Multi-stage drive mechanisms
AssigneeSimmonds Precision Products, Inc.
InventorsMatthew Plumer, Randy Buker
Life of this patent
Estimating the term…
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.
Claims19
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.
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.
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 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, wherein the control surface catch further includes a pin and an output shaft with a detent, wherein the pin is configured and adapted to disengage with the detent to allow rotation of the control surface about the deployment axis in the deployment stage, and then to engage with the detent to stop rotation of the control surface about the deployment axis in the control stage while allowing rotation about the control axis in the control stage.
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 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, 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, 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.
Dependencies are inferred from the claim text.