Wing Aviation LLC

Adem Rudin

Stephen Benson

Adam Woodworth

James Schmalzried

André Prager

Jesse Blake

Kyle A Liske

Nicolas Renold

Evan Twyford

Clark Sopper

Ray Leung

Elizabeth Marshman

Thorsten Schilling

Michael Nowakowski

Kyle Liske

A landing gear assembly for an unmanned aerial vehicle (UAV) includes a shock tower, a pair of leg members, and suspension assemblies. The shock tower is adapted to mount to a frame of a fuselage of the UAV and includes upper and lower end mounts. The leg members are adapted to extend out from opposing sides of the lower end mounts. The leg members are flexible and each include an upper leg section pivotally mounted to the lower end mount and a lower leg section adapted to connect to a ground gear. The suspension assemblies are each mounted to and extend between the upper end mount and a corresponding one of the leg members. The suspension assemblies each include a damper and a spring.

Multistage suspension for UAV landing gear

An example method of manufacturing a wing includes providing a wing frame. The wing frame includes a primary spar, a drag spar, a plurality of transverse frame elements having at least one spar joiner, and a plurality of mounting elements. The primary spar is coupled to the drag spar via the at least one spar joiner. The method further includes placing the wing frame into a mold, wherein the mold defines a shape of the wing. The method also includes injecting the mold with an air-filled matrix material, such that the air-filled matrix material substantially encases the wing frame and fills the defined shape of the wing, and such that the plurality of transverse frame elements provide torsional rigidity to the wing.

Injection molded wing structure for aerial vehicles

Systems for wing structure and attachment to frame for Unmanned Autonomous Vehicle (UAV) are disclosed herein. In one embodiment, a UAV includes an H-frame having a wing spar secured to two or more boom carriers. The wing spar includes two or more mounting locations, where each of the two or more mounting locations of the wing spar secures a horizontal propulsion unit. The boom carriers include a plurality of mounting locations, each of the plurality of mounting locations of the boom carriers securing a vertical propulsion unit. The UAV also includes a pre-formed wing shell attached to the H-frame.

Wing structure and attachment to frame for unmanned aerial vehicles

A modular fuselage for an unmanned aerial vehicle (UAV) includes a battery module, an avionics module, and a mission payload module. The battery module houses a battery to power the UAV. The avionics module houses flight control circuitry of the UAV. The mission payload module houses equipment associated with a mission of the UAV. The battery module, the avionics module, and the mission payload module are detachable from each other and mechanically securable to each other to contiguously form at least a portion of the modular fuselage of the UAV.

Modular fuselage for unmanned aerial vehicle

Systems and methods for assembling Unmanned Autonomous Vehicle (UAV) are disclosed herein. In one embodiment, a method for assembling a UAV includes connecting a wing spar with boom carriers to form an H-frame. The wing spar provides mounting locations for securing horizontal propulsion units, and the boom carriers provide mounting locations for securing vertical propulsion units. The method also includes attaching a fuselage body to the wing spar; attaching a pre-formed wing shell to the H-frame; and attaching pre-formed individual boom shells to their corresponding boom carriers. The H-frame provides structural frame for mounting the wing shell and the boom shells.

Assembly systems and methods for unmanned aerial vehicles

An energy dispersion plug for use in an unmanned aerial vehicle (UAV) includes a blunt head section, a wedge section, and a rim section. The blunt head section has an outer side for receiving an impact force and an inner side opposite the outer side. The wedge section has a base end and a distal end opposite the base end. The wedge section extends at the base end from the inner side of the blunt head section towards the distal end and the distal end has a smaller cross-sectional area than the base end. The wedge section is shaped and sized to fit into an open end of a hollow structural member of the UAV and to transfer impact energy incident upon the blunt head section into the hollow structural member to shatter the hollow structural member into fragments.

Energy dispersion plug for UAV

Wing for an unmanned aerial vehicle

Unmanned aerial vehicle

Growing community of inventors

Mountain View, CA, United States of America

Adem Rudin