A convertible cargo handling assembly may comprise a mat, a fitting, and a removable cargo handling component. The fitting may include a fixed component and a coupling component. The fixed component may be located in an opening defined by the mat. The removable cargo handling component may be located over the mat and removably coupled to the fixed portion of the fitting via a coupling between the coupling component and the fixed component.

The modular autonomous air and road mobility (AARM) vehicle with Vertical Take-off and Landing (VTOL) capability provides combined air and road mobility solution.

AARM is clean energy powered, modular vehicle, which can be undocked and redocked into road module and air module, providing uninterrupted autonomous mobility between air and road. In addition, the modular design enables: Easy navigation through highly populated areas without the need to accommodate fixed wing aircraft on urban roads. Reduced energy consumption and noise levels in urban roads by not having to carry the air propulsion system into urban areas.

The road and air modules dock with each other through a sensor guided docking and load carrying mechanism (SGDMS), allowing connectivity, command and control. The vehicle can be scaled appropriately to serve: personal mobility, shared car, air taxis, regional air transport, cargo and shipping, defense missions, medical evacuations and air ambulances.

A rotor-wing assembly includes a motor, a propeller, and a connection assembly connecting the propeller to the motor. The motor includes a rotating portion. The connection assembly includes a locking member and a reinforcing member arranged between the propeller and the motor. The locking member locks the propeller to the rotating portion. A first end of the reinforcing member is mounted at the rotating portion. A second end of the reinforcing member opposite to the first end is engaged with the locking member, to reinforce the locking member to lock the propeller to the rotating portion.

A modular load carrying apparatus for a rotary wing aircraft and to a method of operating a modular load carrying apparatus. The modular load carrying apparatus may include a tube, first and second caps that are located inside the tube at first and second axial ends, and at least first and second removable platforms that are interchangeably installable on the tube. The second cap comprises a protrusion that protrudes from the axial end, and each one of the at least first and second removable platforms is adapted for being slidable over the first axial end of the tube and restrained by the second cap at the second axial end of the tube.

A VTOL (vertical take-off and landing) box-wing aerial vehicle with multirotor to provide VTOL flight includes a detachable cabin, centered fuselage, a pair of first wings extending outward from the upper portion of the fuselage and a pair of second wings extending outwardly and from the lower portion of the fuselage. The first and second wings are spaced apart longitudinally and vertically. The pylon joints the first wing and second wing at the tip to form the box-wing. The pylon includes heading control rudder. Secured to the wing or pylon or both wing and pylon, an overhead boom extending longitudinally to support a plurality of lift rotors or tiltable rotors for VTOL flight. Finally, the fuselage mounted push rotor or the overhead boom mounted tiltable rotors propel the vehicle forward to generate lift from the wings. Furthermore, the wings are equipped with elevators and ailerons for flight control.

Systems and methods are provided for using an additively manufactured vehicle, such as an UUV, with additively manufactured modules. The vehicle may be configurable such that additively manufactured modules or components may be detachably connected to the vehicle by hand, without the use of tools. Such modules may include connectors adapted to securely attach additional modules that may be detached by hand, without the use of tools. The additively manufactured modules may include ball bearings for rotating modules such as propellers and thrusters, and clips or tabs for detachable connection. The modules may include optical components for communications between a swarm of unmanned vehicles. Such optical modules for underwater vehicles may utilize nephelometry and/or turbidimetry to improve communications parameters based on scattered light measurements.

A vertical takeoff and landing aerial vehicle and a cooling system for the aerial vehicle. Heat dissipation in an arm of an aerial vehicle is achieved by installing a fan in a hollow interior of each of a left linear support and a right linear support of the aerial vehicle, thereby achieving the purposes of lowering temperature in the arm and protecting equipment in the arm.

A cargo module swapping system for an electronic short take-off and landing aerial vehicle, including an autonomously driven robotic vehicle for transporting and swapping cargo modules on an autonomous electric aircraft. The robotic vehicle has two or more robotic arms for controlled material handling and manipulation, each configured to install, remove, and replace cargo bins directly onto the aft end of a forward portion of a central fuselage of an electric short take-off and landing (ESTOL) aircraft. The cargo bins are configured to function as the aft portion of the aircraft central fuselage.

An automated modular vehicle configuration system and method that comprises a Configuration Management Unit in the vehicle that detects assemblies attached to the vehicle and configures the vehicle's autopilot based on the detected assemblies. Each attached assembly comprises mechanical and electrical components, ports and a memory device that contains identification information and data related to the assembly, such as assembly type, propulsion type, position, flight time, manufacturing date. Users can swap assemblies on the vehicle in order to provide different features to the vehicle. In particular this invention relates to drone vehicles that can be configured with different types of propulsion systems with different performance profiles and equipment such as gimbals, cameras, landing gear, measurement payloads and such. The invention also automatically downloads vehicle configuration parameters and autopilot firmware updates. Vehicle configuration and logs can be sent to the cloud for safekeeping and further analysis.

An adjustable fixed structure attachment system 200 for an aircraft wing, the attachment system 200 including a bracket 210 having: a wall 212 for connection to a wing box, a protrusion 214 protruding from the wall 212, and a slot 216 extending through the protrusion 214, wherein the slot 216 has a height and a width, and a bush 220 having a bore 222 extending therethrough for receipt of a pin, wherein the bush 222 is insertable into the slot 216 and dimensioned relative to the slot 216 so that the bush 220 is substantially immovable in a width-wise direction of the slot 216, and is moveable in a height-wise direction of the slot 216 to thereby vary a position of the bush 220 within the slot 216.