Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 1 - 50 out of 61,570

Document Document Title
WO/2018/204772A1
Systems and methods are provided for least one leading drone configured to move to a leading drone future location based on a future location of a base station. A set of base station future locations may form a base station path for the ...  
WO/2018/203189A1
Assemblies and methods for facilitating the assembly of aircraft wings to a fuselage are disclosed. In some embodiments, a wing unit includes features that are configured to define one of more parts of a pressure vessel that is partially...  
WO/2018/201868A1
An anti-unmanned aerial vehicle device and method based on multi-camera tracking and positioning, the anti-unmanned aerial vehicle device, comprising: a bracket, the bracket being defined with a center, a periphery around the center, and...  
WO/2018/201416A1
An unmanned aerial vehicle (200) can include a central body (202) comprising a first body portion (204) and a second body portion (206), where the first body portion (204) is configured to move translationally relative to the second body...  
WO/2018/203191A1
Assemblies and methods for facilitating the assembly of aircraft wings to a fuselage are disclosed. In some embodiments, a wing unit includes features that are configured to define one of more parts of a pressure vessel that is partially...  
WO/2018/201718A1
A photographic component, comprising a yaw-axis connecting arm (1), a pitch motor (2), a pitch-axis connecting arm (3), a roll motor (4), and a camera (5). A first end portion of the pitch motor (2) is fixedly connected to the yaw-axis c...  
WO/2018/203190A1
Assemblies and methods for facilitating the assembly of aircraft wings to a fuselage are disclosed. In some embodiments, a wing unit includes features that are configured to define one of more parts of a pressure vessel that is partially...  
WO/2018/204896A1
The zero carbon emission vehicle as disclosed herein may include a condenser for extracting fluid water from the atmosphere, an electrolyzer for generating hydrogen from the fluid water, and one or more deformable fluid-retaining chamber...  
WO/2018/203973A1
A distance from an aerial vehicle to a terrain feature located forward and lower with respect to the aerial vehicle is measured. A current orientation of the aerial vehicle with respect to a reference orientation is detected. At least th...  
WO/2018/203805A1
The present invention regards a body structure (1) of a vehicle (3), comprising a door structure (5), whereby an interface (7) is defined between the body structure (1) and the door structure (5), which door structure (5) is configured t...  
WO/2018/204783A1
Systems and methods are provided for a network of relay drones utilized as a set of relays or linkages between a base station and a working drone controlled by the base station. The relay drones in the network may augment a communication...  
WO/2018/201417A1
Disclosed are a deformable aircraft, a mobile platform and an operating method therefor. The deformable aircraft comprises: a fuselage (110), the fuselage comprising a first fuselage portion (111) and a second fuselage portion (111), whe...  
WO/2018/202455A1
A manifold assembly (300) configured for integration with a joint cover apparatus in a ducting system to detect leaking gas comprises an elastomeric manifold block (303) having a substantially circular inlet aperture and one or more gas ...  
WO/2018/202585A1
The invention mainly concerns a seat (10) comprising a backrest (11) carrying, on a rear face side, a tray table (15) that can be moved between a deployed position and a stowed position, - said tray table (15) comprising a latch (22) tha...  
WO/2018/203962A1
Various embodiments include devices and methods for mitigating the bias of a magnetometer resulting from operating various hardware components on a device such as a drone or a computing device. Various embodiments may improve the accurac...  
WO/2018/204778A1
Systems and methods are provided for least one leading drone configured to move to a leading drone future location based on a future location of a base station. A set of base station future locations may form a base station path for the ...  
WO/2018/203036A1
An unmanned aerial vehicle (2) comprising: a fixed wing (6); a pair of nacelles (10) connected to the wing (6) and spaced laterally either side of a centreline of the wing (6), wherein each nacelle (10) comprises a stationary portion (14...  
WO/2018/203946A1
A hold open rod assembly (10) includes an outer tubular structure (14) and an inner tubular structure (12) positioned for telescoping movement relative to the outer tubular structure. A locking mechanism (16) retains the hold open rod as...  
WO/2018/203215A1
Test rigs and methods for performing functional tests on a cabin management system (CMS) of a passenger cabin of an aircraft or other mobile platform are disclosed. In some embodiments, a test rig comprises a plurality of components of t...  
WO/2018/201801A1
A cradle head comprises an installation frame for installation of a photographing apparatus and a fastener (30) for fastening the photographing apparatus. The fastener (30) has a first end and a second end fitting with the installation f...  
WO/2018/201813A1
A ducted fan comprises: a duct (1), wherein an air intake and an air outlet are located above and below the duct (1) respectively, the duct (1) has an inner wall and an outer wall disposed with an interval therebetween, an annular space ...  
WO/2018/204776A1
Systems and methods are provided for least one leading drone configured to move to a leading drone future location based on a future location of a base station. A set of base station future locations may form a base station path for the ...  
WO/2018/203520A1
The purpose of the present invention is to provide: a flight function addition device in which a plurality of rotor units are mounted on an article to be transported and the movement of the rotor units is coordinated, whereby the article...  
WO/2018/204134A1
A power conversion unit may include two or more power modules for providing high- voltage direct current power to electrical loads, such as one or more propulsion motors aboard an aerial vehicle. Each of the power modules may be controll...  
WO/2018/198083A1
A system for representing a graphic image on a surface of a support by painting surface (S) areas or drawing signs, of a predetermined shape and position, is described, characterised in that it comprises: at least one autonomous flight a...  
