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Patent Searching and Data


Matches 201 - 250 out of 70,945

Document Document Title
WO/2020/250707A1
The present invention pertains to: a satellite system imaging method which, in satellite remote sensing, enables an artificial satellite to capture an image in response to an event that has taken place on the ground; and a transmitting d...  
WO/2020/249888A1
The present invention concerns an inlet cone (10) for an aircraft turbine engine (1), comprising a frustoconical body (12) and a tip (11) made from elastically deformable material attached to an end (12p) of smaller diameter of the body ...  
WO/2020/252152A1
Methods for optimizing Boundary Layer Control (BLC) systems and related systems (e.g. a Laminar Flow Control (LFC) system or systems, a Static Pressure Thrust (SPT) system or systems, a Boundary Layer Ingestion (BLI) / Wake Immersed Prop...  
WO/2020/249592A1
The invention relates to a support (10) intended to be reversibly installed on an upper part (523) of an uncovered backrest (52) of a seat (50), said support comprising: - a plate (11) intended to bear, completely or partly, against a re...  
WO/2020/244625A1
An edge drive type fan, a double-state switching mechanism and wing, and a vertical takeoff and landing aircraft, relating to the field of aviation. The edge drive type fan comprises a housing (10); the interior of the housing is provide...  
WO/2020/247641A1
Systems and methods are directed toward determining a vehicle orientation based on sensor information. Sensors are positioned along a vehicle body that may be evaluated to determine corresponding values between matching sensor types. Whe...  
WO/2020/245897A1
A landing gear (100) comprises a leg (110A, 110B, 110C), a rotating body (130A, 130B, 130C), and a housing (150). The leg (110A, 110B, 110C) makes contact with the landing surface at one end and moves linearly in the axial direction with...  
WO/2020/245549A1
A space aircraft (1) comprises a fuselage (3), two wings (4A, 4B) arranged on either side of the fuselage (3), and two nacelles (7A, 7B) arranged at the ends of the wings (4A, 4B) and each carrying a horizontal tail (8A, 8B) and a vertic...  
WO/2020/209924A3
A failsafe vale provides"Hole-In-The-Wall"failsafe functionality for thin- wing aircraft control surface actuation systems having a geared rotary actuator powered by a hydraulic rotary motor. The failsafe valve is associated with the hyd...  
WO/2020/245363A1
The invention relates to an aircraft, in particular an aircraft with support surfaces (11, 12), comprising: - a hull (10) for receiving at least one pilot and/or a payload, in particular air freight and/or at least one passenger; - a fir...  
WO/2020/247842A1
A fuel system for a generating unit disposed within an enclosure, the enclosure having an enclosure width and an enclosure height, includes a bulk fuel storage tank and a vertical day tank, a supply line and a return line. The vertical d...  
WO/2020/245553A1
The invention relates to a thrust group (300) for a propulsion device (10), comprising a thrust engine (302), arranged to provide a thrust force (F1, F2) oriented in a direction so as to provide substantially vertical take-off and landin...  
WO/2020/244626A1
Disclosed are an assistance system for assisting launching and recovery of an aircraft, and a launching and recovery method. The assistance system for assisting launching and recovery of an aircraft comprises: a reference platform (1); a...  
WO/2020/247613A1
A UAV is provided. The UAV comprises a plurality of rotors and has a central axis about which the rotors are arranged. The UAV further comprises a parachute, and a parachute deployment assembly comprising: one or more hollow members, eac...  
WO/2020/243835A1
The present application provides a method for the preparation of sugar-modified siloxane oligomers or polymers that one their own, or after dilution in an appropriate solvent, become shear thickening and energy dissipating.  
WO/2020/247870A1
A suspended aerial vehicle system includes an aerial vehicle with a thruster assembly and a supporting line attached to the aerial vehicle that is capable of supporting at least some of the weight of the aerial vehicle. The supporting li...  
WO/2020/245188A1
The invention concerns an aircraft door comprising a lever (3) for emergency opening from outside, disposed in a lever window. The lever (3) for emergency opening from outside comprises: ‚óŹ a main arm (7) comprising a first aerodynamic ...  
WO/2020/245588A1
There is disclosed an aircraft configured to collect air data, the aircraft comprising: a wing structure; a forebody, forward of the wing structure; an afterbody, backward of the forebody; a skin covering the wing, the forebody and the a...  
WO/2020/246970A1
Examples of devices are described herein. In some examples, a device may include a first image sensor to capture images of a fixed pattern that is in a static position relative to a structure. In some examples, the device may fly above t...  
WO/2020/245597A1
A motor drive signal generator configured to combine at least a part of a first input waveform with at least a part of a second input waveform to create a compound waveform, wherein the first waveform is a sine wave and the second input ...  
WO/2020/246136A1
An information processing device having an audio signal generation unit for generating, on the basis of location information of each of a plurality of unmanned aerial vehicles, an audio signal to be played back from a speaker provided in...  
WO/2020/245917A1
One embodiment of the present invention is an anti-G tolerance improving device provided with a valve control unit for controlling the operation of the following valves: a main valve for controlling, with respect to a main supply source ...  
WO/2020/247198A2
A projectile-launched aircraft system includes a projectile launcher including a triggering mechanism, a rotary-wing, hover-capable aircraft including a rotor assembly that includes at least one rotor blade, wherein the rotor blade inclu...  
WO/2020/245366A1
The invention relates to an aircraft comprising: - a hull (10) for receiving at least one pilot and/or a payload, in particular air freight and/or at least one passenger; - at least one front support surface (11) and at least one rear su...  
WO/2020/244591A1
A method for docking a boarding bridge with an aircraft, an electronic equipment and a storage medium are provided. The method includes: planning a path from a position at which an cabin port is located when the boarding bridge is in a p...  
