Adaptive anti-laser system

AIRCRAFT THERMAL MANAGEMENT SYSTEM FOR AN ENERGY STORAGE SYSTEM

ROTATIONAL IONIC ENGINE WITH TOROIDAL COUNTER ELECTRODE

Hybrid turbofan engine for an aircraft, comprising a motor/generator cooled by heat pipes

Methods and system for estimating percentage torque produced by a propulsor configured for use in an electric aircraft

AIRCRAFT PROPULSION SYSTEM WITH VOLTAGE REGULATOR

Hybrid electric hydrogen fuel cell engine

Aircrafts, systems, and methods for providing constant torque on takeoff

MOTOR ASSEMBLY

System and method for the autonomous transition of an electric vertical takeoff and landing aircraft

ELECTRIC AIRCRAFT BATTERY PACK AND METHODS OF USE

Multi-drive unit propulsion system for an aircraft

Parallel hybrid propulsion system

Modular battery configuration with centralized bus on an electric aircraft

Vehicle cabin thermal management system and method

DEVICE FOR PROPULSION IN A VEHICLE

System and method to minimize an aircraft ground turn radius

Electrical energy system for barring rotor

ELECTRIC MACHINE WITH COMBINED ROTOR AND COOLING FAN

ELECTRIC MACHINE WITH AIR COOLED ROTOR

Electric machine having rotor hub with shaped passages for cooling

ENGINE CHARACTERISTICS MATCHING

Gas turbine engine noise reduction

Airship equipped with an electric distributed propulsion system

AIRCRAFT EQUIPPED WITH A DISTRIBUTED PROPULSION SYSTEM HAVING SUCTION AND PRESSURE FANS

SYSTEM AND METHOD FOR LIFT AUGMENTATION OF AIRCRAFT WINGS

System and method for dynamic excitation of an energy storage element configured for use in an electric aircraft

System and method for controlling flight path of a blown lift aircraft

FLYING VEHICLE SYSTEMS AND METHODS

FLYING VEHICLE SYSTEMS AND METHODS

IMPROVED AIRCRAFT PROPULSION ASSEMBLY

Hybrid-electric powertrains for aircraft

COOLING SYSTEM FOR AN AIRCRAFT, AIRCRAFT HAVING A COOLING SYSTEM, AND METHOD FOR COOLING AN ELECTRIC PROPULSION SYSTEM OF AN AIRCRAFT

Vertical take off and landing closed wing aircraft

WASTE HEAT UTILIZING ABSORPTION REFRIGERATION SYSTEM FOR CLIMATE CONTROL AND/OR ELECTRIC SYSTEMS COOLING

Battery Assembly for Aerospace Vehicles

SYSTEM FOR DETERMINATION OF FLIGHT PERFORMANCE OF BIOINSPIRED AERIAL VEHICLE IN SIMULATED SPACE CONDITIONS

After-fan system with electrical motor for gas turbine engines

ACTIVE SOUND ATTENUATION FOR AIRCRAFT ELECTRICAL SYSTEM

CONTROLLING HYBRID-ELECTRIC OR ALL-ELECTRIC POWERTRAINS AND PROPULSION SYSTEMS

MULTI-DRIVE UNIT POWERPLANT FOR AN AIRCRAFT

TEMPERATURE CONTROL SYSTEM AND TEMPERATURE CONTROL METHOD AND AIRCRAFT

MOTOR UNIT AND FLYING OBJECT

METHODS AND SYSTEMS FOR VENTING A FUEL TANK ON A BLENDED WING BODY AIRCRAFT

HYBRID-ELECTRIC PROPULSION SYSTEM EQUIPPED WITH A COUPLER FOR SWITCHING BETWEEN MODES OF OPERATION

AIRCRAFT EQUIPPED WITH FUEL CELL SYSTEM AND THRUST CONTROL METHOD

Propeller propulsion unit for an aircraft

Aircraft comprising at least two turboshaft engines and device configured to be connected to one of the turboshaft engines and method for controlling such an aircraft

