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Patent Searching and Data


Matches 1 - 50 out of 705

Document Document Title
WO/2020/251647A1
A low visibility aid device includes a main body having a front end, a back end, a middle section and an interior space. A mounting bracket extends outward from the main body for securing the device onto a manned aircraft for use during ...  
WO/2020/247641A1
Systems and methods are directed toward determining a vehicle orientation based on sensor information. Sensors are positioned along a vehicle body that may be evaluated to determine corresponding values between matching sensor types. Whe...  
WO/2020/245588A1
There is disclosed an aircraft configured to collect air data, the aircraft comprising: a wing structure; a forebody, forward of the wing structure; an afterbody, backward of the forebody; a skin covering the wing, the forebody and the a...  
WO/2020/245587A1
There is disclosed a fluid sensor for measuring the pressure of a fluid, the fluid sensor comprising: a surface; a recess formed at the surface, the recess being configured to affect the pressure of the fluid flowing at the recess, at le...  
WO/2020/219112A1
An aircraft navigational system for a multiengine aircraft can include a flight planning module configured to receive two or more navigational points defining a route and determine if a first degraded operation ceiling is high enough to ...  
WO/2020/219111A1
A control system for a hybrid electric powerplant of an aircraft can include a master controller configured to receive one or more power settings and to output a heat engine setting and an electric motor setting and a heat engine control...  
WO/2020/211919A1
This alerting system (10) for a light aircraft includes a reception unit (12) for receiving a piece of information to be released, a release unit (40) able to generate an alert for addressing a piece of information received by the recept...  
WO/2020/184934A1
A vertical take-off and landing aircraft using a hybrid electric propulsion system, according to an embodiment of the present invention, includes: a first control step (S1) of changing a destination when an engine (10), a power generator...  
WO/2020/179460A1
This control device comprises: a receiving unit that receives a discretionary wind velocity vector, the vector being measured by at least one external anemometer; a wind force prediction unit that, on the basis of the received wind veloc...  
WO/2020/180381A1
An indicator for a hybrid electric powerplant for an aircraft can be configured to indicate at least an amount or percentage of a total power and/or total torque, and an amount or percentage of an electric motor power and/or electric mot...  
WO/2020/136408A2  
WO/2020/135796A1
A fan assembly (100), an inertial measurement assembly (200), and an unmanned aerial vehicle (400). The fan assembly (100) is mounted on a fuselage (300) of the unmanned aerial vehicle (400), and the fan assembly (100) comprises a suppor...  
WO/2020/126451A1
A cockpit (10) suitable for being installed in a pilot's cabin of an aircraft, the cockpit (10) comprising a floor (5), a plurality of interior furniture items (2, 3) and a dashboard (1) configured to receive a plurality of devices for c...  
WO/2020/129394A1
[Problem] To provide a measurement system that makes it possible to quickly and highly accurately measure a physical quantity on the surface of an object without disturbing the flow over the surface. [Solution] A measurement system 1 com...  
WO/2020/073798A1
A mounting structure for a flight control module (20), a flight control assembly (10) and an unmanned aerial vehicle. The mounting structure for the flight control module (20) comprises a base plate (30) connected to the flight control m...  
WO/2020/073755A1
An unmanned aerial vehicle (500) and a flight control component (400) thereof. The flight control component (400) comprises a flight control module (20) and a mounting plate (10) disposed on the unmanned aerial vehicle (500). The flight ...  
WO/2020/060752A1
A hand-held emergency vision device includes a hand-held emergency vision device having an enclosed tubular housing with a first end and a second end. The enclosed tubular housing has an expanded shape memory form. First and second clear...  
WO/2020/040899A1
Boundary information associated with a three-dimensional (3D) flying space is obtained, including a boundary of the 3D flying space. Location information associated with an aircraft is obtained, including a location of the aircraft. Info...  
WO/2020/040827A1
Systems for determining a flight stage of an aircraft are described in which a vibration sensor and a sensor for determining a pitch of the aircraft are utilized. A server receives signals from the vibration sensor and pitch sensor, and ...  
WO/2020/032570A1
The present invention relates to a newly structured helicopter for effectively extinguishing fires such as forest fires. A helicopter for extinguishing fires according to the present invention comprises a discharging means (B) which is p...  
WO/2020/023314A1
An emergency vision system includes a housing; an inflatable main enclosure having an inflated state and a deflated state, the main enclosure in the deflated state is disposed in the housing, the main enclosure in the inflated state is c...  
WO/2019/246507A1
An aircraft imaging apparatus (100) includes a thermal imaging camera (162), a control circuit (120), an image generating circuit and a display (130). The thermal imaging camera (162) includes an array of pixels and that senses thermal r...  
WO/2019/242014A1
Provided are an RTK positioning device and an unmanned aerial vehicle. The RTK positioning device (100) comprises a case (101) and a circuit board (130) accommodated inside of the case (101). The circuit board (130) comprises a board bod...  
WO/2019/198768A1
The objective of the present invention is to provide a device configuration, a method and the like for performing an imaging survey within a survey space using an unmanned aerial vehicle. Provided is an unmanned aerial vehicle provided w...  
WO/2019/198767A1
Provided are a device configuration, method, etc. for performing imaging investigation in an investigation space using an unmanned aerial vehicle. This imaging investigation system comprises: a flight start platform on which an unmanned ...  
