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Patent Searching and Data


Matches 1 - 50 out of 55,807

Document Document Title
WO/2017/069816A1
A spacecraft (10), such as a satellite, uses a shape memory polymer actuator (18) to deploy one or more deployable parts (14). The shape memory polymer actuator may be formed integrally with a deployable part and/or with a fuselage (12) ...  
WO/2017/067409A1
A seating unit (202, 204) is disclosed as including a first seat (206, 210) and an adjacent second seat (208, 212), the seating unit (202, 204) being convertible between a first configuration in which each of the first seat (206, 210) an...  
WO/2017/067034A1
A microminiature impact monitoring system with ultra-low power consumption based on diode array digitization, relating to the technical field of structural health monitoring of aircrafts. The monitoring system consists of a microminiatur...  
WO/2017/067659A1
The invention relates to an actuating drive (1) for a high-lift system of an aircraft, which actuating drive has an integrated cone brake as a return stop, comprising a brake body (20) mounted on a shaft (12) of the actuating drive for c...  
WO/2017/069524A1
The present invention relates to a flight unit-based freight falling apparatus and a system using the same, and more particularly, to a flight unit-based freight falling apparatus and a system using the same that are capable of safely de...  
WO/2017/067383A1
A seating unit (102, 104) is disclosed as including a seat (106, 110) with a seat back (106a, 110a) and a seat pan (106c, 110c) which are movable relative to each other to convert the seat (106, 110) between a sittable configuration and ...  
WO/2017/067968A1
The invention relates to an aerodynamic body (114) comprising a main part (122) that has an upper face (124) which is designed such that a fluid (128) flows (126) over the upper face in a flow boundary layer (130). The main part (122) ha...  
WO/2017/069320A1
According to the present invention, disclosed is an aerial photographing device comprising: a body part (110) having a streamlined appearance and having a rotation shaft (111) arranged upright on an upper part thereof; a head part (120) ...  
WO/2017/068292A1
The invention relates to an aircraft having at least one wing (5) including, at each end thereof, a fin (6) forming an angle of between 0° and 45° relative to the vertical. According to the invention, each fin (6) has a leading edge (7...  
WO/2017/070648A1
An apparatus is provided including an unmanned aerial vehicle and a transformer monitoring device, particularly for use in a smart grid network system to support a wireless mesh network in the smart grid network and to collect metering d...  
WO/2017/068335A1
An aircraft emergency control system comprises at least one sensor (104A, 104B, 104C) configured to output an electronic signal relating to detection of incapacitation of at least one aircraft crew member. A processor (108) is configured...  
WO/2017/068224A1
The invention relates to a biomimetic and zoosemiotic unmanned aircraft comprising sensors and means for detecting and chasing away animals, essentially characterised in that it is equipped with an open source programmable automatic pilo...  
WO/2017/070186A1
A leg support includes a support element. A reinforcing element is disposed on the support element. The support element is chemically compatible with the reinforcing element. A homogeneous chemical bond is formed between the support elem...  
WO/2017/068998A1
The present disclosure relates to a flight control device, a flight control method, a multicopter, and a program that enable stable flight control. A pixel signal of a partial region of an image acquisition range in an acquired image is ...  
WO/2017/068141A1
The invention relates to a system adapted for providing an operator with augmented visibility, useful in particular to aid aircraft piloting, comprising at least one sensor able to capture image data in a given spectral band and a centra...  
WO/2017/067894A1
The present invention is concerned with an in-aircraft mobility system. In order to assist passengers having limited mobility on board aircraft and to make the use of an on-board toilet as simple as possible, an in-aircraft mobility syst...  
WO/2017/068325A1
A vehicle (10), for transporting a payload (100), and which comprises propulsion means (15) operable to move the vehicle (10) in a horizontal direction; a terrain engaging portion (50); and a support leg (40) with an upper end (41) pivot...  
WO/2017/067412A1
A multi-rotor aircraft comprises: an airbag, comprising a bag body (510); a multi-rotor system, comprising a main support (520) located in an internal space of the airbag, a plurality of motors (550) and a plurality of propellers (560) w...  
WO/2017/069331A1
The present invention relates to a hydrogen recycling flight system and flight method and comprises: a flight fuselage having at least one pair of wings at both sides of the fuselage; a hydrogen gas balloon air-tightly connected to the f...  
WO/2017/068484A1
Class dividers for aircraft passenger cabins comprising pivoting luggage bins (20) are disclosed. The class divider comprises a curtain (24B) mounted inside the passenger cabin to extend into a space allotted for movement of the pivoting...  
WO/2017/069617A1
Dielectric barrier discharge DBD system for an air¬ foil of a wind turbine or an airplane, at least comprising a first exposed electrode, a second encapsulated electrode, and a material separating said electrodes and positioned between ...  
WO/2017/068036A1
Disclosed is a multicopter aircraft comprising at least two drive rotors, the resultant dimensions of the rotor surfaces of the drive rotor(s) (1) on a load side (3) of the multicopter aircraft being significantly greater than the result...  
WO/2017/068871A1
[Problem] To propose a novel and improved information processing device, information processing method, and transportation system which are capable of implementing more stable transportation of goods, with regard to transportation of goo...  
WO/2017/068102A1
The invention concerns a flight control device (1) for an aircraft, comprising: - a housing (2), - a handle (4) mounted rotating relative to the housing (2) about a centre of rotation (O), - a first drive shaft (31), a second drive shaft...  
WO/2017/068246A1
According to the present invention, the device, which is provided with a male element (1) secured to one of the parts (P1) and a female element (2) secured to the other of said parts (P2), comprises a plurality of resilient fastening str...  
