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WO/2018/114545A1 |
Electromechanical device for actuating a movable flight surface (11, 12) having an envelope (20) articulated to an aircraft structure about an axis of rotation (21), comprising: – at least two electric motors (51) for rotating the enve...
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WO/2018/112847A1 |
A control device (10) for controlling a unmanned aerial vehicle (2), comprising: a brainwave collection device (100) for collecting a brainwave signal of a user; a processor (102), which is in communication connection with the brainwave ...
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WO/2018/115540A1 |
The invention relates to a connection/separation device (1) for separating satellites from shuttles or satellite dispensers, which comprises: a plurality of clamps (2, 2') aligned circumferentially and couplable by the internal face ther...
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WO/2018/112907A1 |
Disclosed is a gimbal structure, comprising a gimbal support (1) and a reflective mirror (5) arranged on the gimbal support (1), wherein the gimbal support (1) is used for fixing a photographing device (6) and enables the photographing d...
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WO/2018/113134A1 |
A multi-rotor unmanned aerial vehicle (100), comprising a main vehicle assembly (10) and a plurality of rotor assemblies (20). Each rotor assembly (20) comprises a servomotor (21), a connecting arm (22), and a rotor unit (23). The main v...
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WO/2018/116977A1 |
This seat guide device is equipped with: a plurality of tracks (31) provided in parallel with one another; and a plurality of moving elements (32) which are connected to a plurality of leg parts (15) of a seat and are attached to the tra...
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WO/2018/115334A1 |
The invention relates to a device for locating a drill head of a ground drilling device, comprising a wireless probe, the probe being arranged on or in a flying object.
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WO/2018/117262A1 |
The present invention relates to a double-sided adhesive tape provided with a layered structure having an adhesive layer (IA), a base material, and an adhesive layer (IIA) in that order. A flame retardant (C) is included in adhesive laye...
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WO/2018/112723A1 |
A light source energy boosting system, comprising a reflection propelling unit (120, 220), a light source power unit (110, 210) and a feedback device (140, 240), and characterized in that: the light source power unit (110, 210) comprises...
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WO/2018/116926A1 |
A device-securing apparatus capable of easily changing the securing position at which a device is secured to the floor surface or the like of a structure, the device-securing apparatus being equipped with: a track rail (10) which has a p...
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WO/2018/115651A1 |
An accumulator (23) designed to damp the pressure waves of the hydraulic shocks originating in a downstream section (22) of a duct (2) is arranged inside the duct, with the opening (28) of the accumulator pointing downstream. This result...
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WO/2018/115180A1 |
The present invention relates to a nano-satellite bus, characterized in that it comprises: -a mono-bloc mechanical frame (1) comprising a plurality of posts and edges (2, 2') forming the sides of the said mechanical frame; -a back panel ...
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WO/2018/115498A1 |
System (100) for determining a level of nuisance generated by an industrial installation (200), characterized in that it comprises at least one aerial drone (300), said aerial drone being controllable to move to a measurement point above...
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WO/2018/116083A1 |
An assembly for connecting an engine to an aircraft, including a first support configured to be structurally connected to the engine, a second support configured to be structurally connected to the aircraft, and a thrust link. The thrust...
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WO/2018/118192A1 |
The present disclosure relates to systems and methods for operating aerial vehicles in water-based locations. As an example, a system may include a plurality of landing stations. Each landing station of the plurality of landing stations ...
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WO/2018/113519A1 |
A pan-tilt (1) for an unmanned aerial vehicle, and an unmanned aerial vehicle. The pan-tilt (1) for an unmanned aerial vehicle comprises a first fixed device used for being fixedly mounted on an unmanned aerial vehicle body, a first conn...
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WO/2018/116084A1 |
A hinge assembly for receiving a door, for example for an aircraft storage bin, and including a wall having opposed inner and outer surfaces, an edge of the wall including two spaced apart wall panels extending from a respective one of t...
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WO/2018/115099A1 |
The present invention relates to a passenger boarding bridge, comprising, - a tunnel (2) having a first tunnel section (3) and a second tunnel section (4), the tunnel sections (3, 4) can be telescoped for adjusting the length of the tunn...
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WO/2018/118383A1 |
An innovative passive cooling solution with sealed UAV enclosure system allows heat from a semiconductor chip to be dissipated to the ambient environment through evaporation/condensation phase-change cooling and air cooling a heat sink s...
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WO/2018/118018A1 |
An acoustic panel (200) for an aircraft nacelle (100) may comprise a perforated first skin (220), a second skin (230), and a core (210) sandwiched between them. A camera system (330) may scan a perforation pattern of a damaged portion (3...
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WO/2018/119436A1 |
A multi-layered intelligent display system includes a first LCD display panel; a second OLED display panel; a smart panel disposed behind the second display panel; an LED panel disposed between the second display panel and the smart pane...
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WO/2018/117627A1 |
An unmanned aerial vehicle (UAV) is provided. The UAV includes a first guard grill, a second guard grill configured to be removably combined with the first guard grill and form an external structure and an inner space of the UAV with the...
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WO/2018/118070A1 |
A set of commands for each of a plurality of actuators to alter an aircraft's state responsive to one or more inputs is produced. The set of commands is provided to fewer than all actuators comprising the plurality of actuators.
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WO/2018/116976A1 |
This linear movement guide device (30) is provided with a track rail (31), a slider block (32) attached to the track rail so as to be capable of movement relative thereto via a plurality of rolling bodies, and a position-determining pin ...
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WO/2018/118199A1 |
The present disclosure relates to systems and methods for operating aerial vehicles in water-based locations. Specifically, an exemplary system may include a floating tether station and an aerial vehicle coupled to the floating tether st...
