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Patent Searching and Data


Matches 951 - 1,000 out of 4,011

Document Document Title
WO/2008/037030A1
An aircraft advertising display system includes an emergency drop arrangement, including a ballast release mechanism for releasing ballast which will actuate after the system has been released from an aircraft but prior to the deployment...  
WO2004065214A3
Refers the present object to an unpublished and functional emergency device for aircrafts, to alert in the skies, through illumination originating from laser beam light, the identification of the aircraft, company, number of the flight, ...  
WO/2008/024256A2
A new generation of simplified vehicle electronic systems can be operated by either an onboard (manned) or off-board (remote controlled) operator, or automatically from an on-board system without any human operator. In the latter case, p...  
WO/2008/003546A1
The present invention relates to a method of monitoring the condition of structural components, in which an optical sensor in conjunction with a computing unit ascertains image deviations from successive images of the structural componen...  
WO/2007/002403A3
An optical light guide has a substantially rigid light transmissive body (120) having an input window (140), a distal end (160), a front side (180) and a rear side (200).The light transmissive body (120) has a substantially smooth exteri...  
WO/2007/141795A1
An unmanned air vehicle (UAV) system (10), is provided including a ground station (70), a platform (20) configured for carrying a payload (40) and having a propulsion system (30) for enabling the platform at least to selectively sustain ...  
WO/2007/136262A1
Aircraft vehicle (1), comprising one or more light emitting devices (2,3) arranged to emit a converging light beam (4) which intersect (5) at a predetermined level (6) below the aircraft vehicle. Each light-emitting device may comprise e...  
WO/2007/055634A1
A method for the transport of an aircraft, such as a transport or passenger aeroplane, on the ground after nightfall, a towing tractor being coupled to a nose wheel of the aircraft, the propulsion engines of which are shutdown, the aircr...  
WO/2007/038652A2
An improvement in LED lighting simulative of neon lighting comprises a light cable (3). A clamp (2) coupled to the cable (3) holds an end of the cable (3) in a predetermined bend, and an LED (14) is optically coupled to the cable (3). A ...  
WO/2007/030874A1
A mounting body (21) for attachment to a floor (20) of a helicopter (10) having opposed sides (62) wherein the mounting body (21) is oriented transversely to a longitudinal axis of the helicopter (10) in use and extends between opposed d...  
WO/2006/107989A3
An apparatus and method for providing backlighting for panel displays utilizing fiber optics.  
WO/2007/003403A1
The invention relates to a universal retaining device (1), particularly for fastening different panel elements and/or accessory parts in aircraft, comprising: a base plate (2) for fastening to a substructure; a support plate (3) connecte...  
WO2006091225B1
A rotationally symmetrical anti-collision light (100, 200) for an aircraft utilizing light-emitting diodes (LEDs) is mounted to the fuselage of an aircraft. The LEDs (10, 10', 20, 20') may be configured in one or more concentric rings. T...  
WO2006042052A3
A multicolored LED vehicle interior light is described. In various implementations, a switch is used to select one of a plurality of LED lights, in which one light is of a color, such as red, which is suitable for preserving night vision.  
WO/2006/106730A1
A fuselage information display panel (71) for a flying body, displaying vertically and horizontally arranged display sections (71a) provided by different information items. The display sections changes their colors depending on informati...  
WO/2006/107989A2
An apparatus and method for providing backlighting for panel displays utilizing fiber optics.  
WO/2006/098469A1
A flight control system has a flying body (1) and a ground station (40) that can communicate with each other. A fuselage of the flying body and a payload device are controlled from the ground station. The flying body (1) transmits data o...  
WO/2006/091225A1
A rotationally symmetrical anti-collision light (100, 200) for an aircraft utilizing light-emitting diodes (LEDs) is mounted to the fuselage of an aircraft. The LEDs (10, 10', 20, 20') may be configured in one or more concentric rings. T...  
WO2004000645A8
A position light (200) for use on an aircraft. The aircraft position light uses light sources (302) installed into an alignment fixture (304) which optionally carries away heat generated by the light sources. Light emitted by the light s...  
WO2005042342A3
Method and systems for starting propeller driven aircraft and other devices. A system in accordance with one embodiment of the invention includes a removable fixture (130) that is coupled to the propeller (120) and has at least one porti...  
WO/2006/050350A2
A compact lamp assembly (10) for use in interior vehicle application such as reading and courtesy lighting. The lamp assembly (10) includes a housing (12), a circuit board (14), and an LED (16). The housing (10) has a front wall (20) wit...  
WO/2006/031620A2
A rotating beacon system (10) and a method for synchronizing multiple rotating beacons (20, 30). The rotating beacon system includes two or more rotating beacons (20, 30) and a feedback based control system (60) adapted to sense an angul...  
WO/2006/027762A1
The present invention relates to a collision avoidance warning system for an aircraft (1). The system comprises a light source (8, 9), sensors (10, 11, 12) mounted on the aircraft (1) and processing means for determining the dimensions a...  
WO/2006/010015A1
A white anti-collision light mounted on an aircraft utilizes a set of high¬≠ power light-emitting diodes (LEDs) (110) and dedicated reflectors (120) to distribute the light in a particular pattern that satisfies predetermined intensity r...  
WO2005056384A3
A system and method for an aircraft (10) that provides an IR decoy (12) for an incoming missile (18) to track instead of an engine (14) of the aircraft (10) is disclosed. The IR decoy (12) is deployed during or just after take off, and p...  
WO/2005/120950A1
