Abstract: Embodiments disclosed herein include electronic packages and methods of forming electronic packages. In an embodiment, the electronic package comprises a package substrate, a die coupled to the package substrate, a photonics integrated circuit (PIC) coupled to the die, and a fiber array unit (FAU) optically coupled to the PIC. In an embodiment, the FAU has a base with a first width and a protrusion with a second width that is smaller than the first width.

Abstract: In one embodiment, an integrated circuit package includes a package substrate with a cavity, an integrated circuit device, a bridge, a photonic integrated circuit (PIC), and an electronic integrated circuit (EIC). The integrated circuit device is electrically coupled to the package substrate. The bridge and the PIC are in the cavity of the package substrate, and the bridge is electrically coupled to the package substrate. The EIC is above, and electrically coupled to, the bridge and the PIC.

Abstract: A reduced bridge structure for a photonic integrated circuit (PIC) or any integrated circuit comprising a ring resonator structure. The reduced bridge structure is an architecture including an optical and electrical routing arrangement to reduce the number of bridges around the micro-ring structure of the ring resonator structure. Embodiments reserve one bridge portion for use as a signal trace, not routing the signal trace over a silicon waveguide. By not routing the signal trace over a silicon waveguide, the structure avoids possible interference between the radio frequency (RF) signal on the signal trace and optical communication (a light wave) propagating in the silicon waveguide.

Abstract: Variations in a thermal structure for an open cavity photonic integrated circuit (OCPIC) having an MRR. The structure includes an air trench in fluid communication with an air cavity that is located under the MRR. The air trench is a gap/opening in the oxide that encircles at least a portion of the MRR and extends outward radially therefrom, with a consistent width, to a diameter D1. An oxide cladding is not removed in areas that are used for metal traces and routing. The structure is characterized by straight walls along the air trench. The structure has a lower diameter D2, measured at a bottom/floor of the air cavity. In various embodiments, D2 is substantially equal to D1.

Abstract: Covered cavity structure for Photonic integrated circuits (PICs) that include a micro-ring resonator (MRR) with a heater. Air cavities are etched or otherwise thinned into an overlaying oxide layer, a buried oxide layer, or an underlying silicon layer. Variations in size, shape, and location of the covered air cavity associated with an MRR provide customizable options for thermal management. A thin film across an upper surface covers the air cavity, providing a barrier to underfill in the air cavity and preventing interference of underfill with performance of silicon waveguides. When arrayed into a plurality of MRRs, the thin film can cover the plurality of MRRs.

Abstract: Embodiments disclosed herein include an optoelectronic system. In an embodiment, the optoelectronic system comprises a first substrate, a second substrate over the first substrate, and a micro-ring resonator (MRR) over the second substrate. In an embodiment, a heater is integrated into the MRR, a cladding is over the MRR, and a temperature sensor is over the MRR in the cladding.

Abstract: Embodiments disclosed herein include an on-cavity photonic integrated circuit (OCPIC). In an embodiment, the OCPIC comprises a laser transmitter, that comprises a row with four bumps, and a micro-ring resonator (MRR) in the row between a first bump and a second bump of the four bumps. In an embodiment, a cavity is below the MRR, where a diameter of the cavity is substantially equal to a spacing between the first bump and the second bump.

Abstract: Embodiments disclosed herein include optoelectronic systems and methods of forming such systems. In an embodiment, an optoelectronic system comprises a first substrate, a second substrate over the first substrate, and a micro-ring resonator (MRR) over the second substrate. In an embodiment, a heater is integrated into the MRR, a cladding is over the MRR, and an opening is through the first substrate and the second substrate to expose a bottom surface of the MRR.

Abstract: Embodiments disclosed herein include optoelectronic systems and methods of forming such systems. In an embodiment, an optoelectronic system comprises a first substrate, a second substrate over the first substrate, a micro-ring resonator (MRR) over the second substrate, a heater integrated into the MRR, a cladding over the MRR, an opening through the first substrate and the second substrate to expose a bottom surface of the MRR, and a base spanning across the opening.

Abstract: An electronic device may include a photonic integrated circuit (PIC) coupled with a substrate. The PIC may communicate a photonic signal with one or more optical fibers. The PIC may process the photonic signal into an electronic signal. The PIC may extend between a first end and a second end. An electronic integrated circuit (EIC) may be coupled with the substrate. The EIC may communicate with the PIC. The EIC may transmit the electronic signal to the PIC. The EIC may receive the electronic signal from the PIC. The electronic device may include a lens assembly. The lens assembly may be coupled with the first end of the PIC. In an example, optical interconnects of the PIC are aligned with the lens assembly such that the lens assembly is configured to transmit the photonic signal communicated between PIC and the optical fibers.

