| Document |
Document Title |
|
WO/2021/020279A1 |
This secondary battery is provided with: a positive electrode having, on a belt-like positive electrode foil, a covered part covered with a positive electrode active material layer and a positive electrode active material uncovered part;...
|
|
WO/2021/016816A1 |
A photographing apparatus comprises a camera module (20) and a housing module (10). The camera module (20) comprises a lens holder (22) and at least one lens barrel (21). The housing module (10) comprises a transparent lens (12) and a ho...
|
|
WO/2021/018988A1 |
The invention relates to a device (10) for braking a wheel (R), comprising: • - a brake comprising at least a first actuator (11.1) and a second actuator (11.2) which are designed to apply a braking torque to the wheel (R); • - a con...
|
|
WO/2021/019247A1 |
There is described herein a lattice framework for structural insulated panels (SIPs), wherein the SIPs each comprise a first facesheet and a second facesheet, the lattice framework comprising (a) a plurality of surface struts configured ...
|
|
WO/2021/020999A1 |
The invention relates to wing-in-ground-effect vehicles having an aerodynamic "composite wing" configuration. The technical result is an increase in safety by providing for the static, non-oscillatory and oscillatory stability of a wing-...
|
|
WO/2021/016871A1 |
Provided are a control method and control apparatus for an unmanned aerial vehicle, and a computer-readable storage medium. An unmanned aerial vehicle comprises a fixed-wing power system and a rotor-wing power system. The control method ...
|
|
WO/2021/019288A1 |
A reinforced structural insulated panel (20) that comprises an expanded cork core (30), a pair of facesheets (24, 26) and a fibre reinforced polymer lattice framework (36). The core (30) is sandwiched between the facesheets (24, 26). The...
|
|
WO/2021/017017A1 |
Disclosed is a camera lens for a racing unmanned aerial vehicle, which relates to the related field of camera lenses, and aims to solve the problem in the prior art whereby a lens cannot be cleaned when rainwater is accumulated on a lens...
|
|
WO/2021/020658A1 |
A manned drone system for leisure of the present invention, in which a person can directly ride and pilot and fly a drone, is characterized by comprising: one or more drones (100) having a communication unit (120) for communication with ...
|
|
WO/2021/021412A1 |
A themed aerial vehicle entertainment system or platform useful for generating crowd-pleasing shows or displays through the use of dynamically-coordinated show systems. Instead of use of a fixed flight plan, the new entertainment platfor...
|
|
WO/2021/021170A1 |
Described are support surfaces (such as passenger seat tray tables) that have a pivot about which the support surface is rotatable. The pivot can be coupled with a track and movable relative to the track to adjust a deployed height of th...
|
|
WO/2021/020570A1 |
According to the present invention, an unmanned aerial vehicle equipped with a LiDAR sensor is flown to perform forest measurement on a forest. A rotary shaft or a swing shaft of the LiDAR sensor is mounted on the unmanned aerial vehicle...
|
|
WO/2021/019212A1 |
There is provided an arming apparatus for a store, the apparatus comprising: a first attachment system and a second attachment system; a linking connector coupled with the first attachment system and the second attachment system; and an ...
|
|
WO/2021/019593A1 |
A flight vehicle according to one embodiment of the present invention has a wing, a double-surface power generation solar cell, and a light-reflecting part. The wing has an outer shell member. The outer shell member is translucent. The w...
|
|
WO/2021/018503A1 |
The invention relates to an aircraft window consisting of a monolithic inner pane (1) made of a polymer material and a laminated outer pane (2) made of glass, the panes being separated by an air space (3).
|
|
WO/2021/017235A1 |
A connecting corner box for the root part of a civil aircraft wing upper panel. The connecting corner box comprises a bottom side (9), an upright side (10) and reinforcing ribs (11), wherein the bottom side (9) is provided with notches (...
