Patent application number | Description | Published |
20080203633 | Linear filament compression and torsion spring - A spring including a wire having an elasticity by which the wire is compressible by an external force to a first position at which first and second ends thereof of are separated by a first distance and when the force is removed or an electrical current applied, the wire is extensible in response to an internal spring force to a second position at which the wire is substantially straight. A spring assembly is disclosed including a plurality of inventive wires cross-coupled with a support structure consisting of a plurality of coaxial rings. In the assembly, the wires extend parallel to an axis through a center of the rings. | 08-28-2008 |
20090314890 | COLLAPSIBLE SHAPE MEMORY ALLOY (SMA) NOSE CONES FOR AIR VEHICLES, METHOD OF MANUFACTURE AND USE - A nose cone formed from a shape memory alloy (SMA) having a recoverable strain of at least 2% collapses about the dome for storage, deploys at launch to protect the sensor dome and reduce drag during atmospheric flight and is shed to allow sensing for terminal maneuvers. The SMA is shape-set at elevated temperatures in its Austenite phase with a memorized shape having a radius of curvature greater than that of the sensor dome to reduce aerodynamic drag. The temperature is reduced and the SMA collapsed to conform to the curvature of the sensor dome within the recoverable strain for storage. A first mechanism is configured to return the collapsed SMA to its memorized shape at launch or prior to going supersonic. In one embodiment, the SMA is stored below its Martensite finish temperature in a temperature-induced Martensite phase in which case the mechanism heats the SMA above the Austenite finish temperature to return the material to its memorized shape. In another embodiment, the SMA is stored above its Austenite finish temperature in which case collapsing the SMA places the material in a strain-induced Martensite phase. The mechanism holds the collapsed SMA in place and the releases the stored energy allowing the SMA to return to the memorized shape. | 12-24-2009 |
20100128244 | GIMBALED SYSTEM WITH OPTICAL COUDE PATH AND METHOD TRANSFERRING DATA - Embodiments of a gimbaled system with an optical coudé path and method for transferring data are generally described herein. In some embodiments, the gimbaled system includes optical coudé path to provide a data communication path with a gimbaled payload, an on-gimbal communication laser to transmit modulated camera data via the coudé path, and an off-gimbal communication detector to detect the camera data received via the coudé path. In some embodiments, the optical coudé path may include at least two mirrors to provide a bi-directional communication path through an azimuth axis and an elevation axis of the gimbaled payload. | 05-27-2010 |
20100139264 | SHAPE MEMORY ALLOY SEPARATING APPARATUSES - Embodiments of separating apparatuses are generally described herein. Other embodiments may be described and claimed. In an embodiment, a separating apparatus is provided that comprises a pre-strained member formed from a shape memory alloy that is configured to separate upon application of heat. | 06-10-2010 |
20110163487 | LINEAR FILAMENT COMPRESSION AND TORSION SPRING - A spring including a wire having an elasticity by which the wire is compressible by an external force to a first position at which first and second ends thereof of are separated by a first distance and when the force is removed or an electrical current applied, the wire is extensible in response to an internal spring force to a second position at which the wire is substantially straight. A spring assembly is disclosed including a plurality of inventive wires cross-coupled with a support structure consisting of a plurality of coaxial rings. In the assembly, the wires extend parallel to an axis through a center of the rings. | 07-07-2011 |
20110232278 | SHAPE MEMORY STORED ENERGY ASSEMBLIES AND METHODS FOR USING THE SAME - A shape memory stored energy assembly includes a projectile housing having a projectile lumen. A projectile is within the projectile lumen and the projectile is movable relative to the projectile housing. A shape memory actuator is coupled between the projectile anchored end and the projectile housing. The shape memory actuator is configured to transition from a strained energy stored configuration to a fractured kinetic delivery configuration at a specified temperature range to propel the projectile through the projectile lumen. A method includes storing energy in a shape memory actuator coupled with a projectile. The stored energy in the shape memory actuator is released and propels the projectile. Releasing the stored energy includes heating the shape memory actuator, tensioning the shape memory actuator, and fracturing the tensioned shape memory actuator at a fracture locus to propel the projectile away from the fracture locus. | 09-29-2011 |
20110232562 | SHAPE MEMORY THERMAL SENSORS - Embodiments of separating apparatuses are generally described herein. Other embodiments may be described and claimed. In one embodiment, a thermal sensor assembly includes a shape memory substrate anchored within an isolation housing and braced between first and second anchors. The shape memory substrate is configured to transition from the strained configuration to the fractured configuration at a specified temperature range, and the first substrate end fractures from the second substrate end at the specified temperature. In another embodiment, a fracture indicator is coupled with the shape memory substrate, and the fracture indicator is configured to indicate the fractured configuration corresponding to meeting or exceeding of the specified temperature. In one example, the specified temperature range includes a range of temperatures or a single temperature. | 09-29-2011 |
20110234362 | SHAPE MEMORY CIRCUIT BREAKERS - A shape memory circuit breaker includes a shape memory substrate having first and second opposed substrate ends. The shape memory substrate is configured to transition from a strained conductive configuration to a fractured non-conductive configuration. An isolation housing is coupled with the shape memory substrate. The isolation housing includes first and second anchors coupled near the first and second substrate ends. A brace extends between the first and second anchors, and the brace statically positions the first and second anchors and the respective first and second substrate ends. The shape memory substrate is configured to transition from the strained conductive configuration to the fractured non-conductive configuration at or above a specified temperature range corresponding to a specified overload current range or voltage range, and the first substrate end fractures from the second substrate end at or above the specified temperature range resulting in an open circuit. | 09-29-2011 |
