Abstract: A method of repairing a bonded structure is disclosed. The method can include debonding from a carrier a first semiconductor element that is bonded to a bonding site of the carrier, cleaning the bonding site of the carrier; and bonding a second semiconductor element to the bonding site of the carrier. The bonding can also include directly bonding the second semiconductor element and the carrier. The method can further include reducing the dielectric bond energy via a surface modification between the first semiconductor element and the carrier. Debonding the bonded structure can include delivering a fluid from one or more nozzles to a bonding interface between the first semiconductor element and the carrier to reduce the bond energy. A temperature adjustment pad can also be included to debond the bonded structure.

Abstract: Mitigating surface damage of probe pads in preparation for direct bonding of a substrate is provided. Methods and layer structures prepare a semiconductor substrate for direct bonding processes by restoring a flat direct-bonding surface after disruption of probe pad surfaces during test probing. An example method fills a sequence of metals and oxides over the disrupted probe pad surfaces and builds out a dielectric surface and interconnects for hybrid bonding. The interconnects may be connected to the probe pads, and/or to other electrical contacts of the substrate. A layer structure is described for increasing the yield and reliability of the resulting direct bonding process. Another example process builds the probe pads on a next-to-last metallization layer and then applies a direct bonding dielectric layer and damascene process without increasing the count of mask layers.

Abstract: Direct bonded stack structures for increased reliability and improved yields in microelectronics are provided. Structural features and stack configurations are provided for memory modules and 3DICs to reduce defects in vertically stacked dies. Example processes alleviate warpage stresses between a thicker top die and direct bonded dies beneath it, for example. An etched surface on the top die may relieve warpage stresses. An example stack may include a compliant layer between dies. Another stack configuration replaces the top die with a layer of molding material to circumvent warpage stresses. An array of cavities on a bonding surface can alleviate stress forces. One or more stress balancing layers may also be created on a side of the top die or between other dies to alleviate or counter warpage. Rounding of edges can prevent stresses and pressure forces from being destructively transmitted through die and substrate layers. These measures may be applied together or in combinations in a single package.

Abstract: Representative techniques and devices including process steps may be employed to mitigate the potential for delamination of bonded microelectronic substrates due to metal expansion at a bonding interface. For example, a metal pad having a larger diameter or surface area (e.g., oversized for the application) may be used when a contact pad is positioned over a TSV in one or both substrates.

Abstract: A method of direct hybrid bonding first and second semiconductor elements of differential thickness is disclosed. The method can include patterning a plurality of first contact features on the first semiconductor element. The method can include second a plurality of second contact features on the second semiconductor element corresponding to the first contact features for direct hybrid bonding. The method can include applying a lithographic magnification correction factor to one of the first patterning and second patterning without applying the lithographic magnification correction factor to the other of the first patterning and the second patterning. In various embodiments, a differential expansion compensation structure can be disposed on at least one of the first and the second semiconductor elements.

Abstract: Mitigating surface damage of probe pads in preparation for direct bonding of a substrate is provided. Methods and layer structures prepare a semiconductor substrate for direct bonding processes by restoring a flat direct-bonding surface after disruption of probe pad surfaces during test probing. An example method fills a sequence of metals and oxides over the disrupted probe pad surfaces and builds out a dielectric surface and interconnects for hybrid bonding. The interconnects may be connected to the probe pads, and/or to other electrical contacts of the substrate. A layer structure is described for increasing the yield and reliability of the resulting direct bonding process. Another example process builds the probe pads on a next-to-last metallization layer and then applies a direct bonding dielectric layer and damascene process without increasing the count of mask layers.

Abstract: A bonded structure is disclosed. The bonded structure includes a first element and a second element that is bonded to the first element along a bonding interface. The bonding interface has an elongate conductive interface feature and a nonconductive interface feature. The bonded structure also includes an integrated device that is coupled to or formed with the first element or the second element. The elongate conductive interface feature has a recess through a portion of a thickness of the elongate conductive interface feature. A portion of the nonconductive interface feature is disposed in the recess.

Abstract: Direct bonded stack structures for increased reliability and improved yields in microelectronics are provided. Structural features and stack configurations are provided for memory modules and 3DICs to reduce defects in vertically stacked dies. Example processes alleviate warpage stresses between a thicker top die and direct bonded dies beneath it, for example. An etched surface on the top die may relieve warpage stresses. An example stack may include a compliant layer between dies. Another stack configuration replaces the top die with a layer of molding material to circumvent warpage stresses. An array of cavities on a bonding surface can alleviate stress forces. One or more stress balancing layers may also be created on a side of the top die or between other dies to alleviate or counter warpage. Rounding of edges can prevent stresses and pressure forces from being destructively transmitted through die and substrate layers. These measures may be applied together or in combinations in a single package.

