Multi-stage drive mechanisms

Patent metadata

Field	Value
Publication number	US-9429402-B2
Application number	US-201313869793-A
Country	US
Kind code	B2
Filing date	Apr 24, 2013
Priority date	Apr 24, 2013
Publication date	Aug 30, 2016
Grant date	Aug 30, 2016

Abstract

A multi-stage drive includes a linear actuator configured for linear movement along an actuation axis, and a control surface. The control surface is operatively connected to the linear actuator for rotation about a deployment axis in a deployment stage, and for rotation in a control stage about a control axis that is different from the deployment axis, so that movement of the linear actuator along the actuation axis drives rotation of the control surface in both the deployment stage and in the control stage.

First claim

What is claimed is:

1. A multi-stage drive for deploying and controlling a control surface comprising:
a linear actuator configured for linear movement along an actuation axis; and
a control surface operatively connected to the linear actuator for rotation about a deployment axis in a deployment stage, and for rotation in a control stage about a control axis that is different from the deployment axis, so that movement of the linear actuator along the actuation axis drives rotation of the control surface in both the deployment stage and in the control stage; and
a lock operatively connected to the linear actuator and control surface to lock the control surface against rotation around the control axis in the deployment stage, and to lock the control surface against rotation around the deployment axis in the control stage, wherein the lock includes a link having a first end operatively connected to the control surface for rotation of the control surface around the control axis, wherein the link further includes a second end engaging a swivel cap, and wherein the swivel cap includes a rim that prevents movement of the second end of the link beyond the swivel cap in the deployment stage to prevent movement of the link about the control axis, and wherein the rim of the swivel cap includes a notch that permits movement of the second end of the link in the control stage to allow rotation of the link about the control axis.

2. A multi-stage drive as recited in claim 1 , wherein the deployment axis and the control axis are oriented substantially perpendicular to one another.

3. A multi-stage drive as recited in claim 1 , wherein the linear actuator includes a drive motor and a mechanism for converting rotary motion from the motor into linear motion.

4. A multi-stage drive as recited in claim 1 , wherein the linear actuator is configured for rotation about a pivot axis in the deployment stage, wherein the pivot axis is different from the actuation axis.

5. A multi-stage drive as recited in claim 4 , wherein the pivot axis of the linear actuator is substantially parallel to the deployment axis.

6. A multi-stage drive as recited in claim 1 , wherein the control surface is a canard.

7. A multi-stage drive as recited in claim 1 , wherein the lock includes a control surface catch operatively connected to the control surface to allow rotation of the control surface in the deployment stage about the deployment axis, and to catch the control surface in the control stage to prevent rotation of the control surface about the deployment axis in the control stage.

8. A multi-stage drive as recited in claim 7 , wherein the lock includes a link having a first end operatively connected to the control surface for rotation of the control surface around the deployment axis during the deployment stage and around the control axis in the control stage, wherein the control surface catch is configured and adapted to prevent rotation of the link about the deployment axis in the control stage while allowing rotation about the control axis in the control stage.

9. A multi-stage drive for deploying and controlling a control surface comprising:
a linear actuator configured for linear movement along an actuation axis;
a control surface operatively connected to the linear actuator for rotation about a deployment axis in a deployment stage, and for rotation in a control stage about a control axis that is different from the deployment axis, so that movement of the linear actuator along the actuation axis drives rotation of the control surface in both the deployment stage and in the control stage; and
a lock operatively connected to the linear actuator and control surface to lock the control surface against rotation around the control axis in the deployment stage, and to lock the control surface against rotation around the deployment axis in the control stage, wherein the lock includes a swivel having an inner swivel member and a swivel cap configured for relative rotation, wherein the inner swivel member is operatively connected to the control surface for rotation about the deployment axis, and wherein the swivel includes a catch operatively connected to the inner swivel member and the swivel cap to allow relative rotation of the inner swivel member and the swivel cap in the deployment stage for rotation of the control surface about the deployment axis, and to catch and prevent relative rotation of the inner swivel member and the swivel cap in the control stage to prevent rotation of the control surface about the deployment axis.

10. A multi-stage drive as recited in claim 9 , further comprising:
a link having a first end operatively connected to the control surface for common rotation of the link with the control surface about the deployment and control axes and a second end opposite the first end; and
a swivel including an inner swivel member and a swivel cap configured for relative rotation, wherein the inner swivel member is operatively connected to the second end of the link for rotation about the deployment axis with the link in the deployment stage.

11. A multi-stage drive as recited in claim 10 , further comprising a catch operatively connected to the inner swivel member and the swivel cap to allow relative rotation of the inner swivel member and the swivel cap in the deployment stage for rotation of the control surface about the deployment axis, and to catch with the control surface in a deployed position to prevent relative rotation of the inner swivel member and the swivel cap to prevent rotation of the control surface about the deployment axis in the control stage.

12. A multi-stage drive as recited in claim 10 , further comprising:
an actuator link rotatably linked to the linear actuator; and
a pin extending from the second end of the link with a pin axis defined longitudinally along the pin, wherein the actuator link is rotatably and slideably connected to the pin for rotation about the pin axis in the deployment stage and for sliding along the pin in the control stage.

13. A multi-stage drive as recited in claim 12 , wherein the pin is substantially parallel to the link.

14. A multi-stage drive as recited in claim 9 , wherein the lock includes a control surface catch operatively connected to the control surface to allow rotation of the control surface in the deployment stage about the deployment axis, and to catch the control surface in the control stage to prevent rotation of the control surface about the deployment axis in the control stage.

15. A multi-stage drive as recited in claim 14 , wherein the lock includes a link having a first end operatively connected to the control surface for rotation of the control surface around the deployment axis during the deployment stage and around the control axis in the control stage, wherein the control surface catch is configured and adapted to prevent rotation of the link about the deployment axis in the control stage while allowing rotation about the control axis in the control stage.

16. A multi-stage drive as recited in claim 15 , wherein the lock includes a swivel having an inner swivel member operatively connected to a second end of the link for rotation about the deployment axis, wherein the control surface catch is configured and adapted to allow rotation of the link and the inner swivel member about the deployment axis in the deployment stage, and to prevent rotation of the link and the inner swivel member about the deployment axis in the control stage, while allowing the link to rotate about the control axis in the control stage.

17. A multi-stage drive as rec

Assignees

• Simmonds Precision Products

Inventors

• Plumer Matthew
• Buker Randy

Classifications

• F42B10/14 Primary

  using fins spread or deployed after launch, e.g. after leaving the barrel · CPC title

• Y10T74/18944

  Link connections · CPC title

• F16H21/54

  for conveying or interconverting oscillating or reciprocating motions · CPC title

• Y10T74/18888

  Reciprocating to or from oscillating · CPC title

• F42B10/64

  of fins · CPC title