| Document |
Document Title |
|
WO/2020/182946A1 |
Disclosed is a landing gear system uplock arrangement (300, 500) comprising: a hook (310) defining a gap (314), wherein the hook is movable between a first position, at which the hook is for retaining a movable element (299, 499) of a la...
|
|
WO/2020/185542A1 |
The invention relates to a strut (101, 201), such as fiber composite struts used in aircraft or spacecraft, which has a largest possible outer diameter within a cylindrical installation space of the strut (101, 201). The invention concer...
|
|
WO/2020/184318A1 |
An information processing device (10) is provided with: a detection unit (140) for detecting pressure fluctuation of a fluid filled in a deformable filling part (130) provided to a portion at which leg parts of a mobile body (100) each h...
|
|
WO/2020/179725A1 |
A landing gear lifting/lowering EHA system (10) is provided with: a hydraulic actuator (2) that elevates/lowers landing gear of an aircraft; at least one electric hydraulic pump (31, 32); a hydraulic path (101); pressure sensors (38, 39)...
|
|
WO/2020/180520A2 |
Apparatus to monitor the position of an aircraft landing gear.
|
|
WO/2020/180375A1 |
A power plant a for an aircraft having a hybrid-electric propulsion system including a nacelle body including therein an electric motor directly connected to a gearbox for driving a propeller, wherein the gearbox is connected directly to...
|
|
WO/2020/178946A1 |
Information pertaining to the distress condition of a person in distress is readily communicated to a head station, etc. A recognition marker (1) is assigned a digital recognition code (2) pertaining to prescribed information, the reco...
|
|
WO/2020/156078A1 |
A wing assembly (100), comprising a wing (10) configured to be mounted on a body (200), a tiltrotor assembly (20) mounted on the wing (10), and a landing gear (30) mounted on the tiltrotor assembly (20); when a tiltrotor unmanned aerial ...
|
|
WO/2020/154035A1 |
A method of inspection or maintenance of a curved ferromagnetic surface (150) using an unmanned aerial vehicle (UAV) (100) having a releasable crawler (130) is provided. The method includes: flying the UAV from an initial position to a p...
|
|
WO/2020/145485A1 |
A drone including a vertical wing serving as a landing support according to an embodiment of the present invention comprises: a main body part of the drone; at least one pair of horizontal wing parts formed on the main body part so as to...
|
|
WO/2020/142434A1 |
Systems and methods for mechanically rotating an aircraft about its center-of-gravity (CG) are disclosed. The system can enable the rear, or main, landing gear to squat, while the nose landing gear raises to generate a positive pitch ang...
|
|
WO/2020/142457A1 |
Systems and methods for mechanically rotating an aircraft about its center-of-gravity (CG) are disclosed. The system can enable the rear, or main, landing gear to squat, while the nose landing gear raises to generate a positive pitch ang...
|
|
WO/2020/135637A1 |
A logistics unmanned aerial vehicle comprises a fuselage (1) and four rotary blade shafts (2) extending through the fuselage (1) and arranged in a criss cross fashion. Two ends of the rotary blade shaft (2) respectively extend out of the...
|
|
WO/2020/135448A1 |
An unmanned aerial vehicle (100), comprising an unmanned aerial vehicle body (10) and an undercarriage assembly (40) mounted on the unmanned aerial vehicle body. The undercarriage assembly comprises a mounting plate, an undercarriage (42...
|
|
WO/2020/118445A1 |
A structural component, or parts thereof, for a machine system or vehicle, such as an aircraft, is provided. In some examples, the structural component includes at least one embedded passageway or line. In other examples, the passageway ...
|
|
WO/2020/108341A1 |
Disclosed is an aircraft landing gear comprising a landing gear bracket (1), a landing gear wheel (2) and an electric motor (3). The electric motor (3) is provided on the landing gear bracket (1).When the aircraft starts to taxi and take...
|
|
WO/2020/112859A1 |
An unmanned aerial vehicle (UAV) (100) includes a body constructed to enable the UAV to fly and three or more legs connected to the body and configured to land and perch the UAV on a curved ferromagnetic surface (50). Each leg includes a...
