Abstract: A bowl may be configured to include an outer body that has a u-shaped cross section, and the outer body may have a bottom configured to support the bowl on a surface, the bottom also including a circular groove around a circumference of the bottom and a bracket within the circular groove, wherein a foot is inserted within the groove, and wherein the foot is secured to the circular groove by the bracket. The bowl may include an inner body, wherein the inner body is concave and dome-shaped. The inner body may hold a liquid or solid, and the inner body is connected to an upper edge of the outer body. An internal cavity is formed by the outer body and inner body, and the internal cavity is insulative. The connection formed by the upper edge of the outer body and the inner body may be seamless.

Abstract: This disclosure relates to a lid assembly that has a lid assembly for a container, such as a drinking container, that includes a lid member, and a pouring member, wherein the lid member and pouring member are releasably connected to the container. The lid member may include a body member, a handle portion connected to the body member, an internal threaded portion, an internal receiving portion, and a lid gasket member arranged in the internal receiving portion. The pouring member may include a spout collar, a spout, and a spout opening extending through the spout, wherein the spout extends from the spout collar and includes an upper end above an upper surface of the spout collar. The lid assembly has a closed orientation that prevents liquid from flowing through the opening of the pouring member and an open orientation that allows liquid to flow through the opening of the pouring member.

Abstract: A system for disrupting Radio Frequency communication of a plurality of unmanned aircraft. The system comprises: a directional antenna; a transmitter; a drive system connected to the directional antenna and configured to move the directional antenna; and a control system. The control system causes the transmitter to generate a signal waveform configured to disrupt Radio Frequency communication of an unmanned aircraft for emission by the directional antenna, and causes the drive system to move the directional antenna such that each of the plurality of unmanned aircraft is irradiated intermittently by the emitted radiation. Each of the plurality of unmanned aircraft is irradiated for a first period of time and not irradiated for a second period of time, the second period of time is less than or equal to 5 seconds.

Abstract: A system for disrupting Radio Frequency communication of a plurality of unmanned aircraft. The system comprises: a directional antenna; a transmitter; a drive system connected to the directional antenna and configured to move the directional antenna; and a control system. The control system causes the transmitter to generate a signal waveform configured to disrupt Radio Frequency communication of an unmanned aircraft for emission by the directional antenna, and causes the drive system to move the directional antenna such that each of the plurality of unmanned aircraft is irradiated intermittently by the emitted radiation. Each of the plurality of unmanned aircraft is irradiated for a first period of time and not irradiated for a second period of time, the second period of time is less than or equal to 5 seconds.