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Patent Searching and Data


Matches 601 - 650 out of 62,196

Document Document Title
WO/2018/157426A1
A propeller, a power assembly and an aircraft, the propeller comprising a propeller base and a blade (1) connected thereon. The blade (1) has an angle of attack of 14.05°±2.5° and a chord length of 11.94mm±5mm at a position where the...  
WO/2018/158531A1
The invention relates to a device and a method for the connection and linear separation of two elements (1, 2), such as the two stages of a spacecraft, consisting in using a tube (4) containing a pyrogenic-type material (5) and a glue (3...  
WO/2018/160764A1
A hose mounting assembly that includes a mounting member having a base and a main body portion. The main body portion includes first and second ends, a curved tie tunnel defined therethrough, and a curved mounting surface. The base inclu...  
WO/2018/158576A1
One type of kite system for the extraction of energy from the wind includes a kite connected to a base unit using a tether. The kite system comprises: an anhedral wing having wing tips and a central part located vertically higher than th...  
WO/2018/160740A1
A three-axis spacecraft including a spacecraft body including first and second opposing radiator/equipment panels, first and second opposing mounting panels, an earth deck and a zenith deck. The zenith deck faces the Earth when the space...  
WO/2018/160559A1
In a preferred embodiment, a retrofittable PRM lavatory complex occupies the same footprint as a preexisting outboard dual-lavatory complex. The two lavatories are separated by a common articulating wall that is typically positioned in a...  
WO/2018/158766A1
An airborne vehicle made of thermally non-conductive materials and method for thermal conduction in an airborne vehicle are disclosed. The airborne vehicle comprising at least one structural element made of material with high thermal con...  
WO/2018/159256A1
A takeoff and landing device (5) is provided with: a fixed device (55) or a communication unit (57) that can switch between a first state in which an unmanned aircraft (3) is prevented from taking off from a host device, and a second sta...  
WO/2018/157833A1
An unmanned aerial vehicle: arm assemblies (12, 13, 14, 15) of the unmanned aerial vehicle may be folded and unfolded relative to a casing so as to facilitate transportation and storage of the unmanned aerial vehicle. At the same time, t...  
WO/2018/157287A1
Provided are a method and device for controlling the landing of an unmanned aerial vehicle, and an unmanned aerial vehicle. The method for controlling the landing of an unmanned aerial vehicle comprises: receiving status information abou...  
WO/2018/158927A1
The present invention highly precisely estimates the shape of an object irrespective of whether there are variations in the altitude of the shape of the object, and avoids a collision between the object and a flying vehicle during flight...  
WO/2018/158686A1
A remote piloted aircraft (1) comprising a secondary flight assembly (4) adapted to intervene in case of failure of the aircraft (1) or in an emergency, said secondary flight assembly (4) being provided with an additional control unit (5...  
WO/2018/158549A1
The aircraft (10) comprises a fuselage (11) and a rhombohedral wing structure (12) comprising front wings (13, 14) mounted on a front wing-root support (17) and rear wings (15, 16) mounted on a rear wing-root support (18). One end of eac...  
WO/2018/158746A1
The present disclosure relates launch systems, launch vehicles for use with the launch system, and methods of launching articles utilizing the launch vehicle and/or the launch system. In particular, various improvements for electroantima...  
WO/2018/158634A1
An aerodynamic lifting system for a VTOL aircraft is provided that includes a lifting structure defining a leading edge portion, a trailing edge portion, an upper surface extending between the leading edge portion and the trailing edge p...  
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/2018/158575A1
A kite having multiple sections for use in a power-generation system, the kite comprising a top panel and a bottom panel, and at least one rib connection piece extending between the top panel at a first end and the bottom panel at the se...  
WO/2018/153759A1
An aircraft-towed device, comprises a frame including a leading pole (12a) and a trailing pole (12b), the poles being substantially transversal to a flight direction; an aerodynamic damping structure (16) attached to the trailing pole (1...  
WO/2018/156618A1
The present invention discloses improvements to mechanical and electro-mechanical force simulators for aircraft pilot controllers, and particularly foot-actuated controllers. In particular, the invention replaces conventional foot-actuat...  
WO/2018/152770A1
A cradle head assembly (100), comprising: a fixed bracket (110); at least two mounting seats (130) disposed opposite to the fixed bracket (110) and disposed at intervals; a shock absorbing mechanism (120) connected between the fixed brac...  
WO/2018/152916A1
A battery compartment (10) and an unmanned aerial vehicle (200). The battery compartment (10) comprises a first housing (11), a second housing (12), and a sealing piece (13); an abutting face (111) is formed at the periphery of the first...  
WO/2018/157176A1
Transfer of objects between spacecraft can be achieved in a low gravity environment. A capture device can be part of a module that facilitates visualization of a vessel that approaches the capture device. The module can facilitate positi...  
WO/2018/157061A1
A tape drive comprises a roll of a tape (202) that can be extended from a rolled state to an extended state. The tape includes a rigid material that supports the tape and a pliable material disposed at least partially on one side of the ...  
WO/2018/152784A1
An airframe (10) and an unmanned aerial vehicle (100). The airframe (10) comprises a housing (12) and fans (14). An air vent (121) is separately provided on both ends of the housing (12) to be communicated with the internal space of the ...  
