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Patent Searching and Data


Matches 551 - 600 out of 61,901

Document Document Title
WO/2018/152174A1
Systems and methods are described for registering and monitoring a status of a plurality of units of an in-flight entertainment system disposed within a vehicle. Using a portable computing device, each of the units can be registered with...  
WO/2018/151712A1
An aerial vehicle can proceed to a target location upon receiving a message based on a ground vehicle being at an aerial vehicle deploy location. A user can be identified from an image captured at the target location. The aerial vehicle ...  
WO/2018/151576A1
A system, devices and method are disclosed herein. The system may include a network interface, a memory, the two devices and a processor, which implements the method. The method may include receiving by a first device a location of a sec...  
WO/2018/149182A1
A pan-tilt and an unmanned aerial vehicle. The pan-tilt comprises: a first circular member (60); a second circular member (66), the second circular member (66) being fitted outside the first circular member (60); a rotational member (70)...  
WO/2018/150226A1
An ammunition container (200) loading device (10) is provided for attachment to a weapon mount (100). The ammunition container (200) loading device (10) comprises a first tray (20). The first tray (20) comprises a supporting base part (2...  
WO/2018/152525A2
Disclosed is a networked array of radar enclosures that can be arranged to cover a desired geographical location. The array can detect moving objects in the coverage area. When warranted, elements of the array can also control the moveme...  
WO/2018/150332A1
A system comprising, a plurality of unmanned aerial vehicles and a single controller for controlling said plurality of unmanned aerial vehicles, wherein the single controller is configured such that it can broadcast a command to all of t...  
WO/2018/150883A1
Provided is a capturing system for capturing an object to be captured in outer space, wherein the success rate of missions is increased at low costs. This capturing system 1 for capturing an object T to be captured in outer space compris...  
WO/2018/151990A1
Aerial vehicles may be configured to control their attitudes by changing one or more physical attributes. For example, an aerial vehicle may be outfitted with propulsion motors having repositionable mounts by which the motors may be rota...  
WO/2018/151729A1
A container includes a transportation section and a drone section. The drone section has a drone place holder and a door. The drone place holder is accessible when the door is in an open position. The container includes a processor that ...  
WO/2018/151777A1
A vertical take-off and landing aircraft which uses fixed rotors for both VTOL and forward flight operations. The rotors form a synthetic wing and are positioned to achieve a high span efficiency. The rotors are positioned to even out th...  
WO/2018/146406A1
The invention relates to a device for retaining a panel (9), such as panel with a curved profile. The device comprises a frame (10) having two side-members (11) and two cross-members (12), as well as a system (2) for adjusting the shape ...  
WO/2018/145356A1
A modularized driving component and a combined model. The modularized driving component comprises power modules (10) and a control module (20) that are independently separable. The power modules (10) are used for generating a driving for...  
WO/2018/147760A1
The invention relates to spacecraft of the platform type, developed in accordance with the CubeSat standard. The present spacecraft comprises a body in the shape of a parallelepiped and consisting of an upper panel and side panels, faste...  
WO/2018/146548A1
An aerial system, preferably including one or more housings. A housing for an aerial system, preferably including: a first and second piece that cooperatively surround one or more propellers of the aerial system; and a retention mechanis...  
WO/2018/145261A1
A multifunctional camera, comprising a connector (1), at least two rotation members (2) respectively disposed on the connector, and a rotation member driving mechanism. Each rotation member is provided with a camera body (100) correspond...  
WO/2018/146422A1
The invention relates to a method for controlling the speed and the power of a turbine engine propeller, wherein at least two operating modes are implemented: - one operating mode, called "speed mode", in which the pitch (β) of the prop...  
WO/2018/147535A1
Provided is a wind power generation system using a jet stream, implemented by including: an aerial vehicle flying in the air without a winch so as to produce electric power through wind power generation while performing an autonomous fli...  
WO/2018/146528A1
A drone (10), a system of drones and a method for using a drone, where the drone is configured to support an object, is disclosed. The drone includes a first base portion (12a) having a first inner wall (14a), a second base portion (12b)...  
WO/2018/145675A1
Tail sitter aircraft, comprising a fuselage (4) and a pair of wings (5), each wing having a leading edge (50) and a trailing edge (55), wherein each of the wings (5) is provided with a propeller propulsion unit and a plurality of control...  
WO/2018/147810A1
According to various embodiments, there is provided an aircraft including: a fuselage defining a body frame with longitudinal, lateral and height axes extending perpendicular to each other and intersecting in a center of gravity of the a...  
WO/2018/148248A1
Disclosed herein is a booster aircraft system having a host aircraft and one or more booster UAVs coupled thereto. When necessary, such as during takeoff and climb of the host aircraft, the booster UAVs operate to boost the thrust of the...  
WO/2018/146503A1
Recovery Method and Device for damaged Large Passenger Aircraft Recovery of damaged airliners is performed by supporting it with a raster of pre-assembled scaffolds (2) with extendable stamps (19) and load-sensing headpieces (29), furthe...  
WO/2018/147925A1
A satellite system operates at altitudes between 100 and 350 km relying on vehicles including a self-sustaining ion engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are...  
WO/2018/146031A1
The invention relates to a stamping lacquer composition for riblet structures based on a prepolymer composition, which comprises a system of: a) at least one photoinitiator having an absorption range in the long-wave UV range and b) at l...  
