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WO/2018/234523A1 |
The invention relates to a method for detecting damage to a rotor of an aircraft, wherein the aircraft has actuators for actively reducing vibration, the method comprising the steps: determining actuator manipulated variables in a refere...
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WO/2018/230552A1 |
An assist system (10A) comprises: a detection unit (12) mounted in an aircraft capable of hovering, the detection unit (12) being provided on the outside of the fuselage (31), and detecting objects that could be obstacles; imaging units ...
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WO/2018/232196A1 |
The present disclosure relates to aircraft and aircraft flight control systems, methods, and apparatuses. A condition-aware aircraft configured to make in-flight decisions autonomously, based on the most up-to-date information, to perfor...
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WO/2018/223378A1 |
An unmanned aerial vehicle control method and device, and an unmanned aerial vehicle. The method comprises: acquiring state information about an unmanned aerial vehicle (S101); determining a control instruction according to the state inf...
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WO/2018/217210A1 |
A method for providing adaptive control to a fly-by-wire aircraft includes measuring via at least one first sensor a characteristic of at least one component of the aircraft and measuring via at least one second sensor a state of the air...
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WO/2018/196494A1 |
An unmanned aerial vehicle control method and device and an unmanned aerial vehicle, belonging to the technical field of unmanned aerial vehicle control. The method comprises: monitoring the running state of each power motor in an unmann...
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WO/2018/195214A1 |
An autonomous distress tracking system for an aircraft is described. The system can include a transponder configured to transmit radio frequency (RF) emissions and an RF detector unit configured to detect the RF emissions. The system can...
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WO/2018/189299A1 |
An uplock (101) for use with an aircraft component. The uplock comprises a hook (102) configured to engage a capture pin (126) mounted on the aircraft component. The hook (102) is mounted for movement between a closed position and an ope...
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WO/2018/189249A1 |
The invention relates to a device (1) for measuring rotor blade movements of an aircraft over the entire rotor rotation in flight, having at least one rotatably arranged rotor blade (2) and an image recording unit (4) for recording image...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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/2018/110088A1 |
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/2018/112404A1 |
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...
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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 (...
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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 ...
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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...
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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...
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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...
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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 ...
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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 ...
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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...
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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...
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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...
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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) ...
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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...
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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...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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