343results about "Separate antenna unit combinations" patented technology

A mobile terminal includes: a casing including a metal frame and a rear cover, wherein the metal frame is provided with a plurality of slots to divide the metal frame into a plurality of metal parts arranged at intervals; an antenna bracket being provided with a plurality of wirings; a first antenna assembly including a plurality of antenna structures, wherein the plurality of antenna structures are formed based on a plurality of metal parts arranged at intervals and a plurality of wirings, and a working frequency band of the plurality of antenna structures is a sub-6G frequency band; and a second antenna assembly including a plurality of millimeter-wave antenna modules, wherein a working frequency band of the plurality of millimeter-wave antenna modules is a millimeter-wave frequency band.

A circular polarized penta-band antenna device and a method for fabricating the antenna device are provided. The antenna device includes: a substrate; a primary L-band antenna formed on the substrate; and a plurality of secondary antennas formed on a top surface of the L-band antenna. The plurality of secondary antennas includes: an X-band antenna; a K-band1 antenna; a K-band2 antenna; and a Ka-band antenna. Each of the X-band, K-band1, K-band2, and Ka-band antennas has a corner-truncated patch structure configured to generate left-hand circular polarization (LHCP). Each of the antennas operates simultaneously to enable multi-band communication and a shared aperture is formed across all antennas.

The invention discloses a wide-angle scanning dual-frequency circularly-polarized common-aperture phased-array antenna, and mainly solves the problems that an existing common-aperture phased-array antenna is difficult to realize dual-frequency aperture multiplexing and small in scanning angle. The antenna comprises N * N rectangular small-sized common-aperture antenna arrays which are closely arranged and a feed transmission structure, and an antenna unit in each sub-array comprises a Ka wave band transmitting left-hand circularly polarized antenna and a K wave band receiving right-hand circularly polarized antenna which are formed by alternately stacking and pressing two substrates made of different materials, the two antennas with different frequency bands adopt different feed forms and different rotary arraying modes, metalized blind holes are added around the antennas, and segmented cutting grooves and gaps are formed in antenna patches. A feed transmission structure comprising a left-handed circular polarization port and a right-handed circular polarization port is correspondingly arranged below the antennas of different wavebands, and each port is connected with a phase shifter. The wide-angle scanning antenna can realize large-wide-angle scanning in a range of 60 degrees, has the advantages of miniaturization, low profile and integration of transmitting and receiving, and can be used for a low-orbit satellite communication system and multi-band fusion and intelligent networking.

A relay satellite platform communication device for space-ground networking belongs to the field of relay satellites, and is formed by system-level integration of four core technologies including a structure-electrical integrated central bearing frame, an integrated three-surface pluggable modular system, a conformal antenna integrated multifunctional shell and an internal and external cooperative heat pipe heat dissipation network. A framework-module-skin three-layer deep coupling system framework is constructed, six faces of a center bearing structure are divided into a movable area and a static area, the movable area is used for achieving function reconfiguration and on-orbit maintenance, and the static area is used for deploying a high-reliability platform foundation system which is fixed once launched. According to the invention, the problems of difficulty in on-orbit maintenance, low reliability and efficiency bottleneck caused by discrete architecture and functional coupling of a traditional relay satellite are solved, and a high-reliability, high-flexibility and easy-to-maintain satellite platform foundation is provided for constructing a dynamic reconfigurable space-ground integrated information network.

The application belongs to the technical field of antennas, and discloses a coupled resonator decoupling network system applied to MIMO antenna array double-frequency coupling suppression, which comprises a radiating antenna array, a metal floor, a transmission line structure, a single-branch matching network, a three-port double-frequency CRDN structure and a dielectric substrate; the radiating antenna array, the transmission line structure, the single-branch matching network and the three-port double-frequency CRDN structure are printed on the upper layer of the dielectric substrate, and the metal floor is printed on the lower layer of the dielectric substrate; the application has clear principles, mature technology, stable structure, low cost, simple processing technology and is suitable for large-scale production; the application realizes the suppression of mutual coupling of the antenna array in two frequency bands at the same time in a limited space, is suitable for the double-frequency decoupling demand of a compact space multi-antenna system, does not occupy too much additional volume, has low profile and scalability, and can be popularized to different antenna types and other working frequency bands.

Provided in the present application are an antenna unit, an antenna device, a communication apparatus, and a communication system. The antenna unit comprises a balun structure and a radiation arm. The radiation arm comprises a first metal piece and a plurality of second metal pieces, wherein the plurality of second metal pieces are arranged at intervals, at least some of the plurality of second metal pieces are connected to each other by means of a metal wire, and at least one second metal piece is connected to the first metal piece by means of the metal wire. The antenna unit can reduce mutual interference between antenna portions at different frequency bands while simplifying the structure of the antenna unit.