WO/2019/198155A1
The purpose of the present invention is to provide a flight control mechanism for controlling flight of an unmanned aerial vehicle by controlling collision between the vehicle and a boundary surface, an unmanned aerial vehicle equipped w...  
WO/2019/195512A1
A cockpit pressurization and oxygen warning system (100) includes a cabin pressure input (146) and an aircraft pressure input (312). A pilot interface (200) includes a first visual indicator (210) having a first recognizable characterist...  
WO/2019/183428A1
An internal combustion engine for an aircraft includes a crankshaft configured to drive a driven element; a camshaft coupled to the crankshaft; and an ignition controller coupled to the camshaft and including a visual indicator, the visu...  
WO/2019/177830A1
An object-based integrity verification method (330) for detecting hazardously misleading information contained in an output image of a graphics processing unit comprises steps of: identifying a plurality of safety-critical graphic object...  
WO/2019/124686A1
A flight controller of a vertical take-off and landing aircraft, according to one embodiment of the present invention, controls a tilt angle of a main rotor on the basis of a vertical posture control signal in a low-speed flight state. W...  
WO/2019/099538A1
Systems and aircraft are provided. An avionics system includes a storage device and one or more data processors. The storage device stores instructions for monitoring an actual performance of the aircraft. The one or more data processors...  
WO/2019/089966A1
A technique for finding and estimating the locations of atmospheric thermals for the purpose of exploiting the updraft energy to enable the aircraft to remain aloft while reducing or eliminating the need to expend fuel or energy and oper...  
WO/2019/082063A1
The present invention relates to a control device with control panel (1) for air vehicles and for controlling the suitability of inputs entered into the control panel (CP) by a pilot in order to operate air vehicle and to give automatic ...  
WO/2019/061000A1
The present disclosure provides methods and systems for providing a lateral center of gravity of an aircraft on an aircraft display. A fuel distribution in the aircraft fuel tanks is determined. A lateral center of gravity of the aircraf...  
WO/2019/059889A1
A portable computerized device for an aircraft control system includes an input system for inputting commands, a device display for displaying information on the computerized device, a processor, a wireless communication module, and a no...  
WO/2019/053058A1
The invention relates to an autogyro (1), comprising a rotor (3), which can be set into autorotation, an instrument panel (9), which has at least one display unit (11) and/or at least one operating unit (12), the instrument panel (9) hav...  
WO/2019/043645A1
A method and a system are disclosed for determining an estimation of an anemometric parameter of an aircraft, the anemometric parameter selected from a group comprising at least one of an angle of attack, a sideslip angle and a calibrate...  
WO/2019/016930A1
The present invention determines, with a high degree of accuracy, the magnitude of influence exerted by wind on a moving body from information acquired from the moving body. This data processing device is provided with: an acceleration a...  
WO/2019/018805A1
A method of calculating a climb-dive marker (CDM) that is visibly present on a display even as the aircraft approaches a roll angle of +/- 90° is provided. An exemplary CDM method comprises obtaining, an X-axis velocity, a Y-axis veloci...  
WO/2019/000397A1
Provided in the present invention is an unmanned aerial vehicle (100), comprising: a fuselage (10), a rotor assembly and a barometer (40); the rotor assembly is disposed on the fuselage (100), and the barometer (40) is disposed outside o...  
WO/2018/236181A1
The present invention relates to a mobile platform-based AHRS flight control apparatus and, more specifically, to a mobile platform-based AHRS flight control apparatus of an unmanned flying object comprising a drone frame (10) on which a...  
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...  
WO/2018/209770A1
A barometer assembly (10) and a drone (100). The barometer assembly (10) is used in the drone (100). The drone (100) comprises a central frame (20), an arm (30) extending outwards from the central frame (20), a power assembly (40) dispos...  
WO/2018/167472A1
The present subject matter relates to an aircraft stabilization system (200). The aircraft stabilization system (200), amongst other components, may include multiple sensors (202), a processing unit (206), and multiple stabilization unit...  
WO/2018/102318A1
In accordance with at least one aspect of this disclosure, a computer implemented method includes receiving imaging data from an imaging system of an aircraft, and creating a new flight plan or a modified flight plan of the aircraft base...  
WO/2018/094824A1
A fixing buckle (50) and an unmanned aerial vehicle (100) having same. The fixing buckle (50) is used for fixing a sensor (70) on a support, and comprises a buckle body (51) and a limiting part (511) provided on the surface of the buckle...  
WO/2018/081559A1
An air data probe (10) and associated method of method of measuring air data is disclosed. The air data probe includes a plurality of air pressure sensors, and a body (14) that encloses a hollow interior cavity (16), where the body (14) ...  
WO/2018/070103A1
Provided are a detachable unit that makes it possible to make work for calibrating the various sensors provided to an unmanned aerial vehicle more efficient and to unitize an unmanned aerial vehicle control function, and a sensor calibra...  
WO/2018/060392A1
Aircraft comprising a fuselage (1) divided by a floor (2) into an o upper volume (3) and a lower volume (4) through which joists (5) extend that support the floor and delimit, along with the fuselage and the floor, two side chambers (6),...  
WO/2018/043988A1
Disclosed are an unmanned aerial vehicle for aerial reconnaissance, which performs object detection and object hitting on the basis of image information, and an unmanned defense system and method using the same. The unmanned aerial vehic...  

Matches 1 - 50 out of 705