Abstract: An improved in-vehicle infotainment (IVI) system and methodology facilitating the display, computation, receipt and transmission of enhanced data elements and data files. System and methodology comprising an improved IVI system with an enhanced series of software and firmware capable of communicating with external data servers, processing enhanced protocols, transmitting data elements in report form with data attachments, and displaying the received enhanced data elements onto callout icons overlaid onto a GPS navigation interface. Additional system and methods include protocols for external servers to receive, encode, decode, compress, decompress, store, compute and transmit emergency reports and aggregate data files.

Abstract: An improved system and method to interlink a plurality of independently owned non-centralized registered autonomous aircraft identified by ESN, SN, MID, Remote ID or FAA registration number within a dedicated network for remote route deployment. System is comprised of a web-based application, aircraft identification protocol, aircraft selection protocol, aircraft flight path prioritization protocol and route avoidance protocol that establishes a communication protocol with a qualified aircraft for the purpose of routing to multiple destinations. Methodology includes recognizing a unique identifier to qualify the make, model, flight time, range and maximum payload for an automated aircraft.

Abstract: Static OEM hard-wired in-vehicle infotainment system method to capture and transmit vehicle route data for a defined geo-fenced area. Collects and transmits vehicle data to cloud server and maps geo-fenced area using GPS coordinates to produce report and vehicle route onto infotainment screen. Collective summery report and graphical display for all vehicles within a defined GPS Geo-Fenced area can also be displayed. Additional methodology includes GPS Proximity Based Advertising and Infotainment System Advertising. GPS Proximity Based Advertising defines radius around a GPS location, displaying advertisement when vehicle enters the radius. Infotainment System Advertising receives advertisement via software or firmware, onto the OEM hard-wired in-vehicle infotainment system memory.

Abstract: Static OEM hard-wired in-vehicle infotainment system method to capture and transmit vehicle route data for a defined geo-fenced area. Collects and transmits vehicle data to cloud server and maps geo-fenced area using GPS coordinates to produce report and vehicle route onto infotainment screen. Collective summery report and graphical display for all vehicles within a defined GPS Geo-Fenced area can also be displayed. Additional methodology includes GPS Proximity Based Advertising and Infotainment System Advertising. GPS Proximity Based Advertising defines radius around a GPS location, displaying advertisement when vehicle enters the radius. Infotainment System Advertising receives advertisement via software or firmware, onto the OEM hard-wired in-vehicle infotainment system memory.

Abstract: Static vehicle infotainment system method to capture and transmit vehicle route data for a defined geo-fenced area. Collects and transmits vehicle data to cloud server and maps geo-fenced area using GPS coordinates to produce report and vehicle route onto infotainment screen. Collective summery report and graphical display for all vehicles within a defined GPS Geo-Fenced area can also be displayed. Additional methodology includes GPS Proximity Based Advertising and Infotainment System Advertising. GPS Proximity Based Advertising defines radius around a GPS location, displaying advertisement when vehicle enters the radius. Infotainment System Advertising receives advertisement via software or firmware, onto the infotainment system memory.

Abstract: Systems and methods for determining turbine pressure related loads and for condition monitoring are provided. The systems and methods may measure at least one pressure differential on an airfoil. At least one pressure differential may be used to determine a root bending moment associated with the blade. Additionally or alternatively, at least one pressure differential may be used to determine a low-speed shaft moment for a turbine on which the blade is mounted. Still further, at least one pressure differential and/or moment may be used to gauge wear/fatigue and/or damage to one or more wind turbines. Based on this information, a controller may modify various operating characteristics of the turbine or blade to address the fatigue or damage.

Abstract: Systems, apparatuses, and methods are provided for actuating one or more load management devices on a wind turbine and/or a wind turbine blade. Each actuator may exhibit one or more beneficial qualities including appropriate actuation speed/force characteristics, size and/or weight characteristics, and/or increased reliability and consistent operation in a variety of operating conditions. According to some aspects, the actuator may be a direct pneumatic actuator, a ramp slide pneumatic actuator, a scissor actuator, a linear induction actuator, a belt actuator, a closed cam follower actuator, a screw drive actuator, a solenoid actuator, a rack and pinion actuator, a cylindrical cam follower actuator, a Y-belt actuator, an offset rotary drive actuator, a tape style actuator, a rigid tape actuator, a deformable membrane actuator, a memory alloy actuator, and/or a crank slide actuator.

