Abstract:
Systems, methods, and devices are provided that combine an advance vehicle configuration, such as an advanced aircraft configuration, with the infusion of electric propulsion, thereby enabling a four times increase in range and endurance while maintaining a full vertical takeoff and landing (“VTOL”) and hover capability for the vehicle. Embodiments may provide vehicles with both VTOL and cruise efficient capabilities without the use of ground infrastructure. An embodiment vehicle may comprise a wing configured to tilt through a range of motion, a first series of electric motors coupled to the wing and each configured to drive an associated wing propeller, a tail configured to tilt through the range of motion, a second series of electric motors coupled to the tail and each configured to drive an associated tail propeller, and an electric propulsion system connected to the first series of electric motors and the second series of electric motors.
Abstract:
This disclosure is directed to varying a speed of one or more motors in an unmanned aerial vehicle (UAV) to reduce unwanted sound (i.e., noise) of the UAV. A UAV may include motors coupled with propellers to provide lift and propulsion to the UAV in various stages of flight, such as while ascending, descending, hovering, or transiting. The motors and propellers may generate noise, which may include a number of noise components such as tonal noise (e.g., a whining noise such as a whistle of a kettle at full boil) and broadband noise (e.g., a complex mixture of sounds of different frequencies, such as the sound of ocean surf). By varying the controls to the motors, such as by varying the speed or revolutions per minute (RPM) of a motor during operation by providing random or pseudo-random RPM variations, the UAV may generate a noise signature with reduced tonal noise.
Abstract:
An unmanned aerial vehicle (i.e., drone) has a main body having top and bottom halves shaped to resemble beverage bottle caps, and hinged to one another in a clamshell arrangement to surround an interior compartment. The main body is mounted on a landing gear structure having at least two support legs. For propulsion, multiple rotors (e.g., 4 to 6) are each mounted on collapsible booms that are hingedly mounted to the frame structure of the landing gear assembly. The unmanned aerial vehicle is equipped with spotlights, LEDs that change color, laser lights, strobe lights, multiple speakers, a video display screen, a video camera, a video projector, a satellite/GPS antennae, a digital music storage and playing device, a voice recording and playback device connected to the multiple speakers, at least one battery power source and a computer control module (CPU) for wireless communication with a remote control device.
Abstract:
A bearing arrangement for an electric motor used for propelling an unmanned aerial system. The bearing arrangement includes three bearings having rolling bearing elements, one of which has a contact angle that is nominally zero and at least one other of which has a contact angle that is nominally non-zero.
Abstract:
The present invention provides methods and apparatus for unmanned aerial vehicles (UAVs) with improved reliability. According to one aspect of the invention, interference experienced by onboard sensors from onboard electrical components is reduced. According to another aspect of the invention, user-configuration or assembly of electrical components is minimized to reduce user errors.
Abstract:
A tethered flight control system for a small unmanned aircraft. The tethered flight control system can have a mobile base, a tether arm, a tether spout, and a remote-controlled winch that can hold a tether line, which can be connected to a small unmanned aircraft. By controlling the tether line using the winch, the small unmanned aircraft can be prevented from flying out of range or out of control. The winch can have a high-speed motor configured to remove substantially all slack from the tether line while the small unmanned aircraft is in flight. The winch can be controlled from a hard-wired winch remote, which can take the form of a foot pedal device having one or more foot pedals. The tether line can be attached to the small unmanned aircraft through a tether attachment apparatus, which can have a travel bar, two or more rotor protectors, and a mounting section.
Abstract:
A helicopter includes a mast, a main rotor, an engine, a radiator, and a body cover. The engine and the radiator are housed in the body cover. The body cover includes a first opening penetrated by the mast, a second opening that is located at a more forward position than the first opening and configured to introduce air to the radiator, and a third opening located at a position that is more forward than the first opening and more rearward than the radiator. The third opening is located at a higher position than the second opening and the radiator.
Abstract:
An unmanned aerial vehicle (“UAV”) is configured with a redundant power generation system on-board the UAV. A redundant power system on-board the UAV can selectively utilize an auxiliary power source during operation and/or flight of the UAV. The power system on-board the UAV may include a battery and at least one auxiliary power source comprising a combustion engine. The combustion engine on-board the UAV may be selectively operated to charge the battery when a charge level of the battery is below a full charge level, and/or to power one or more propeller motors of the UAV.
Abstract:
Described herein is a mobile apparatus for capturing images that includes a body, a propulsion device coupled to the body and actuatable to propel the body in response to a motion control command. The mobile apparatus also includes a low-resolution camera coupled to the body and configured to capture a plurality of low-resolution images. Further, the mobile apparatus includes a transceiver coupled to the body. The transceiver is configured to wirelessly receive the motion control command and wirelessly transmit the plurality of low-resolution images.
Abstract:
Vehicles such as unmanned air vehicles that are capable of movement from an open, flight configuration to an enclosed configuration in which all major flight components can be protected by an outer shell are disclosed. In the enclosed configuration, the vehicles can take on standard geometric shapes such as a rectangular prism, sphere, cylinder, or another shape, so as to not be recognizable as an unmanned air vehicle. Embodiments of vehicles can also include interchangeable and/or wireless motor arms, motor arms which are electrically connected to the remainder of the vehicle only when in an open configuration, remote controllers removably attached to the remainder of the vehicle, and clip or other attachment mechanisms for attachment to objects such as backpacks.