Abstract: An aerodynamic vehicle includes an aerodynamic heat exchanger formed as one or more body panels disposed along an outer surface of the vehicle having one or more fluidic chambers or micro-channels. The aerodynamic heat exchanger is adapted to provide effective and highly efficient heat transfer, and also to provide substantially reduced or negligible contribution to the aerodynamic drag. The aerodynamic heat exchanger may provide adequate heat rejection capacity throughout vehicle operating conditions that advantageously results in increased fuel economy and overall vehicle performance.

Abstract: A thermal management system for an electric vehicle having a drivetrain flow path coupling one or more motors and one or more inverters to an aerodynamic heat exchanger comprising one or more body panels disposed along an outer surface of the vehicle, the aerodynamic heat exchanger having one or more fluidic chambers or micro-channels. The drive flow path is decoupled from the vehicle's chiller and/or refrigeration cycle under all operating conditions. The drivetrain may be further characterized by the one or more motors being disposed proximate one or more wheels of the vehicle, such as within the wheel skirt or cowling, to capitalize on passive or free cooling via ambient airflow about the wheel. The thermal management system may further include a refrigeration cycle wherein the cabin and the battery pack are provided cooling in a parallel configuration or in a serial configuration.

Abstract: An aerodynamic vehicle includes an aerodynamic heat exchanger formed as one or more body panels disposed along an outer surface of the vehicle having one or more fluidic chambers or micro-channels. The aerodynamic heat exchanger is adapted to provide effective and highly efficient heat transfer, and also to provide substantially reduced or negligible contribution to the aerodynamic drag. The aerodynamic heat exchanger may provide adequate heat rejection capacity throughout vehicle operating conditions that advantageously results in increased fuel economy and overall vehicle performance.

Abstract: An electric vehicle having a heat exchanger formed in an aerodynamic airfoil shape comprising one or more body panels disposed along an outer surface of the vehicle having one or more fluidic chambers or micro-channels. The heat exchanger is adapted to provide effective and highly efficient heat transfer, and also to provide substantially reduced or negligible contribution to the aerodynamic drag. The heat exchanger includes a supplemental heat exchange system wherein at least a portion of the heat exchange capacity is provided by an inner heat exchange surface of the heat exchanger exposed to an interstitial space within the vehicle. Airflow is forced, via a fan for example, from an aerodynamically-efficient inlet, over the inner heat exchange surface, and exhausted through an aerodynamically-efficient outlet, thereby providing a supplemental heat exchange system including substantially reduced or negligible contribution to the aerodynamic drag.

Abstract: The present disclosure describes computer systems and computer-implemented methods for use in an agricultural operation. Vehicle location information for at least one agricultural vehicle is received, and the vehicle location information is used to determine a vehicle path. Vehicle state information is received from the vehicle and is used to determine whether the vehicle is in a working or non-working state. The vehicle path is then rendered on a map display, with the map display visually distinguishing between sections of the vehicle path traversed while the vehicle is in the working state and sections of the vehicle path traversed while the vehicle is in the non-working state.

Abstract: A robotic surgical tool includes a drive housing having a lead screw extending from a first end of the drive housing, a carriage movably mounted to the lead screw at a carriage nut secured to the carriage, and an elongate shaft extending from the carriage and penetrating the first end, the shaft having an end effector arranged at a distal end thereof and comprising a proximal shaft portion releasably coupled to a distal shaft portion at a releasable interface. Proximal and distal portions of one or more mechanisms of the surgical tool extend from the carriage to the end effector within the proximal and distal shaft portions, respectively, and the one or more mechanisms are operable to operate or articulate the end effector.

Abstract: A surgical tool comprising a drive housing having a first end, a spline extending from the first end and having a spline pinion gear mounted to the spline, a drive input that rotatably couples the spline to the first end and provides an input pinion gear; a clutch interposing the spline and input pinion gears and defining an internal gear, and an armature. The armature may be operatively coupled to the clutch and operable to shift the clutch from a first position, where the internal gear simultaneously mates with the spline and input pinion gears such that rotation of the drive input correspondingly rotates the spline, to a second position, where the internal gear is disengaged from the input pinion gear such that the spline is rotatable independent of the drive input.