WO/2020/245359A1
The invention relates to a seat system, in particular an aircraft seat system, comprising at least one seat device (14, 16) having at least one seat (24, 26, 28, 38) and a system for additionally booking and/or removing a booking (42), w...  
WO/2020/246951A1
A reconfigurable power processing unit for a spacecraft including a plurality of power modules. Each of the power modules includes a first power source and a second power source. The first power source and the second power source are con...  
WO/2020/245587A1
There is disclosed a fluid sensor for measuring the pressure of a fluid, the fluid sensor comprising: a surface; a recess formed at the surface, the recess being configured to affect the pressure of the fluid flowing at the recess, at le...  
WO/2020/247031A1
Electroaerodynamic devices and their methods of operation are disclosed. In one embodiment, ions are formed by dielectric barrier discharge using a time varying voltage differential applied between a first electrode and a second electrod...  
WO/2020/245388A1
The invention relates to an aircraft (1), in particular an aircraft with support surfaces (11, 12), comprising a hull (10) for receiving at least one pilot and/or a payload, in particular air freight and/or at least one passenger, and at...  
WO/2020/245390A1
The invention relates to an aircraft and to a method for operating an aircraft (1), in particular an aircraft with support surfaces (11, 12), comprising a hull (10) for receiving at least one pilot and/or a payload, in particular air fre...  
WO/2020/244596A1
A path planning method for a boarding bridge, including: obtaining the preset wing anti-collision line (S1000); obtaining the position of the cabin door and the cabin port, and generating the path connecting the cabin door and the cabin ...  
WO/2020/245513A1
The invention relates to a thrust unit (300) for a propulsion device (10), comprising a thrust motor (302), arranged to provide a thrust force (F1, F2) oriented in a direction so as to provide substantially vertical take-off and landing ...  
WO/2020/246931A1
A dispenser (1) for storing and launching countermeasures (13), where the dispenser (1) is adapted for storing the countermeasures in a magazine (11), where the dispenser (1) is provided with at least one launch opening (10) and where th...  
WO/2020/246168A1
This method for estimating a right-under point position of an on-orbit object comprises: a photographing step for photographing an observation image of the on-orbit object (X) together with a known object of which orbit is known; a first...  
WO/2020/247647A1
Aspects of the present disclosure are directed to an unmanned aerial system (UAS) configured to navigate a UAS corridor. The UAS includes a navigation system that includes one or more sensors, configured to gather environmental data, and...  
WO/2020/245305A1
A method of evaluating a structural integrity of an aerial vehicle comprising one or more engines comprises selectively driving said engine/s of said aerial vehicle according to a driving pattern unsuitable to put or maintain the aerial ...  
WO/2020/245193A1
The invention relates to a method and a system for determining the capability of a sensor contained in a satellite to access a target region (8). The position (5) of the satellite is ascertained, the viewing radius of the sensor in the d...  
WO/2020/245535A1
The invention relates to an assembly comprising a nacelle element, such as a cover, a device for locking the nacelle element, a key for locking/unlocking the locking device and a indicator (20) for indicating the position of the locking ...  
WO/2020/243925A1
A rotor structure, comprising a protective support (11), a turning mechanism (12), a driving source (13), and a rotor (14). The protective support (11) has an accommodating space for accommodating the rotor (14), and the protective suppo...  
WO/2020/247148A2
An electrically powered vertical takeoff and landing aircraft (EVTOL) includes a payload module, a plurality of electrical power sources, a wing, and a plurality of electric thrust generators. The wing is pivotally attached to the payloa...  
WO/2020/223114A3
Systems, devices, and methods including: a latching mechanism (116) comprising: a first latch (116A) configured to attach to a door (114) of an unmanned aerial vehicle (UAV) (110); a second latch (116B) configured to attach to a portion ...  
WO/2020/245527A1
Load transfer device (1) for transferring a useful load (5), using an on-board crane, between an aerostat and the ground, comprising an upper lifting portion (2) which is designed to be attached to lifting cables (3) and a lower portion ...  
WO/2020/245379A1
The invention relates to an aircraft (1) and to a method for operating an aircraft (1), in particular an aircraft with support surfaces (11, 12), a hull (10) for receiving at least one pilot and/or a payload, in particular air freight an...  
WO/2020/245102A1
The invention relates to a collection device (1 ) for stacking trays (20) of a tray conveyor (100) comprising a stack receiver (10) for receiving several trays (20) from the tray conveyor (100) stacked on top of each other and a cover (3...  
WO/2020/239699A1
A flow body for an aircraft, in particular for a wing leading edge device, is proposed, the flow body having a curved front skin having a leading edge and at least one trailing-edge component coupled with at least one spanwise edge of th...  
WO/2020/239470A1
The invention relates to an air intake lip (2a) of an aircraft turbomachine nacelle extending along an axis X, in which an air flow circulates from upstream to downstream, the lip (2a) extending annularly about the X-axis and having an i...  
WO/2020/239606A1
An aircraft wing (10) comprising a fixed wing (1) and a wing tip device (12) rotatable about a hinge (16) at the tip of the fixed wing. The wing further comprises an actuation assembly (11) for rotating the wing tip device about the hing...  
WO/2020/239464A1
The invention relates to an air intake lip (2a) of an aircraft engine nacelle (1) extending along an axis X, in which an air flow (F) circulates from upstream to downstream, the lip (2a) extending annularly about the X-axis and having an...  
WO/2020/243451A1
An article of manufacture, a force reduction release mechanism (100) and system for selectively maintaining and releasing components under tensile tension, the release mechanism offering mechanical gain such that the force required to ac...  

Matches 201 - 250 out of 70,945