AIRCRAFT EQUIPPED WITH FUEL CELL SYSTEM

Electric power system architecture and fault tolerant VTOL aircraft using same

ELECTRIC TILTROTOR AIRCRAFT WITH TILTING COAXIAL MOTORS AND GEARBOX

VERTICAL TAKE-OFF AND LANDING AERODYNE OPTIMISED FOR HORIZONTAL FLIGHT

AIRCRAFT MONITORING SYSTEM AND METHOD FOR ELECTRIC OR HYBRID AIRCRAFTS

APPARATUS FOR COOLING AN ELECTRIC PROPULSION ENGINE

AIRCRAFT FLUID RELEASE SYSTEM

SHAFTLESS ELECTRIC FLUID-FLOW DEVICE

AIRCRAFT PROPULSION SYSTEM

AIRCRAFT

Aircraft propulsion utilizing a safety critical energy management system

ELECTRIC PROPULSION ASSEMBLY COMPRISING AT LEAST ONE ELECTRIC MOTOR POSITIONED IN FRONT OF A TRANSMISSION SYSTEM, AIRCRAFT COMPRISING AT LEAST ONE SUCH PROPULSION ASSEMBLY

Aircraft fluid ice protection system

Co-operating electrical isolation and thermal interface layers in a high voltage power converter

ELECTRIC PROPULSION SYSTEM HAVING INTEGRATED ELECTRICAL AND THERMAL ARCHITECTURE AND RELATED METHODS OF OPERATING AND IMPLEMENTING SAME

Hybrid electric hydrogen engine for aircraft

Emergency power unit for electric aircraft

Hydrogen electric hybrid power plant for hovercar and control method

HYBRID-ELECTRIC AIRCRAFT PROPULSION SYSTEM AND METHOD

VTOL M-wing configuration

AIRCRAFT WITH ENGINE-DRIVEN PERMANENT MAGNET GENERATOR

BATTERY MONITORING METHOD, BATTERY AND UNMANNED AERIAL VEHICLE

Parallel control loops for hybrid electric aircraft

ELECTROMAGNETIC GYROSCOPIC STABILIZING PROPULSION SYSTEM METHOD AND APPARATUS

Electrical power system

Apparatus and method for optimizing motor performance in an electric aircraft

Electrically powered vehicles with redundant power distribution circuits

ASSEMBLY AND METHOD FOR GAUGING FUEL OF ELECTRIC AIRCRAFT

Systems and methods for package delivery with unmanned aerial vehicles

SYSTEM AND METHOD FOR DEFINING BOUNDARIES OF A SIMULATION OF AN ELECTRIC AIRCRAFT

OIL CIRCULATION SYSTEM FOR HYBRID ELECTRIC ENGINE

HYBRID-ELECTRIC SINGLE ENGINE DESCENT FAILURE MANAGEMENT

CHARGING SYSTEM AND METHOD FOR AIRBORNE CHARGING OF ELECTRICAL AIRCRAFT

Transition gauge for electric aircraft

PREFLIGHT TEMPERATURE MANAGEMENT OF AN ELECTRIC AIRCRAFT ENERGY SOURCE

ELECTRIC PROPULSION UNIT COMPRISING AT LEAST TWO INDEPENDENT SUPPORTS, AIRCRAFT COMPRISING AT LEAST ONE SUCH ELECTRIC PROPULSION UNIT

Aircraft propulsion system with intermittent combustion engine and electric transmission system and method for operating the same

Method for converting an airplane with a combustion engine to an electrical reaction propulsion airplane

Electrically powered engine

AIRCRAFT POWERPLANT WITH BOOSTED GAS TURBINE ENGINE

Hybrid power systems for different modes of flight

POWER DISTRIBUTION CIRCUITS FOR ELECTRICALLY POWERED AIRCRAFT

Thrust allocation using optimization in a distributed flight control system

Adjusting aircraft powerplant power split to control powerplant vibrations

Propulsor assembly powered by a dual motor system

Aircraft propulsion system with intermittent combustion engine and electric transmission system and method for operating the same

Hybrid aircraft and landing launch/recovery system

VERTICAL TAKEOFF AND LANDING (VTOL) AIRCRAFT SYSTEMS AND METHODS

Vertical takeoff and landing (VTOL) aircraft systems and methods

Systems and methods for predicting degradation of a battery for use in an electric vehicle

Plasma engine using ion extraction

ELECTRICAL MACHINE WITH AN AXIAL AIR GAP FOR AN AIRCRAFT

Fuel Cell and Method of Forming a Fuel Cell

METHOD FOR DETERMINING AT LEAST ONE POWER LIMIT OF A HYBRID DRIVE TRAIN FOR A TRANSPORT VEHICLE, IN PARTICULAR AN AIRCRAFT

ELECTRICAL SUPPLY SYSTEM OF AN ELECTRICAL PROPULSION SYSTEM OF AN AIRCRAFT

RANGE EXTENDING ENERGY POD (REEP) FOR AN AIRCRAFT

Aircraft having a hybrid power source with power generation sources controlled according to drive unit power requirements

