Abstract: A lateral flow assay device of the present disclosure has numerous features to ensure correct operation of the device under gravity, such as vent pockets for enabling the flow of sample fluid from one chamber to the next when the vent pocket is unsealed. The vent pockets have protrusions to help prevent accidental resealing. The device also can have a gasket to ensure free air movement between open vent pockets. Flow control features that protrude horizontally into a chamber proximal to an outlet act to deflect the flow to the side of the chamber opposite from the outlet, prior to the flow entering the outlet. Such features can reduce the flow velocity of the sample fluid and increase the effective fluid flow path length, enhance mixing of reagents with a sample, and enabling more accurate control of fluid flow in the device.

Abstract: An automated method for performing an assay of the present disclosure can be performed in a microfluidic device that is a lateral flow device having numerous features to ensure correct operation of the device under gravity, such as vent pockets for enabling the flow of sample fluid from one chamber to the next when the vent pocket is unsealed. Each chamber can have a reagent recess proximal to an inlet end of the chamber. A reagent pellet formed in a reagent recess can be effectively mixed with a sample as the sample flows into the chamber. A flexible circuit with patterned metallic electrical components disposed on a heat stable material can be in direct contact with fluid in the chambers and has resistive heating elements aligned with, for example, a chamber for performing an amplification reaction.

Abstract: An energy dispersion plug for use in an unmanned aerial vehicle (UAV) includes a blunt head section, a wedge section, and a rim section. The blunt head section has an outer side for receiving an impact force and an inner side opposite the outer side. The wedge section has a base end and a distal end opposite the base end. The wedge section extends at the base end from the inner side of the blunt head section towards the distal end and the distal end has a smaller cross-sectional area than the base end. The wedge section is shaped and sized to fit into an open end of a hollow structural member of the UAV and to transfer impact energy incident upon the blunt head section into the hollow structural member to shatter the hollow structural member into fragments.

Abstract: An energy dispersion plug for use in an unmanned aerial vehicle (UAV) includes a blunt head section, a wedge section, and a rim section. The blunt head section has an outer side for receiving an impact force and an inner side opposite the outer side. The wedge section has a base end and a distal end opposite the base end. The wedge section extends at the base end from the inner side of the blunt head section towards the distal end and the distal end has a smaller cross-sectional area than the base end. The wedge section is shaped and sized to fit into an open end of a hollow structural member of the UAV and to transfer impact energy incident upon the blunt head section into the hollow structural member to shatter the hollow structural member into fragments.

Abstract: Method and apparatus for secure wireless commerce are described.