Abstract: Aspects include a system for transferring a payload between drones. The system includes a first aerial drone having a first transfer member and a first controller. The first controller including a processor configured to change a first altitude and first orientation of the first aerial drone. A second aerial drone is provided having a second transfer member and a second controller, the second transfer member having a cone member on one end, the second transfer member being configured to receive the payload. The second controller including a processor configured to change a second altitude and a second orientation of the second aerial drone. The controllers cooperate to dispose the first transfer member within the cone member and transfer the payload from the first aerial drone to the second aerial drone.

Abstract: An example operation may include one or more of receiving a request to authorize an in-flight transfer of a parcel between a source unmanned aerial vehicle (UAV) and a target UAV, authenticating, via a blockchain, an identity of the source UAV and an identity of the target UAV based on one or more predefined keys included in the request, and in response to the blockchain authentication being successful, initiating delivery of the parcel from the source UAV to the target UAV while one or more of the source UAV and the target UAV are in-flight.

Abstract: An example operation may include one or more of receiving a request to authorize an in-flight transfer of a parcel between a source unmanned aerial vehicle (UAV) and a target UAV, authenticating, via a blockchain, an identity of the source UAV and an identity of the target UAV based on one or more predefined keys included in the request, and in response to the blockchain authentication being successful, initiating delivery of the parcel from the source UAV to the target UAV while one or more of the source UAV and the target UAV are in-flight.

Abstract: A method and system for eye tracking according to one or more embodiment is presented. Aspects include overlaying, on a display of an ocular device, an image comprising an inner transparent region and an outer semitransparent region. Aspects also include overlaying one or more characters within the outer semitransparent region and tracking, by a sensor, an eye movement of the user to obtain a user emphasis of the one or more characters within the outer semitransparent region. Aspects also include receiving an input from the user to indicate the selection of the one or more characters based on the user emphasis.

Abstract: Aspects include a system for transferring a payload between drones. The system includes a first aerial drone having a first transfer member and a first controller. The first controller including a processor configured to change a first altitude and first orientation of the first aerial drone. A second aerial drone is provided having a second transfer member and a second controller, the second transfer member having a cone member on one end, the second transfer member being configured to receive the payload. The second controller including a processor configured to change a second altitude and a second orientation of the second aerial drone. The controllers cooperate to dispose the first transfer member within the cone member and transfer the payload from the first aerial drone to the second aerial drone.

Abstract: Aspects include a system for transferring a payload between drones. The system includes a first drone having a first member and a first controller, the first member having a first coupling device on one end, the first member being configured to carry a payload, the first controller being configured to change a first altitude and orientation of the first drone. A second drone includes a second member and controller, the second member having a second coupling device on one end, the second member being configured to receive the payload, the second controller being configured to change a second altitude and orientation of the second drone. The controllers cooperate to change at least one of first and second orientations to operably engage the first coupling device to the second coupling device for transferring the payload from the first member to the second member.

Abstract: Aspects include a system for transferring a payload between drones. The system includes a first drone having a first member and a first controller, the first member having a first coupling device on one end, the first member being configured to carry a payload, the first controller being configured to change a first altitude and orientation of the first drone. A second drone includes a second member and controller, the second member having a second coupling device on one end, the second member being configured to receive the payload, the second controller being configured to change a second altitude and orientation of the second drone. The controllers cooperate to change at least one of first and second orientations to operably engage the first coupling device to the second coupling device for transferring the payload from the first member to the second member.

Abstract: Embodiments of the invention relate to a primary contact or primary body comprising of a primary material with a propensity to corrode. A location on a surface of the primary body is an active location and functions to interface with a secondary body. The active location has a first surface and an oppositely disposed second surface. An anode material is applied to the second surface adjacent to the active location on the first surface. The primary body is exposed to a corrosive material. The anode material functions to divert a galvanic corrosive medium from the active location to the applied anode material.

Abstract: Aspects include a system for transferring a payload between drones. The system includes a first drone having a first member and a first controller, the first member having a first coupling device on one end, the first member being configured to carry a payload, the first controller being configured to change a first altitude and orientation of the first drone. A second drone includes a second member and controller, the second member having a second coupling device on one end, the second member being configured to receive the payload, the second controller being configured to change a second altitude and orientation of the second drone. The controllers cooperate to change at least one of the first and second altitude, and the first and second orientation to operably engage the first coupling device to the second coupling device for transferring the payload from the first member to the second member.

Abstract: Embodiments of the invention relate to a primary contact or primary body comprising of a primary material with a propensity to corrode. A location on a surface of the primary body is an active location and functions to interface with a secondary body. The active location has a first surface and an oppositely disposed second surface. An anode material is applied to the second surface adjacent to the active location on the first surface. The primary body is exposed to a corrosive material. The anode material functions to divert a galvanic corrosive medium from the active location to the applied anode material.

Abstract: A system contains a land grid array socket with a first set of socket interconnections configured to connect to a set of circuit board electrical connectors, each socket interconnection in the first set extending from a top surface to a bottom surface. A second set of socket interconnections are configured to reversibly connect to a set of circuit card electrical connectors. A circuit board can include a mounting surface fastened to the land grid array socket. A set of electrical connectors within a socket connector zone can be connected to at least some of the first set of socket interconnections. A board cutout section is located beneath a second interconnection zone and configured to receive a circuit card.

