Sierra Nevada Corporation

Sierra Nevada Company, LLC

Stephen Morris

Jean-Francois Clavreul

Curtis Leo

Emily Agostino

Mikhail Blinkov

Frederick Naaman

Hervé Hilaire

Sean Foxen

A modular VTOL drone aircraft can include a primary processor, a plurality of propellers, one or more line replacement modules ('LRMs') and one or more line replacement units (“LRUs”). LRMs can include a fuselage, a center wing, two booms, two outer wings, two vertical tails, a horizontal tail, and/or an engine. LRUs can include an avionics module, a radio communications assembly, a sensor package assembly, an ISR assembly, and/or a deployable payload assembly. Each LRM and LRU can be self-contained and removably attached to the remainder of the VTOL drone. Each LRM can be readily interchanged with another similar LRM, which can be of a different size. LRM interfaces can include a blind mate electric connector and/or a floating connector.

Modular fixed VTOL with line replaceable units

A dual use UAV or 'drone' can include a battery and primary processor located at a fuselage, as well as two separate modular units removably coupled to the fuselage and in communication with the primary processor. The two separate modular units can interact with each other to provide an enhanced operation while the drone is in flight. One modular unit can be an ISR unit having a video camera, and the other modular unit can be a cargo unit. The enhanced operation can involve the ISR unit using its video camera to identify a delivery location for a cargo pod of the cargo unit. Alternative modular units can include a secondary ISR unit, a cargo fuel pod unit, or a robotic arm assembly. Standardized interfaces coupled to the fuselage can enable the ready removal of one modular unit and installation of another one.

Dual ISR-payload capable UAV

Methods, systems and apparatus for the deployment and retrieval of child UAVs from a V-TOL UAV Mothership. The Mothership may be piloted from a base station to one or more destination locations. At the destination location, one or more child UAVs may be deployed from a cargo bay module. The child UAVs perform tasks or complete a mission before coordinating their retrieval with the V-TOL UAV Mothership. The Mothership may plan an intercept course to retrieve the child UAVs in mid-flight or coordinate a hovering type retrieval with the child UAVs. The child UAVs are retrieved through an actuated frontal opening which provides access to the cargo bay without having to navigate through turbulence created beneath the hovering Mothership by the vertical thrust rotors.

In-flight UAV deployment and retrieval platform

An unmanned aerial vehicle includes a fuselage having a first side and a second side, a first arm disposed on a first side of the fuselage, wherein the first arm is coupled to one or more first propellers, wherein the first arm is adapted to move between a first folded position in which the first arm is in a folded state inside the fuselage and a first extended position in which a first section of the first arm and the one or more first propellers are outside the fuselage, and a second arm disposed on the second side of the fuselage, wherein the second arm is coupled to one or more second propellers, wherein the second arm is adapted to move between a second folded position in which the second arm is in a folded state inside the fuselage and a second extended position in which a second section of the second arm and the one or more second propellers are outside the fuselage.

Compact foldable multicopter unmanned aerial vehicle for cargo delivery

Unmanned aircraft

A VTOL drone aircraft can include a rechargeable battery, a primary processor, lift propellers, an internal combustion engine with a thrust propeller, a generator, and a power regulation controller. The generator can receive power from the internal combustion engine and deliver electrical power to the rechargeable battery, the lift propellers, or both. The power regulation controller can regulate dynamically power delivery from the internal combustion engine to the thrust propeller and the generator, and from the generator to the rechargeable battery based upon changing conditions during flight. The power regulation controller can prevent operation of the generator when peak power is needed from the internal combustion engine for the thrust propeller. The power regulation controller can also control a clutch coupled to the thrust propeller to regulate the delivery of power to the thrust propeller when the internal combustion engine is active.

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Sunnyvale, CA, United States of America

Stephen Morris