Abstract: The present invention relates to an airside system for a vehicle HVAC system and to a HVAC apparatus, system and method having a multidirectional vent formed integrally with a mount adapted to receive a user interface in the form of a centrally disposed touch screen. The vent/interface assembly may be disposed inside the vehicle cabin including, but not limited to, the dashboard and/or instrument panel. The one or more outlets of the vent may be disposed partially or completely around the touch screen perimeter. Each outlet may flow in one or more directions, be individually adjustable either automatically or manually, or be stationary. The assembly may be configured to position the user interface offset from the dashboard. The outlet(s) of the vent may be partially or completely hidden behind the user interface. On/off and directional control of each outlet may be achieved by means of vanes, blades, and/or slots.

Abstract: A robotic surgical tool for a robotic instrument driver that includes a handle having a first end, at least one spline rotatably coupled to the handle and extending proximally from the first end, a carriage movably mounted to the at least one spline and including a first layer and a second layer operatively coupled to the first layer. At least one spline extends through a portion of at least one of the first and second layers and the carriage translates along the at least one spline. The robotic surgical tool also includes an elongate shaft extending from the carriage and penetrating the first end, the shaft having an end effector arranged at a distal end thereof and an activating mechanism coupled to one or both of the first and second layers and actuatable to operate a function of the end effector.

Abstract: Disclosed is a helicopter having a longitudinal axis, a lateral axis and a vertical axis, a helicopter centre of mass and a maximum gross mass of less than 5000 kg, the helicopter comprising a fuselage elongate along the longitudinal axis, the fuselage comprising an aerodynamically shaped shell defining a front, a rear, a top and a bottom of the fuselage and a passenger cabin therein having two forward-facing front seating positions for the pilot and a co-pilot or a passenger, and forward-facing rear seating positions for at least 2 passengers, optionally 3 passengers; a primary fuel cell mounted substantially behind the passenger cabin; the front seating position for the pilot having a centre of mass at a first location substantially in front of the rotor hub location, and the primary fuel cell having a centre of mass at a second location substantially behind the rotor hub location; a landing gear arrangement; a power plant mounted substantially above and behind the passenger cabin, wherein the primary fuel

Abstract: Disclosed is a collective control arrangement for a helicopter having a plurality of rotor blades, the collective control arrangement comprising: an armrest for a pilots seat, the armrest comprising an elongate channel; and a collective handle comprising: a first end slidably disposed in the elongate channel for coupling to one or more helicopter actuators that control collective pitch of the plurality of rotor blades; and a second end for gripping by a pilot. Advantageously the armrest comprises an elbow support portion configured to be located backwards of the hollow when the armrest is installed in the helicopter.

Abstract: A surgical instrument and method of operating same includes an end effector and a shaft assembly. The shaft assembly has proximal and distal shaft portions respectively extending along proximal and distal axes, a first elongate member, and an articulation section. The articulation section extends between the proximal and distal shaft portions and is configured to articulate about a first articulation axis and about a second articulation axis to thereby respectively deflect the end effector along a first plane and a second plane. The articulation section has a first lumen radially offset from the proximal and distal axes that longitudinally intersects the first and second articulation axes. The first lumen movably supports the first elongate member such that the radial spacing of the first elongate member is maintained relative to the proximal and distal axes at each of the first and second articulation axes during deflection of the end effector.

Abstract: The present disclosure describes computer systems and computer-implemented methods for use in an agricultural operation. Vehicle location information for at least one agricultural vehicle is received, and the vehicle location information is used to determine a vehicle path. Vehicle state information is received from the vehicle and is used to determine whether the vehicle is in a working or non-working state. The vehicle path is then rendered on a map display, with the map display visually distinguishing between sections of the vehicle path traversed while the vehicle is in the working state and sections of the vehicle path traversed while the vehicle is in the non-working state.

Abstract: A light helicopter typically for 5 occupants is disclosed which achieves a hitherto unprecedented combination of range, speed and payload by adopting a novel approach to construction and positioning of components which affect overall aerodynamics in forward flight at speeds in excess of 70 metres per second and mass distribution and management of centre of gravity as fuel is consumed, load bearing strength and drag.