Abstract: A system contains a land grid array socket with a first set of socket interconnections configured to connect to a set of circuit board electrical connectors, each socket interconnection in the first set extending from a top surface to a bottom surface. A second set of socket interconnections are configured to reversibly connect to a set of circuit card electrical connectors. A circuit board can include a mounting surface fastened to the land grid array socket. A set of electrical connectors within a socket connector zone can be connected to at least some of the first set of socket interconnections. A board cutout section is located beneath a second interconnection zone and configured to receive a circuit card.

Abstract: A method of producing a land grid array (LGA) interposer structure, including an electrically insulating carrier plane, and at least one interposer mounted on a first surface of said carrier plane. The interposer possesses a hemi-toroidal configuration in transverse cross-section and is constituted of a dielectric elastomeric material. A plurality of electrically-conductive elements are arranged about the surface of the at least one hemi-toroidal interposer and extend radically inwardly and downwardly from an uppermost end thereof into electrical contact with at least one component located on an opposite side of the electrically insulating carrier plane.

Abstract: A method of producing a module arrangement which includes a land grid array (LGA) interposer structure, including an electrically insulating carrier plane, and at least one interposer mounted on a first surface of said carrier plane. The interposer possesses a hemi-toroidal configuration in transverse cross-section and is constituted of a dielectric elastomeric material. A plurality of electrically-conductive elements are arranged about the surface of the at least one hemi-toroidal interposer and extend radically inwardly and downwardly from an uppermost end thereof into electrical contact with at least one component located on an opposite side of the electrically insulating carrier plane.

Abstract: A method of producing a land grid array (LGA) interposer structure, including an electrically insulating carrier plane, and at least one interposer mounted on a first surface of said carrier plane. The interposer possesses a hemi-toroidal configuration in transverse cross-section and is constituted of a dielectric elastomeric material. A plurality of electrically-conductive elements are arranged about the surface of the at least one hemi-toroidal interposer and extend radically inwardly and downwardly from an uppermost end thereof into electrical contact with at least one component located on an opposite side of the electrically insulating carrier plane.

Abstract: A method of producing a land grid array (LGA) interposer structure, including an electrically insulating carrier plane, and at least one interposer mounted on a first surface of said carrier plane. The interposer possesses a hemi-toroidal configuration in transverse cross-section and is constituted of a dielectric elastomeric material. A plurality of electrically-conductive elements are arranged about the surface of the at least one hemi-toroidal interposer and extend radically inwardly and downwardly from an uppermost end thereof into electrical contact with at least one component located on an opposite side of the electrically insulating carrier plane. A plurality of slots are formed in the sidewall of said interposer for the venting of gases and pressure therethrough.

Abstract: A method of producing a land grid array (LGA) interposer structure, including an electrically insulating carrier plane, and mounting at least one interposer on a first surface of said carrier plane. The interposer possesses a hemi-toroidal configuration in transverse cross-section and is constituted of a dielectric elastomeric material. At least one sidewall of the interposer is slitted to facilitate the venting of gases and pressure therethrough. The method includes arranging a plurality of electrically-conductive elements about the surface of the at least one hemi-toroidal interposer and extending them radically inwardly and downwardly from an uppermost end thereof into electrical contact with at least one component located on an opposite side of the electrically insulating carrier plane.

Abstract: An apparatus is disclosed for aligning socket housing segments for an area array device. Each socket housing segment includes at least a first surface and a second surface, with the second surface opposite the first surface. The second surface of each socket housing segment provides electrical connections for a portion of the area array device. Socket contact pads are disposed on the first surfaces of the plurality of socket housing segments. The socket contact pads correspond to substrate contact pads disposed on a substrate. One or more alignment structures are disposed at a space between the socket housing segments. Each alignment structure is coupled to at least two of the socket housing segments. The one or more alignment structures maintain a predetermined alignment of each socket housing segment so that the socket contact pads align with the substrate contact pads during a surface mount connection process.

Abstract: A land grid array (LGA) interposer structure, including an electrically insulating carrier plane, and at least one interposer mounted on a first surface of said carrier plane. The interposer possesses a hemi-toroidal configuration in transverse cross-section and is constituted of a dielectric elastomeric material. A plurality of electrically-conductive elements are arranged about the surface of the at least one hemi-toroidal interposer and extend radically inwardly and downwardly from an uppermost end thereof into electrical contact with at least one component located on an opposite side of the electrically insulating carrier plane. Provided is also a method of producing the land grid array interposer structure.

Abstract: A method of producing a land grid array (LGA) interposer structure includes mounting at least one interposer on a first surface of an electrically insulating carrier plane. The interposer selectively having a hemi-toroidal, conical, dome-shaped conic section, generally cylindrical or hemi-spherical configuration in transverse cross-section and being constituted of a dielectric elastomeric material. The method includes positioning a plurality of electrically-conductive elements about the surface of the hemi-toroidal interposer that extend radially inwardly and downwardly from an uppermost end thereof. The method further includes mounting said at least one component comprising at least one hemi-toroidal interposer mounted on said opposite side of said carrier plane.