Abstract: Embodiments the present disclosure provide a MTP memory cell and methods for forming the same. The MTP memory cell includes a FinFET transistor having a storage node formed around the channel region and a metal gate electrode around the storage node. The memory cell may be implemented by either n-channel transistor or p-channel transistor.

Abstract: A non-volatile memory (NVM) device. The NVM device includes: a semiconductor substrate having a plurality of fin-type structures; a select transistor formed on the semiconductor substrate, the select transistor including a gate layer disposed over a first dielectric isolation layer positioned over a first section of the plurality of fin-type structures, where the select transistor is a P-channel metal oxide semiconductor transistor; a storage device formed on the semiconductor substrate, the storage device including a storage gate layer disposed over a second dielectric isolation layer positioned over a second section on the plurality of fin-type structures, where the storage gate layer is arranged to trap charges, and where the storage device is a P-channel storage device, where the select transistor is coupled to the storage device; and the first section of the plurality of fin-type structures is adjacent to the second section of the plurality of fin-type structures.

Abstract: The invention relates to a mechanism type antenna for tracking starlink satellite, including a horizontal shaft adjustment device, arranged on a base; a set of disk antenna 180° rotational symmetrically arranged on the left and right sides above the horizontal shaft adjustment device, which are respectively driven by a first arm and a second arm, to achieve synchronous reverse cross swing; a starlink satellite orbit adjustment device, arranged on a swivel seat; so as to achieve handover tracking of low orbit starlink satellites, an elevation angle adjustment device and a set of polarization adjustment device; whereby using two disk antennas swing in opposite direction to form an antenna which can quickly handover to new target satellites, which can replace the two independent conventional antennas used by VSTA and the electronically phased array antenna of starlink system, so as to achieve cost down and reduce failure rate.

Abstract: A transistor includes: a substrate; a first fin and a second fin protruding upwardly from a top surface of the substrate, wherein the first fin and the second fin are concentric, and each of the first fin and the second fin comprises a first straight section, a second straight section in parallel with the first straight section, a first curved section, and a second curved section; a first drain and a second drain; a first source and a second source; a first curved channel and a second curved channel located at the first curved section of the first fin and the first curved section of the second fin, respectively; and a third curved channel and a fourth curved channel located at the second curved section of the first fin and the second curved section of the second fin, respectively.

Abstract: A semiconductor device structure is provided. The semiconductor device structure includes a semiconductor substrate. The semiconductor device structure includes a gate stack over the semiconductor substrate. The gate stack includes a first insulating layer, a charge trapping structure, a second insulating layer, and a gate electrode. The first insulating layer separates the semiconductor substrate from the charge trapping structure. The charge trapping structure is between the first insulating layer and the second insulating layer. The gate electrode is over the second insulating layer. The charge trapping structure includes a first layer and a second layer. The first layer includes zinc oxide, tin dioxide, titanium oxide, zinc tin oxide, indium oxide, indium zinc oxide, indium gallium zinc oxide, zinc oxynitride, tin oxynitride, titanium oxynitride, zinc tin oxynitride, indium oxynitride, indium zinc oxynitride, or indium gallium zinc oxynitride.

Abstract: A semiconductor device structure is provided. The semiconductor device structure includes a semiconductor substrate. The semiconductor device structure includes a gate stack over the semiconductor substrate. The gate stack includes a first insulating layer, a charge trapping structure, a second insulating layer, and a gate electrode. The first insulating layer separates the semiconductor substrate from the charge trapping structure. The charge trapping structure is between the first insulating layer and the second insulating layer. The gate electrode is over the second insulating layer. The charge trapping structure includes a first layer and a second layer. The first layer includes zinc oxide, tin dioxide, titanium oxide, zinc tin oxide, indium oxide, indium zinc oxide, indium gallium zinc oxide, zinc oxynitride, tin oxynitride, titanium oxynitride, zinc tin oxynitride, indium oxynitride, indium zinc oxynitride, or indium gallium zinc oxynitride.

Abstract: A semiconductor device structure is provided. The semiconductor device structure includes a semiconductor substrate. The semiconductor device structure includes a gate stack over the semiconductor substrate. The gate stack includes a first insulating layer, a first layer, a second layer, a second insulating layer, and a gate electrode. The first insulating layer separates the semiconductor substrate from the first layer. The second layer is between the first layer and the second insulating layer. The gate electrode is over the second insulating layer. There is a P-N junction between the first layer and the second layer. The semiconductor device structure includes a first doped region and a second doped region in the semiconductor substrate. The first layer, the first doped region, and the second doped region have a first type conductivity, which is opposite to a second type conductivity of the second layer.

Abstract: A Low Noise Block downconverter (LNB) with high isolation, and more particularly, to a low-noise-block downconverter design for horizontal wave and vertical wave of a linear polarization; wherein, a horizontal probe and a vertical probe are directly set on a printed circuit board to receive the aforesaid waves; a waveguide chamber of the horizontal probe is divided into two chambers, a front chamber and a back chamber; a waveguide chamber of the vertical probe is transversely extended from a side waveguide, and the waveguide chamber of the vertical probe is also divided into two chambers; thereby the horizontal and vertical probe respectively receives the waves when facing to the rear side of the waveguide chambers for separating the horizontal and vertical wave and reducing the coupling of each other; thus, increasing the isolation and preventing the mutual interference of the horizontal and vertical wave.

Abstract: A transceiver module for a satellite antenna comprises a base and a cover. The base includes a transducer extending between a first end plate and a second end plate in a first direction, a first filter portion including a number or first grooves extending in the first direction and arranged along a second direction orthogonal to the first direction, and a waveguide to guide signals toward a third end plate. The cover serves as a second filter portion for the transceiver module and includes a number of second grooves arranged along the second direction. The base includes the transducer, the first filter portion and the waveguide as an integral member.