WO/2018/195575A1
Unmanned aircraft (1), having a drive unit (2) for allowing the aircraft (1) to fly in the airspace and a data processing unit (3) configured to head for a position or a temporal sequence of positions of the aircraft (1) in the airspace ...  
WO/2018/197080A1
Disclosed is an electrically driven wheeled device, in particular a smart wheel, comprising at least one main wheel part (12), at least one connection unit (14) for connecting the main wheel part (12) to an external unit (16), and at lea...  
WO/2018/195968A1
A method for use in controlling a terminal device, comprising: determining a flight trajectory sequence of each unmanned aerial vehicle from among a plurality of unmanned aerial vehicles; determining an action sequence of an unmanned aer...  
WO/2018/196882A1
An aerial vehicle, comprising a fuselage (1) and wings (2). First channels (201) are provided inside of a wing (2). Multiple first inlets (202) are provided on the upper surface (101) of the wing. Multiple first pressure openings (203) a...  
WO/2018/196810A1
Disclosed is an aircraft, comprising a fuselage (1) and a wing (2), a first open channel (12) for extending the fluid flow path being provided at a front portion (211) and/or a middle portion (212) of a windward side (21) of the wing (2)...  
WO/2018/195771A1
Disclosed are a control method for driving motor rotation, and an electronic governor. The method comprises: acquiring addressing information; determining a rotation direction of a motor according to the addressing information; and provi...  
WO/2018/197120A1
An aerodynamic body for use on an aircraft is presented. The aerodynamic body includes at least a first perforated surface portion (25) and an ice-protection system (31). The first perforated surface portion (25) has perforations, the ic...  
WO/2018/195724A2
An aircraft, comprising a main frame (100), a swing motor (200) and at least one pair of wings (300). The swing motor (200) outputs reciprocating swing motion, and has a swing arm (204) that is mounted on the main frame (100) and is capa...  
WO/2018/197801A1
The invention relates to a system for securing a glazing to the vehicle structure, comprising a first, outer primary half-frame (1) and a second, inner primary half-frame (2), the first and second primary half-frames (1) and (2) being at...  
WO/2018/197265A1
The present invention relates to a wing(2) for an aircraft, comprising: a main wing (4) having an outer skin (6) defining an interior space (8) of the main wing, a slat (10), and a connection assembly (12) for movably connecting the slat...  
WO/2018/198126A1
ABSTRACT OF THE DISCLOSURE A passenger-carrying aerial vehicle operating as part of an integrated ground-and-air transport infrastructure, allows critical portions of a route to be completed by air transport. In some implementations, the...  
WO/2018/197772A1
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). At least two w...  
WO/2018/199361A1
The present invention relates to a drone flight reservation control system, and the system enables safe operation of a drone through a drone flight reservation control and a drone flight restriction control with respect to a flight restr...  
WO/2018/199808A1
An aerodynamic surface of an aircraft comprises a main part with a leading and a trailing edge and having an aerodynamic profile, and also vortex generators in the form of teeth having edges along the length thereof. The teeth are mounte...  
WO/2018/200879A1
An electric tail-sitter aircraft configured to transport passengers and/or cargo between locations. The aircraft includes a flight module, a ground module and a payload module. The flight module is a wing that can rotate with respect to ...  
WO/2018/198313A1
[Problem] To provide an action plan creation system which allows automatic flight of an unmanned aerial vehicle and which simplifies input of parameters necessary for aerial photography. [Solution] This action plan creation system 1 is p...  
WO/2018/196789A1
A safety device for a boarding bridge travelling mechanism (100), comprising an inner protective shroud mechanism, an outer protective shroud mechanism, a connecting mechanism, and an induction and control mechanism. The inner protective...  
WO/2018/200858A1
This application describes systems, methods, and devices to enhance the safety and functionality of unmanned rotorcraft by improving reliability, transparency, operational capabilities, and effectiveness. Embodiments include integration ...  
WO/2018/197448A1
The invention relates to a method for attenuating vibrations of an aircraft wheel/brake assembly arising during braking, the brake comprising rotor discs (2b) rotationally driven with the wheel by means of bars (5) secured to the wheel a...  
WO/2018/199460A1
Disclosed is an unmanned transport system using an unmanned aerial vehicle. There may be provided an unmanned delivery port, including a body in which a storage shelf for keeping one or more delivery goods has been formed, an input door ...  
WO/2018/200093A1
Airframes configured for stable in-flight transition between forward flight and vertical takeoff and landing are described herein. In one embodiment, an aircraft can include a fuselage, opposed wings extending from opposed sides of the f...  
WO/2018/195574A1
The invention relates to a system (1) formed of at least two unmanned aerial vehicles (10), wherein each aerial vehicle (10) comprises a drive unit, a flight control unit (13) for controlling the flight path of the aerial vehicle (10) by...  
WO/2018/196135A1
The present invention relates to the technology of unmanned aerial vehicles and discloses an electronic governor (1000) and an unmanned aerial vehicle. The electronic governor (1000) comprises: a capacitor (1111); a first circuit board (...  
WO/2018/200066A1
A lighting system for an unmanned autonomous vehicle (UAV) adapts to the environment around the UAV to ensure status notification lights are visible to an operator and/or abide by regulatory lighting requirements. A processor of the UAV ...  
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...  

Matches 1 - 50 out of 61,570