An antenna structure includes a substrate, a plurality of reflective plates, a grounding plate, a radiating member, a signal feeding via and a plurality of conductive vias. The substrate has opposite first and second surfaces and comprises liquid crystal polymer. The reflective plates are arrayed on the first surface of the substrate. The grounding plate is disposed on the second surface of the substrate and overlapped with the reflective plates in a normal direction of the substrate. The grounding plate further includes an opening. The radiating member is disposed on the first surface of the substrate and physically separated from the reflective plates. The signal feeding via is coupled with the radiating member and penetrates through the substrate to be exposed in the opening of the grounding plate. The conductive vias penetrate through the substrate and respectively connect the reflective plates and the grounding plate.

A radio frequency surface wave attenuator structure is provided. The structure may be configured to be operably coupled with a plurality of other radio frequency surface wave attenuator structures to form a metamaterial. The radio frequency surface wave attenuator structure may include a patch disposed in a first plane and defining a patch area and a backplane disposed in a second plane and extending along the second plane to be shared with the other surface wave attenuator structures. The structure may further include a via spring having a number of turns and being comprised of a conductive material. The via spring may electrically couple the patch to the backplane. The structure may further include a dielectric disposed between the patch and the backplane.

An antenna apparatus includes a feed via, a patch antenna pattern which is electrically connected to a first end of the feed via, a plurality of first conductive array patterns, respectively disposed to be spaced apart from the patch antenna pattern and arranged to correspond to at least a portion of a side boundary of the patch antenna pattern, and a first conductive ring pattern spaced apart from the patch antenna pattern and the plurality of conductive array patterns and configured to surround the patch antenna pattern and the plurality of conductive array patterns.

An apparatus for electromagnetic interference shielding is described herein. The apparatus includes an electromagnetic bandgap (EBG) structure. The EBG structure is attached to a surface of the apparatus such that noise propagation is mitigated. The apparatus may be a chassis of an electronic device, and the EBG structure may be attached to one surface of the chassis. Further, the apparatus may be a heat sink, and the EBG structure can be attached to one surface of the heat sink.

An illustrative example antenna device includes a substrate, a transmission line supported on the substrate, and a plurality of conductive patches supported on the substrate. Each conductive patch has a first end coupled to the transmission line and a second end coupled to ground. The plurality of conductive patches are arranged in sets including two of the conductive patches facing each other on opposite sides of the transmission line.

A multifunctional electromagnetic structure is presently disclosed. Said structure is a true electromagnetic bandgap (EBG) material, with both surface and leaky waves suppressed from the whole structure along all lateral directions. It is also an antenna element, configured to radiate to the broadside direction. The structure has two metallization layers of concentric rings between a square-shaped radiating top metal layer and a bottom ground plane. The lower concentric ring is connected to the ground plane through a plurality of vias, while the patch of the top metal layer is fed with a probe. The EBG unit cells may be used as antenna elements in a phased array environment, where they eliminate scan blindness from the array structure along all scan directions.

An antenna apparatus includes a ground pattern having a through-hole; an antenna pattern disposed above the ground pattern and configured to either one or both of transmit and receive a radio-frequency (RF) signal; a feed via penetrating through the through-hole and having one end electrically connected to the antenna pattern; and a meta member comprising a plurality of cells repeatedly arranged and spaced apart from each other, each of the plurality of cells comprising a plurality of conductive patterns, and at least one conductive via electrically connecting the plurality of conductive patterns to each other, wherein the meta member is disposed along at least portions of side boundaries of the antenna pattern above the ground pattern, and extends above the antenna pattern.

The present invention provides a circularly polarised, CP, antenna device for multiband GNSS. It comprises a spiral antenna and a high impedance surface, HIS, comprising a conductive layer comprising a first region and a separate second region, and a ground plane. The first region of the conductive layer is provided with at least one resonant element of a first resonant frequency and the second region of the conductive layer is provided with at least one resonant element of a second resonant frequency.

A dual-band antenna and a wireless communications device are disclosed. The dual-band antenna includes a first antenna arranged on a first printed circuit board (PCB), a second antenna arranged on a second PCB, and a reflection panel. An operating frequency band of the first antenna is a first frequency band. An operating frequency band of the second antenna is a second frequency band. The first frequency band is higher than the second frequency band. The second PCB is disposed between the first PCB and the reflection panel. The reflection panel includes an artificial magnetic conductor. A resonant frequency band of the artificial magnetic conductor includes the second frequency band. The first frequency band is outside the resonant frequency band. The dual-band antenna has a small size.

An assembly for electromagnetic interference (EMI) shielding to prevent incident radiation from penetrating through a gap to an interior of an aircraft includes an electromagnetic band gap (EBG) structure. The EBG structure has a patch-and-via array connected to a ground layer. The EMI shielding includes a conductive adhesive and is flexible for conforming attachment to curved aircraft surfaces. The shielding may be located on a deflector plate that is parallel to an adjacent aircraft surface, on the airframe surface opposite to the deflector plate, or in both locations. The assembly filters out penetrating electromagnetic energy and prevents highly resonant cavity mode build-ups of electromagnetic energy inside a nacelle or other enclosure effectively protecting electrical equipment in the interior.