|
|
WO/2020/112887A1 |
An unmanned aerial vehicle (UAV) (500) for landing and perching on a curved ferromagnetic surface is provided. The UAV includes a plurality of articulated legs (850). Each articulated leg includes: a magnet configured to magnetically att...
|
|
WO/2020/107099A1 |
An aircraft capable of vertical take-off and landing comprises a fuselage, at least one processor carried by the fuselage and a pair of aerodynamic, lift-generating wings extending from the fuselage. A plurality of vectoring rotors are r...
|
|
WO/2020/103037A1 |
Provided is a multirotor unmanned aerial vehicle (1), comprising: a body (11), multiple arms (12), and a number of rotor assemblies (13) equal to the number of arms (12). The multirotor unmanned aerial vehicle (1) is provided with a firs...
|
|
WO/2020/097367A1 |
Devices and systems of the inventive concept provide a durable, all-weather manned or unmanned aircraft that is capable of vertical flight and provides improved stability upon payload launch or delivery. The payload bay is positioned alo...
|
|
WO/2020/095435A1 |
This flight vehicle (100) has: a plurality of propellers (2); a plurality of motors (3) for driving the respective propellers (2); a device body (20) comprising a control device (21) for controlling the motors (3), and a wireless device ...
|
|
WO/2020/075562A1 |
The purpose of this invention, i.e. to stabilize the quality of coating work performed on a structure surface using an unmanned aircraft, is achieved by: an unmanned aircraft that comprises a rotor, a coating device, and a wheel that can...
|
|
WO/2020/076198A1 |
This invention is designed for all kinds of aircrafts, whether commercial or military. It is small sized wheels hidden inside streamlined hulls (aerofoil covers) installed beneath the aircraft's airframe, engines or both, specifically at...
|
|
WO/2020/070521A1 |
Disclosed is a transportation device (1) for transporting a load over a surface, for example, formed from water or earth. The transportation device comprises propulsion element(s) (5, 6) that generate an aerodynamic lift force and a driv...
|
|
WO/2020/066889A1 |
The present invention addresses the problem of providing an unmanned aerial vehicle with which it is possible to perform a painting operation on a surface of a structure with stable quality. The problem is solved by an unmanned aerial ve...
|
|
WO/2020/058624A1 |
The invention concerns a landing gear (10) of an aircraft comprising: - at least one wheel (20), - an electric taxiing system (30) comprising an electric taxiing motor (32) and capable of rotating said wheel, and - a braking system (40) ...
|
|
WO/2020/053606A1 |
This invention is about a set of common features that will characterize any machine of the new type to be produced within the set of pumps, turbines and blowers. The machines in this new category, as will be here described, will be told ...
|
|
WO/2020/055365A2 |
It's a method which the wheels of airplanes spinning with wind power,with a motor or a different way. It will reduce friction of tyres, touching onto the ground while landing. So, the method will stop expense for tyres to renew. Plus, he...
|
|
WO/2020/045995A1 |
According to the present invention: power is supplied from a fuel cell, so as to reduce the weight of a drone and enable a long-time operation of the drone; a fuel cell power pack of the drone maintains the general weight balance by itse...
|
|
WO/2020/041325A1 |
An approach is provided for enhancing the safety and functionality of unmanned rotorcraft by improving reliability, transparency, operational capabilities, and effectiveness. Embodiments include integration of rotorcraft with objects att...
|
|
WO/2020/040746A1 |
A deceleration feedback algorithm for an aircraft braking system is provided. The algorithm prevents the aircraft brakes for releasing to clearance during a braking operation, while maintaining differential pilot/co-pilot braking inputs....
|
|
WO/2020/032262A1 |
Provided is an unmanned aircraft which delivers packages, the unmanned aircraft comprising a plurality of rotor blades (709a), a plurality of first motors (711), a body (712), a connection body (730), a movable part (740), and a processi...
|
|
WO/2020/025439A1 |
An aircraft landing gear assembly comprising: a ground contacting part, an aircraft attachment part, and a component comprising: a first base member and a second base member separated along a first longitudinal axis, a plurality of first...