To ensure isolation between multiple antenna elements disposed within a narrow space while also reducing the size of an on-board antenna device, this on-board antenna device (100) comprises: an antenna case (101); a base (102) that forms an accommodation space together with the antenna case (101); and a first antenna element (122) and a second antenna element (123) that are accommodated in the accommodation space. The first antenna element (122) and the second antenna element (123) at least transmit or receive radio waves of different frequency bands. The first antenna element (122) has, in at least a portion thereof, a meandering shape in a first direction that intersects a polarized wave of a radio wave transmitted or received by the second antenna element (123).

A multi-resonant antenna comprises a main antenna and an additional radiation element. The main antenna comprises a main portion and a feeding portion. The main portion forms a split ring. The feeding portion extends outward of the main antenna from the main portion. The additional radiation element extends outward of the main antenna directly from the feeding portion.

A filter device includes an insulating body including a first outer electrode and a second outer electrode, a first inductor coupled to the first outer electrode, and a resonant circuit including a second inductor and a capacitor. The first inductor is coupled to the second outer electrode and to the resonant circuit. The first inductor and the second inductor are stacked in the insulating body. At least one of the first inductor and the second inductor includes a plurality of inductor patterns. The first inductor and the second inductor are alternately disposed in a stacking direction and are magnetically coupled.

An antenna and receiver design is described herein that allows a spacecraft to safely and accurately perform an autonomous flight safety system, an ascent, an entry, a re-entry, a landing, and / or an orbit determination. For example, a spacecraft can be equipped with 180-degree dual-opposed antennas and two receivers. A signal captured by a first antenna can be routed to a secondary radio frequency (RF) of the first receiver and to a combiner. A signal captured by a second antenna can be routed to a secondary RF of the second receiver and to the combiner. The mixer can perform the phase combination operation on the signals captured by the first receiver and the second receiver to produce a phase combined signal, and can route the phase combined signal to the primary RF of the first receiver and to the primary RF of the second receiver.

An antenna assembly includes a first antenna and a second antenna. The first antenna includes a first radiator, a first signal-source, a first matching circuit, and a first adjusting circuit. The first signal-source is electrically connected to the first matching circuit to the first radiator, and the first adjusting circuit is configured to adjust a resonant frequency-point of the first antenna to make the first antenna support an electromagnetic wave signal in a first frequency band. The second antenna includes a second radiator, a second signal-source, a second matching circuit, and a second adjusting circuit. The second signal-source is electrically connected to the second matching circuit to the second radiator, the second adjustment circuit is configured to adjust a resonant frequency-point of the second antenna to make the second antenna support an electromagnetic wave signal in a second frequency band and a third frequency band.

The application discloses a kind of laser preparation vehicle antenna, is prepared by numerical control system control, applied to antenna technical field, including upper shell and bottom shell, the bottom shell is provided with screw below, the screw is connected to form a closed mounting space with the upper shell and the bottom shell, ceramic PCB is provided in the mounting space, ceramic body is installed above the ceramic PCB, a plurality of thimbles are installed in the side of the ceramic PCB, main antenna, diversity antenna, MOM4-antenna, WIFI-1 antenna, WIFI-2 antenna, GPS and BT antenna are sequentially connected with thimble on the ceramic PCB, the application has the characteristics that the drawing of multi-surface composite structure upper antenna circuit is realized.

An antenna device includes: a first antenna used for communication in a first frequency band; a second antenna that is arranged close to the first antenna and used for communication in a second frequency band; a first line that is directly or indirectly connected to the first antenna and increases an impedance of the second frequency band at a feeding point of the first antenna more than an impedance of the first frequency band at a feeding point of the first antenna; and a first antenna duplexer or a first filter connected to the first antenna via the first line.

This application describes multi-band antenna systems and base stations. An example antenna system a frequency selective surface (FSS); at least one radiating element array on a first side of the FSS; and at least one feeding network corresponding to the at least one radiating element array, wherein the at least one feeding network corresponding to the at least one radiating element array is connected to the FSS according to a direct current connection manner or a segmented direct current connection manner, or the at least one feeding network corresponding to the at least one radiating element array is integrated on the FSS.

