| Document |
Document Title |
|
WO/2020/220215A1 |
Provided are a spray head device, a spraying system, a movable platform and a spraying operation method therefor. The spray head device (100) comprises a first sub-spray head (110), a second sub-spray head (120) and a switch device (130)...
|
|
WO/2020/221498A1 |
The invention relates to a table device (T) for an interior of a vehicle, with a table element (2) positionable from a non-use position into a use position. According to the invention, it is provided that - the table element (2), which i...
|
|
WO/2020/223733A1 |
Exemplary embodiments provided herein include an attachment and deployment system and method. Exemplary embodiments may use features together or separately as desired. The attachment feature may be used to periodically couple a solar sail.
|
|
WO/2020/221610A1 |
The present invention relates to an assembly (10) of individual seats (11.1, 11.2) intended to be installed in an aircraft cabin, the assembly (10) comprising: - a first seat (11.1) and a second seat (11.2), a central console (18) arrang...
|
|
WO/2020/222674A1 |
The group of inventions relates to the field of aviation. An aircraft train consisting of an aircraft having a nuclear power plant and an additional aircraft comprises an aircraft having a nuclear power plant that includes a nuclear reac...
|
|
WO/2020/223722A1 |
Methods, devices, and systems for ground traffic aircraft management are described herein. One device includes a user interface, a memory, and a processor configured to execute executable instructions stored in the memory to receive airp...
|
|
WO/2020/223114A2 |
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/2020/220195A1 |
Disclosed are an unmanned aerial vehicle control method, device and spraying system, and an unmanned aerial vehicle and a storage medium. The method comprises: acquiring position information and attitude information of an unmanned aerial...
|
|
WO/2020/222667A1 |
The present application relates to a sound insulating panel, suitable for use as a deflecting surface in jet blast deflectors. Therefore, it is described a jet blast deflector fence, comprised of detachable sound insulating panels, formi...
|
|
WO/2020/223115A2 |
Systems, devices, and methods including: at least one unmanned aerial vehicle (UAV) (108A,B); at least one battery pack (114) comprising at least one battery (120); and at least one motor (112) of the at least one UAV, where the at least...
|
|
WO/2020/222193A1 |
A multifunctional area on an aircraft or other passenger transportation vehicle that is configured to be altered in various ways in order to accommodate various activities at different points of travel. For example, the area may be confi...
|
|
WO/2020/220190A1 |
Disclosed are an unmanned aerial vehicle control method and a related device. The method comprises: performing a flight lock operation on an unmanned aerial vehicle; acquiring an image of a user photographed by a photographing apparatus ...
|
|
WO/2020/217624A1 |
Provided is a control device that controls a flying body including a double-sided light-receiving solar battery panel provided on a main wing, the control device comprising: a positional relationship acquisition unit that acquires the po...
|
|
WO/2020/219980A1 |
A redundant power supply system for aircraft seats, includes: a first power supply module having a first AC to DC power converter configured to supply power to a first auxiliary board, the first auxiliary board being configured to supply...
|
|
WO/2020/219995A1 |
In one embodiment a solar array circuit is provided capable of being utilized in a high altitude long endurance aircraft. The solar array circuit includes a solar array string having a plurality of solar cells connected in series. Multip...
|
|
WO/2020/219765A1 |
Systems, devices, and methods including a first flight control computer (FCC) (112) of two or more FCCs (112, 113); a second FCC (113) of the two or more FCCs; at least one selector (182) in communication with the first FCC; and at least...
|
|
WO/2020/215362A1 |
The present invention discloses an intelligent parametric design method for wings of a miniature flapping-wing aircraft. The following steps are adopted to carry out the parametric design of the wings: (1) generating in the X-Y coordinat...
|
|
WO/2020/219900A1 |
A rotor blade pitch control system (15) comprising a rotor blade (19a, 19b, 19c, 19d) rotatable about both a central axis (20) and a pitch axis (24a, 24b, 24c, 24d), a pitch drive rotor (32a, 32b, 32c, 32d) rotatable about the central ax...