|
|
WO/2021/017718A1 |
A lifting table used for transferring an aircraft catering trolley, said lifting table comprising a fixed device (1), a movable device (2), and a protective plate. A surface of the fixed device (1) is provided with two empty slots (11). ...
|
|
WO/2021/019879A1 |
An information processing device according to one embodiment of the present technology is provided with an acquisition unit, a connection unit, and a smoothing unit. The acquisition unit acquires path information that includes a path, wh...
|
|
WO/2021/019679A1 |
[Problem] To provide: a flight vehicle flying system that can properly support flying of the flight vehicle when flying the flight vehicle while watching an image acquired by the flight vehicle; and a method for flying the flight vehicle...
|
|
WO/2021/019487A1 |
The problem addressed by the present invention is that of enhancing the functionality and efficiency of a lightweight aircraft designed for use on short-haul routes. The technical effect to be achieved by the use of the invention is that...
|
|
WO/2021/021152A1 |
Described are track fitting assemblies for passenger seats. Each track fitting assembly includes a track fitting main body and an anti-rattle shear body. The track fitting main body is connectable to a leg of the passenger seat and inclu...
|
|
WO/2021/017750A1 |
Disclosed is an anti-fall aircraft with a pair of semi-conical air bags mounted on the left and the right of the aircraft body thereof, wherein the lower portion of the aircraft body (1) is provided with a landing gear, and the tail of t...
|
|
WO/2021/019291A1 |
An electric powered paraglider is provided. An electric powered paraglider includes a frame which includes a plurality of connector points. The electric powered paraglider also includes a propulsion unit mechanically coupled to the frame...
|
|
WO/2021/020569A1 |
According to the present invention, an unmanned aerial vehicle equipped with a LiDAR sensor is flown to perform forest mensuration of a forest on an inclined surface. The LiDAR sensor is mounted on the unmanned aerial vehicle in such a w...
|
|
WO/2021/019422A1 |
A shock strut is provided that includes a first energy absorption stage or load limiter and a second energy absorption stage or load limiter. The second energy absorption stage or load limiter includes one or more disc springs (205). The...
|
|
WO/2021/019209A1 |
An aircraft passenger seat unit (100) configured for use adjacent an aisle (600) of an aircraft cabin (1) is disclosed. The seat unit comprises a seat (110), a footrest (109), and a movable panel (113). The movable panel (113) is movable...
|
|
WO/2021/022253A1 |
Systems and methods for controlling satellites are provided. In one example embodiment, a computing system can obtain a request for image data. The request can be associated with a priority for acquiring the image data. The computing sys...
|
|
WO/2021/019827A1 |
Provided is a system for satellite operators by which information relating to retrieved ground stations can be easily obtained. An information processing device according to the present technology is provided with a user interface unit w...
|
|
WO/2021/020119A1 |
In a secondary battery, a cathode includes a coated part coated by a cathode active material layer and a cathode active material uncoated part on a cathode foil having a strip shape, and an anode includes a coated part coated by an anode...
|
|
WO/2021/019803A1 |
An engine according to at least one embodiment is provided with: a piston group including three or more pistons that are radially disposed; and a plurality of combustion chambers present on a plane on which the piston group is present, w...
|
|
WO/2021/017533A1 |
Disclosed is a safety belt capable of automatic binding, comprising a seat; a sealing cavity is provided inside of a base of the seat; an air pump is fixed to a side wall of the sealing cavity; a safety belt is fixed to the air outlet en...
|
|
WO/2021/020660A1 |
A ground station for supporting a tethered drone, and a tethered drone system comprising same, according to an embodiment of the present invention, comprise: a power supply unit for supplying power to a tethered drone through a cable; a ...
|
|
WO/2021/019250A1 |
A flight control system (20) comprising: • at least one drive unit (4); • at least one wing (5) operatively connected to the at least one drive unit; and • a controller (21) configured to: • send a control signal to the at least ...
