An inflatable beacon antenna assembly includes an inflatable sock, an antenna, an attachment port, and a ballast. The inflatable sock may have an inflated state and a deflated state, where the inflatable sock assumes an elongated configuration in the inflated state. The antenna may extend along the length of the inflatable sock. The attachment port may be configured for operable connection to an inflation mechanism. Two or more integrated antennas can be used for multi-frequency VHF/UHF beacon operation and/or a GPS antenna for position location.

An inflatable beacon antenna assembly includes an inflatable sock, an antenna, an attachment port, and a ballast. The inflatable sock may have an inflated state and a deflated state, where the inflatable sock assumes an elongated configuration in the inflated state. The antenna may extend along the length of the inflatable sock. The attachment port may be configured for operable connection to an inflation mechanism. Two or more integrated antennas can be used for multi-frequency VHF/UHF beacon operation and/or a GPS antenna for position location.

The present disclosure relates to the technical field of antennas and provides a dual-frequency current-balancing quadrifilar helical antenna, which belongs to the technical field of antennas in multi-mode global satellite navigation system. The dual-frequency current-balancing quadrifilar helical antenna comprises a radiating part and a feeding part, wherein: the radiating part comprises a hollow column and four sets of spiral arms with the same specifications and equal intervals; the spiral arms are wound on a surface of the hollow column and the feeding part is mounted at an end of the hollow column; each set of spiral arms comprises a main radiating arm and an auxiliary radiating arm; terminals of the main radiating arm and the auxiliary radiating arm are open-circuited or short-circuited, and a coupling component is arranged at an open-circuited or short-circuited terminal. The dual-frequency current-balancing quadrifilar helical antenna provided in the present disclosure can increase the energy of a parasitic frequency band, improve the performance of the parasitic frequency band, and reduce the size of the antenna.

A four-arm helical antenna is provided, including: a metal top surface; four groups of helical antennas connected to the metal top surface to constitute a hollow cylinder, wherein any group of helical antennas comprises an antenna main arm and an antenna branch aria connected to each other, and the antenna main arm comprises a first bending portion arranged on a side surface of the hollow cylinder and a second bending portion arranged on a top surface of the hollow cylinder, and the antenna branch arm comprises a third bending portion arranged on the side surface of the hollow cylinder. The whole four-arm helical antenna is easy to adjust, and the antenna size can be adjusted flexibly according to installation requirements, and it's more suitable for miniaturization application requirements of the four-arm helical antenna.

A four-arm helical antenna is provided, including: a metal top surface; four groups of helical antennas connected to the metal top surface to constitute a hollow cylinder, wherein any group of helical antennas comprises an antenna main arm and an antenna branch aria connected to each other, and the antenna main arm comprises a first bending portion arranged on a side surface of the hollow cylinder and a second bending portion arranged on a top surface of the hollow cylinder, and the antenna branch arm comprises a third bending portion arranged on the side surface of the hollow cylinder. The whole four-arm helical antenna is easy to adjust, and the antenna size can be adjusted flexibly according to installation requirements, and it's more suitable for miniaturization application requirements of the four-arm helical antenna.

An antenna device includes a first antenna and a second antenna provided in a case. The first antenna includes a first capacitance loading element and is configured to at least one of receive and transmit a signal in a first frequency band. The second antenna includes a second capacitance loading element and is configured to at least one of receive and transmit a signal in a second frequency band. The second frequency band is higher than the first frequency band. The second capacitance loading element is disposed at a front side of the first capacitance loading element.

An antenna device includes a first antenna and a second antenna provided in a case. The first antenna includes a first capacitance loading element and is configured to at least one of receive and transmit a signal in a first frequency band. The second antenna includes a second capacitance loading element and is configured to at least one of receive and transmit a signal in a second frequency band. The second frequency band is higher than the first frequency band. The second capacitance loading element is disposed at a front side of the first capacitance loading element.

Disclosed are examples of systems, apparatus, methods and computer program products for locating unmanned aerial vehicles (UAVs). A region of airspace may be scanned with two scanning apparatuses. Each scanning apparatus may include one or more directional Radio Frequency (RF) antennae. The two scanning apparatuses may have different locations. Radio frequency signals emitted by a UAV can be received at each of the two scanning apparatuses. The received radio frequency signals can be processed to determine a first location of the UAV.

Disclosed are examples of systems, apparatus, methods and computer program products for locating unmanned aerial vehicles (UAVs). A region of airspace may be scanned with two scanning apparatuses. Each scanning apparatus may include one or more directional Radio Frequency (RF) antennae. The two scanning apparatuses may have different locations. Radio frequency signals emitted by a UAV can be received at each of the two scanning apparatuses. The received radio frequency signals can be processed to determine a first location of the UAV.

A communications device may include an RF device, and an antenna. The antenna may include a conductive ground plane, an elongate support extending from the conductive ground plane, and a helically wound conductive strip carried by the elongate support. The communications device may have a coaxial cable coupling the RF device and the antenna. The coaxial cable may include an inner conductor and an outer conductor surrounding the inner conductor. The outer conductor may be coupled to the conductive ground plane and the inner conductor may extend through the conductive ground plane and be coupled to a proximal end of the helically wound conductive strip.