Abstract: Representative techniques and devices including process steps may be employed to mitigate the potential for delamination of bonded microelectronic substrates due to metal expansion at a bonding interface. For example, a metal pad having a larger diameter or surface area (e.g., oversized for the application) may be used when a contact pad is positioned over a TSV in one or both substrates.

Abstract: Devices and techniques including process steps make use of recesses in conductive interconnect structures to form reliable low temperature metallic bonds. A fill layer is deposited into the recesses prior to bonding. First conductive interconnect structures are bonded at ambient temperatures to second metallic interconnect structures using direct bonding techniques, with the fill layers in the recesses in one or both of the first and second interconnect structures.

Abstract: Representative techniques and devices including process steps may be employed to mitigate the potential for delamination of bonded microelectronic substrates due to metal expansion at a bonding interface. For example, a through-silicon via (TSV) may be disposed through at least one of the microelectronic substrates. The TSV is exposed at the bonding interface of the substrate and functions as a contact surface for direct bonding.

Abstract: Bonded structures and methods of direct hybrid bonding are disclosed. Non-conductive regions of two elements, such as dies or wafers, are first bonded together to form a bonded structure. Aligned conductive regions of the bonded structure, such as metal pads or traces, are then annealed to expand and bridge a gap between them. The anneal includes rapid thermal processing (RTP), such as with radiant heating. The bond interface between the first and second conductive features includes rapid growth structure(s) indicative of the inclusion of RTP in the anneal. Additional non-RTP anneal phases can also be employed.

Abstract: Representative techniques provide process steps for forming a microelectronic assembly, including preparing microelectronic components such as dies, wafers, substrates, and the like, for bonding. One or more surfaces of the microelectronic components are formed and prepared as bonding surfaces. The microelectronic components are stacked and bonded without adhesive at the prepared bonding surfaces.

Abstract: An element, a bonded structure including the element, and a method forming the element and the bonded structure are disclosed. The element can include a non-conductive region having a cavity. The element can include a conductive feature formed in the cavity. The conductive feature includes a center portion and an edge portion having first and second coefficients of thermal expansion respectively. The center and edge portions are recessed relative to a contact surface of the non-conductive region by a first depth and a second depth respectively. The first coefficient of thermal expansion can be at least 5% greater than the second coefficient of thermal expansion. The bonded structure can include the element and a second element having a second non-conductive region and a second conductive feature. A conductive interface between the first and second conductive features has a center region and an edge region.

Abstract: Representative implementations of techniques and methods include processing singulated dies in preparation for bonding. A plurality of semiconductor die components may be singulated from a wafer component, the semiconductor die components each having a substantially planar surface. Particles and shards of material may be removed from edges of the plurality of semiconductor die component. Additionally, one or more of the plurality of semiconductor die components may be bonded to a prepared bonding surface, via the substantially planar surface.

Abstract: Representative techniques and devices including process steps may be employed to mitigate the potential for delamination of bonded microelectronic substrates due to metal expansion at a bonding interface. For example, a through-silicon via (TSV) may be disposed through at least one of the microelectronic substrates. The TSV is exposed at the bonding interface of the substrate and functions as a contact surface for direct bonding.

Abstract: A bonded structure can include a carrier including a first conductive contact and a second conductive contact, a first singulated element including a third conductive contact directly bonded to the first conductive contact without an adhesive, and a second singulated element including a fourth conductive contact directly bonded to the second conductive contact without an adhesive, wherein the first and second conductive contacts are spaced apart by a contact spacing of no more than 250 microns.

Abstract: Devices and techniques including process steps make use of recesses in conductive interconnect structures to form reliable low temperature metallic bonds. A fill layer is deposited into the recesses prior to bonding. First conductive interconnect structures are bonded at ambient temperatures to second metallic interconnect structures using direct bonding techniques, with the fill layers in the recesses in one or both of the first and second interconnect structures.

Abstract: Techniques for joining dissimilar materials in microelectronics are provided. Example techniques direct-bond dissimilar materials at an ambient room temperature, using a thin oxide, carbide, nitride, carbonitride, or oxynitride intermediary with a thickness between 100-1000 nanometers. The intermediary may comprise silicon. The dissimilar materials may have significantly different coefficients of thermal expansion (CTEs) and/or significantly different crystal-lattice unit cell geometries or dimensions, conventionally resulting in too much strain to make direct-bonding feasible. A curing period at ambient room temperature after the direct bonding of dissimilar materials allows direct bonds to strengthen by over 200%. A relatively low temperature anneal applied slowly at a rate of 1° C. temperature increase per minute, or less, further strengthens and consolidates the direct bonds.

Abstract: A bonded structure comprises a frame element having a cavity formed through its thickness. The frame element is directly bonded to a first element at a first side and to a second element at a second side enclosing the cavity. The frame element may comprise a through substrate via (TSV). Redundant conductive contact pads may be formed in bonding layers for enhanced direct bonding quality and reliability.