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Patent Searching and Data


Matches 101 - 150 out of 72,018

Document Document Title
WO/2021/061983A1
A control system for an onboard oxygen generating system (OBOGS) includes a gain control communicatively coupled to an oxygen sensor configured to measure an oxygen concentration outputted from the OBOGS. The gain control selectively swi...  
WO/2021/056456A1
A spraying assembly (100), comprising a spray head assembly (110), a pressure switch (120), a water pump device (130) and a main pipe (141), the main pipe (141) being obliquely provided relative to the horizontal plane, and the pressure ...  
WO/2021/061079A1
The present invention relates to a vibration isolator (10), which is arranged identically and adjacently in multiple numbers on the adapter (3), comprises an upper connector (20) adjusted to be connected to a payload (2) placed on an ada...  
WO/2020/263393A3
Systems, devices, and methods including: at least one unmanned aerial vehicle (UAV) (101); at least one flight control computer (FCC) (110) associated with each UAV, where the FCC controls movement of each UAV; at least one computing dev...  
WO/2021/058280A1
The present invention relates to a process for producing a structured article (A1M1) in which a material (M1) comprising at least one micro- and/or nanostructured surface (SU1) containing a plurality of micro-scale and/or nano-scale surf...  
WO/2021/056179A1
The embodiments of the present invention provide an intelligent auxiliary lighting system, method and device, and a movable platform, wherein the intelligent auxiliary lighting system is arranged on the movable platform and comprises: a ...  
WO/2021/058080A1
The invention relates to a galley module (1) for an aircraft, comprising at least one heating and/or cooling unit having at least one first compartment (2) for drinks and/or food, wherein the temperature of said compartment can be condit...  
WO/2021/058560A1
The invention relates to a system for suction of the boundary layer of a wing and protection against icing of this wing, comprising a wall (2) comprising micro-perforations (13, 14) and delimiting a leading edge (3) extended by a pressur...  
WO/2021/059330A1
Provided is an automatic inspection system which is for a passenger boarding bridge, and can perform automatic inspection on a passenger boarding bridge in order to improve cooperation with people such as workers. An example of an automa...  
WO/2021/056430A1
A system integrating wireless power supply and communication (100), a radar device (1000), and an unmanned aerial vehicle (2000). The system integrating wireless power supply and communication (100) comprises a wireless power supply modu...  
WO/2021/061810A1
An aerial vehicle is programmed or configured to respond to reports of events or conditions within spaces of a facility. The aerial vehicle travels to a location of a reported event or condition and captures data using onboard sensors. T...  
WO/2021/058411A1
The present application relates to an aircraft assembly. The aircraft assembly has a first structural component and a second structural component. A fastener fastens the first component to the second component. The first structural compo...  
WO/2021/060994A1
The invention relates to a method for pollinating palms by means of drones. It is a new and efficient method that reduces the time spent on palm pollination operations, with more efficient productivity and in a shorter time. In addition,...  
WO/2021/056925A1
An unmanned aircraft for automatically intercepting and capturing an unmanned aerial vehicle, comprising a nose (1), a body (2), and a tail (3). The nose (1) consists of a guide head (101) and a connecting member (102) disposed inside th...  
WO/2020/254984A3
An aerodynamic louver system used in one or more of the following operations: control, adjust, or stabilize, aid in controlling, adjusting or stabilizing a spacecraft's orientation, angle of attack, lift, or position. There could be mult...  
WO/2021/059322A1
[Problem] To provide an aerial vehicle that can stably land at a destination. [Solution] An aerial vehicle according to the present invention is an aerial vehicle that can travel in at least a front-back direction, comprising: a lift gen...  
WO/2021/056157A1
An adjustment structure and an adjustment method therefor, a seal, a coaxial line, a gimbal and a movable device. A machine arm adjustment structure comprises: a machine base (2), a machine arm (1) and a seal (3). The machine arm may mov...  
WO/2021/062229A1
The 3D extension linkage 100 can include at least one arm that includes two elements connected by a joint. The linkage can include an actuation mechanism, additional arms and/or each arm can include more than two elements, tie rods and/o...  
WO/2021/056194A1
An unmanned aerial vehicle (UAV) (10), comprising: a housing (100), a flight control motherboard (700), a battery (600), and an electronic speed control (ESC) module (401). The flight control motherboard (700), battery (600), and ESC mod...  
WO/2021/058955A1
The invention relates to a lock, in particular to a lock for a secondary cockpit barrier, and a secondary cockpit barrier comprising the same and a barrier body for blocking access to an aircraft cockpit.  
WO/2021/059134A1
A spacecraft servicing system to provide in-orbit servicing through the umbilical connectors of a spacecraft. In one embodiment, a manipulator arm maneuvers a servicer umbilical to form an electrical connection between a servicer spacecr...  
WO/2021/060492A1
The purpose of the present invention is to assist a suitable avoidance action, when a collision of space objects in outer space is predicted in advance, and a storage unit (140) stores orbit prediction information (51) which is a predict...  
WO/2021/059787A1
A control device of this embodiment comprises: an acquisition unit that acquires information indicating the strain of a vane of a structure, and information indicating a control amount of a movable vane of the structure; a first determin...  
WO/2021/034362A3
Presented are a method and apparatus for an aircraft flight surface actuation system including a motor having an output shaft. A gearbox is coupled with the output shaft, whereby a first driving force output via the motor is converted to...  
WO/2021/058819A1
The present invention relates to an optomechanical system (200) based on one or more optomechanical elementary cells (400), to the use of the optomechanical system to locally determine flow variables or accelerations, to a flow sensor as...  