This application provides an antenna structure and electronic device, including: a first antenna, a second antenna, and a feed point; a first radiator and a second radiator of the first antenna are symmetrically arranged with respect to the perpendicular bisector between the first and second connection points, and the other ends of the first and second radiators extend in mutually distancing directions; one end of the second transmission line of the second antenna is electrically connected to the feed point, and the other end of the second transmission line is electrically connected to one end of a third radiator of the second antenna; the other end of the third radiator is grounded. The antenna structure provided by this application achieves hotspot dispersion, reduces SAR values, and enables simultaneous operation of low-frequency, mid-frequency, and high-frequency antennas under low SAR conditions, solving the problem in the prior art where low-frequency, mid-frequency, and high-frequency antennas cannot operate simultaneously under low SAR conditions.

The disclosed technology relates to an antenna module comprising: at least one array of antenna elements (101); at least one layer comprising a frequency selective surface (102; 107) configured to control the transmission and reflection of electromagnetic waves; and a reflector (104), the reflector comprising an opening. In accordance with the disclosed techniques, one of the at least one layer comprising a frequency selective surface (FSS) is mounted on / to the opening in the reflector (104), and an antenna element (106) mounted on the at least one FSS layer (107) is capacitively coupled to a conductive reflector material surrounding the opening in the reflector (104).

An electronic device according to an embodiment comprises: a processor; a housing; a first conductive part; a second conductive part; a first wireless communication circuit configured to transmit or receive a first signal in a first frequency band through at least a portion of the first conductive part; a second wireless communication circuit configured to transmit or receive a second signal in a second frequency band different from the first frequency band through at least a portion of the second conductive part; and a matching circuit electrically connected to the second conductive part.

A base station antenna sector includes: a first reflector comprising a first flat panel and a plurality of first radiating elements mounted thereon; a second reflector comprising a second flat panel and plurality of second radiating elements mounted thereon; a radome surrounding the first and second reflectors; wherein the second reflector is pivotally movable relative to the first reflector.

An electronic device according to an embodiment comprises: a processor; a housing; a first conductive part; a second conductive part; a first wireless communication circuit configured to transmit or receive a first signal in a first frequency band through at least a portion of the first conductive part; a second wireless communication circuit configured to transmit or receive a second signal in a second frequency band different from the first frequency band through at least a portion of the second conductive part; and a matching circuit electrically connected to the second conductive part.

A mobile device may include a first antenna positioned on a first substrate, the first antenna in communication with a global navigation satellite system (GNSS) receiver to receive first radio signals from at least four GNSS satellites and convert the first radio signals into first electronic signals and a second antenna positioned on a second substrate between 30 degrees and 90 degrees from the first antenna. With such multi-band antenna design, arrangement, and positioning, the GNSS receiver may maximize the number of satellites it can track which results in improved geometry of tracked satellites, which reduces dilution and precision and improves location accuracy of the GNSS receiver.

The invention relates to the technical field of antennas, in particular to a multi-frequency broadband common-caliber circularly polarized antenna. The antenna comprises a grounding plate, a patch radiator, a plurality of monopole groups and a feed assembly, the grounding plate is arranged at the bottom of the whole antenna, the patch radiator is arranged above the grounding plate, each monopole group corresponds to one frequency band and comprises a plurality of monopoles, the monopoles are distributed in the circumferential direction of the patch radiator, and the feed assembly is arranged above the patch radiator. The multiple monopoles of the multiple monopole groups are sequentially arranged in a staggered mode, one end of each monopole is electrically connected with the grounding plate, the other end of each monopole is in an open circuit state, and the patch radiator inputs radio frequency signals through the feed assembly. The antenna provided by the invention has the characteristics of multi-frequency independent tuning and design flexibility, high efficiency, light weight, low-cost structural characteristics, structural expandability and engineering realization simplicity and convenience.

To provide a system and method that allows more antennas to be present on a spacecraft while minimizing the platform volume used for antennas. [Solution] The multiband concentric helical antenna system 100 includes bases 115, 125, a first helical antenna 110, and at least a second helical antenna 120, wherein the second helical antenna is located within the first helical antenna, the first helical antenna has a first frequency band, and the second helical antenna has a second frequency band that is not the same as the first frequency band, and the first and second helical antennas are connected to the base and located within an opening in the base. The multiband helical antenna system may further include N additional antennas, which can be used as a single radiating element or in an array of radiating elements.

A vehicle antenna includes a low profile housing having a first end and a second end and having a first side and a second side. An antenna assembly is disposed in the low profile housing. The antenna assembly includes a first cellular antenna at a first end and a second cellular antenna at a second end. The antenna assembly includes a first ground element at the first side and a second ground element at the second side. The first cellular antenna is operably coupled to the first ground element, and the second cellular antenna is operably coupled to the second ground element. The first ground element is isolated from the second ground element.