WO/2018/154105A1
A device for the decontamination of materiel, notably an aircraft such as a military helicopter (1), using a nuclear, biological and/or chemical decontaminant. The device comprises: • a protective cover (2) that can be adapted to the s...  
WO/2018/155739A1
A vertical take-off and landing aircraft and a transition method therefor are disclosed. The vertical take-off and landing aircraft comprises: a flight fuselage including a front wing part and a rear wing part; a plurality of tilting pro...  
WO/2018/155529A1
In order to reduce fuselage downtime and quickly perform fuselage repairs, the present invention comprises: a fatigue estimation unit (22) that estimates the fatigue life of a prescribed area of an fuselage, on the basis of the level of ...  
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/2018/153758A1
The invention relates to an aircraft-towed device, comprising a support structure (10) that is substantially flat when deployed, including a leading pole (12a) and a trailing pole (12b), the poles being transversal to a flight direction;...  
WO/2018/154603A1
The present subject matter relates to an apparatus (100) that use of a tuft of numerous wires as a drag enhancing system for spacecrafts (102). When these ultra-thin wires are used in high numbers and deployed on-board a spacecraft, they...  
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/2018/156506A1
An unmanned autonomous vehicle assessment and reporting system may conduct patch scan analyses of a roof. Damage points on the roof may be evaluated for severity and assigned a severity value. A remediation status may be objectively deve...  
WO/2018/152909A1
A cradle head device (100) and an unmanned aerial vehicle (300) using the same. The unmanned aerial vehicle (300) comprises a fuselage (200), and the cradle head device (100) is fixed to the fuselage (200). The cradle head device (100) c...  
WO/2018/156991A8
A method for controlling an unmanned aerial vehicle within a flight operating space. The unmanned aerial vehicle includes one or more sensor arrays on each spar. The method includes determining, using a plurality of sensor arrays, a flig...  
WO/2018/157082A1
A sensor pin coupled to a latch is described herein. The sensor pin includes a sensor pin body including a sensor, a sensor bolt extending from the sensor pin body and having a rod cavity arranged at a non-straight angle with regard to a...  
WO/2018/153756A1
The invention relates to an aircraft-towed device, comprising a meshless frame including a leading pole (12a) and a trailing pole (12b), the poles being substantially transversal to a flight direction;an aerodynamic damping structure (16...  
WO/2018/156165A1
An apparatus configured to reduce acoustic interactions between a propeller and a surface of an aircraft positioned downstream of the propeller includes a surface modification element of the surface of the aircraft. The surface modificat...  
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/2018/153821A1
The method for on-board electrical power distribution according to the invention consists of producing a protected segregation interface (4A) between the primary distribution (2A) and the secondary distribution network for electrical pow...  
WO/2018/154592A1
Neutral Axis Duct with Tandem Telescopic Thrust Vectoring Leading and Trailing Edge Propellers for Multi-Mode Spatial Vehicle [NADTVPMSV] is a single monocoque chassis frame for a multi-mode vehicle that can travel in all land, air, over...  
WO/2018/152783A1
Disclosed is an image processing method, applied in an aircraft (100). The aircraft (100) is provided with an imaging device (10). The processing method comprises the steps of: (S22) controlling the imaging device (10) to perform imaging...  
WO/2018/156991A1
A method for controlling an unmanned aerial vehicle within a flight operating space. The unmanned aerial vehicle includes one or more sensor arrays on each spar. The method includes determining, using a plurality of sensor arrays, a flig...  
WO/2018/153757A1
The invention relates to an aircraft-towed device, comprising a support structure (10) that is substantially flat when deployed; a transmission antenna (14) mounted on the support structure, having a conductor wound in a loop near the ed...  
WO/2018/152785A1
Disclosed is an unmanned aerial vehicle (100), comprising a body (10) and a battery module (40). The body (10) comprises a bottom portion (11) facing the ground. The battery module (40) comprises a battery having a top portion (41) oppos...  
WO/2018/152792A1
Disclosed are a foldable frame (100), a frame assembly (200) and an unmanned aerial vehicle (300). The foldable frame (100) is applied to the unmanned aerial vehicle (300) and comprises a central frame (2) and at least one folding struct...  
WO/2018/156139A1
A computer is programmed to determine a trajectory of a moving target based on data from one or more vehicle sensors. The computer is programmed to deploy an aerial drone from the vehicle to track the moving target based on the determine...  
WO/2018/153734A1
An aircraft including a body and a pair of wings connected to the body by a mounting structure, the wings being movable between a first position in which the wings extend laterally from the body, and a second position in which the wings ...  
WO/2018/156041A3
The present invention relates to a propulsion system and vertical take-off and landing (VTOL) aircraft. A VTOL aircraft (100) uses a modular propulsion system (101) containing three multiple propellers (102, 103) and (104). The multiple ...  
WO/2018/156972A1
A safety system for an aerial vehicle, preferably including: a ballistic subsystem, preferably including one or more rockets operable to adjust motion of the aerial vehicle and a mounting unit that couples the ballistic subsystem to the ...  
WO/2018/153563A1
The invention relates to an artificial neural network (3) which is taught via a database (9) containing at least road accident data and which is connected to an unmanned aerial vehicle (1) transmitting environmental data to the neural ne...  

Matches 601 - 650 out of 62,196