An illuminating system, device, and method are provided to illuminate an in-flight refueling operation involving a first aircraft (110), serving as a tanker aircraft and carrying the illuminating system (115) of the present invention, an...  
WO/2005/113334A1
An aircraft with a fluid-duct system for extraction of the laminar layer and/or blowing out of fluid at vulnerable places of the outer skin, wherein the fluid-duct system (26, 19, 18) by means of switchable valves (6, 4) is connectable t...  
WO/2005/100915A1
An aerial imaging system has an image storage medium locatable in an aircraft, a controller that controls the collection of image data and stores it in the storage medium and a digital camera assembly that collects image data from a regi...  
WO/2005/090157A1
An aircraft rear position light device (1) has a modular configuration. The device utilizes solid-state light sources. In an exemplary embodiment, the light sources are side-emitting light-emitting diodes (LEDs) (40), which are attached ...  
WO/2005/080198A1
There is disclosed a plurality of sufficient closely-packed functional units which are interconnected to form a non¬≠planar payload module assembly (40). Advantageously, the payload modular structure (40) is compact with few piece parts,...  
WO/2005/078545A1
The group of inventions relates to methods for controlling a helicopter position in a low-speed and hovering mode above a specified point. The inventive method consists in carrying out the television tracking of a surface under the helic...  
WO/2005/075288A1
An airship equipped with a function for projecting a video image from a video image projecting means, e.g. a projector, onto a video image display means disposed in the airship body, wherein the optical path of the video image being proj...  
WO/2005/066024A1
The invention relates to a modular optronic system (30) onboard a carrier, such as a combat aircraft, a helicopter or a drone aircraft. The inventive system comprises at least one optronic element (41, 42) having a target line that can b...  
WO/2005/063571A1
The invention proposes that a camera (18) takes a technical picture of an air outlet valve (10) of an aircraft, and the picture taken of the outlet valve (10) is displayed on a picture display unit (20), for example in the cockpit of the...  
WO/2005/061324A1
An aircraft forward position lighting device (1) has a modular configuration, including a mounting module (20) containing solid-state light sources, e.g., light-emitting diodes (LEDs) (210, 230). The mounting module also includes reflect...  
WO/2005/056384A2
A system and method for an aircraft (10) that provides an IR decoy (12) for an incoming missile (18) to track instead of an engine (14) of the aircraft (10) is disclosed. The IR decoy (12) is deployed during or just after take off, and p...  
WO/2005/044663A1
Pilot director Lights (PDLs) mounted on the exterior of a refueling tanker aircraft (10) utilize light emitting diodes (LEDs) (213) as a light source to provide visual information to the pilot of an approaching aircraft (30). The PDLs ma...  
WO/2005/025986A1
The invention provides a control station (5) for use an surveillance aircraft. Controls for each surveillance accessory (lights, cameras etc) are lead to a station having a single VDU (8) and a single hand control (10). The VDU (10) and ...  
WO2005009840A3
Methods and apparatus for illumination of aerial refueling hoses are disclosed. In one embodiment, a conduit for transferring a flowable material includes a wall member. A plurality of optical fibers are at least one of formed within an ...  
WO2004009723A8
Low light level illumination is applied to rotary blades (102, 202) of vehicles to increase visibility to minimize ground injuries. Either photoluminescent paint (208) or photoluminescent film (104) may be affixed to rotary blades (102, ...  
WO/2005/009840A2
Methods and apparatus for illumination of aerial refueling hoses are disclosed. In one embodiment, a conduit for transferring a flowable material includes a wall member. A plurality of optical fibers are at least one of formed within an ...  
WO2004094230A3
A window mounting system for optical sensors including a removable connection for window replacement, an alignment system to assure precision registration of the window or dome with the sensor internal optics, and thermal insulation to l...  
WO/2004/102296A1
The system guarantees a protection against voluntary crashes resulting from a malicious act by a person on board or from an error of trajectory, comprising an Overflight Area Protection System OAPS (54), operating in the manner of a Terr...  
WO/2004/094231A1
A lighting device includes one or more diode light sources (32), which are configured to emit light into the peripheral edges of a light guide (20). The light guide (20) includes a set of diffusing elements (22) for scattering the emitte...  
WO/2004/094230A2
A window mounting system for optical sensors including a removable connection for window replacement, an alignment system to assure precision registration of the window or dome with the sensor internal optics, and thermal insulation to l...  
WO/2004/074097A1
The present invention is an apparatus and method for monitoring events on board a transportation vehicle. The apparatus includes a communication system configured to stream data from the transportation vehicle (26) to an external locatio...  
WO2004042672A3
A hazard avoidance system for a vehicle (10) utilizes data related to a location of a collision threat (12), conditions at the location, and vehicle operating parameters (148) to select a light illumination routine that is optimal to att...  
WO/2004/065214A2
Refers the present object to an unpublished and functional emergency device (1 ) for aircrafts (2), to alert in the skies, through illumination originating from laser beam light (6), the identification of the aircraft (2), company, numbe...  
WO/2004/063642A1
Carbon dioxide as a refrigerant is filled in a refrigerant circuit (10) of a refrigeration apparatus. In the refrigerant circuit (10), a first compressor (21) and a second compressor (22) are arranged in parallel. The first compressor (2...  
WO2004009723A3
Low light level illumination is applied to rotary blades (102, 202) of vehicles to increase visibility to minimize ground injuries. Either photoluminescent paint (208) or photoluminescent film (104) may be affixed to rotary blades (102, ...  

Matches 951 - 1,000 out of 4,011