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Patent Searching and Data


Matches 1 - 50 out of 636

Document Document Title
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...  
WO/2018/011791A3
A device, system and method is provided for obtaining and processing turbulence data via communication devices located on-board airplanes. Turbulence data obtained by a plurality of communication devices may be received during flights on...  
WO/2018/002878A1
An aircraft avionic system for use in an equipped aircraft includes a controller and a display. The controller provides output data to the display, with the output data producing visual images on the display. An angle of attack data sour...  
WO/2017/221859A1
[Problem] The present invention addresses the problem that functional components for causing multiple moving bodies to operate in a coordinated manner have to be designed individually in conformity to functional components for causing th...  
WO/2017/208179A1
The present disclosure describes displaying on a flight deck (12) graphical presentations indicative of performance limitations of an aircraft (10) resulting from an in-flight aircraft reconfiguration. The graphical presentations are co-...  
WO/2017/191543A1
Systems, devices and methods for alerting a crew of an aircraft or other mobile platform of a relevant condition associated with the aircraft are disclosed. One exemplary method comprises receiving data indicative of an existence of the ...  
WO/2017/162862A1
The invention concerns an aircraft probe for resisting formation and propagation of ice comprising: • a base that is intended to be attached to an aircraft; • a housing extending from the base, said housing comprising:  a body ext...  
WO/2017/138049A1
The control system (100) includes a flying body (10) and a base station (50). The base station is equipped with a light source unit which irradiates guide light of a predetermined wavelength. The flying body is equipped with: a propulsio...  
WO/2017/073241A1
Provided is a technique with which it is possible to measure the airspeed of a low-speed flight vehicle along a horizontal direction. An airspeed measurement system for a low-speed flight vehicle, wherein the airspeed measurement system ...  
WO/2017/055975A1
A method of and a system for presenting an operating status of an aircraft engine. The method comprises accessing a first indication indicative of a position of an aircraft engine start switch and accessing a second indication indicative...  
WO/2017/053913A1
A truss-reinforced radome crown structure (TRRCS) that functions in combination with an aircraft and a communication radome or antenna. The TRRCS maintains and protects a radome and antenna located on an aircraft's fuselage. The TRRCS in...  
WO/2017/021414A1
A display management system 10 is provided for displaying a graphical representation of flight envelope information of an aircraft. Included in the display management system is a control module 20 being coupled to the display management ...  
WO/2017/002055A2  
WO/2016/209225A1
Examples disclosed herein relate to control of a drone. In one example, aerial movement of the drone is controlled. In the example, it is determined, based on a plurality of devices, whether the drone is within a line- of-sight with at l...  
WO/2016/204843A3
Systems, apparatuses and methods for landing an unmanned aircraft on a mobile structure are presented. Sensors on the aircraft identify a predetermined landing area on a mobile structure. The aircraft monitors the sensor data to maintain...  
WO/2016/204843A2
Systems, apparatuses and methods for landing an unmanned aircraft on a mobile structure are presented. Sensors on the aircraft identify a predetermined landing area on a mobile structure. The aircraft monitors the sensor data to maintain...  
WO/2016/195816A2
An avionics display for rotorcraft provides a depiction of 360 degrees of terrain and obstacles about the rotorcraft using a top plan view at above a predetermined altitude that transitions to an angle perspective view as the altitude dr...  
WO/2016/195816A3
An avionics display for rotorcraft provides a depiction of 360 degrees of terrain and obstacles about the rotorcraft using a top plan view at above a predetermined altitude that transitions to an angle perspective view as the altitude dr...  
WO/2016/190933A3
Vehicle navigation methods, systems and computer program products are provided that create a composite video image of a scene from video images of the scene generated by a plurality of video image sensors. The video image from each image...  
WO/2016/190933A2
Vehicle navigation methods, systems and computer program products are provided that create a composite video image of a scene from video images of the scene generated by a plurality of video image sensors. The video image from each image...  
WO/2016/164624A1
A system for and method of indicating an angle of attack of an aircraft is provided. The system utilizes measurements from existing aircraft sensors so that a dedicated angle of attack sensor is not required. The system enables and benef...  
WO/2016/130716A2
A method of unmanned aerial vehicle (UAV) operation, including: receiving from a customer a first data request (400), the first data request (400) having: a first geographic coverage area, and a refresh rate for the first geographic cove...  
WO/2016/130721A2
A method of migrating unmanned aerial vehicle (UAV) operations between geographic survey areas, including: uploading a first plurality of flight missions (604) into a first UAV pod; deploying the UAV pod (606); autonomously launching the...  
WO/2016/125139A2