Abstract: A system for treating an eye includes a laser light source providing photoactivating light. The system includes a scanning system to receive the photoactivating light as a laser beam and to move the laser beam over a cornea treated with a cross-linking agent. The system includes a controller that provides control signal(s) to programmatically control the laser light source and the scanning system. The control signal(s) cause the laser beam to visit region(s) of the cornea more than once according to a scan pattern and expose the region(s) to the photoactivating light. The photoactivating light causes the cross-linking agent in the exposed region(s) to react with oxygen to generate cross-linking activity in the exposed region(s). The scan pattern causes a predetermined period of time to pass between visits by the laser beam to the exposed region(s), the predetermined period of time allowing oxygen in the exposed region(s) to replenish.

Abstract: A surgical tool includes a drive housing having opposing first and second ends and a drive input rotatably mounted to the drive housing at the first end, a carriage mounted entirely within the drive housing and movable between the first and second ends via actuation of the drive input, an instrument driver matable with the drive housing at the first end, a drive output matable with the drive input such that rotation of the drive output rotates the drive input and translates the carriage within the drive housing, a shaft coupled to and extending distally from the carriage and penetrating the first end and the instrument driver, and a fin connected to the carriage and accessible by a user at an exterior of the drive housing, the fin being manually translatable along the exterior of the drive housing between the first and second ends to thereby translate the carriage.

Abstract: Described herein are systems, methods, and other techniques for controlling a velocity of a construction machine operating within a construction site. Sensor data is captured using one or more sensors of the construction machine while the construction machine is moving at the velocity in a forward or a backward direction. An actual surface of the construction site is estimated based on the sensor data. A deviation between a target surface and the actual surface is calculated. An actual performance metric is calculated based on the deviation. The actual performance metric is compared to a target performance metric to determine a velocity adjustment. The velocity of the construction machine is adjusted by the velocity adjustment.

Abstract: Disclosed is a ground movement system for a helicopter having a fuselage and rotor blades fixed to the top of the fuselage, the ground movement system comprising at least three wheels secured below the fuselage of the helicopter, the wheels being retractable during flight; a motor positioned in the hub or on the undercarriage leg of each of at least two of the wheels, wherein each motor is operable to rotate the wheel in forward and backward directions; wherein each motor allows the wheel to rotate freely when unpowered; at least one user interface operable to receive user input commands to control the speed and direction of travel of the helicopter using the ground movement system; and a control arrangement to provide control signals to each of the motors based on the user input commands.

Abstract: Disclosed is an autopilot system for a helicopter, the helicopter having: a cyclic and a collective that are physically coupled to helicopter actuators that control cyclic and collective pitch of main rotor blades of the helicopter and anti-torque pedals that are physically coupled to helicopter actuators that control the pitch of tail rotor blades of the helicopter; and at least one servomechanism configured to amplify force applied by the pilot to the cyclic, collective and/or anti-torque pedals; wherein the autopilot system comprises an autopilot actuator configured to: in an autopilot mode, control direction or orientation of the helicopter by applying force to a control link that is physically coupled to one of the helicopter actuators; and in a manual mode, provide stability or control augmentation by applying a force on one of the cyclic, the collective or one or both of the anti-torque pedals to influence the pilot's inputs to urge the helicopter away from a particular flight condition dependent on mo

Abstract: Disclosed is a pitch and roll control arrangement for controlling both lateral and longitudinal orientation of an aircraft having at least one pilots seat, wherein the control arrangement comprises a handle (5110) positionable substantially above the pilot's seat and shaped to be gripped by a pilot (10); an elongate connector (5112) that extends in a generally forward direction from the handle portion to a forward joint; an elongate transverse arm (5116) extending generally transversely from the forward joint of the connector to a mounting location forward and to the side of the pilot in use; a mounting arrangement configured to support the transverse arm at the mounting location to permit the transverse arm to move laterally sideways and fore and aft and to constrain the forward joint to move generally horizontally as the handle is moved fore and aft and laterally by the pilot; a control coupling associated with the mounting arrangement arranged to provide at least one moving connection which moves in respon