Abstract: An antenna mount for a satellite antenna comprises an adjustment plate with a first cam slot, a first bracket and a first cam. The first bracket includes a first base, a first sidewall extending from the first base and having a second cam slot aligned with the first cam slot, and a second sidewall extending in parallel with the first sidewall from the first base. The first cam is adapted to attach the adjustment plate to an inner surface of the first sidewall. The first cam includes a first shaft protruding from the first sidewall through the first and second cam slots and rotatable with respect to the first sidewall, and a first disc coupled with the first shaft and adapted to fit within the first cam slot so that the adjustment plate is rotatable with respect to the first sidewall as the first shaft is rotated from the exterior of the first sidewall.

Abstract: An antenna system and a corresponding method for satellite lock-on applied to vehicles automatically lock on at least one satellite in the space by means of a lock-on signal. The technique features on a scan driving signal that initiates a space scan of the antenna system so as to obtain a scan data. According to peak values of the scan data, coordinates of a plurality of satellites in the space are realized and individually recorded. Then, after receiving a lock-on signal, the satellite coordinate of the satellite to be locked is retrieved so as to drive the antenna to point at the satellite to be locked.

Abstract: A satellite antenna includes an antenna dish, a connecting arm, a pole, at least one clamp and a cover bracket. The antenna dish may include a front surface and a rear surface. The connecting arm has a first end and a second end, wherein the first end is coupled with the rear surface of the antenna dish. The pole may extend transversely with respect to the connecting arm and may include a channel extending from one end to the other end of the pole. The at least one clamp may each include a base with an opening that allows the pole to pass through. The cover bracket may include a front cover to seal the second end of the connecting arm, and a first cover integral with the front cover that includes a first side and a second side. The first cover may support the pole over the connecting arm on the first side and engage with the connecting arm with the second side.

Abstract: An antenna mount for a satellite antenna comprises an adjustment plate with a first cam slot, a first bracket and a first cam. The first bracket includes a first base, a first sidewall extending from the first base and having a second cam slot aligned with the first cam slot, and a second sidewall extending in parallel with the first sidewall from the first base. The first cam is adapted to attach the adjustment plate to an inner surface of the first sidewall. The first cam includes a first shaft protruding from the first sidewall through the first and second cam slots and rotatable with respect to the first sidewall, and a first disc coupled with the first shaft and adapted to fit within the first cam slot so that the adjustment plate is rotatable with respect to the first sidewall as the first shaft is rotated from the exterior of the first sidewall.

Abstract: A filter unit comprises a cover and a base. The cover includes a number of first grooves, and the base includes a number of second grooves aligned with the first grooves. At least one of the cover or the base includes an alloy of zinc and aluminum, wherein the weight percentage of zinc is greater than that of aluminum.

Abstract: A mobile digital signal transceiving device comprises a multimedia interface, a processing unit and a radio frequency (RF) signal transmitter. The multimedia interface reads at least one multimedia data stored in at least one multimedia memory device. The processing unit transfers the multimedia data into a terrestrial broadcast data in a digital video broadcasting-terrestrial (DVB-T) data format, and modulates the terrestrial broadcast data in order to generate an RF signal. The RF signal transmitter transmits the RF signal so that the RF signal may be received by at least one mobile multimedia device.

Abstract: A transceiver module for a satellite antenna comprises a base and a cover. The base includes a transducer extending between a first end plate and a second end plate in a first direction, a first filter portion including a number or first grooves extending in the first direction and arranged along a second direction orthogonal to the first direction, and a waveguide to guide signals toward a third end plate. The cover serves as a second filter portion for the transceiver module and includes a number of second grooves arranged along the second direction. The base includes the transducer, the first filter portion and the waveguide as an integral member.

Abstract: A method for satellite lock-on in an antenna system by channel selection is initiated by receiving a channel selection signal. The channel selection signal is flagged to retrieve satellite parameters corresponding to the selected channel from a pre-stored satellite channel table which provides a correlation among the channels, the bands and the satellite coordinates. Then, according to the retrieved satellite parameters, an antenna control signal and thus a drive signal are generated orderly to drive the antenna to direct at the satellite responsible to the selected channel.

Abstract: A filter unit comprises a cover and a base. The cover includes a number of first grooves, and the base includes a number of second grooves aligned with the first grooves. At least one of the cover or the base includes an alloy of zinc and aluminum, wherein the weight percentage of zinc is greater than that of aluminum.

Abstract: An antenna system and a corresponding method for satellite lock-on applied to vehicles automatically lock on at least one satellite in the space by means of a lock-on signal. The technique features on a scan driving signal that initiates a space scan of the antenna system so as to obtain a scan data. According to peak values of the scan data, coordinates of a plurality of satellites in the space are realized and individually recorded. Then, after receiving a lock-on signal, the satellite coordinate of the satellite to be locked is retrieved so as to drive the antenna to point at the satellite to be locked.

Abstract: The present invention discloses a satellite disc antenna and its structure for displaying an integrally formed trademark through hollow holes by a visual contrast effect. The antenna is formed by punching holes on a metal plate to constitute a holed plate with densely distributed hollow holes, while maintaining the disc surface of a desired trademark pattern free of holes, so that the integrally formed trademark pattern can be shown clearly on the disc surface by the visual contrast effect. The satellite disc antenna can be manufactured synchronously without requiring any printing or coating. The invention can reduce the influence of climate changes and prevent the trademark pattern from being peeled off easily. Further, the hollow holes can be used for reducing the wind resistance, enhancing the durability of the antenna and maintaining the reliability of receiving signals.