|
|
WO/2020/217004A1 |
A system for monitoring an aircraft engine, comprising: an acquisition module (3) for acquiring current measurements of physical size, referred to as input (ME) and output (MS) physical sizes, relative to the aircraft engine (15), a modu...
|
|
WO/2020/217607A1 |
Provided is a multicopter for painting that is suitable for painting a large structure or building of any shape.　The multicopter for painting (100) has: a multicopter (1); a frame (2) that is provided on the multicopter (1) and that is...
|
|
WO/2020/219998A1 |
In one implementation in a high altitude long endurance solar powered aircraft, a method for controlling a solar cell array is provided which includes determining an operating point of the of the solar array, including regulating a curre...
|
|
WO/2020/217497A1 |
The present invention provides an unmanned aerial vehicle that can easily connect a transported item to a tip of a wire member hanging down from an aerial vehicle body. An unmanned aerial vehicle 1 according to one aspect of the present ...
|
|
WO/2020/219278A1 |
A multi-rotor aircraft includes a fuselage, a propulsion engine coupled to the fuselage that generates thrust to propel the aircraft along a first vector during forward flight, and rotors coupled to the fuselage, each rotor comprising bl...
|
|
WO/2020/219112A1 |
An aircraft navigational system for a multiengine aircraft can include a flight planning module configured to receive two or more navigational points defining a route and determine if a first degraded operation ceiling is high enough to ...
|
|
WO/2020/217623A1 |
Provided is a control device for controlling an aerial vehicle having a double-sided light receiving type solar cell panel disposed on a main wing, the control device comprising: a positional relationship acquisition unit that acquires t...
|
|
WO/2020/218569A1 |
A nose fairing (10) is coupled to a main body (12) of a rocket (11) so as to be capable of separating therefrom. This nose fairing comprises: a pair of fairing pieces (40), (50) which are capable of separating after a prescribed time has...
|
|
WO/2020/218957A1 |
A method for type state estimation of a user equipment connected to a wireless communication network. The method comprises updating (S2), recursively, of a type state estimate. The type state estimate is a probability for the user equipm...
|
|
WO/2020/217007A1 |
The invention concerns an electrical energy supply network (1) of an aircraft equipped with a plurality of electrical loads (C1, C2) to be supplied, the supply network (1) comprising at least two generators (2, 3) of a turbogenerator of ...
|
|
WO/2020/217026A1 |
The invention relates to an air intake (3) for a nacelle (1) of an aircraft engine (6), the air intake (3) comprising a front lip (31) connecting a substantially cylindrical internal wall (32) and a substantially cylindrical external wal...
|
|
WO/2020/219994A1 |
In one embodiment, a solar powered high altitude long endurance aircraft power bus architecture is provided which includes a main DC power bus, with a battery connected to the main DC power bus. This embodiment includes a plurality of so...
|
|
WO/2020/216713A1 |
The present application relates to an air intake (2) for a turbojet engine nacelle comprising an annular structure (21, 22) and a rear bulkhead (23), the annular structure (21, 22) comprising at least one portion (21A) of an outer shroud...
|
|
WO/2020/215271A1 |
An unmanned vehicle is disclosed. The unmanned vehicle is equipped with a projection unit, which is configured to project a display image onto a remote plane so that the display image is visible on the remote plane surface. Accordingly, ...
|
|
WO/2020/217715A1 |
A movable body according to an embodiment of the present invention has an imaging unit, a first detection unit, and a control unit. The first detection unit detects the front surface direction of the movable body. The control unit contro...
|
|
WO/2020/168189A3 |
Wind speed and direction experienced by the UAV at altitude is determined by placing an accelerometer, gyroscope and compass on the UAV. A change in velocity experienced by the UAV is determined by the accelerometer. An orientation relat...
