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Patent Searching and Data


Matches 701 - 750 out of 3,567

Document Document Title
WO/2014/134713A1
A proximity sensor for detecting non-contact detection of a target using a fibre optic strain sensor and a system for operating multiple such proximity sensors is disclosed. The proximity sensor includes an optic fibre that has an optic ...  
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/2014/117248A1
A switch assembly is disclosed having a switch with an actuator moveable from an armed position to a disarmed position. A housing is attached to the switch and contains a cam that holds the switch actuator in the armed position. A trigge...  
WO/2014/106712A1
A method for managing an electric power network (1) of an aircraft, the power network (1) comprising at least one distribution bus arranged to supply electrical loads, at least one generator (G1, G2) of a propulsion engine of the aircraf...  
WO/2014/081614A1
A viewing device for an aircraft includes an image receiver adapted to receive an image of a predetermined spatial area of an exterior of an aircraft, an image projector adapted to display the image of the predetermined spatial area, and...  
WO/2013/074177A3
A turret assembly for attachment on the undersurface of an aircraft that reduces performance limitations due to gimbal lock and reduces the cross section profile of the assembly. The assembly includes a roll actuator including a drive sh...  
WO/2014/057037A1
An aircraft (10) is provided with at least one multifunctional light unit (16) comprising at least one light source (18) for outboard light emission, which unit is provided on sideway facing areas (20) of the aircraft. The multifunctiona...  
WO/2014/028091A3
A helicopter collision-avoidance system is disclosed. An exemplary system includes at least one lamp, such as a light emitting diode (LED) lamp, an incandescent lamp, a halogen lamp, an infrared lamp, or the like; a radar emitter configu...  
WO/2013/181402A3
A lighting arrangement for an aircraft includes a navigational lighting group (42) disposed at a leading edge (36) of a wing (38) of the aircraft. The navigational lighting group includes at least one right of way light (50, 52). The lig...  
WO/2013/142413A3
Anti-icing solid state aircraft lamps are disclosed. The anti-icing solid state aircraft lamp includes at least one solid state light source, a substantially optically transparent cover optically coupled to the at least one solid state l...  
WO/2013/190109A3
The invention relates to an electrical circuit adapted for cutting off an electrical supply to an electrical equipment, said electrical circuit receiving as input at least two discrete electrical signals xi, i=1, N, the electrical circui...  
WO/2014/022316A1
A power stabilizing device in a system includes as a portion of a power converter section, a second PWM converter provided between a second primary AC bus and a second DC bus in an electric system and configured to perform mutual convers...  
WO/2014/018163A1
A modular light emitting diode (LED), remote phosphor, and other lighting technologies lighting assembly includes a plurality of lighting subassemblies and a power supply electrically coupled with the plurality of lighting subassemblies ...  
WO/2007/021013A3
[PROBLEMS] An aircraft in which a payload box can be easily replaced according to purpose of use. [MEANS FOR SOLVING PROBLEMS] An aircraft in which a payload box (400) having various kinds of equipment including a camera loaded in it is ...  
WO/2014/011806A2
Aircraft washlight systems having an asymmetric lens are disclosed. An example vehicle cabin illumination system includes a light source located one side of a surface of a vehicle cabin, and an asymmetric lens through which the light pas...  
WO/2013/190044A1
The invention relates to an electric circuit suitable for cutting off an electric power supply of an electric device, the circuit including an electrical device and a supply voltage source of the electrical device, also having as inputs ...  
WO/2013/186536A1
A method of providing apparatus comprising: providing a first store and a first payload on or in the first store, the first store being for mounting to the outside of an aircraft (4); acquiring aerodynamic properties, moments of inertia,...  
WO/2013/004991A3
Casings (100) and housings for use in high speed airflow (for example for mounting on a high speed vehicle) are described. In one embodiment, a housing for imaging equipment is described. The housing has a tapering form with symmetrical ...  
WO/2013/181402A2
A lighting arrangement for an aircraft includes a navigational lighting group disposed at a leading edge of a wing of the aircraft. The navigational lighting group includes at least one right of way light. The lighting arrangement also i...  
WO/2013/149719A1
Escape route marking for an aircraft with an oblong luminous strip (16) made of a photoluminescent material, a housing (14) in which the luminous strip (16) is arranged and which is formed so as to be translucent or transparent at least ...  
WO/2013/142413A2
Anti-icing solid state aircraft lamps are disclosed. The anti-icing solid state aircraft lamp includes at least one solid state light source, a substantially optically transparent cover optically coupled to the at least one solid state l...  
WO/2013/121709A1
A movable body measuring system comprises: a plurality of receiving stations (1-1 to 1-4) that receive response signals from a movable body (aircraft 5); and a central station (3) that measures the position of the movable body on the bas...  
WO/2013/051967A3
The invention relates to aircraft takeoff or landing indicator devices. The method for the visual landing of an aircraft comprises determining the altitude of the aircraft on the basis of an on-board altimeter and using the human eye. Th...  
WO/2013/094526A1
This control apparatus is provided with: a sea route control unit (20) that makes an unmanned aircraft travel in a direction that intersects the traveling direction of an escort ship, within a prescribed search area width in the directio...  
WO/2013/090756A1
The present disclosure is directed to a light emitting diode (LED) signal light. In one embodiment, the LED signal light includes at least one visible LED, at least one infrared (IR) LED, a reflector, wherein the reflector collimates a l...  
WO/2013/053538A1
The invention relates to an aerial camera (1), comprising at least one objective (13), a number of optoelectronic and/or electronic components (2b, 3b, 4), and a housing (1a), which comprises the at least one objective (13) and the optoe...  
WO/2013/051300A1
The present invention addresses the problem of obtaining a disaster circumstance ascertainment system with which it is possible to rapidly provide information for efficiently carrying out rescue activities, including identifying disaster...  
WO/2012/165887A3
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/2013/033924A1
A dual-axis ball head for use in an unmanned aerial vehicle, a triple-axis ball head for use in the unmanned aerial vehicle, and a multi-rotor aerial vehicle, comprising a machine frame component, a transmission component, and a photogra...  
WO/2013/033925A1
A dual-axis ball head for use in an unmanned aerial vehicle and a triple-axis ball head for use in the unmanned aerial vehicle, comprising a machine frame component, a transmission component, and an image-capturing component (1). The mac...  
WO/2011/120110A8
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/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...  

Matches 701 - 750 out of 3,567