To provide a small-sized half-wavelength antenna device capable of adjusting directivity. A half-wavelength antenna device for a vehicle includes: a conductive plate 10; a half-wavelength element 20; and a parasitic element 30. The conductive plate 10 has a feeding part 11 and a ground 12. The half-wavelength element 20 is vertically installed on the conductive plate 10 so as to be connected to the feeding part 11 but insulated from the ground 12. The parasitic element 30 is disposed in proximity and parallel to the half-wavelength element 20 so as to be electromagnetically coupled thereto but insulated from the ground 12.

An antenna module includes a first dielectric substrate at which a first radiating electrode with a flat plate shape is disposed and a second dielectric substrate at which a second radiating electrode shape is disposed. The first dielectric substrate has a first surface and a second surface that are opposite each other. The first radiating electrode is disposed on the second surface of the first dielectric substrate or at a position between the first and second surfaces of the first dielectric substrate. The second dielectric substrate includes a region that is arranged so as abut the first dielectric substrate and a region that is in contact with the first surface of the dielectric substrate. A normal direction of the radiating electrode is different from a normal direction of the radiating electrode.

Compact Direct IV Antenna. Antenna (100) comprising at least: - an electrically conductive enclosure (110) formed by a lower surface (111) surrounded by lateral edges (112) and closed by a cover (140) having a partially reflective outer surface; - a substrate (120) placed at the bottom of the enclosure on the lower surface of the enclosure; and - a radome (150) placed in the enclosure opposite the substrate and capable of protecting the antenna from temperatures exceeding 1000 °C; characterized in that the antenna also comprises a radiating element (130) placed on the substrate in the enclosure and capable of emitting a signal at at least a first frequency, and a grid (160) placed on a surface of the radome opposite the radiating element so as to form an air gap (170) between the grid and the substrate. Figure for the abstract: Fig. 1

Adaptive tunable antenna system includes a first radiating element having an elongated length and a second radiating element extending from a distal end of the first radiating element. The first radiating element is for a high band of operation and the second radiating element is for a low-band of operation. The second radiating element is a helical member including a plurality of turns. A low-band circuit selectively bypasses one or more of the turns of the second radiating element in response to a control signal.

An antenna device is disclosed. According to one embodiment of the present disclosure, the provided antenna device comprises: one or more antenna boards which extend in the longitudinal direction, and which are formed such that each thereof has one or more circuit patterns; a dielectric formed such that a contact position for the one or more circuit patterns may be changed at the upper side of each of the one or more antenna boards; a connector protruding at the lower side of each of the one or more antenna boards from one surface thereof; and an antenna filter detachably coupled to the connector.

The utility model provides a monomer coplanar circularly polarized dual-frequency antenna, which comprises an upper-layer radiation electrode, a dielectric substrate, a lower-layer radiation electrode, a reflecting layer and a feed point needle, and is characterized in that the upper-layer radiation electrode and the lower-layer radiation electrode are respectively mounted on the upper surface and the lower surface of the dielectric substrate; the feed point needle is fixed in the dielectric substrate and is electrically connected with the upper-layer radiation electrode and the lower-layer radiation electrode in an electromagnetic coupling mode, and the upper-layer radiation electrode comprises a first frequency band radiation electrode and a second frequency band radiation electrode which are detachable; a gap of a geometric symmetry structure is arranged between the first frequency band radiation electrode and the second frequency band radiation electrode, and the bottom of the feed point needle is connected with the reflecting layer. The dual-frequency circularly polarized antenna solves the problems of poor circularly polarized radiation performance, low electrical index, low integration level, heavy weight, poor process adaptability, low reliability, limited working temperature and the like of the dual-frequency circularly polarized antenna in the prior art.

To provide a compact, half-wavelength antenna device with adjustable directivity. [Solution] The half-wavelength antenna device for vehicles consists of a conductive plate 10, a base 40, a half-wavelength element 20, and a powerless element 30. The conductive plate 10 has a power supply section 11 and a ground 12. The base 40 is made of a plate-shaped dielectric that is erected on the conductive plate. The half-wavelength element 20 is The base 40 is a plate-shaped component that is positioned on one side of the base 40, connected to the power supply unit 11, and insulated from the ground 12. The unpowered element 30 is a plate-shaped component that is positioned on the other side of the base 40, parallel to and close to the half-wavelength element 20 so as to electromagnetically couple to the half-wavelength element 20 via the base 40, and is insulated from the ground 12.