DRIVE UNIT FOR A ROTARY-WING AIRCRAFT, AND ROTARY-WING AIRCRAFT

High efficiency hydrogen fueled high altitude thermodynamic fuel cell system and aircraft using same

ELECTRIC MACHINE

FLEXIBLE ARCHITECTURE FOR AN AEROSPACE HYBRID SYSTEM AND OPTIMIZED COMPONENTS THEREOF

Vertiport with handling robots and a turntable

Aircraft motor driver

Dual-chemistry propulsion system for electric vertical take-off and landing aircraft

Aircraft

Electric ducted fan propulsor

Electrical fault isolation in a power distribution network of an aircraft

METHOD OF DESIGN AND MANUFACTURE OF A POWER ELECTRONICS CONVERTER FOR AN ELECTRICAL POWER SYSTEM, POWER ELECTRONICS CONVERTER FOR AN AIRCRAFT, AND AN AIRCRAFT

POWER ELECTRONICS CONVERTER WITH STACKED CARRIER SUBSTRATES

Thermal interface materials

VENTING ASSEMBLY FOR BATTERY EJECTA ON A SIDE DIFFERENT FROM AN EGRESS

Power electronics heat removal

Apparatus and a method for determining a resource remaining datum of an electric aircraft

Aircraft accessory drive system

AIRCRAFT PROPULSION SYSTEM WITH VARIABLE SPEED ROTATING STRUCTURE

Integrated thermal management apparatus

SYSTEMS AND METHODS FOR PROPULSOR SYNCHRONIZATION

Systems and methods for power distribution in electric aircraft

MOTOR UNIT AND AIRCRAFT

Vertical take-off and landing aircraft with deployable rotors

Distributed propulsion system for vertical take off and landing closed wing aircraft

Ground effect flight vehicle

Systems and methods for an electric vertical takeoff and landing aircraft braking system

Wireless charging of an electric aircraft

Hybrid electric secondary power and battery charging architecture and control system

System and method for automated flight plan reporting in an electric aircraft

VAPOR COMPRESSION SYSTEM FOR AEROSPACE APPLICATIONS

Power electronics converter

Slotless electric motor having improved transient capability

MECHANICAL DISCONNECTS FOR PARALLEL POWER LANES IN HYBRID ELECTRIC PROPULSION SYSTEMS

Power module and clutch mechanism for unmanned aircraft systems

THERMAL MANAGEMENT SYSTEM FOR AN AIRCRAFT INCLUDING AN ELECTRIC PROPULSION ENGINE

ROTOR WING AIRCRAFT WITH PROPULSION APPARATUS ON ROTATING POLE

High-altitude wind turbine aircraft system and method of use

Aircraft electric motor

System for establishing a primary function display in an electrical vertical takeoff and landing aircraft

STOWABLE ELECTRIC-HYBRID PROPFAN

ACTIVE COMPRESSOR STALL RECOVERY

SYSTEMS AND METHODS FOR MULTI-MODULE CONTROL OF A HYDROGEN POWERED HYBRID ELECTRIC POWERTRAIN

Systems and methods for aircraft wing plug

Hybrid propulsion drive train system for tiltrotor aircraft

Propulsor assembly powered by a dual motor system

Electric power system for a vehicle

Special electric propulsion system to power paragliders and other small, light aircraft

Electric aircraft

TEXTILE AIRFOIL STRUCTURE FOR A WING SYSTEM, AND TRANSPORT DEVICE

HYBRID HEAVY LIFT DRONE

Systems and methods for overvoltage protection on loads for use in an electric aircraft

Computing device and method for determining a revised flight plan as a function of battery temperature

Systems and methods for displaying a pilot display for an aircraft

Propulsion unit with foldable propeller blades and method for stopping the propeller in an indexed angular position

Systems and methods for propulsion

Hybrid propulsion systems for an electric aircraft

AIRCRAFT HAVING A DRIVE-AND-ENERGY SYSTEM FOR LOW-EMISSION CRUISING FLIGHT

Magnetic locking system of an electric aircraft rotor and methods thereof

Electrically propelled aircraft with partially rated converter

Aircraft with removable pod and wing for transporting cargo on pallets

Electric tiltrotor aircraft

Hybrid electric vertical takeoff and landing aircraft

System and method for speed control as a function of battery capability in an electric aircraft

