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Matches 1 - 50 out of 3,263

Document Document Title
WO/2018/187701A1
Some embodiments described herein relate to a drone landing platform. One or more sensors (122A) coupled to the drone landing platform (120A) can detect local conditions in the vicinity of the drone landing platform. A communications sys...  
WO/2018/183871A1
A carpet tile having a greige good, an adhesive layer, and a secondary backing material. The greige good has a primary backing component and a plurality of fibers attached to the primary backing component. The adhesive layer has an adhes...  
WO/2018/182797A1
This document describes a system and method through which unmanned aerial vehicles (UAVs) and other vehicles (e.g., unmanned underwater vehicles (UUVs), also known as autonomous underwater vehicles (AUVs), unmanned water-surface vehicles...  
WO/2018/182944A1
An autonomous drone integrated with wide bandwidth, high energy acoustic wave generators sent to evict and eradicate agricultural pests within a patrolling area. The drone hovering close to a plant bombards its leaves and fruits with hig...  
WO/2018/161646A1
A propeller protection apparatus (130), an arm (120), and an unmanned aerial vehicle (100). The propeller protection apparatus (130) comprises a protective rod (132), a connecting rod (134), and a holding portion (136). One end of the co...  
WO/2018/164710A1
A boarding guidance system includes a beacon (202A) associated with a passenger seat (400A). The beacon is configured to communicate (506) with a passenger guiding device (102) and determine a distance between the passenger guiding devic...  
WO/2018/158258A1
Aircraft Ground Proximity Detection The present invention provides a system for detecting proximity of a ground service equipement (GSE) to a stationary aircraft comprising at least one GSE monitoring device adapted to be mounted to a GS...  
WO/2018/155534A1
The present invention makes it possible for a worker to readily reach a damaged point of an airframe and serves to reduce downtime of the airframe required for repairs. The present invention includes: a damage discriminating unit (21) th...  
WO/2018/156335A2
Disclosed herein is a distributed pressure sensor system that quickly detects and counters changes in lift, onset of stall, and flutter. The distributed pressure sensor system may employ a plurality of integrated pressure ports distribut...  
WO/2018/155700A1
The present invention addresses the problem of providing a flight management system for managing flight plans of flying objects that fly between ports. This flight management system which is equipped with multiple port management devices...  
WO/2018/155536A1
In order to accurately detect damage in an aircraft (1), using only a small number of sensors, the present invention comprises: a classification creation unit (11) that places aircraft having similar usage environment information into th...  
WO/2018/149255A1
The present invention relates to intelligent warehousing technology. Provided in the present disclosure are a parachute system and a safety protection method for an unmanned aerial vehicle. The parachute system for an unmanned aerial veh...  
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/2018/144576A1
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/2018/140069A1
An ejectable flight data recorder for robust retention of flight data and aiding in locating an aircraft after an emergency situation comprises: a buoyant housing comprising an internal cavity, a door for access to at least a portion of ...  
WO/2018/133006A1
A landing gear control method and device for an unmanned aerial vehicle, user equipment unit, unmanned aerial vehicle, and unmanned aerial vehicle system. The method comprises: detecting whether a ground height of an unmanned aerial vehi...  
WO/2018/117878A1
The subject of the invention is a device protecting the flight data recorder ejected from an aircraft, whose task is to provide protection against physical damage of the flight data recorder during a plane crash and to assist reliable se...  
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...  
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...  
WO/2018/112404A1
Systems and methods are provided for autonomous airborne vehicle control using a millimeter-wave (MMW) radar. Embodiments of the present disclosure enable a MMW radar system to support an unmanned aerial vehicle (UAV) in accomplishing mi...  
WO/2018/104632A1
The present invention relates to a nacelle (41) for an aircraft turbojet engine, comprising a thrust-reversing device, said nacelle comprising: - a fixed structure (43) and - a movable structure (45), translatably movable along an axis (...  
WO/2018/103641A1
A retractable drone, comprising: a main cabin (1) and a motor blade mechanism; a left and a right side of the main cabin (1) are provided with a protective cover (2) respectively, and the protective cover (2) slidably connects the motor ...  
WO/2018/104584A1
The present invention discloses an apparatus for use in an emergency device (200), where the apparatus comprises a modem (121), a real time clock (131, 205), a positioning functionality, the power enabled emergency device (200) moving fu...  
WO/2018/098774A1
An apparatus, method and device for controlling forced landing. The method for controlling forced landing comprises: obtaining a signal for indicating power loss or partial power loss of an unmanned aerial vehicle; and when the signal fo...  
WO/2018/087671A1
The present disclosure provides an aircraft (10), as well as systems and methods for reducing current flow to electrical systems onboard an aircraft (10). A signal return network (220) is spaced from a composite structure (210) and first...  
WO/2018/086483A1
An impact damper device comprises at least one rubber and air-based shock absorber set (1) arranged in a support frame comprising a fixed plate (6) and a blocking plate (5) arranged in parallel and aligned with each other, and connected ...  
WO/2018/083337A3
The invention relates to a drone deployment system, an emergency protection device, a drone and a delivery chute. The drone deployment system comprises a container that can be transported by means of a vehicle, such as a lorry, train or ...  