A device, system and method is provided for obtaining and processing turbulence data via communication devices located on-board airplanes. Turbulence data obtained by a plurality of communication devices may be received during flights on...  
WO/2016/105324A1
The group of inventions relates to means for enhancing vehicle safety. An autonomous modular device contains means for recording, controlling and reacting, signaling means, an electronic module, a cluster module, and at least one membran...  
WO/2016/084000A1
An auxiliary safety system for controlling the attitude of an aircraft (1) provides sensors placed on the aircraft (1) which identify stalling and/or other critical flying conditions that are imminent and/or have occurred, an electronic ...  
WO/2016/053452A1
A method of controlling noise of an aircraft includes storing a plurality of predefined noise modes; receiving a selection of a selected noise mode from the plurality of predefined noise modes, the selected noise mode identifying at leas...  
WO/2016/037035A1
An airspeed estimation system of an aircraft includes an electronic airspeed rate modeler unit configured to output an estimated airspeed rate signal indicating an estimated airspeed rate of the aircraft. The estimated airspeed rate sign...  
WO/2015/130360A3
A system for enhancing vision inside an aircraft cockpit (10) includes a primary display system (34) configured to receive the signals related to flight data (33) and display visual representations based on the flight data (33). The syst...  
WO/2015/126513A2
Peripheral vision hover drift cueing methods, systems and computer readable media are disclosed. For example, a system can include one or more sensors, and a peripheral vision hover drift cueing controller coupled to the one or more sens...  
WO/2015/108590A3
Methods and systems for augmenting situational awareness using a controllable window are described. An environmental condition within a field of view of the controllable window is determined. Light transmissivity of the controllable wind...  
WO/2015/079155A1
The invention relates to a system (2) for generating non-propulsive energy in an aircraft, including: an auxiliary power unit (20) including a gas turbine (21) and a fuel cell (22); a pathway (23) for the intake of outside air into the a...  
WO/2015/059085A1
Air data sensing apparatus (10) comprising: an aircraft panel; a blister (12) arranged on a surface (8) of the aircraft panel, the blister (12) comprising an upstream portion (12a) and a downstream portion (12b), the upstream portion (12...  
WO/2014/168566A1
The invention relates to a distributed display device (40, 45, 50, 55) for a vehicle comprising a set of subsystems, wherein said display device comprises at least one operator station (10; 20; 30), comprising at least one display unit (...  
WO/2014/155446A1
The purpose of the invention is to suppress variations in brightness degradation in a display. A display device (1) according to the invention displays information using self-illuminating type display elements and is provided with a disp...  
WO/2014/136068A1
A method provides alert information, regarding an aircraft wheel braking system, to an operator of an aircraft during an aircraft landing. An input of a target deceleration rate for the landing aircraft is received prior to the aircraft ...  
WO/2014/133598A1
A method and apparatus for displaying an energy state (121) of an aircraft (100). The energy state of the aircraft is identified by a processor unit based on a speed (112) of the aircraft and an altitude (114) of the aircraft. An indicat...  
WO/2014/133250A1
The present invention relates to a brightness adjusting system for an illumination panel of an aircraft operation console, the system comprising: a controller for controlling voltage; a power IC for outputting power; a digital potentiome...  
WO/2014/081337A1
The invention relates to aviation technology. The system for depicting information for controlling an aircraft comprises an orientation sensor, making it possible to determine three angular coordinates of the position of a line of observ...  
WO/2014/047578A1
The flight of an aircraft is represented in terms of Earth-based reference system data for a first position and a second position of the aircraft that are separated by a time increment. A centripetal acceleration of the aircraft is deter...  
WO/2014/023989A1
The present disclosure relates to a checklist display system (100), a method, a graphical interface (120) and a computer program product. The checklist display system, method, graphical interface and computer program product display in a...  
WO/2013/160390A3
The present invention relates to a device (10) for cabin pressure difference warning for an aircraft or spacecraft (1), comprising a cabin pressure difference sensor means (12) for detecting the current cabin pressure difference ΔΡ, a ...  
WO/2013/144157A1
The invention relates to a method for determining a credibility state of measurements from an incidence sensor of an aircraft, including at least one test (90, 100) of the consistency between the incidence measurements from said sensor a...  
WO/2013/144126A2
This method for determining a state of credibility of measurements made by static and total pressure sensors and incidence sensors of an aircraft comprises the following steps: - determining (31) a speed of the aircraft, from static and ...  
WO/2013/144126A3
This method for determining a state of credibility of measurements made by static and total pressure sensors and incidence sensors of an aircraft comprises the following steps: - determining (31) a speed of the aircraft, from static and ...  

Matches 1 - 50 out of 636