WO/2018/145355A1
A vertical take-off and landing aircraft having fixed wings, comprising a fuselage (100), wings (210) symmetrically distributed relative to the fuselage (100), and vertical tails (310) vertically connected to the wings (210) and symmetri...  
WO/2018/146862A1
Provided is a fan blade which is made of a composite material and which will not suffer damage even if a large foreign object collides with the fan blade. A fan blade (20) is provided with a blade body (21) composed of a composite materi...  
WO/2018/148636A1
An unmanned aerial vehicle includes an atmospheric sensor configured to measure an atmospheric condition. The unmanned aerial vehicle includes a rotor motor configured to drive rotation of a propeller of the unmanned aerial vehicle. The ...  
WO/2018/145173A1
A device (10) for adjusting the control surfaces (40) of an aircraft (50) is described, comprising an elongate structural body (20) formed by a base (201) arranged on a first end (22) and attached to the structure of the aircraft (50) an...  
WO/2018/147522A1
The present invention relates to a flying lighting device having a heat dissipation part provided in a gimbal, the device being capable of: minimizing a region, at which light has not been emitted because of shadow, by emitting light abo...  
WO/2018/146220A1
The invention relates to a small satellite (10) which is capable of formation flying, in particular a nanosatellite or picosatellite with a mass weight of 10 kg or less, for LEO applications, comprising a housing (12) and at least one in...  
WO/2018/144960A1
Containment vessels are adapted to facilitate blast and dispersion mitigation. According to one example, a containment vessel may include at least one containment layer. At least one expansion member may be coupled to the at least one co...  
WO/2018/141072A1
An inflatable, amphibious landing gear comprising one or more inflated pontoons with wheels attached and with one or more air bladders below each inflated pontoon. When the air bladders are inflated, they extend below the wheels and prov...  
WO/2018/144080A1
Systems and methods for integrated power and thermal management in a turbine-powered aircraft are provided. The systems may include rotationally-independent first and second auxiliary power unit shafts, a power turbine, a first compresso...  
WO/2018/145132A2
A method and apparatus for removing a coating from a gas turbine engine component enabling repair of the component, including application of a braze alloy, without fluoride ion cleaning uses electrolytic stripping of the component in an ...  
WO/2018/144000A1
A vehicle jump start system includes an aerial drone including first and second electrically conductive end effectors electrically connected to a power source.  
WO/2018/141470A1
The invention relates to a method for producing electric energy by means of a fuel cell system operated using a reformate gas, said method comprising the following steps: preparing a fuel cell system with a first reactor (R1) for convert...  
WO/2018/142725A1
Provided are an attachment device for an aircraft landing guidance flashlight and an aircraft landing guidance flashlight device, whereby adjustment of the angle of the flashlight is not required when the aircraft landing guidance flashl...  
WO/2018/141843A1
A base unit (1), e.g. a luminaire, comprises fixation means (3, 5, 15) configured to fixate a module (11), e.g. a light module, in the base unit. The fixation means, e.g. comprising one or more protrusions (15), one or more recesses (3) ...  
WO/2018/144544A1
A daisy-chain aerial vehicle includes at least two component aerial vehicles. Each component aerial vehicle includes at least one wing having a wing body, a trailing edge, and a wingtip, the wing body shaped like an airfoil. At least one...  
WO/2018/142319A1
A device (1) is described for braking the fall of a load comprising a sling (2) and a braking element (3, 30), said sling (2) comprising a first end (21) constrainable to an anchoring point; a second end (22) constrainable to said load; ...  
WO/2018/142402A1
Apparatuses for a projectile are provided, the projectile configured for weapons barrel launching, examples of the apparatus comprising a body, an inflation system and external walls. The body is inflatable by the inflation system, from ...  
WO/2018/144915A1
A system and method for resisting an uncontrolled descent or uncontrolled flight condition of an aerial vehicle. The system includes a control system, sensors, an inflation device, and a descent-restraint system. The control system detec...  
WO/2018/142925A1
An in-flight battery changing method for multicopters according to an aspect of the present invention is provided with: a first step of securing a supply path for supplying a battery between both multicopters while both a supply-side mul...  
WO/2018/144929A1
A method for image generation, preferably including: generating a set of mission parameters for a UAV mission of the UAV associated with aerial scanning of a region of interest; controlling the UAV to perform the mission; generating an i...  
WO/2018/142470A1
[Problem] To provide a camera control device that enables a photographer to intuitively and easily control a camera mounted to a drone. [Solution] This camera control device 9 transmits a camera control signal to a panning-direction driv...  
WO/2018/144576A1
A technique for adaptively disrupting UAVs detects a target UAV using a camera, monitors the target UAV's communications using a directional antenna aligned with the camera, and attempts to communicate with the target UAV to request that...  
WO/2018/142058A1
Clevis (100), particularly for a turbomachine, comprising a body (102) comprising means (104) of attachment to a casing (105) and at least one aperture (106) for fitting a hinge pin, characterised in that said body is formed in one piece...  
WO/2018/142246A1
A backup actuation control unit for controlling an actuator dedicated to a given surface. The backup actuation control unit comprises a processing unit operatively connected to one of a flight control computer and a backup flight control...  
WO/2018/143860A1
The invention relates to a method for the application of heating mats (10) on a wing/blade of a wind power station or other devices for the purpose of achieving deicing also during operation when necessary. Temperature measurement and de...  

Matches 551 - 600 out of 61,901