Abstract: An end effector assembly of a surgical instrument includes an ultrasonic blade adapted to receive ultrasonic energy from a source of ultrasonic energy to vibrate the ultrasonic blade. A jaw member is movable relative to the ultrasonic blade from a spaced-apart position to an approximated position for clamping tissue. A jaw liner is engaged with the jaw member such that the jaw liner contacts the ultrasonic blade when the jaw member is in the approximated position. The ultrasonic blade is adapted to receive electrosurgical energy from a source of electrosurgical energy. The ultrasonic blade defines a distal tip. The distal tip of the ultrasonic blade is configured to direct electrosurgical energy.

Abstract: An end effector assembly of a surgical instrument includes an ultrasonic blade. A jaw member is movable relative to the ultrasonic blade from a spaced-apart position to an approximated position. The jaw member includes a structural body. The structural body defines a first side facing the ultrasonic blade and a second side facing away from the ultrasonic blade. A jaw liner is engaged with the first side of the structural body such that the jaw liner contacts the ultrasonic blade when the jaw member is in the approximated position. An electrode is engaged with the second side of the structural body. The electrode is adapted to connect to a source of electrosurgical energy. The electrode defines a first portion and a second portion. The first portion of the electrode is in contact with the structural body and the second portion of the electrode tapers to a pointed edge.

Abstract: An articulating surgical instrument includes a housing, a shaft extending distally from the housing, an end effector assembly, and an articulating component interconnecting the shaft and end effector assembly. The articulating component includes a proximal disk connected to the shaft, a distal disk connected to the end effector assembly, an intermediate disk, a first flexible interconnect connecting the proximal and intermediate disks, and a second flexible interconnect connecting the intermediate and distal disks. The first flexible interconnect defines a single plane of bending to enable articulation of the end effector assembly relative to the shaft within a first plane. The second flexible interconnect defines a single plane of bending substantially perpendicular to the single plane of bending of the first flexible interconnect to enable articulation of the end effector assembly relative to the shaft within a second plane substantially perpendicular to the first plane.

Abstract: A surgical end effector includes an ultrasonic blade and a jaw member. The blade is adapted to receive ultrasonic and electrosurgical energy and defines a distal face. The jaw member is movable relative to the blade from a spaced-apart to an approximated position for clamping tissue and includes a structural body having a body portion and a distal cap portion. The distal cap portion defines an electrode that receives electrosurgical energy. The jaw member further includes a jaw liner engaged within the body portion and extending therefrom towards the blade such that, in the approximated position, the jaw liner contacts the blade to define a gap distance between the electrode and the distal face to facilitate bipolar electrosurgical tissue treatment upon conduction of bipolar energy between the electrode and the distal face and through tissue in contact therewith.

Abstract: A computer-implemented method of object enhancement in endoscopy images includes capturing an image of an object within a surgical operative site via an imaging device, determining a size of the object based on the captured image of the object, displaying the captured image of the object, and displaying on the displayed captured image of the object a representation of the determined size of the object.

Abstract: In one embodiment, automated storage target selection includes automatically selecting a storage node of a plurality of candidate storage nodes as a function of a plurality of selection criteria. Further, a backup data object is transmitted to the selected storage node. In one embodiment, selecting a storage node includes retrieving stored user-defined parameters for selection criteria for selecting a storage node, retrieving storage node-defined parameters for selection criteria, comparing user-defined parameters and storage node-defined parameters, and selecting a storage node as a function of the comparing. In another aspect of the present description, comparing user-defined parameters and storage node-defined parameters includes broadening a first user-defined parameter to a second user-defined parameter broader than the first user-defined parameter if no candidate storage nodes have a storage node-defined parameter within the first user-defined parameter.

Abstract: In one embodiment, automated storage target selection includes automatically selecting a storage node of a plurality of candidate storage nodes as a function of a plurality of selection criteria. Further, a backup data object is transmitted to the selected storage node. In one embodiment, selecting a storage node includes retrieving stored user-defined parameters for selection criteria for selecting a storage node, retrieving storage node-defined parameters for selection criteria, comparing user-defined parameters and storage node-defined parameters, and selecting a storage node as a function of the comparing. In another aspect of the present description, comparing user-defined parameters and storage node-defined parameters includes broadening a first user-defined parameter to a second user-defined parameter broader than the first user-defined parameter if no candidate storage nodes have a storage node-defined parameter within the first user-defined parameter.

Abstract: In one embodiment, automated storage target selection includes automatically selecting a storage node of a plurality of candidate storage nodes as a function of a plurality of selection criteria. Further, a backup data object is transmitted to the selected storage node. In one embodiment, selecting a storage node includes retrieving stored user-defined parameters for selection criteria for selecting a storage node, retrieving storage node-defined parameters for selection criteria, comparing user-defined parameters and storage node-defined parameters, and selecting a storage node as a function of the comparing. In another aspect of the present description, comparing user-defined parameters and storage node-defined parameters includes broadening a first user-defined parameter to a second user-defined parameter broader than the first user-defined parameter if no candidate storage nodes have a storage node-defined parameter within the first user-defined parameter.

Abstract: In one embodiment, automated storage target selection includes automatically selecting a storage node of a plurality of candidate storage nodes as a function of a plurality of selection criteria. Further, a backup data object is transmitted to the selected storage node. In one embodiment, selecting a storage node includes retrieving stored user-defined parameters for selection criteria for selecting a storage node, retrieving storage node-defined parameters for selection criteria, comparing user-defined parameters and storage node-defined parameters, and selecting a storage node as a function of the comparing. In another aspect of the present description, comparing user-defined parameters and storage node-defined parameters includes broadening a first user-defined parameter to a second user-defined parameter broader than the first user-defined parameter if no candidate storage nodes have a storage node-defined parameter within the first user-defined parameter.

Abstract: A missile guidance system in which a projectile or missile is fired toward predetermined target with the missile being tracked on its flight toward the target by radar, processing the radar information in a computer apparatus and finally computing a new trajectory from the missile to the target and transmitting correction signals to a correction device on the missile including thrusters on the missile to cause the trajectory of the missile to be changed to the newly computed trajectory for the missile. This system corrects the trajectory of the missile while in flight by recomputing a trajectory from the missile to the predetermined target and making appropriate corrections each time. Thisenables the missile to only contain radar reflecting means, and correction detection and control means on the missile rather than having gyro and other type devices on board the missile which take up a considerable amount of space and weight.

Abstract: A laser missile guidance system in which a projectile or missile is fired ward a predetermined target with the missile being tracked on its flight toward the target by laser radar, processing the laser radar information in a computer apparatus and finally computing a new trajectory from the missile to the target and transmitting correction signals to a correction device on the missile including thrusters on the missile to cause the trajectory of the missile to be changed to the newly computed trajectory for the missile. This system corrects the trajectory of the missile while in flight by recomputing a trajectory from the missile to the predetermined target and making appropriate corrections each time. This enables the missile to only contain laser radar reflecting means, and correction detection and control means on the missile rather than having gyro and laser type devices on board the missile which take up a considerable amount of space and weight.