Abstract: An electrosurgical generator that can be used, for example, to provide radio-frequency (RF) energy for localized tissue coagulation, cutting, ablation, and to create lesions in nervous tissue. The generator can provide controls for line power, RF power, setting temperature and/or power, for selecting preset temperature and power combinations, and for selecting programmed treatment profiles. The generator can have a display to display the desired probe and tissue temperature, measured probe impedance, actual probe and/or tissue temperature, delivered power, treatment time, mode setting, preset selection, and messages, and indicators for RF Power On, Stimulation On, and Fault Condition. The generator can include the ability to generate low frequency pulses to stimulate nerves and to assist in the proper placement of the electrosurgical probe in the location that is causing pain.

Abstract: A method includes recognizing an electrosurgical probe coupled to an electrosurgical generator, selecting a mode of the electrosurgical generator based upon the recognized probe, setting a therapy profile based upon the selected mode, and displaying the therapy profile. The generator can include user inputs for modifying the therapy profile. A computer implemented method for achieving a target temperature includes: a) receiving the target temperature; b) calculating a first set temperature; c) commanding a first output power level until a measured temperature is equal to or greater than the first set temperature; d) calculating an updated set temperature based upon the target temperature; e) commanding a second output power level until the measured temperature is equal to or greater than the updated set temperature; and repeating d and e until the updated set temperature is equal to the target temperature.

Abstract: A firefighting apparatus is adapted for use in a host aircraft comprising a fuselage defining an interior and an exterior. The firefighting apparatus includes a pressurizeable retardant tank disposed in the interior of the host aircraft, the retardant tank being capable of roll-on and roll-off installation, an ejection tube in fluid communication with the retardant tank, and a door plug for mounting within a fuselage orifice in the host aircraft. The door plug provides for fluid communication of retardant from the retardant tank through the ejection tube to the exterior of the host aircraft. At least one sensor is operably connected to the firefighting apparatus to effect user-discernable data for effecting retardant delivery.

Abstract: A method includes recognizing an electrosurgical probe coupled to an electrosurgical generator, selecting a mode of the electrosurgical generator based upon the recognized probe, setting a therapy profile based upon the selected mode, and displaying the therapy profile. The generator can include user inputs for modifying the therapy profile. A computer implemented method for achieving a target temperature includes: a) receiving the target temperature; b) calculating a first set temperature; c) commanding a first output power level until a measured temperature is equal to or greater than the first set temperature; d) calculating an updated set temperature based upon the target temperature; e) commanding a second output power level until the measured temperature is equal to or greater than the updated set temperature; and repeating d and e until the updated set temperature is equal to the target temperature.

Abstract: An autonomous marine vehicle is disclosed, the vehicle comprising a rigid hull having an interior and a periphery, a deck joining the rigid hull at the periphery; and a rigid mast pivotally attached to the deck, the mast housing a plurality of sensors capable of effecting communication to and from said vehicle. In preferred embodiments, the vehicle further comprises various sensors and mission-specific hardware. Sensors include mast-mounted audio/video devices, radar, GPS and RF antennas, and other positioning and collision avoidance devices. Mission-specific hardware include refueling probes, fire protection systems, towing assemblies, flame thrower assemblies, liquid spray assemblies, and work pup assemblies.

Abstract: The system and apparatus of this invention provides for a rapidly loaded, palletized, non-dedicated fixed or rotary wing aircraft based, manned observation, sensor launch system, with self-powered sensing and targeting pod, multi-frequency antenna array, and with C4I analysis and control capabilities. The system may be used to deploy and manipulate autonomous and remote control vehicles, for the purpose of recovering and protecting persons in peril; containing/remediating toxic spills; sensing/detection; fire fighting; ship towing; or surface based refueling and support. Although not the primary purpose, this system can also be used for to support an offensive weapons system which could be used to selectively eliminate various targets with a standoff delivery capability.