Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 451 - 500 out of 61,901

Document Document Title
WO/2018/163159A1
A multirotor aircraft that includes a chassis, vertical rotors, foldable wings, and a means for deploying and folding the foldable wing. The foldable wing is attached to the chassis and the means for deploying and folding the foldable wi...  
WO/2018/165057A1
An aircraft can include a frame and a plurality of electrical rotors coupled to the frame. The aircraft can further include a control system physically coupled to the frame and communicatively coupled with each of the plurality of electr...  
WO/2018/161193A1
A four-axis aerial vehicle provided with lights comprises a control circuit (4), a wireless transceiver module (5), motors (11), a battery (9), a fuselage (10), and a top anti-collision rod (1). The control circuit (4) is connected to vo...  
WO/2018/163571A1
An information-processing device operating in an imaging device mounted in a mobile entity, which, when image capture by the imaging device fails, notifies the mobile entity to the effect that image capture has failed.  
WO/2018/163699A1
[Problem] To provide a control system for a flight vehicle that causes the flight vehicle to fly autonomously without the use of GPS and without storing flight routes, and a control device for the same. [Solution] A control system 2 for ...  
WO/2018/165093A1
A system and method for acquiring store comprise establishing an electronic communication between a mobile device and a unmanned vehicle; tracking in a store by the unmanned vehicle a customer having the mobile device; collecting data by...  
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/2018/158767A1
Generally, a vehicle comprising at least one hydrogen releasing element is provided. The vehicle can include at least one hydrogen releasing element coupled to a body of the vehicle. The vehicle can include a hydrogen combustion region p...  
WO/2018/158392A1
A method (600) for testing control logic for a propeller driven by a gas turbine engine of an aircraft includes overriding (602) a signal indicating the aircraft is operating in a ground mode. The method can further include testing (604)...  
WO/2018/159968A1
A body protection apparatus for use in a vehicle for carrying people according to the present invention is a seat employed in a vehicle in/on which people ride, and comprises a safety device for covering a passenger so as to protect the ...  
WO/2018/158511A1
The present invention relates to a redundant and dissimilar system (10) for monitoring the status of contactors (22) of an aircraft control stick (20). This monitoring system (10) comprises at least one electrical power source (2), at le...  
WO/2018/158756A1
A vehicle arresting system includes a base layer comprising a crushable aggregate (54) and a cover layer comprising a cementitious material having an oven-dry density of 1602 kg/m3 (100 Ib/ft3) or less. The system also may include an arr...  
WO/2018/158255A1
A control system (20) has both a first and second processing modules (22, 24) for controlling retraction and extension of a landing gear assembly (14) on an aircraft (10). The processing modules can operate independently of each other an...  
WO/2018/158586A1
An aerial delivery container is provided for release from an aircraft, the container comprising a housing comprising a hold for containing a payload; and an impact absorbing structure provided to the housing for absorbing the force of an...  
WO/2018/157633A1
Provided is a shock absorber (100), comprising a connecting portion (102) and buffering portions (101) respectively located on either end of the connecting portion, wherein the cross-sectional size of the shock absorber gradually decreas...  
WO/2018/160215A1
This invention relates to magnetic propulsion systems. Previously, motors required electronic control systems for efficiency. Embodiments of the present invention use a first axel (120) joined to a first permanent magnet (113) of a first...  
WO/2018/157393A1
An aerial dispensing method is disclosed. The method may comprise obtaining a wind velocity, the wind causing a drift to a substance dispensed from an unmanned aerial vehicle (UAV), and controlling one or more components of the UAV based...  
WO/2018/158757A1
A vehicle arresting system includes a base layer comprising a crushable aggregate and a cover layer comprising a cementitious material having an oven-dry density of 1602 kg/m3 (100 lb/ft3) or less. The system also may include an arrestor...  
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...  

Matches 451 - 500 out of 61,901