WO/2021/058329A1
Disclosed is a hybrid multirotor propulsion system (100) for an aircraft, comprising: a plurality of propulsion units (PU), each propulsion unit (PU) comprising a propeller (Pr), an electromotor (EU) and a peripheral differential gearbox...  
WO/2021/058916A1
Method for manufacturing a fire-resistant part of an air conditioning system (9) for an air or rail transport vehicle (8), characterised in that it comprises at least the following steps: a step (10) of obtaining a part comprising at lea...  
WO/2021/054178A1
The present disclosure relates to an unmanned aerial vehicle, a control method, and a program which make it possible to safely achieve interaction with an object to be recognized. A state estimation unit estimates the state of the object...  
WO/2021/054879A1
The present invention regards a method of securing a movable latch member of a self- securing latch arrangement (1) configured to latch an aircraft door (3, 803) to an aircraft fuselage (7). The present invention also regards the self-se...  
WO/2021/055403A1
A drone-based delivery system includes a drone (200) that delivers an item (210), and a landing station (100) for landing said drone. The landing station includes a retractable receiving box (160) and a storage compartment (150) to recei...  
WO/2021/051785A1
An electromagnetic steering engine and an aircraft. The electromagnetic steering engine comprises a driving coil (10), a permanent magnet (11), a coil fixing holder (12), and a permanent magnet fixing holder (13); the permanent magnet (1...  
WO/2021/051243A1
A method for installing an air inlet duct protective cover of an aircraft engine, comprising the following steps: a. inflating a protective fabric cover; b. the protective cover supporting a certain prefabricated outer shape to achieve t...  
WO/2021/051774A1
The present application relates to an aircraft, an aircraft control method and apparatus, and a computer-readable storage medium. The aircraft is provided with at least one sensor. The method comprises: detecting the state of an electric...  
WO/2021/054600A1
A drone docking structure is disclosed. The present invention comprises a drone and cargo to be transported by the drone. The drone comprises: a body part for controlling flight; a plurality of wing parts for flight; a drone landing devi...  
WO/2021/053355A1
A wing mounting, comprising: • a base (11); • a wing bracket (25) pivotally mounted to the base, configured to rotate relative to the base within an operational angular range; and • at least one biasing element configured to bias t...  
WO/2021/052893A1
The present invention relates to a method for detecting mines 30 below the water surface in shallow water, the method comprising the following steps: a) flying an aircraft 10 over a suspect region, an aircraft 10 having at least one firs...  
WO/2021/055549A1
Ion Harvesting Technology harvests high voltage electricity, including from atmospheric ions. A wire, or conductive tether, may be used to connect ion harvesting material (typically carbon, but including any materials such as metals, met...  
WO/2021/053846A1
A braking force generation device (1) has: a first mode in which a deflector (3) and a blocker door (4) are retracted with respect to a wing (10); a third mode in which, while the leading edge (3a) and the trailing edge (3b) of the defle...  
WO/2021/053841A1
Provided is a mobile body comprising: an optical wireless communication unit that executes optical wireless communication with another mobile body; an object detection unit that detects an object around the mobile body; an object informa...  
WO/2021/053786A1
[Problem] To provide an aerial vehicle that can efficiently and safely transition from hovering to horizontal flight. [Solution] This aerial vehicle is provided with a flight unit including airfoils and rotary wings disposed to the airfo...  
WO/2021/052087A1
A manipulation method suitable for a non-redundant SGCMG group. The method comprises the steps: 1) determining, according to configurations and synthetic angular momentums of n SGCMGs, nominal frame angle vectors of the configurations of...  
WO/2021/053532A1
A tray (1) for releasably engaging a trolley, the tray (1) comprises a body (2) describing a sealed volume (V), the sealed volume (V) having a phase change material (PCM) received therein, the tray (1) comprising an engagement means (4) ...  
WO/2021/054521A1
The present invention relates to a system and a method for supplying fuel to an electric cart by using an aerial refueling drone. A fuel supply control server for controlling supply of fuel to at least one electric cart by using at least...  
WO/2021/016192A3
A patient litter basket spin control assembly for use on a patient litter basket is provided. The assembly comprises thruster unit for discharging an air stream and is mounted on the patient litter basket. At least one sensor is associat...  
WO/2021/053875A1
This flying device 1 comprises: an electric power acquisition unit 12 which receives supply of electric power from a prescribed mobile body 2; a flight control unit 171 which causes the flying device 1 to fly within a prescribed range wi...  
WO/2021/053021A1
Disclosed is an aircraft system (10) for an aircraft (1). The aircraft system comprises a controller (100) that is configured to receive at least one signal during a take-off procedure of the aircraft. The signal may comprise information...  
WO/2021/053407A1
The invention is related to the field of aircraft specifically to unmanned drones with multiple propellers and protection against external influences. Disc-shaped multi-propeller aircraft with a protective frame (1) consists of outer (2)...  
WO/2021/052217A1
The invention aims to fully protect a camera againt an impact applied from the outside of an unmanned aerial vehicle and prevent the quality of a captured image from being affected. The control device comprises: a frame control portion u...  
WO/2021/055223A1
A modular floor system with an integral utility for temporary installation in an unfinished ircraft fuselage to facilitate construction. The system includes multiple floor modules, each ncluding a catch pan defining a pan volume, a grid ...  
WO/2021/051278A1
An earth surface feature identification method and device, an unmanned aerial vehicle, and a computer readable storage medium. The method comprises: obtaining earth surface image information (S101); processing a plurality of pieces of co...  

Matches 101 - 150 out of 72,018