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WO/2012/058260 |
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...
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WO/2012/055663 |
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 ...
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WO/2012/044964 |
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...
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WO/2012/030076 |
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...
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WO/2012/030076 |
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...
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WO/2012/019695 |
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...
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WO/2012/012036 |
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...
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WO/2012/006158 |
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...
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WO/2012/003512 |
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...
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WO/2012/003512 |
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...
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WO/2011/133598 |
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...
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WO/2011/131817 |
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...
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WO/2011/120110 |
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...
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WO/2011/114278 |
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...
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WO/2011/114278 |
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...
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WO/2011/106623 |
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...
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WO/2011/095660 |
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...
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WO/2011/081289 |
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,...
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WO/2011/081289 |
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,...
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WO/2011/077152 |
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...
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WO/2011/074245 |
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...
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WO/2011/066410 |
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...
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WO/2011/058076 |
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...
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WO/2011/052822 |
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 ...
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WO/2011/051526 |
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)...
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WO/2011/051526 |
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)...
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WO/2011/047998 |
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...
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WO/2011/045001 |
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.
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WO/2011/045001 |
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.
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WO/2011/032909 |
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...
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WO/2011/029127 |
A lighting assembly, including a base supporting a row of one or more light emitting elements in an outward facing configuration for emitting light away from said base; and one or more optical elements, each corresponding to a different ...
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WO/2011/029432 |
The invention relates to a device and a method for determining and indicating, on board of an airplane (101), any climate-relevant effects of a contrail produced by the airplane (101). The method for determining and indicating, on board ...
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WO/2011/017812 |
An automated aircraft flight data and delivery management system and method operates in a normal state and a demand state. The demand state may be self-initiated or manually-initiated, and may be triggered during situations which include...
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WO/2011/014940 |
A system of video cameras for aircraft used to monitor the interior of commercial passenger and cargo aircraft in general, belonging to the electric and electronic fields, using wire-based or wireless video cameras to monitor all interio...
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WO/2011/012138 |
The invention relates to an autonomous stratospheric aircraft which is lighter than air and to a method for providing radio and optical communication, television broadcasting and monitoring with the aid of an apparatus arranged on said a...
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WO/2011/010942 |
The present invention relates to an automated distress locator transmitter assembly adapted to be installed on transportation means such as aircrafts and the like comprising : a base member having a primary enclosure downwardly formed fr...
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WO/2011/010641 |
Provided is an image capturing device for optically scanning an image-capturing target by moving toward a predetermined scanning direction and for capturing an image of the image-capturing target. The image capturing device comprises: a ...
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WO/2011/005851 |
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 ...
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WO/2011/005851 |
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 ...
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WO/2010/140082 |
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...
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WO/2010/140082 |
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...
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WO/2010/122017 |
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...
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WO/2010/079042 |
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...
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WO/2010/079042 |
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...
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WO/2010/079042 |
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...
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WO/2010/076520 |
The invention relates to an aeronautical vehicle (2) comprising a spectrometer (4) suitable for generating a spectral analysis of radiation reflected by a portion (12) of the earth's surface, the vehicle (2) being in orbit around the ear...
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WO/2010/065999 |
The present system provides a buoyancy system for moving an object (401) in a body of water. The system comprises at least one inflatable body (17) which, when inflated, increases the buoyancy of the object (401), and an inflation appara...
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WO/2010/067858 |
A desired search range is efficiently monitored. Provided is a monitoring device which is mounted in the body of an airplane flying in the sky and monitors the state of the sea from the sky, the monitoring device being provided with a l...
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WO/2010/065037 |
An eccentric fitting assembly includes an outer eccentric fitting which defines an outer axis, the outer eccentric fitting defines an opening offset from the outer axis and an inner eccentric fitting which defines an inner axis, the inne...
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WO/2010/064548 |
The unmanned aircraft is equipped with a camera, a laser ranging system, and a drive unit. The laser ranging system measures the distance to an object in the camera field of view. The drive unit rotates the field of view. Information on ...
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