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Patent Searching and Data


Matches 851 - 900 out of 4,026

Document Document Title
WO/2013/032078A1
The present invention relates to a method and system for unmanned airborne collection and transmission of information during flight, and to technology for performing an unmanned flight using an air-collecting body, descending from a pred...  
WO/2013/019210A1
An unmanned aircraft system has an airframe and a payload pod detachably secured to the unmanned aircraft system under the airframe and a nacelle attached atop the airframe. The UAS is payload agnostic and provides the platform to which ...  
WO/2013/006210A1
Data recording systems (100) and methods (400) for synchronizing data of a plurality of different data types on a single packet (300). The methods involve: receiving the data and an audio frame containing voice data and timing data commu...  
WO/2012/118731A3
Lighter-than-air systems, methods, and kits for obtaining aerial images are described. For example, various methods for determining planned ascent, drift, and/ or descent of a lighter-than-air system are described. In addition, various s...  
WO/2012/148232A3
The present invention relates to an aircraft, and more specifically, to an aircraft instrument display system which automatically recognizes the facial image of a pilot to verify the identity of the pilot, and then displays and memorizes...  
WO/2012/162910A1
An aviation recorder submarine search device and a method thereof are provided. The device comprises a black box (1), and the black box (1) is set in an ejection tube device (2), and a first cabin door (3) is set on one side of the eject...  
WO/2012/165887A2
The present invention pertains to a technique for supplying power to an object in midair, and more specifically, to a ground-level power supply system for a small unmanned aerial robot to continuously supply power as a power source for t...  
WO/2012/148232A2
The present invention relates to an aircraft, and more specifically, to an aircraft instrument display system which automatically recognizes the facial image of a pilot to verify the identity of the pilot, and then displays and memorizes...  
WO/2012/131105A1
The invention relates to an aircraft (11) comprising a system for observing part of the external environment of the aircraft. The environment observation system comprises a camera, known as a panoramic camera (21, 22, 23), including a st...  
WO/2012/131101A1
The invention relates to an aircraft (11) comprising an enclosure and a system for surveilling areas of interest inside the enclosure. The enclosure includes a transverse aisle (13) and a longitudinal aisle (15) that intersect at an inte...  
WO/2012/044964A3
Methods for estimating a yaw angle of a body reference system of a device relative to a gravitational reference system using motion sensors and a magnetometer attached to the device are provided. A method includes (A) receiving measureme...  
WO/2012/058260A3
Embodiments of the present invention relate to a system for monitoring the characteristics of key components of aeronautical machines (e.g., airplanes, helicopters, etc.), processing obtained data, and delivering prognostic health indica...  
WO/2012/083733A1
A navigation light comprises: a light source (1), a transparent lampshade (2), a reflective mask (3) and a baseboard (4). The reflective mask (3) and the transparent lampshade (2) are connected as a whole and fixed together on the basebo...  
WO/2012/055663A3
Disclosed is a method and an arrangement to determine an incidence of loading of an aircraft structure, wherein a true reality of at least one aircraft structural section is superposed with the virtual reality of the aircraft structural ...  
WO/2012/080280A1
The general field of the invention is that of aircraft cockpit display systems requiring enhanced alertness for certain nighttime missions or flights. The system according to the invention comprises strictly blue-colored lighting means: ...  
WO/2012/058260A2
Embodiments of the present invention relate to a system for monitoring the characteristics of key components of aeronautical machines (e.g., airplanes, helicopters, etc.), processing obtained data, and delivering prognostic health indica...  
WO/2012/055663A2
Disclosed is a method and an arrangement to determine an incidence of loading of an aircraft structure, wherein a true reality of at least one aircraft structural section is superposed with the virtual reality of the aircraft structural ...  
WO/2012/030076A3
The present invention relates to a rotor driven flight vehicle incorporating small bottom wings for use as a type of unmanned aircraft. Lower wing type flight vehicles of the prior art need complicated structures which are formed by comb...  
WO/2012/003512A3
An aircraft hover system for enabling an aircraft to hover at a target spatial location represented by GPS location coordinates. The hover system includes a display screen rendering a display including live video feed of the terrain belo...  
WO/2011/131817A3
System for providing an enhanced night vision of a scene from an observation place, such as a system for providing an enhanced night vision of the scene (15) of an aerial refuelling operation of tanker aircraft (11), the system operating...  
WO/2012/044964A2
Methods for estimating a yaw angle of a body reference system of a device relative to a gravitational reference system using motion sensors and a magnetometer attached to the device are provided. A method includes (A) receiving measureme...  
WO/2012/030076A2
The present invention relates to a rotor driven flight vehicle incorporating small bottom wings for use as a type of unmanned aircraft. Lower wing type flight vehicles of the prior art need complicated structures which are formed by comb...  
WO/2012/019695A1
The invention relates to a method and a system (10) for displaying information on an electrical display unit (18) in an aircraft cabin (11). The system (10) comprises a generating unit (12) for generating at least one signal which clearl...  
WO/2012/012036A1
Methods and apparatus are provided to control flow separation of an ambient flow along a surface and about a turret (12), such as by reducing flow separation aft of the turret. By reducing flow separation, the resulting turbulence may be...  
WO/2012/006158A1
In one possible embodiment, a UAV payload module retraction mechanism is provided including a payload pivotally attached to a housing. A biasing member is mounted to bias the payload out of the housing and a winch is attached to the payl...  