Electrical energy storage system for an aircraft

POWER COMPONENT FOR ELECTRIC OR HYBRID AIRCRAFT

ELECTRIC POWER SYSTEM OF MOVING OBJECT

Active blade-pitch change systems and methods

VERTICAL-TAKE-OFF AERIAL VEHICLE WITH AEROFOIL-SHAPED INTEGRATED FUSELAGE AND WINGS

ELECTRIC MOVABLE BODY

Aircraft electric motor

Modular battery systems for aircraft

ELECTRICALLY DRIVEN DUCTED FAN ENGINE

CHARGE STATUS CONTROL SYSTEM, CHARGE STATUS CONTROL METHOD, AND AIRCRAFT

Hydrogen steam and inter-cooled turbine engine

Flying body

COMPACT AERIAL MISSION MODULAR MATERIAL HANDLING SYSTEM

Triplex Fully Redundant Fly-by-Wire Architecture

Aircraft

HIGH VOLTAGE CONVERTER FOR USE AS ELECTRIC POWER SUPPLY

Methods and systems for electric propulsor fault detection

POWER SUPPLY APPARATUS AND POWER SUPPLY MANAGEMENT SYSTEM

Auxiliary fan based hybrid cooling systems for electric machines

Rotorcraft autorotation control through electrical braking

CONTROL DEVICE FOR AIRCRAFT

CONTROL APPARATUS FOR AIRCRAFT

AERIAL VEHICLE AND CONTROL METHOD THEREOF, USING HYBRID DISTRIBUTED PROPULSION SYSTEM

AIRCRAFT POWERPLANT(S) FOR AN AIRCRAFT WITH ELECTRIC MACHINE CONTROLLED PROPULSOR SPEED

SYSTEM FOR A VERTICAL TAKEOFF AND LANDING AIRCRAFT WITH AN IN-BOOM LIFT PROPULSOR

METHOD AND SYSTEM FOR REDUCING NOISE OF HYBRID POWER PLANT

Rotor for an electric aircraft motor comprising a plurality of magnets

Aerial moving body and wireless power transmission system

Systems and methods for locking a battery for an electric aircraft

SYSTEM AND METHODS FOR VENTING OF A POWER SOURCE OF AN ELECTRIC VEHICLE

FLIGHT VEHICLE

ESTIMATING SYSTEM AND ESTIMATION METHOD AND AIRCRAFT

ELECTRIC VERTICAL TAKEOFF AND LANDING (EVTOL) AIRCRAFT LIFT MOTOR WITH AIR COOLING

METHOD OF REDUCING NOISE OF AIRCRAFT HAVING HYBRID POWER PLANTS

Power supply system, flying object, and method for controlling power supply system

POWER GENERATION CONTROL SYSTEM, POWER GENERATION CONTROL METHOD, AND AIRCRAFT

CHARGE CONTROL SYSTEM AND CHARGE CONTROL METHOD AND AIRCRAFT

AIRCRAFT AND METHOD OF OPERATING AN AIRCRAFT POWER SYSTEM MODULE

Battery charge difference calculation system

Propulsion system for an aircraft and method for protecting the propulsion system

Battery charge difference calculation system

UAV configurations and battery augmentation for UAV internal combustion engines, and associated systems and methods

Electric vertical take off and landing vehicle

System and method to minimize an aircraft ground turn radius

Apparatus for a ground-based battery management for an electric aircraft

Systems and methods for fault detection and control in an electric aircraft

Compact electric propulsion unit comprising a statically determinate engine mount, and aircraft comprising at least one such electric propulsion unit

Modular fuel cell assembly

Systems and method of operating a fuel cell assembly, a gas turbine engine, or both

ELECTRIC AIRCRAFT PROPULSION ASSEMBLY AND METHOD

Flying object control device, flying object control method, and non-transitory computer-readable storage medium storing program

Method and Apparatus for Controlling Electrical Machines Operating with a Turbine Engine

ELECTRIC AIRCRAFT PROPULSION ASSEMBLY AND METHOD

Aircraft propulsion unit

IINTEGRATED MULTIMODE THERMAL ENERGY TRANSFER SYSTEM, METHOD, AND APPARATUS FOR ELECTRIC MULTIROTOR AIRCRAFT

ANTI-STALL SYSTEM WITH A FUEL CELL

METHOD OF UTILIZING AN ELECTRIC AIRCRAFT BATTERY BAY FOR PAYLOAD STORAGE

Systems and methods for point to-point wireless power transmission for beam riding, power and data distribution sharing, wirelessly powered mobile systems