Abstract: A mounting arrangement for a load compensating device is provided. The mounting arrangement includes a cover sheet connected to a housing via a plurality of protrusions. The cover sheet may form a portion of a surface of an airfoil rotor blade. The housing may include a plurality of clamps extending outward from the housing and configured to contact an inner surface of the airfoil rotor blade. By tightening the clamps onto the interior surface, the device is mounted to the blade and the cover sheet may deform to correspond to the airfoil geometry of the airfoil rotor blade. The mounting arrangement may further include a mounting plate configured to permit the housing to float within the aperture formed in the airfoil rotor blade, and a tab arranged on one end of the mounting plate to distribute centrifugal force to the surface of the airfoil rotor blade.

Abstract: An apparatus and system for automatically deploying an air deflector of a load compensating device when there is a loss of communication or power is provided. In some examples, the apparatus and system may include a spring configured to rotate a gear, thereby deploying the air deflector. In some arrangements, the spring may be a torsion spring and may be biased to rotate the gear when released from a hold position maintained by a latch. The latch may be controlled by a release mechanism, such as a solenoid, that may be configured to activate upon occurrence of a communication loss event. The release mechanism may release the latch, thereby releasing the spring and deploying the air deflector.

Abstract: Systems, apparatuses, and methods are provided for actuating one or more load management devices on a wind turbine and/or a wind turbine blade. Each actuator may exhibit one or more beneficial qualities including appropriate actuation speed/force characteristics, size and/or weight characteristics, and/or increased reliability and consistent operation in a variety of operating conditions. According to some aspects, the actuator may be a direct pneumatic actuator, a ramp slide pneumatic actuator, a scissor actuator, a linear induction actuator, a belt actuator, a closed cam follower actuator, a screw drive actuator, a solenoid actuator, a rack and pinion actuator, a cylindrical cam follower actuator, a Y-belt actuator, an offset rotary drive actuator, a tape style actuator, a rigid tape actuator, a deformable membrane actuator, a memory alloy actuator, and/or a crank slide actuator.

Abstract: A mounting arrangement for a load compensating device is provided. The mounting arrangement includes a cover sheet connected to a housing via a plurality of protrusions. The cover sheet may form a portion of a surface of an airfoil rotor blade. The housing may include a plurality of clamps extending outward from the housing and configured to contact an inner surface of the airfoil rotor blade. By tightening the clamps onto the interior surface, the device is mounted to the blade and the cover sheet may deform to correspond to the airfoil geometry of the airfoil rotor blade. The mounting arrangement may further include a mounting plate configured to permit the housing to float within the aperture formed in the airfoil rotor blade, and a tab arranged on one end of the mounting plate to distribute centrifugal force to the surface of the airfoil rotor blade.

Abstract: A machine includes a thermal ramp chamber; a thermal soak chamber coupled to the thermal ramp chamber; and a cooling chamber coupled to the thermal soak chamber. The cooling chamber can be an indirect cooling chamber including a thermal buffer that includes a substrate carrier. Each of the chambers can include an independently controlled elemental reactant source containing and supplying vapor having both i) independent control of a total vapor pressure of an elemental reactant containing vapor and ii) independent control of a partial vapor pressure of an elemental reactant vapor within that chamber.

Abstract: A method for changing the position of fibers in a nonwoven web to improve the isotropy of the web by using angled stream of fluid wherein the streams form a substantially coplanar curtain and impinge on the fibers at their leading ends, trailing ends or sides.

Abstract: A method for changing the position of fibers in a nonwoven web to improve the isotropy of the web by using angled stream of fluid wherein the streams form a substantially coplanar curtain and impinge on the fibers at their leading ends, trailing ends or sides.

Abstract: Disclosed is a low cost, easy to use cleaning apparatus to unclog or clean drain pipes or other conduits by directing high pressure water into contact with any solids in the pipe comprising a spray nozzle mounted in the end of a flexible water supply tube having, surrounding the nozzle, self centering fingers integrally formed by cutting slits or notches in the end of the supply tube and then inserting the nozzle which radially spreads the fingers.

Abstract: A pipe thawing apparatus has a heat exchanger for heating water. An electric water pump has an outlet coupled to an inlet of the heat exchanger. A flexible feed tube is coupled to an outlet of the heat exchanger. The electric water pump has an electric motor that is coupled to a source of electric power through a cyclical power interrupting device. The cyclical power interrupting device cyclically connects and disconnects the electric motor of the pump to the source of electric power cyclically turning the electric motor on and off. The water pump thus supplies a pulsating stream of water to the heat exchanger which in turn feeds a pulsating stream of heated water into the flexible feed tube. The flexible feed tube is advanced in the pipe to be thawed so that a pulsating stream of heated water is directed into the pipe, preferably against the ice to be melted. A return line is coupled between the pipe and an inlet of the water pump so that the water used by the apparatus is continuously recirculated.