|
|
WO/2020/217340A1 |
This satellite constellation (200) is provided with three artificial satellites (210A-210C) which monitor a target region on the earth (101). Each artificial satellite has an elliptical orbit that is heliosynchronous and has an orbital i...
|
|
WO/2020/219111A1 |
A control system for a hybrid electric powerplant of an aircraft can include a master controller configured to receive one or more power settings and to output a heat engine setting and an electric motor setting and a heat engine control...
|
|
WO/2020/217058A1 |
The present disclosure pertains to an unmanned aerial vehicle system. Some exemplary implementations may include: a mounting frame (110) onto which at least a payload (30) is affixed; a plurality of fuel cell stacks (50) operable in a pr...
|
|
WO/2020/219415A1 |
A counter-rotating (CR) axial electric motor assembly is presented, with two oppositely rotating drive members, that is utilized to power any device that has traditionally employed an electric motor to supply rotational power.
|
|
WO/2020/219727A1 |
Systems and methods for mounting motors include a housing configured to secure motor supported by a motor support framework coupled to and housed within the housing. The motor support framework is suspended from the housing by one or mor...
|
|
WO/2020/215304A1 |
A sea-land-air-underwater adapted vehicle capable of vertical take-off and landing, comprising a fuselage (1), two main wings (2), auxiliary wings (3), a vertical tail wing (4), a rudder (5), a horizontal tail wing (6), elevators (7), a ...
|
|
WO/2020/218066A1 |
[Problem] To make it possible to automate inspection of an object by using a flying object. [Solution] An inspection system includes: a capturing information receiving unit for receiving an image of an object to be inspected that has bee...
|
|
WO/2020/217027A1 |
The invention relates to an air intake for an aircraft engine nacelle, the air intake comprising a front lip connecting a substantially cylindrical internal wall and a substantially cylindrical external wall, a front mounting flange conf...
|
|
WO/2020/215165A1 |
An impactor apparatus for use with a rotorcraft, comprises a reeling apparatus adapted to be transported by the rotorcraft, the reeling apparatus including at least a spool, an actuation system for rotating a spool in a winding direction...
|
|
WO/2020/217117A1 |
An aircraft (1, 1', 1''', 1'''', 1''''', 1'''''', 1''''''', 1'''''''', 1''''''''', 1'''''''''', 1''''''''''', 1'''''''''''', 1''''''''''''') capable of vertical take-off and landing is described, comprising a first propulsion unit (6a, 6...
|
|
WO/2020/216057A1 |
As the distance to a determined subject changes, it sometimes results in the inability to stably perform photographing control. The control device can include a circuit configured to apply a first contrast evaluation filter for an area c...
|
|
WO/2020/217662A1 |
The purpose of the present disclosure is to provide a home delivery box, a home delivery system, a flying body, and a home delivery method, with which theft prevention property can be improved. This home delivery box (2) comprises a case...
|
|
WO/2020/216737A1 |
An embodiment of the present invention provides an aerostructure assembly of an aircraft comprising a first aerostructure portion (201) extending in a direction between a first position (bl) and a second position (b2) and comprising stru...
|
|
WO/2020/217025A1 |
The invention relates to an air intake (3) for a nacelle (1) for an aircraft engine (6), the air intake (3) comprising a front lip (31) connecting a substantially cylindrical internal wall (32) and a substantially cylindrical external wa...
|
|
WO/2020/188604A3 |
The present invention discloses a VTOL aircraft with retractable wings and TEMCS (trailing edge mounted control surface) mounted tilt-able engines. The aircraft has two hover modes; a first hover mode with retracted wings which allows ta...
|
|
WO/2020/219818A1 |
An aircraft hoist system includes hoist equipment arranged in an aircraft, the hoist equipment including a motor, a cable, and a hook portion. The aircraft hoist system also includes at least one sensor configured to obtain measurements ...
|
