Abstract: Piezoelectric actuators for synthetic jets and other devices are disclosed having orthotropic piezoelectric bimorphs with increased out-of-plane displacements for greater responsiveness to applied electric fields. In some embodiments, the piezoelectric actuators may include interdigitated electrodes applied to a surface of a piezoelectric plate to produce greater in-plane strains in the plate and greater out-of-plane displacements of a flexible diaphragm of the synthetic jet. In other embodiments, the actuator includes an orthotropic piezoceramic plate having a greater d coupling coefficient in one in-plane direction and in the other in-plane direction to cause desired diaphragm out-of-plane displacements when an electric field is applied by electrodes.

Abstract: A synthetic vacuum generator has a case enclosing an interior cavity with an aperture through the case in communication with the cavity. A piston and a check valve are mounted in the case in fluid communication with the cavity and the aperture. The piston and check valve are configured with symbiotic resonant response to establish an outflow there through and inducing an inflow through the aperture upon reciprocation of the piston at a predetermined frequency.

Abstract: A synthetic jet actuator and a method for optimizing a synthetic jet actuator to meet operating requirements and physical constraints may include estimating dimension and a resonance frequency of an air cavity of the synthetic jet actuator, and using the estimated resonance frequency to the estimate dimensions of a piezoelectric actuator of the synthetic jet actuator. Individual simulations of the air cavity and piezoelectric actuator, and a coupled simulation may be performed using the estimated dimensions, and the dimensions may be revised and simulations re-executed to match the resonance frequencies of the air chamber and the piezoelectric actuator. The method maybe yield a synthetic jet actuator having a resonance frequency of the piezoelectric actuator that is approximately equal to a quarter-wavelength resonance frequency of the air cavity.

Abstract: An aperture partitioning element for an imaging system is disclosed. The aperture partitioning element includes a plurality of segments each including a reflective surface and a body. The plurality of segments are each independently moveable in at least one of an x-axis, a y-axis, and a z-axis of the aperture partitioning element. The aperture partitioning element also includes at least one positioner received within the body of a corresponding segment. The at least one positioner is actuated to move the corresponding segment in at least one of the x-axis, the y-axis, and the z-axis.

Abstract: A vibration damping system employs a component having a directionally sensitive element thereon, mounted to an aircraft, which experiences dynamic excitation that induces bending deflection in the component that will reorient the directionally sensitive element. At least one tuned mass damper is mounted on the component in an orientation in which an internal mass of the tuned mass damper is moveable such that the tuned massed damper absorbs and attenuates at least a portion of the deflective motion, to thereby suppress bending deflection of the component in the particular axial direction and generally maintain the linearity of the directionally sensitive element.

Abstract: A window includes a substantially transparent polymer window member and means for selectively stiffening the window member over its area to reduce sound transmitted through the window.

Abstract: A jet generator is controlled by providing an input signal at a variable frequency to the jet generator and to a simulated electrical load of the jet generator, measuring a difference in signals between the jet generator and the simulated electrical load to identify an optimum flow of a jet generated by the jet generator, and tuning the frequency of the input signal to maintain the jet at the optimum flow.

Abstract: A self-monitored controlled optical component system may include an electrostrictive actuator, a capacitor matched in capacitance to the electrostrictive actuator, a current source connected to the electrostrictive actuator and to the capacitor that supplies an electric current to the electrostrictive actuator and to the capacitor, an optical element connected to be moved by the electrostrictive actuator, and a comparator connected to receive a first output current from the electrostrictive actuator and a second output current from the capacitor, and output a differenced sensoriactuator signal proportional to the difference between the first output current and the second output current, the sensoriactuator signal representing a current associated with movement of the optical element by the electrostrictive actuator.

Abstract: A vehicle may include an operative sub-system positioned within a body of the vehicle, and a sensor assembly secured to the operative sub-system. The sensor assembly may include at least one sensor configured to detect vibration or shock energy, directed into the operative sub-system; and a processing unit configured to determine damage to the operative sub-system as damage data that is based on one or both of a magnitude and duration of the vibration or shock energy detected by the sensor(s). The sensor assembly may be self-powered.

Abstract: A self-monitored controlled optical component system may include an electrostrictive actuator, a capacitor matched in capacitance to the electrostrictive actuator, a current source connected to the electrostrictive actuator and to the capacitor that supplies an electric current to the electrostrictive actuator and to the capacitor, an optical element connected to be moved by the electrostrictive actuator, and a comparator connected to receive a first output current from the electrostrictive actuator and a second output current from the capacitor, and output a differenced sensoriactuator signal proportional to the difference between the first output current and the second output current, the sensoriactuator signal representing a current associated with movement of the optical element by the electrostrictive actuator.

