first forward motor assembly adapted to apply torque to a first output shaft coupled to the first fin and a second output shaft coupled to the second fin such that the first output shaft and the second output shaft rotate in a first rotational direction;

a second rearward motor assembly adapted to apply torque to a third output shaft coupled to the third fin and a fourth output shaft coupled to the fourth fin such that the third output shaft and the fourth output shaft rotate in a second rotational direction,

wherein the first motor assembly and second motor assembly are mounted axially along an axis of the projectile such that a first portion of the first motor assembly is telescopically received within a second portion of the second motor assembly.

16. The actuator system of claim 15, wherein:

the first motor assembly comprises a first planetary gear system including a first gear member having a first face gear for mating engagement with a first pinion gear of the first output shaft and a second face gear for mating engagement with a second pinion gear of the second output shaft, and

the second motor assembly comprises a second planetary gear system including a second gear member having a third face gear for mating engagement with a third pinion gear of the third output shaft and a fourth face gear for mating engagement with a fourth pinion gear of the fourth output shaft.

17. The actuator system of claim 16, wherein:

the first face gear is disposed forward of the first pinion gear, and the second face gear is disposed aft of the second pinion gear, and

the third face gear is disposed forward of the third pinion gear, and the fourth face gear is disposed aft of the fourth pinion gear.

18. The actuator system of claim 16, wherein:

the first planetary gear system further includes

a first ring gear coupled to the first gear member;

a first plurality of planetary gears for mating engagement with the first ring gear; and

a first motor adapted to drive the first plurality of planetary gears and cause the rotation of the first gear member; and

the second planetary gear system further includes

a second ring gear coupled to the second gear member;

a second plurality of planetary gears for mating engagement with the second ring gear; and

a second motor adapted to drive the second plurality of planetary gears and cause the rotation of the second gear member.

19. The actuator system of claim 18, wherein the first motor is at least partially disposed within the second gear member.

20. The actuator system of claim 18, wherein the second gear member further includes a plurality of windows through which a plurality of motor mounts attach the first motor to a housing of the projectile.