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WO/2018/117592A1 |
Disclosed is an electronic device comprising: a housing; a seating portion formed inside the housing such that a first external electronic device and a second external electronic device are seated thereon; at least one interface that is ...
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WO/2018/117851A4 |
The present document discloses method, system and device for maritime pilotage involving a pilotage control center where a request for pilotage assistance for a vessel is received. After negotiating the request and - if agreed - the foll...
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WO/2018/114659A1 |
A method for producing a wind turbine rotor blade (200) is disclosed. The wind turbine rotor blade (200) has at least one inner blade section (210) and an outer blade section (220) as well as a connection element (600). The inner blade s...
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WO/2018/112637A1 |
The present disclosure relates to a mechanism for releasably securing components of a spacecraft together during launch until such time as the mechanism is commanded to release those components. Upon command, the components are then rele...
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WO/2018/111358A1 |
A launching system may include a multirotor platform that includes a plurality of motors and propellers. The multirotor platform may be launched from a launch tube and actuated to transition from a storage state to a flight state where t...
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WO/2018/108148A1 |
An unmanned aerial vehicle, comprising a fuselage (1) and multiple arms (2) disposed at left and right sides of the fuselage (1), said unmanned aerial vehicle also comprising a sliding mechanism; open grooves (3,11) are provided on the f...
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WO/2018/109582A1 |
A slat (50) for an aircraft wing comprises a leading edge (51) defining a leading edge line (61), a trailing edge (52) defining a trailing edge line (62), the leading and trailing edges line defining a slat plane, the chord distance (69)...
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WO/2018/110848A1 |
An electronic device is provided. The electronic device includes a communication circuit configured to establish a communication channel with an aerial vehicle, a sensor configured to collect location information and orientation informat...
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WO/2018/109251A1 |
The invention relates to a liftable truck container (1) for supplying aeroplanes, which comprises a rolling chassis (2) with stabilising feet (3) where a structure (4) and covering (5) of the container (1) is mounted, the covering (5) ha...
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WO/2018/110382A1 |
Provided is a flying device having: an acquisition unit that acquires communication quality information in which position information indicating a position and the communication quality at the position indicated by the position informati...
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WO/2018/110788A1 |
The present invention relates to a shooting system using a drone, and disclosed is a shooting system using a drone, which comprises a laser gun and a sensor capable of receiving laser light instead of a shotgun and a pigeon used in a con...
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WO/2018/108834A1 |
A propulsion system for a vehicle (10) includes a propulsor (102) for generating a thrust for the vehicle, a motor (104) operable with the propulsor for driving the propulsor, a motor mount (164) for mounting the motor in or to the vehic...
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WO/2018/110650A1 |
A moving body (2) is provided with a main body (21), a propulsion engine (22), and an energy supply unit (3). The propulsion engine (22) propels the main body (21). The energy supply unit (3) supplies energy to the propulsion engine (22)...
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WO/2018/111059A1 |
The invention relates to the field of transport by air and water and to power engineering, in particular to designs of bladed propellers. A rotating-blade propeller comprises a plurality of blades which are independently connected to spi...
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WO/2018/112161A2 |
Systems and methods for reducing switching losses in an electrical system in an aircraft are provided. In one example implementation, a method can include receiving DC power at an inverter of an electrical power system of an aircraft. Th...
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WO/2018/107972A1 |
An arm and an unmanned aerial vehicle, the arm comprising a first arm segment (11) and a second arm segment (12), the first arm segment (11) being provided with a locking part (112) and the second arm segment (12) being provided with a l...
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WO/2018/108616A1 |
The invention relates to a longitudinal adjustment device (50) for a seat, particularly an aircraft passenger seat, said longitudinal adjustment device (50) comprising at least one rail arrangement (100), said rail arrangement (100) comp...
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WO/2018/110088A1 |
An unmanned aircraft 1 according to one embodiment of the present invention is able to properly make an emergency landing in case of an abnormality. The unmanned aircraft 1 is configured as a multicopter which flies with the lift and thr...
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WO/2018/109255A1 |
The invention relates to a method for producing reinforced monocoque structures and to the structure obtained, the method comprising: using base components (1) made from a partially cured composite material and joining the base component...
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WO/2018/111101A1 |
An insect elimination system eliminates a flying insect in an airspace. The system comprises: - a camera configured to provide image data representative of at least part of the airspace; - an unmanned aerial vehicle, UAV, comprising a pr...
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WO/2018/107564A1 |
Disclosed is an unmanned aerial vehicle, comprising a fixed-wing fuselage (10), a fixed-wing power assembly (20) and multiple rotor power assemblies (30). The fixed-wing power assembly is provided on the fixed-wing fuselage. The multiple...
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WO/2018/111360A1 |
Unmanned aerial vehicles and flight planning methods and apparatus are disclosed. An example apparatus includes an unmanned vehicle including a body and a propulsion source to propel the unmanned vehicle during flight; and a route planne...
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WO/2018/107956A1 |
Provided in the present invention is an unmanned aerial vehicle and a power assembly thereof, a propeller and a propeller base assembly. The power assembly comprises a drive device, a propeller, and a propeller base assembly. The propell...
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WO/2018/110308A1 |
This flapping device (1A) is provided with: a power source (20); a power transmission mechanism (30); wing bodies (40R, 40L) driven by the power transmission mechanism (30); a first biasing part (60A); and a second biasing part (60B). Th...
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WO/2018/107416A1 |
A manually operable mechanism for mechanically and electrically connecting parts of an unmanned aerial vehicle (UAV) comprises a first engaging means (20) associated with a first part of the UAV including at least one first electrical co...
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