United States of America As Represented by the Administrator of Nasa

Other

Michael J Logan

Robert L Fox

Qamar A Shams

Fred Albert Marconi, Jr

Christopher L Fox, Legal Representative

Joseph Micah Prendergast

Melanie L Fox, Legal Representative

Thomas L Vranas

Brittney N Lipp

Walter C Babel, Iii

Mary Beth Riehlman

Mark A Motter

John C Ingham

Richard Deloach

Sean A Laughter

Terry Anne Bocklet

Theodore R Kuhn, Iii

James K Adams

A vape cleaning device for easily and thoroughly cleaning vape coils for reuse and avoiding the need for frequent replacement. The device has a base enclosing a fan oriented to direct air upwardly, a heat block suspended above the fan, a heating element coupled to the heat block, and a shield coupled to the base and having a central opening. A cup is removably positioned in the central opening of the shield and in contact with the heat block to be heated thereby. A vape coil holder may removably suspended in the cup that the vape coil is submerged in a cleaning fluid in the cup. After the cup has been warmed to a predetermined temperature for a cleaning cycle, the cup may be removed and the vape coil holder suspended from the shield. The fan may then be operated for a predetermined time period for a drying cycle.

Vape coil cleaning device

Systems, methods, and devices are provided that enable robust operations of a small unmanned aircraft system (sUAS) using a compound wing. The various embodiments may provide a sUAS with vertical takeoff and landing capability, long endurance, and the capability to operate in adverse environmental conditions. In the various embodiments a sUAS may include a fuselage and a compound wing comprising a fixed portion coupled to the fuselage, a wing lifting portion outboard of the fixed portion comprising a rigid cross member and a controllable articulating portion configured to rotate controllable through a range of motion from a horizontal position to a vertical position, and a freely rotating wing portion outboard of the wing lifting portion and configured to rotate freely based on wind forces incident on the freely rotating wing portion.

Compound wing vertical takeoff and landing small unmanned aircraft system

A self-contained avionics sensing and flight control system is provided for an unmanned aerial vehicle (UAV). The system includes sensors for sensing flight control parameters and surveillance parameters, and a Global Positioning System (GPS) receiver. Flight control parameters and location signals are processed to generate flight control signals. A Field Programmable Gate Array (FPGA) is configured to provide a look-up table storing sets of values with each set being associated with a servo mechanism mounted on the UAV and with each value in each set indicating a unique duty cycle for the servo mechanism associated therewith. Each value in each set is further indexed to a bit position indicative of a unique percentage of a maximum duty cycle for the servo mechanism associated therewith. The FPGA is further configured to provide a plurality of pulse width modulation (PWM) generators coupled to the look-up table. Each PWM generator is associated with and adapted to be coupled to one of the servo mechanisms.

Self-contained avionics sensing and flight control system for small unmanned aerial vehicle

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Chesapeake, VA, United States of America

Michael J Logan