Abstract: An electronic device may include a photonic integrated circuit (PIC) coupled with a substrate. The PIC may communicate a photonic signal with one or more optical fibers. The PIC may process the photonic signal into an electronic signal. The electronic device may include an electronic integrated circuit (EIC) coupled with the substrate. The EIC may communicate with the PIC. The EIC may transmit the electronic signal to the PIC. The EIC may receive the electronic signal from the PIC. The electronic device may include a lens assembly. The lens assembly may include at least one gradient refractive index (GRIN) lens.

Abstract: An electronic device and associated methods are disclosed. In one example, the electronic device includes a laser package. In selected examples, the laser package can include a substrate having a substrate front surface and defining a cavity that extends into the substrate front surface. The laser package can further include a photonic integrated circuit (PIC) attached to the substrate within the cavity at a first surface of the PIC, and laser circuitry communicably coupled to a second surface of the PIC opposite the first surface.

Abstract: Embodiments disclosed herein include electronic packages and methods of assembling an electronic package. In an embodiment, an electronic package comprises a package substrate with a stepped top surface, and a first die on a first plateau of the stepped top surface. In an embodiment, a second die is on a second plateau of the stepped top surface, where the second die extends over the first die, In an embodiment, a third die is on a third plateau of the stepped top surface, where the third die extends over the second die.

Abstract: An integrated circuit (IC) package comprising an optical die comprising a configurable optical switch. The configurable optical switch comprises an optical switch operably coupled to one or more optical transceivers. An optical connector comprises at least one exo-package optical port. The at least one exo-package optical port is operably coupled to the configurable optical switch. The configurable optical switch is to pass an optical signal on the at least one of the one or more exo-package ports to at least one of the one or more optical transceivers, and an IC die comprising electronic circuitry is operably coupled to the one or more optical transceivers.

Abstract: The removal of heat from silicon photonic integrated circuit devices is a significant issue in integrated circuit packages. As presented herein, the removal of heat may be facilitated with an optically compatible thermal interface structure on the silicon photonic integrated circuit device. These thermal interface structures may include stack-up designs, comprising an optical isolation structure and a thermal interface material, which reduces light coupling effects, while effectively conducting heat from the silicon photonic integrated circuit device to a heat dissipation device, thereby allowing effective management of the temperature of the silicon photonic integrated circuit device.

Abstract: A capacitance-sensing circuit may include a channel input associated with measuring a capacitance of a unit cell of a capacitive sense array. The capacitance-sensing circuit may also include a capacitive hardware baseliner that is coupled to the channel input. The capacitive hardware baseliner generates a baseline current based on a time constant of the channel input associated with the measuring of the capacitance of the element of the capacitive sense array using the programmable baseline resistor. The capacitive hardware baseliner provides the baseline current at the channel input to provide a charge for a sense capacitor. A change in the charge of the sense capacitor is provided by the baseline current indicating a presence of a tough object proximate to the element.

Abstract: Embodiments described herein may be related to apparatuses, processes, and techniques related to a dual polarization chiplet that may be used by an optical receiver to split multi-polarized light traveling on a single fiber and carrying two or more light signals into two or more fibers each carrying the particular light signal. The dual polarization chiplet may also be used by an optical transmitter to combine multiple light signals to be transmitted onto a single fiber, where each of the multiple light signals are represented by a different polarization of a wavelength on the single fiber. Other embodiments may be described and/or claimed.

Abstract: Embodiments described herein may be related to apparatuses, processes, and techniques related to a bidirectional optical grating coupler that may be used for testing. A photonic apparatus includes a first layer with electro-optical circuitry that is optically coupled with a bidirectional optical grating coupler. A second layer is physically coupled with a first side of the first layer and includes a first light path to optically coupled with the bidirectional optical grating coupler. A third layer is physically coupled with a second side of the first layer opposite the first side of the first layer, and includes a second light path that optically couples with the bidirectional grating coupler. Operational testing of the electro-optical circuitry is based in part on light received or transmitted through the second light path. Other embodiments may be described and/or claimed.

Abstract: Embodiments disclosed herein include photonics systems with a dual polarization module. In an embodiment, a photonics patch comprises a patch substrate, and a photonics die over a first surface of the patch substrate. In an embodiment, a multiplexer is over a second surface of the patch substrate. In an embodiment, a first optical path from the photonics die to the multiplexer is provided for propagating a first optical signal, and a second optical path from the photonics die to the multiplexer is provided for propagating a second optical signal. In an embodiment, a Faraday rotator is provided along the second optical path to convert the second optical signal from a first mode to a second mode before reaching the multiplexer.

Abstract: A vehicle guidance system and method of forming the same. The vehicle guidance system includes a transport guideway having an at least partial tube structure; vehicle tracks; a vehicle, having a fuselage with an uppermost surface and a lowermost surface, that travels over the vehicle tracks; and at least one track channel assembly arranged on an inside of the at least partial tube structure. The at least one track channel assembly is arranged so that, as the vehicle travels over the vehicle track, the at least one track channel assembly is located between the uppermost surface and the lowermost surface of the fuselage.