WO/2017/068497A1
A method of forming a composite part (10) having a skin (12) and at least one elongated stiffener (14) extending from the skin (12), the method comprising: providing a mold (20) having a mold surface (22, 26) and a respective elongated c...  
WO/2017/069728A1
A propulsion system includes at least one group of electric thrusters that are spatially distributed in a multi-axis system. A controller is in communication with each of the electric thrusters. The controller is configured to differenti...  
WO/2017/068154A1
The invention relates to an actuator (10) including a magnetohydrodynamic wheel (20) comprising a fluidic ring and at least one magnetohydrodynamic pump for moving a conductive liquid. Each magnetohydrodynamic pump comprises a means for ...  
WO/2017/064411A1
The invention relates to a tool (10) for handling an aircraft turbojet pod, the tool (10) including a frame (14) that comprises at least one top support bar (16a) that is hinged about at least one first top axis (A) of rotation by means ...  
WO/2017/064209A2
An aircraft fuel tank inerting system (100), comprising an oxygen absorption unit (30) containing a Cobalt or a Cobalt derived material.  
WO/2017/065411A1
The present invention relates to a drone charging platform system for charging a drone which flies the sky by using battery power and, more specifically, to a drone charging platform system configured to selectively provide charging serv...  
WO/2017/065594A1
The present invention relates to a surveillance system and method using drones. The surveillance system using drones according to the present invention may comprise: a drone unit configured to move autonomously in accordance with a prese...  
WO/2017/063088A1
A rotary wing aircraft having dual main rotor assemblies, wherein each main rotor is positioned laterally on linkages and are equidistant in a transverse direction from either side of the fuselage. The rotational axis of each rotor is mo...  
WO/2017/066662A1
Disclosed is a technique for landing a drone using a parachute. The technique includes a parachute deployment system (PDS) that can deploy a parachute installed in a drone and land the drone safely. The parachute may be deployed automati...  
WO/2017/065858A2
A propulsion system coupled to a vehicle. The system includes an ejector having an outlet structure out of which propulsive fluid flows at a predetermined adjustable velocity. A control surface having a leading edge is located directly d...  
WO/2017/065216A1
In the present invention, an unmanned flight vehicle flies along a catenary curve, thereby detecting the state of an electric wire more accurately. The state detection device is equipped with: an imaging unit for capturing a scenery imag...  
WO/2017/066559A1
A control assembly for a pocket-style screen (22) or door. Top and bottom guide rollers (60,64) carried by the screen (22) travel along adjustable guide rails (26,28) mounted in the pocket. A magnet assembly (42) includes a stationary ma...  
WO/2017/065106A1
The purpose of the present invention is to provide a remote-control type unmanned aircraft and a control handover method for the remote-control type unmanned aircraft such that the control thereof can be smoothly handed over among multip...  
WO/2017/064646A1
Stringer-less fuselage structures and associated methods of manufacturing are disclosed. In some embodiments, a fuselage structure includes a composite fuselage skin (24) including a plurality of tear straps (32) formed in the composite ...  
WO/2017/064288A1
An adapter rail system (1) for mounting objects to a floor rail (2) in a transportation means comprises at least one elongate adapter rail element (6), at least one arresting element (22) and at least one movement rail element (34), wher...  
WO/2017/065347A1
The present invention relates to a guard drone and a mobile guard system using the same. Disclosed are a guard drone and a mobile guard system capable of protecting a person to be guarded, using the same, wherein the guard drone detects ...  
WO/2017/066607A1
A system including a coupling (100) configured to couple a hose associated with a tanker aircraft to a nozzle associated with a receiving aircraft. The coupling may include a housing that houses a main poppet and a pilot poppet. The main...  
WO/2017/065102A1
Provided is a flying-type inspection device that can use a small unmanned aircraft to perform inspection while controlling angle and distance with respect to a planar inspection target. Also provided is an inspection method. The present ...  
WO/2017/064886A1
A cooling device (10) is equipped with: a heat sink (16) having a plurality of first heat dissipating fins (24) and a plurality of second heat dissipating fins (26); and a compressor (32), as an air blower for circulating cooling air (CA...  
WO/2017/064717A1
There is provided, in accordance some embodiment, a method for enhancing autorotation performance of a rotary-wing aircraft in emergency events. The method comprises an action of receiving a request for emergency thrust from a user inter...  
WO/2017/065824A1
Passenger seat assemblies including net backrests are described. An example passenger seat assembly can include a lower frame (14) configured to support a seat bottom (36) of the passenger seat. The passenger seat assembly can also inclu...  
WO/2017/064103A1
The invention relates to a component configurator (1) for generating variants of an aircraft component (11) to be installed. The component configurator (10) comprises a detection unit (12) for detecting a characteristic of the component ...  
WO/2017/065706A1
The invention relates to the back panels (10) of aircraft seats, characterized in that said back panels (10) are positioned behind the seats, used to hide the seat structure (60) and its structural elements and mechanisms, they contain s...  
WO/2017/066649A1
Disclosed is a technique for landing a drone using a parachute. The technique includes a parachute deployment system (PDS) that can deploy a parachute installed in a drone and land the drone safely. The parachute may be deployed automati...  
WO/2017/065103A1
Provided is a small unmanned aircraft control method that makes it possible to set a flight path in accordance with present ground conditions and fly a small unmanned aircraft. A method for controlling the flight of a small unmanned airc...  

Matches 1 - 50 out of 55,807