20130070238 | MICRO-RADIAN CLASS LINE OF SIGHT AND CENTRATION STABILIZATION SYSTEM - This document discusses apparatus and methods for aligning and centering an articulated laser projection system. In an example, a laser projection system can include an alignment stabilization system configured to align an optical path to a reference and a centration stabilization system configured to center the optical path within an aperture. The alignment stabilization system can have an alignment stabilization processing path configured to receive alignment information from an alignment sensor, and the centration stabilization system can have a centration stabilization processing path configured to receive centration information from a centration sensor. | 03-21-2013 |
20130126148 | SYSTEM AND METHOD FOR A SWITCHABLE HEAT SINK - According to an embodiment of the disclosure, a system for selectively dissipating thermal energy includes a heat-generating structure, a first heat sink, a second heat sink, and a heat transfer element. The heat-generating structure generates thermal energy. The first heat sink is in thermal communication with the heat-generating structure. The heat transfer element is configured to be selectively positioned between the first heat sink and the second heat sink to establish a path for the transfer of thermal energy between the first heat sink and the second heat sink. Upon positioning the heat transfer element between the first heat sink and the second heat sink, at least a portion of the thermal energy from the heat-generating structure is allowed to travel through the first heat sink and through the heat transfer element to the second heat sink. | 05-23-2013 |
20130200208 | CHORD-EXPANDING AIR VEHICLE WINGS - An air vehicle wing includes foldable ribs coupled to a leading-edge spar. The ribs each have multiple rib segments which are foldable (hinged) relative to each other. Extension linkages, each with multiple extension linkage segments, pass through openings in the rib segments, and may be coupled to the rib segments with pin couplings, able to change relative angle between the individual rib segments and the extension linkage segments to which they are coupled. A skin may cover the ribs, to provide an outer surface of the wing that may be unfolded as the wing is expanded from a stowed, small-chord condition, to a deployed, large-chord condition. | 08-08-2013 |
20140102090 | HEAT-ACTUATED RELEASE MECHANISM - A release mechanism passively releases a mechanically coupling as a result of a temperature rise. The release mechanism includes a breakable element, such as a shape memory alloy (SMA) element, that is configured to break when the element is heated to a predetermined temperature. The breakage of the breakable element releases a mechanical coupling, such as a coupling holding a lid onto a container. The release mechanism may be part of a handle or other device to close the container. The release mechanism may have a mechanical load on it prior to release, a load that in part passes through the breakable element. Most of the load may pass through one or more other members of the release mechanism, providing the force for separation after the release mechanism is triggered. The release mechanism may be used to provide a passive way of releasing a mechanical coupling in response to heating. | 04-17-2014 |
20140215936 | FRICTION DAMPING MECHANISM FOR DAMPED BEAMS AND OTHER STRUCTURES - A system includes a structure configured to undergo oscillatory movement. The system also includes a friction damping clamp coupled to the structure. The friction damping clamp includes a housing having a groove. The friction damping clamp also includes a roller positioned at least partially within the groove, where the groove has first and second ramps. The roller is configured to move up each ramp of the groove so that more compression is applied on the structure and to move down each ramp of the groove so that less compression is applied on the structure. The roller may be configured to apply more compression on the structure to increase friction between portions of the structure, to apply less compression on the structure to decrease friction between the portions of the structure, and to apply substantially no compression on the structure when the roller is located at a center of the groove. | 08-07-2014 |
20140306473 | ROBOTIC GRABBER AND METHOD OF USE - A robotic finger includes a shape-memory alloy and a shape-memory polymer connected to and adjacent to the shape-memory alloy. Heating the shape-memory polymer causes it to soften, heating the shape-memory alloy causes the alloy to bend in the direction of the shape-memory polymer to press the shape-memory polymer against an object to be grasped, and cooling the shape-memory polymer causes it to stiffen and to retain its shape. An opposing member is positioned to cooperate with the finger to grasp an object positioned between the finger and the opposing member. A selectively controllable heat source is capable of applying heat to the finger. | 10-16-2014 |
20150084353 | PASSIVE SAFETY MECHANISM UTILIZING SELF-FRACTURING SHAPE MEMORY MATERIAL - A system includes a structure having a first structural element and a second structural element. The system also includes a latch configured to releasably secure the first structural element to the second structural element. The latch includes first and second portions. The latch also includes a ball lock configured to hold the first and second portions of the latch together when the ball lock is engaged. The ball lock is also configured to allow the first and second portions of the latch to separate when the ball lock is disengaged. The latch further includes a shape memory material member configured to fracture when exposed to an elevated temperature and thereby disengage the ball lock. The shape memory material member could include an elongated structure that is configured to decrease in length when exposed to the elevated temperature. The elongated structure could have at least one notch. | 03-26-2015 |