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Patent Searching and Data


Matches 151 - 200 out of 62,272

Document Document Title
WO/2018/228419A1
Disclosed are a height measurement device and a boarding bridge having same. The height measurement device has a height measurement sleeve and a distance measurement mechanism; the height measurement sleeve is vertically provided in an a...  
WO/2018/231321A2
An expendable rotary wing unmanned aircraft capable of storage in a cylindrical housing includes a longitudinally extending body having an upper end and a lower end; and a pair of counter-rotating coaxial rotors each located at respectiv...  
WO/2018/229969A1
An aircraft structure manufacturing device, provided with: a jig fur supporting a component of an aircraft structure; a plurality of raising/lowering stands; and a control unit (900) for controlling the position of a support part of the ...  
WO/2018/232196A1
The present disclosure relates to aircraft and aircraft flight control systems, methods, and apparatuses. A condition-aware aircraft configured to make in-flight decisions autonomously, based on the most up-to-date information, to perfor...  
WO/2018/229506A1
An electrically powered propellor apparatus comprising an axial flux electric machine. The axial flux electric machine comprises a rotor, at least one stator and a shaft. The shaft mounts the rotor and the shaft is mounted in at least tw...  
WO/2018/229753A1
A payload elevator system and method are disclosed, configured for providing a plurality of alternative payload elevator configurations, each payload elevator configuration being configured for transporting a payload module. A composite ...  
WO/2018/231800A1
Propulsion systems that generate thrust from pressure generated by thermally decomposing a chemical blowing agent (CBA). In some embodiments, the CBA decomposes exothermically such that once thermal decomposition has been initiated, the ...  
WO/2018/227309A1
The invention relates to a process for manufacturing a composite panel (PC, PC'), said process comprising the following steps: a) providing at least one first ply (NP1, NP1') of a woven or nonwoven dry material, said first ply defining a...  
WO/2018/229391A1
The invention relates to a remote platform for controlling and tracking inspections of surfaces of predetermined objects by inspection robots (31a, 31b), comprising a reference database (11) of said predetermined objects; a module (14) f...  
WO/2018/231310A2
A spacecraft propulsion method uses cosmic ray triggered nuclear micro-fusion events to provide repeated or continuous thrust for artificial gravity during a space flight. In one embodiment, successive packages of deuterium-containing mi...  
WO/2018/231511A1
Some novel features pertain to a quad-rotor or other unmanned aerial drone having a planar vapor chamber mounted to a processor of the drone to cool the processor. The processor may be enclosed in a protective central housing. The vapor ...  
WO/2018/227270A1
A system for providing both driving and charging functionality by using a plurality of traction inverters and a plurality of energy storage devices coupled to one another across the electric motor; an AC/DC converter front-end circuit in...  
WO/2018/231714A1
A high throughput fractionated satellite (HTFS) system and method where the functional capabilities of a conventional monolithic spacecraft are distributed across many small or very small satellites and a central command and relay satell...  
WO/2018/229349A1
The present invention relates to a sleeve (1) connecting a blade (2) to the hub of a rotor (10) of a rotary-wing aircraft (5). The sleeve (1) comprises a leading edge, a trailing edge, and a protuberance arranged on said trailing edge. T...  
WO/2018/223748A1
Disclosed is a duct fan, comprising: a duct (1) having a central axis, an air inlet and an air outlet being respectively located at an upper end and a lower end of the duct (1); a propeller hub shaft arranged on the central axis of the d...  
WO/2018/226549A1
A radome assembly (20) includes a frame (30) conforming in contour with an aircraft fuselage (14) for being fixedly mounted thereto. A radome (32) having an aerodynamically streamlined elongate contour including a central bulb (34) is sp...  
WO/2018/226268A1
A flight vehicle has an engine that includes air inlet, an isolator (or diffuser) downstream of the air inlet, and a combustor downstream of the isolator. The isolator includes a bulged region that has at least one dimension, perpendicul...  
WO/2018/226287A1
A method, operable in the presence of ambient cosmic rays, is provided for braking a craft upon approach to a planet, moon or other space body, e.g. in preparation for landing. Deuterium-containing particle fuel material is projected in ...  
WO/2018/223680A1
Disclosed is a pedal applied to a vehicle and comprising: fixing members (2) configured to be mounted on the vehicle; and a pedal body (1) fixedly connected to the fixing members (2), wherein the pedal body (1) comprises a pedal portion ...  
WO/2018/226172A2
Balancing the drone is difficult with engines (5), when drones are equipped with engine (5) to increase the flight time. However, balancing the drone can be made easy by providing the drone with electric motor (10) or electric motor that...  
WO/2018/225010A1
Liquid fuel tank comprising a plurality of liquid level detection capacitive sensors, each arranged along an edge of the fuel tank such that the capacitance of said sensors varies with the volume of fuel present in the fuel tank, wherein...  
WO/2018/223597A1
An integrated system for storing an unmanned aerial vehicle, the system comprising a vertical column (2) and an accommodating chamber (11). The vertical column (2) is configured to support and secure the accommodating chamber (11), and i...  
WO/2018/226269A1
A flight vehicle has a propulsion system that includes an air inlet, an isolator (or diffuser) downstream of the air inlet, and a combustor downstream of the isolator. The isolator includes an obstruction that protrudes inwardly from an ...  
WO/2018/225112A1
[Problem] To provide an aerial vehicle wherein the flight efficiency can be improved. [Solution] An aerial vehicle according to the present invention relates in particular to a aerial vehicle having a loading section whereon a payload an...  
WO/2018/225757A1
This unmanned aerial vehicle is provided with a main body unit, a propulsion unit which has a rotor blade and a motor for rotating the rotor blade about a rotation shaft and which is attached to the main body unit, a rechargeable battery...  
