Intel Corporation

Intel Deutschland Gmbh

Fabian Oberndorfer

Klaus Doth

Martin Stobbe

Markus Luetzenburger

Stefan Klar

Daniel Gurdan

Jan Stumpf

Michael Achtelik

Wolfgang Rottner

Raffael Lustig

Jan Nicolaas Zelhorst

Disclosed is a drone rotor cage. The drone rotor cage may include a motor housing, a plurality of spars, and a plurality of ribs. The plurality of spars may extend from the motor housing. Each of the plurality of spars may have a spar height and a spar thickness. The spar height may be greater than the spar thickness. Each of the ribs may extend from a respective one of the plurality of spars. Each of the plurality of ribs may have a rib height and a rib thickness. The rib height may be greater than the rib thickness. The plurality of spars and the plurality of ribs may define a space sized to allow a rotor to spin freely when the rotor cage is attached to a drone.

Drone rotor cage

Methods and devices are presented for controlling or reducing amount of downwash generated by a drone. A drone including a plurality of arms including rotors may be configured to operate and fly with arms in an elevated position with respect to a horizontal plane. The elevated arms may allow a drone to fly with reduced vertical downwash.

Drones and methods for reducing downwash of drones

A ground station device for a plurality of unmanned aircraft, comprising an upper face, which comprises a plurality of receptacles for positioning a plurality of unmanned aircraft, a data interface for connecting the ground station device to a control unit, and a power supply device for charging the unmanned aircraft. The ground station device is designed to be stackable so as to form a stack with at least one other ground station device.

Ground station device for a plurality of unmanned aircraft

Multi-stage reduction of impact forces are disclosed. An example apparatus to reduce impact energy of an aircraft during landing includes a rotatable landing leg having a proximal end near an axis of rotation and a distal end opposite the proximal end, a first flexible portion of the proximal end, where the first flexible portion is to engage a first engaging portion at a first rotation angle of the rotatable landing leg, and a second flexible portion of the distal end, where the second flexible portion is to engage a second engaging portion at a second rotation angle of the rotatable landing leg.

Multi-stage reduction of impact forces

According to various aspects, an unmanned aerial vehicle may include one or more electric drive motors. Each drive motor of the one or more electric drive motors may include a first drive rotor structure; a second drive rotor structure, the first drive rotor structure being coaxially aligned with the second drive rotor structure, the first drive rotor structure including a first magnetic arrangement and the second drive rotor structure including a second magnetic arrangement.

Unmanned aerial vehicle and method for driving an unmanned aerial vehicle

Flexible printed circuit boards and related methods are disclosed herein. An example printed circuit board includes a controller interface coupled to a surface of the printed circuit board between a first end of the printed circuit board and a second end of the printed circuit board. The example printed circuit board includes a connector coupled to the surface proximate to the first end. The example printed circuit board includes a notch formed between the controller interface and the connector. The notch is to form a narrowed portion of the printed circuit board to enable the printed circuit board to bend at the narrowed portion.

Growing community of inventors

Krailling, Germany

Fabian Oberndorfer