Abstract: A method and apparatus for identifying a position of a deployable system. An apparatus comprises a sensor device. The sensor device comprises a sensor configured to detect at least one of first vibrations from a deployable system in a first position or second vibrations from the deployable system in a second position in which the first vibrations are different from the second vibrations. The sensor is further configured to generate information from detecting at least one of the first vibrations or the second vibrations.

Abstract: A vibration isolation assembly for an aerodynamic object comprises a viscoelastic inner layer disposed on the aerodynamic object and being configured to attenuate vibration. The vibration isolation assembly further comprises a rigid or stiff outer layer disposed on an inner layer. The vibration isolation assembly may attenuate the transmission of aerodynamically-induced vibration to components contained or mounted to the aerodynamic object.

Abstract: A synthetic jet muffler includes an exit end, a propagation path for conducting a first sound wave emitted by a synthetic jet generator to the exit end, and a shroud for conducting a second sound wave emitted from the synthetic jet generator in a direction opposite to the first sound wave to the exit end, wherein the shroud is disposed so that the first and second sound waves travel different distances to effect noise cancellation at the exit end.

Abstract: A jet generator is controlled by providing an input signal at a variable frequency to the jet generator and to a simulated electrical load of the jet generator, measuring a difference in signals between the jet generator and the simulated electrical load to identify an optimum flow of a jet generated by the jet generator, and tuning the frequency of the input signal to maintain the jet at the optimum flow.

Abstract: A synthetic jet muffler includes an exit end, a propagation path for conducting a first sound wave emitted by a synthetic jet generator to the exit end, and a shroud for conducting a second sound wave emitted from the synthetic jet generator in a direction opposite to the first sound wave to the exit end, wherein the shroud is disposed so that the first and second sound waves travel different distances to effect noise cancellation at the exit end.

Abstract: A strain amplification structure has a frame with a hexagonal structure incorporating a plurality of rigid beams that are connected to opposing end beams by a plurality of flexible joints. A piezoceramic actuator assembly is connected to the opposing end beams having a collar including an opening. A shaft providing an output is connected to the plurality of rigid beams with flexible joints and passes through the opening in the collar for non-interfering motion orthogonal to the actuator assembly.

Abstract: A strain amplification structure has a frame with a hexagonal structure incorporating a plurality of rigid beams that are connected to opposing end beams by a plurality of flexible joints. A piezoceramic actuator assembly is connected to the opposing end beams having a collar including an opening. A shaft providing an output is connected to the plurality of rigid beams with flexible joints and passes through the opening in the collar for non-interfering motion orthogonal to the actuator assembly.

Abstract: A strain amplification structure has a frame with a hexagonal structure incorporating a plurality of rigid beams that are connected to opposing end beams by a plurality of flexible joints. A piezoceramic actuator assembly is connected to the opposing end beams having a collar including an opening. A shaft providing an output is connected to the plurality of rigid beams with flexible joints and passes through the opening in the collar for non-interfering motion orthogonal to the actuator assembly.

Abstract: A system, apparatus, and method are disclosed for a resonant scanner for three-dimensional (3D) mapping. The system, apparatus, and method employ a small, lightweight articulating device that performs as a 3D Laser Detection and Ranging (LADAR) laser from a moving scanner platform in a way that provides geolocation and takes advantage of mechanical resonance to amplify motion in the tilt axis. The device is used to map terrain in 3D space. The disclosed method involves resonating the scanner platform of the device with a spring about a pivot. The method further involves determining with a position sensor the tilt position and/or resonance rate of the scanner platform. Further, the method involves applying torque with an actuator to the scanner platform, and controlling with a controller the resonance of the scanner platform.

Abstract: A system, apparatus, and method are disclosed for a resonant scanner for three-dimensional (3D) mapping. The system, apparatus, and method employ a small, lightweight articulating device that performs as a 3D Laser Detection and Ranging (LADAR) laser from a moving scanner platform in a way that provides geolocation and takes advantage of mechanical resonance to amplify motion in the tilt axis. The device is used to map terrain in 3D space. The disclosed method involves resonating the scanner platform of the device with a spring about a pivot. The method further involves determining with a position sensor the tilt position and/or resonance rate of the scanner platform. Further, the method involves applying torque with an actuator to the scanner platform, and controlling with a controller the resonance of the scanner platform.