WO/2018/223742A1
A cradle head comprises: at least two sequentially connected driving components; and a supporting housing (14) for installation of a photographing device. One of the at least two driving components is installed inside the supporting hous...  
WO/2018/226200A1
An aircraft seat cushion, combining comfort, durability as well as passenger protection and maneuverability under extreme conditions is provided in accordance with the present invention. The main constituent elements of the subject seat ...  
WO/2018/224565A2
The present invention discloses a method and flight controller for controlling an aircraft, comprising the following step: - determining the pitch control input δE for at least one pitch moment generator element, based on the lift contr...  
WO/2018/224809A1
A cover for an intake of an air-breathing engine in a missile is disclosed. The cover comprises a closure for closing the inlet so as to prevent ingress of debris; and a fastening attachable to an aircraft-mounted launcher and configured...  
WO/2018/225706A1
A sound-absorbing panel to be used affixed to a jet engine of an aircraft, provided with: a resin core layer 20 having a first surface, a second surface disposed on the side opposite from the first surface, and multiple partitions extend...  
WO/2018/224808A1
A method of producing an aircraft battery system, the method comprising: identifying a volume of free space on an aircraft (100); arranging a plurality of electrical power cells (112, 114) such that the plurality of cells (112, 114) are ...  
WO/2018/225688A1
Provided is a multilayer heat-insulating material which reduces a deterioration in heat-insulating performance at the periphery of a mounting means for mounting on a mounting subject and which facilitates deformation into a desired shape...  
WO/2018/223378A1
An unmanned aerial vehicle control method and device, and an unmanned aerial vehicle. The method comprises: acquiring state information about an unmanned aerial vehicle (S101); determining a control instruction according to the state inf...  
WO/2018/224657A1
The present invention relates to a method and a device for lifting a load (20), wherein at least one drone (9) carries at least some of the load. According to the invention, multiple drones (9, 9b) are connected to each other or at least...  
WO/2018/224058A1
The invention concerns a system of wheel suspension for motor vehicles and/or airplanes with a suspension mechanism for attaching a wheel and attached to a frame, where suspension mechanism (1) arranged in plane (3) of the suspension of ...  
WO/2018/224440A1
Ice protection systems of aircraft and related methods are disclosed. In one embodiment, the system comprises a gas-discharge lamp configured to emit infrared radiation toward an inner surface of an aircraft skin and an electric power so...  
WO/2018/224919A1
A method for repairing the surface of rotor blades or aircraft wings, comprising (c) a composite substrate (1); and (d) a protection layer (2) having at least one area of at least partial damage, the method comprising: (vii) removing at ...  
WO/2018/224947A1
A composite crushable member (10) comprising a reinforcing composite (12) is disclosed herein. The composite crushable member comprises a reinforcing region (16) and a trigger region (18a-18e) and at least one of a first physical propert...  
WO/2018/224998A1
An attitude control and thrust boosting system (100) for a space launcher is disclosed, wherein the space launcher is equipped with a rocket engine (303) provided with an exhaust nozzle. The exhaust nozzle comprises a divergent portion (...  
WO/2018/224803A1
A phased array antenna and apparatus incorporating the same An electromagnetic phased array (100) is disclosed comprising a plurality of antenna elements (102), each antenna element (102) comprising at least three constituent antennae (1...  
WO/2018/224691A1
The current invention concerns an improved system for cargo delivery through (unmanned) aerial vehicles (preferably UAVs or drones) to specifically designed home stations. Additionally, a method is described according to which the system...  
WO/2018/224327A1
A control system for a moveable control surface on a wing or stabilizer of an aircraft, for example a flying car, comprising: a wing or stabilizer having a moveable control surface; a mounting structure for mounting the wing or stabilize...  
WO/2018/224033A1
An aircraft with imitation beetle elytron wings, belonging to the technical field of aviation. Imitation beetle elytron wings (2) are used as horizontal wings of an aircraft. The left and right imitation beetle elytron wings (2) are conn...  
WO/2018/225769A1
This unmanned aerial vehicle is provided with a main body unit, a propulsion unit which has a rotor blade and a motor for rotating the rotor blade about a rotation shaft and which is attached to the main body unit, a rechargeable battery...  
WO/2018/224567A1
The invention relates to a control method for controlling a yaw angle γ z and a roll angle γ x of an aircraft (1) that takes off vertically, said aircraft having at least two drive groups (3) arranged in opposite side regions of the ai...  
WO/2018/223089A2
Systems and methods are contemplated for favorably improving flight dynamics of aircraft, including enhanced aerodynamic braking and improved flight maneuverability. Air braking systems selectively position a first set of blades at a neg...  
WO/2018/220336A1
The invention relates to an actuator for an aircraft, comprising a connecting device comprising a rod (2) provided with a free end (3) for coupling the actuator (1) to a device (4) to be actuated. Furthermore, the free end (3) of the rod...  
WO/2018/218370A1
Disclosed is an aircraft and a method of controlling an aircraft. The aircraft comprises a continuous wing assembly extending from port to starboard sides of the aircraft. The aircraft is controlled partially by flexing portions of the w...  
WO/2018/219831A1
The invention relates to a luggage conveyor device (1, 2, 3) for efficiently supplying a plurality of inspection objects to be inspected or individual items in general to an inspection device (4). According to the invention, the conveyor...  
WO/2018/219662A1
The invention relates to a mobile transport container (30) for a vehicle, in particular for an unmanned aerial vehicle, comprising at least one flexible hollow body for load securing transport goods (33), wherein the flexible hollow body...  

Matches 151 - 200 out of 62,272