|
|
WO/2020/022582A1 |
The present invention relates to a solar panel management apparatus for monitoring a plurality of solar panels and cleaning foreign substances off the solar panels, while freely moving around in a solar power plant. The present invention...
|
|
WO/2020/012093A1 |
The present invention concerns a landing gear (1) for a light aircraft, i.e. weighing less than 5.7 tonnes, the landing gear consisting of at least one wheel (3) attached to a chassis or to a fuselage of the aircraft by means of a connec...
|
|
WO/2020/006641A1 |
A method of controlling and optimizing braking and directional control of a vehicle operated on a contaminated, compliant, or non-compliant surface. The method includes steps of: collecting data from a plurality of sensors, the data bein...
|
|
WO/2020/000644A1 |
An unmanned aerial vehicle (100) and aerial vehicle frame (10) thereof. The aerial vehicle frame (10) comprises a central body, foot supports (1), and multiple aerial vehicle arms. The central body comprises a bottom housing (2), a mount...
|
|
WO/2020/002918A1 |
An unmanned aerial vehicle has a thrust body (1) including a control system, thrusters (4, 5) to generate lift and direct the UAV in response to control signals from the control system. A spherical fender cage (2) envelopes the thrust bo...
|
|
WO/2019/227209A1 |
There is provided a rotorcraft undercarriage assembly and a method of landing a rotorcraft. The assembly includes: an upper hub attached to the rotorcraft; a lower hub; and at least three arms, each arm comprising: a rotary actuator moun...
|
|
WO/2019/220115A1 |
The invention provides an aircraft landing gear (100) comprising a first oleo strut (10) comprising a sleeve portion (11) and a slider portion (13), the slider portion being slidable within a hydraulic fluid chamber (12) of the sleeve po...
|
|
WO/2019/205460A1 |
Disclosed is a landing gear structure and an unmanned aerial vehicle. The landing gear structure (100) comprises a landing gear (10) and a quick-release assembly (20). The landing gear (10) comprises a main body portion (14) and an inser...
|
|
WO/2019/203229A1 |
A landing device (10) comprises: a pair of skids (20) arranged parallel to a longitudinal axis of an airframe (12) of a rotary wing aircraft (11); a cross tube (30) that is mounted to the airframe, that links the pair of skids, and that ...
|
|
WO/2019/198393A1 |
This anti-vibration device for an unmanned aircraft is configured by an anti-vibration rubber being interposed between the airframe body and legs of the unmanned aircraft which are connected to each other, the anti-vibration rubber being...
|
|
WO/2019/200088A1 |
A package delivery drone comprises at least one propeller for generating lift and an article containment area for containing an article to be carried by the drone. The floor of the article containment area comprises a dynamic support sur...
|
|
WO/2019/190870A1 |
In some embodiments, systems and methods provide a retail delivery unmanned aerial vehicle, comprising: a frame; a plurality of motors cooperated with the frame; a plurality of propellers each secured with one of the motors; a vehicle co...
|
|
WO/2019/183328A1 |
A wheel well fairing (230) for reducing drag on an aircraft fuselage configured with an open wheel well (111) for stowing landing gear of the aircraft. The wheel well fairing includes a Coanda fairing having a convex-shaped lower portion...
|
|
WO/2019/178007A1 |
A thin air bag/bladder, which when packaged and attached to an air valve system is inserted into an inflatable boat, or inflatable structure to repair a puncture or leak. This valve and adapter system is used to fasten and lock the valve...
|
|
WO/2019/173990A1 |
Provided is a mounting mechanism for mounting legs of the unmanned aerial vehicle, the legs are disposed below the center frame of the unmanned aerial vehicle, and a carrier for carrying a payload is also disposed below the center frame,...
|
|
WO/2019/172256A1 |
Provided is a flying robot for performing a specified operation, said flying robot comprising a body, and a propulsion part having a plurality of propulsion units that generate propulsive power by the driving of a rotor and are provided ...
|