WO/2018/083337A2
The invention relates to a drone deployment system, an emergency protection device, a drone and a delivery chute. The drone deployment system comprises a container that can be transported by means of a vehicle, such as a lorry, train or ...  
WO/2018/085839A1
Systems and methods of forming fiber reinforced polymer (FRP) composites with electrostatic dissipative properties are described herein. The FRP composite is bonded to a surface and integrates a grounding system to dissipate electro-stat...  
WO/2018/084125A1
[Problem] Provided is a drone with an airbag with which it is possible to prevent the danger of injuring a person when a crashed drone collides with the person. [Solution] A first airbag 11 is provided in a state surrounding a drone 9 wi...  
WO/2018/076468A1
A shielding apparatus (50) and an unmanned aerial vehicle (100), the shielding apparatus (50) being used in the unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises a global positioning system module (40), and the s...  
WO/2018/076467A1
An alarm system (100), applied to a movable platform. The alarm system (100) comprises a sounding device (12) and a control unit (15). The control unit (15) is connected to the sounding device (12), and controls the sounding device (12) ...  
WO/2018/075903A2
An aerial vehicle comprising an airframe, an aircraft flight controller to provide an output control signal, and a planar printed circuit board positioned on the airframe. The printed circuit board may include coupled thereto a processor...  
WO/2018/075903A3
An aerial vehicle comprising an airframe, an aircraft flight controller to provide an output control signal, and a planar printed circuit board positioned on the airframe. The printed circuit board may include coupled thereto a processor...  
WO/2018/066043A1
Provided is a delivery rotary-wing aircraft capable of stably landing on a destination free of influence from an updraft occurring in a region, such as tall buildings. This rotary-wing aircraft comprising a plurality of rotary wings, a c...  
WO/2018/061280A1
A flight restriction setting system according to an embodiment comprises a damage detection unit and a flight restriction calculation unit. The damage detection unit detects damage that occurred on a structure that constitutes an aircraf...  
WO/2018/064657A1
An unmanned aerial vehicle (UAV) landing system is disclosed. The UAV landing system includes a memory; an imaging device; and a processor in communication with the memory and imaging device, wherein the processor is configured to: acqui...  
WO/2018/053994A1
Embodiments include devices and methods for adaptive image processing in an unmanned autonomous vehicle (UAV). In various embodiments, an image sensor may capture an image, while a processor of the UAV obtains attitude information from o...  
WO/2018/055827A1
A damage detection system according to an embodiment comprises a physical quantity detection unit, a flight condition changing unit, and a damage detection unit. The physical quantity detection unit detects the physical quantity of a str...  
WO/2018/051572A1
[Problem] To achieve a stable airspeed control that takes remote turbulence into account. [Solution] This aircraft speed information providing system is provided with: an airspeed measurement device that measures the present airspeed of ...  
WO/2018/048774A1
Described herein are methods and systems to dampen oscillations of a payload coupled to a tether of a winch system arranged on an unmanned aerial vehicle (UAV). For example, the UAV's control system may dampen the oscillations by causing...  
WO/2018/045413A1
There is provided a system for determining real-time parameters of an aircraft, the system comprising: at least two sensing apparatus, each of the at least two sensing apparatus including a plurality of in-ground sensors; and at least on...  
WO/2018/045661A1
An information protection method for an unmanned aerial vehicle, the unmanned aerial vehicle comprising an ARM controller (1) and an information protection module (4). The method comprises: an ARM controller (1) transmitting, back to a c...  
WO/2018/048627A1
Some embodiments provide an aerial monitoring system to monitor a geographic area, comprising: a unmanned aerial vehicle (UAV) comprising: a plurality of lift motors to drive a propeller; a substructural support supporting the lift motor...  
WO/2018/042927A1
[Problem] To provide a mechanism of radio communication for a device that flies around freely in a three-dimensional space. [Solution] A circuit provided with: an acquisition unit that acquires information relating to a flight; and a mea...  
WO/2018/044243A8
This invention is system designed in particular to separate the plane's black box (data recording box) in case of being exposed to an accident that causes its drowning in the sea, ocean, or, elsewhere waters, yet in a following step to t...  
WO/2018/044243A1
This invention is system designed in particular to separate the plane's black box (data recording box) in case of being exposed to an accident that causes its drowning in the sea, ocean, or, elsewhere waters, yet in a following step to t...  
WO/2018/041253A1
A black box control method comprises: acquiring current flight data of an aircraft, wherein the flight data comprises a collision signal, a loss-of-control signal, and a stall signal; determining, according to the flight data, whether th...  
WO/2018/038441A1
An electronic device is provided. The electronic device includes a gimbal; a first camera; a second camera to detect a point of interest on ground; at least one sensor; a first motor; a second motor to operate the first camera and the se...  
WO/2018/032264A1
An unmanned aerial vehicle machine body anti-collision structure, comprising a machine casing (1), an inner side wall of the machine casing (1) being fixedly provided with a buffer box (2), a side wall of the machine casing (1) being pro...  

Matches 1 - 50 out of 3,263