|
|
WO/2021/017004A1 |
Provided are a locking structure (100), a propeller (200), a power device (300), a power assembly, and an unmanned aerial vehicle (1000). The locking structure (100) comprises a mounting base (10) and a locking assembly (20). The locking...
|
|
WO/2021/020117A1 |
This secondary battery comprises an electrode wound body having a winding structure, a positive electrode current collector plate, and a negative electrode current collector plate, which are housed in an exterior can, wherein: the positi...
|
|
WO/2021/019655A1 |
The purpose of the present invention is to provide an unmanned aerial vehicle for which the fall speed is reduced even when rotor blades are stopped and for which the possibility of contact with a building or the like is also reduced. Th...
|
|
WO/2021/019210A1 |
An aircraft passenger accommodation unit (3) is disclosed. The aircraft passenger accommodation unit (3) comprises a seat (6), a wall (91), an ottoman (15), and a console (11). An access path (7) comprising a width is defined between the...
|
|
WO/2021/018050A1 |
A wind speed measurement and calculation method, a wind speed estimator, and an unmanned aerial vehicle (10). The wind speed measurement and calculation method comprises: on the basis of flight data and attribute data of the unmanned aer...
|
|
WO/2021/016706A1 |
An aircraft landing gear includes a shock strut with a rod slidably received within a cylinder. A beam is rotatably mounted to the rod, and wheels are mounted to the beam. The landing gear further includes a link assembly with an upper l...
|
|
WO/2021/016881A1 |
Disclosed is a power assembly (100). The power assembly (100) comprises a driving device (10), a propeller (20), and an elastic member (60). The driving device (10) comprises a rotating shaft (14). The propeller (20) comprises propeller ...
|
|
WO/2020/247198A3 |
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/2021/019557A1 |
The present invention relates to a vertical rotor assembly for an aerial vehicle, comprising a rotor (102) and a connecting element assembly attached to the rotor (102) at one end and to a frame (100) of the aerial vehicle at the other e...
|
|
WO/2021/015251A1 |
Provided is an unmanned aerial vehicle that can carry an aerosol container, the unmanned aerial vehicle comprising: a discharge unit that has a discharge opening, and that discharges the contents of an aerosol container from the discharg...
|
|
WO/2021/014235A1 |
A rotor (3, 3') for an aircraft (1) is described that has a mast (50), an attenuating device (7, 7') to attenuate the transmission of vibrations from the mast (50) in a plane orthogonal to the first axis (A), and a transmission device (1...
|
|
WO/2021/014082A1 |
Disclosed is a method for erecting the structure of an aerostat (1) in successive horizontal sections, starting from the top horizontal section, comprising an iteration of the following steps, starting from a current state of completion ...
|
|
WO/2021/014234A1 |
A rotor (3, 3', 3'') for an aircraft (1) is described that has a mast (150), an attenuating device (7, 7', 7'') to attenuate the transmission of vibrations from the mast (150) in a plane orthogonal to the first axis (A); and a transmissi...
|
|
WO/2021/015201A1 |
The present invention addresses the problem of controlling a distant mobile body with high accuracy. The problem is solved by a remote piloting system and a piloting device therefor. The remote piloting system is provided with a mobile...
|
|
WO/2021/014880A1 |
Provided are a toroidal continuously-variable transmission and an aircraft drive mechanism-integrated power generation device which, by making an oil jet stream less susceptible to the influence of wind produced by rotation of a power ro...
|
|
WO/2021/012476A1 |
A method for controlling loading of an airport catering truck, comprising: when a power battery drives loading work, driven supporting legs to be supported only when the state of the whole truck satisfies the conditions of the normal wor...
|
|
WO/2021/013980A1 |
The invention relates to a camera system (1) for aircraft (F), in particular to an aircraft camera system (2) comprising a cover (4) and a camera. The camera system (1) also comprises a base plate (3). The camera (5) is physically divide...
|