Aircraft Component Longevity

Fuel cells configured to deliver bi-polar high voltage DC power

Power supply system of aircraft

INTEGRATED ELECTRIC PROPULSION ASSEMBLY

Method and system for propulsion in an electric aircraft

Aerial vehicle

POWER SUPPLY CIRCUIT OF AIRCRAFT

ELECTRODE ASSEMBLY WITH HEAT SPREADING LAYER, BATTERY CELL AND BATTERY EMPLOYING SUCH ELECTRODE ASSEMBLIES

Electrical systems

MULTIPURPOSE AND LONG ENDURANCE HYBRID UNMANNED AERIAL VEHICLE

Method of transporting a battery for an unmanned aerial vehicle

ELECTRIC FLYING VEHICLE WITH MULTIPLE INDEPENDENT PROPULSION MODULES

Charging System for Aircraft and Drones

Detachable power supply for UAV

ATTITUDE CONTROL DEVICE

Fault tolerant turbo-generator system

Adaptive battery charging system and method

HYBRID TURBOMACHINE FOR AIRCRAFT WITH AN ACTIVE ACOUSTIC CONTROL SYSTEM

BLENDED WING BODY TANKER AND METHOD OF USE

Powertrain system of an aircraft including cyrogenic cooling loop for superconducting electronics and method of operating the same

Power supply circuit of moving object

Hybrid-Electric Aircraft Propulsion System and Method for Operating the Same

COORDINATED FAULT RESPONSE IN RECTIFIERS OF HYBRID AIRCRAFT

HYBRID VTOL AERIAL VEHICLE

Vertical take-off and landing (VTOL) aircraft

AIRCRAFT

Methods and systems for optimizing battery recharge management for use with an electric vertical take-off and landing aircraft

Hybrid aircraft having rectifier with integrated protection

MOTOR AND AIRCRAFT

Power supply circuit of moving object

Power-data nodes for an aircraft system

POWER SOURCE ASSEMBLY FOR AN ELECTRIC VERTICAL TAKE-OFF AND LANDING (EVTOL) AIRCRAFT

Electric aircraft battery pack and methods of use

CONTROL METHOD OF AERO WIND POWER GENERATION DEVICE

Control device for flight vehicle

Unmanned aerial vehicle for low-pressure hydrogen transport

Electric power supply system for vehicle

Propulsion channel for aircraft

ELECTRIC MOTOR COOLING SYSTEMS AND METHODS

Flying vehicle systems and methods

Boundary layer ducted fan propulsion system

Electric motor nacelle for a vertical take-off and landing aircraft and aircraft comprising such a nacelle

High traffic-rate aerial transportation system with low-footprint vertiport

Drones and drone systems

SYSTEM AND METHOD FOR REPLACING A BATTERY IN A VEHICLE

Electrically driven distributed propulsion system

Cooling of a fuel cell assembly

METHOD FOR CONTROLLING DRONE HAVING MULTI-DEGREE-OF-FREEDOM FLIGHT MODE

System and method for lift augmentation of an aircraft tailplane

AIRCRAFT CONTROL SYSTEM, AIRCRAFT CONTROL METHOD, AND STORAGE MEDIUM

SYSTEMS AND METHOD OF OPERATING A FUEL CELL ASSEMBLY

HYBRID POWER SYSTEM

Systems and method of operating a fuel cell assembly

Short takeoff and landing vehicle with forward swept wings

FLEXIBLE BATTERY SYSTEM FOR A VEHICLE

BATTERY PACK FOR AN ELECTRIC VEHICLE

ELECTRIC MACHINES FOR AIRCRAFT ENGINE FAULT DETECTION

Systems and methods for estimating flight range of an electric aircraft

Aircraft fuel tanks including self-sealing fabric

Aero wind power generation apparatus

Drone airstation method and system

Short take off and landing aircraft

AIRCRAFT HAVING REVERSE THRUST CAPABILITIES

System for establishing a primary function display in an electrical vertical takeoff and landing aircraft

POWER SOURCE FOR AN AIRCRAFT

Methods and apparatuses for generating an electric aircraft flight plan

FIREWALL ASSEMBLIES FOR HYBRID ELECTRIC AIRCRAFT POWERPLANTS

Ground-based aircraft movement

High voltage distribution systems and methods

Apparatuses and methods for preconditioning a power source of an electric aircraft

System and method for the prioritization of flight controls in an electric aircraft

ARCHITECTURE FOR AN ELECTRIC POWER GENERATOR FOR AVIATION

VERSATILE CONTROL OF A PROPULSION SYSTEM WITH A FUEL CELL

Aircraft thrust management with a fuel cell