WO/2011/114278A3
The application discloses an aeronautical input/output device (70) for flight task management which comprises a display unit (90) with a housing (97), and a keyboard unit (91) which is adapted to communicate with the display unit (90). T...  
WO/2012/003512A2
An aircraft hover system for enabling an aircraft to hover at a target spatial location represented by GPS location coordinates. The hover system includes a display screen rendering a display including live video feed of the terrain belo...  
WO/2011/133598A3
An aircraft ceiling module includes a ceiling panel (12) with integrated lighting, valences (16) and wiring. LED lighting units (14) are mounted directly to the ceiling panel, and one or more valence panels (16) are connected to the ceil...  
WO/2011/047998A3
The present invention relates to a control device (10) for a cabin of an aircraft or spacecraft, comprising a first control means (11) for actuating at least one camera (21-23) by means of at least one first control signal (51), set up f...  
WO/2011/120110A1
The present object refers to an aeronautical safety device coupled to the aircraft black box, which will be activated when the equipment submerges to a certain depth, after an air accident occurring on oceans, rivers or lakes. The device...  
WO/2011/114278A2
The application discloses an aeronautical input/output device (70) for flight task management which comprises a display unit (90) with a housing (97), and a keyboard unit (91) which is adapted to communicate with the display unit (90). T...  
WO/2011/045001A3
The present invention relates to a warning light for aircraft, comprising a light source (110) and a wide-angle lens (120), the light source being optically connected to the wide-angle lens.  
WO/2011/106623A1
A method and associated illumination system are provided for illuminating an interior of a vehicle with a modular area illumination system, the modular area illumination system comprising: a system controller; and a plurality of an intel...  
WO/2011/095660A1
The invention relates to a laser-technology-based system that can be used to manoeuvre any type of aircraft on the ground, providing the crew with a visual reference and thus preventing the vast majority of situations in which the safety...  
WO/2011/032909A3
The invention relates to components (100, 120, 140) of an aircraft network (200), which can automatically configure and repair said network (200). The invention also relates, in particular, to a control device (100) for an aircraft netwo...  
WO/2011/081289A9
Provided is a convenient airplane seat system having a modified seat arrangement to reduce contact and interference between adjacent passengers. In the airplane seat system, a plurality of seats, each having a seat part, a backrest part,...  
WO/2011/051526A9
Aerial system for transmitting video and images via satellite in real time, composed of two main parts: the shipped part (30) which has sensors (1) and (2) for capturing video and images, an electronic switch (3), several coders (4), (5)...  
WO/2010/079042A4
The invention relates to an aeroplane structure comprising structural elements (10, 12, 13); a first plurality of lines (11) fixed to structural elements (10); a second plurality of lines (14, 15) fixed to structural elements (12, 13), t...  
WO/2011/081289A1
Provided is a convenient airplane seat system having a modified seat arrangement to reduce contact and interference between adjacent passengers. In the airplane seat system, a plurality of seats, each having a seat part, a backrest part,...  
WO/2011/077152A1
Disclosed is air vehicle mounted or mountable transmitting and/or receiving equipment (1) including a transmitting and/or receiving turret (7) allowing at least a forward field of view, said device being mounted or mountable on a fuselag...  
WO/2011/074245A1
Provided is an electronic system mounted on an aircraft, wherein it is possible to reduce the number of wires and electronic devices needed by integrating the control system. Specifically, the airframe (80) of an aircraft (100) is divide...  
WO/2011/066410A1
Embodiments include an assembly comprising: (a) a camera support structure comprising: a masthead (320) disposed on the distal end of a mast (210) wherein the masthead (320) is configured to receive an imaging element (1110); where a pro...  
WO/2011/058076A1
The invention relates to an integrated end-to-end maintenance platform (1) for maintenance of an aircraft (8) comprising a customer interface for selecting a customized service package including modular services of different aircraft mai...  
WO/2010/079042A3
The invention relates to an aeroplane structure comprising structural elements (10, 12, 13); a first plurality of lines (11) fixed to structural elements (10); a second plurality of lines (14, 15) fixed to structural elements (12, 13), t...  
WO/2011/051526A1
Aerial system for transmitting video and images via satellite in real time, composed of two main parts: the shipped part (30) which has sensors (1) and (2) for capturing video and images, an electronic switch (3), several coders (4), (5)...  
WO/2011/052822A1
The present invention relates to a portable unmanned airship for magnetic-force surveying and to a magnetic-force surveying system employing the same, comprising: a main airship body propelled under its own power using the buoyancy of a ...  
WO/2010/122017A3
The invention relates to a multi-functional module (100) for a passenger utility conduit (101) in an aircraft (500), comprising a first interface (102) and at least one utility unit (103) for providing a passenger with services. The firs...  
WO/2011/045001A2
The present invention relates to a warning light for aircraft, comprising a light source and a wide-angle lens, wherein the light source is optically connected to the wide-angle lens.  
WO/2011/005851A3
The invention is an aerostat assembly, specifically an aerostats assembly including a camera for aerial photography. The aerostat assembly includes a boom assembly joined to a buoyant aerostat balloon. The boom assembly includes a pivot ...  
WO/2010/140082A9
A UAV with an engine (34) attached to rear (38) of its fuselage by an engine mounting assembly with the rotational axis of the engine generally parallel with the axis (45) of the fuselage. The engine mounting assembly includes a fuselage...  

Matches 851 - 900 out of 4,026