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Patent Searching and Data


Matches 1,001 - 1,050 out of 4,011

Document Document Title
WO/2004/042672A2
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...  
WO2001086442A3
Techniques for inter-application communication and handling of I/O devices in an Integrated Modular Avionics (IMA) system enable the integration of multiple applications (B) while maintaining strong spatial and temporal partitioning betw...  
WO2003055077A3
The disclosed electronic processing apparatus calculates and applies calibrations to sensors that produce quasi-sinusoidal, quadrature signals. The apparatus includes either or both of fixed and programmable electronic circuits. The appa...  
WO2002075235A3
A stealth airborne suspended operating system, such as imaging sensor (camera 12), dusting sprinkling device etc., for suspension and operation beneath an aircraft (10), the system comprising a suspension device (14) of predetermined len...  
WO/2004/009723A2
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/2004/000645A1
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...  
WO/2003/102505A1
An airborne reconnaissance system comprising: (1) Gimbals having at least two degrees of freedom; (2) At least one array of light sensors positioned on the gimbals, for being directed by the same within at least two degrees of freedom; (...  
WO/2003/095894A1
A light source utilizes a parabolic reflector (10, 10a) to collimate light emitted at greater than a predetermined angle (alpha) relative to the optical axis Ao of an LED (42) arranged at the focus of the reflector. An optional collimati...  
WO2002101289A3
An efficient redundant light distribution system includes redundant light generation enclosures providing light to a collector array 10, coupled to an ultraviolet to red converter 20, a combination array 30, a distribution array 40 and m...  
WO2003054775A3
The presend invention achieves an accurate and quick centreline identification in a docking guidance system and further a verification of a centreline configuration. Heretofore, it is proposed to scan (S1) an apron in front of a docking ...  
WO/2003/078246A1
A vertical take-off and landing miniature aerial vehicle includes an upper fuselage segment (12) and a lower fuselage segment (14) that extend in opposite directions from a rotor guard assembly (16). A rotor (52) rotates within the rotor...  
WO2003058586B1
Erfindungsgemäss vorgeschlagen wird eine Vorrichtung zur Wiedergabe von Lichtstrahlung an einer Hülle eines Luftfahrzeuges, mit mindestens einer Lichtquelle zur Erzeugung von Lichtstrahlung mindestens einer Projektionseinrichtung zur W...  
WO/2003/077217A1
An apparatus for monitoring persons within predetermined areas, characterised by comprising: - a plurality of tags (2), irremovably applicable to persons (6) wearing them and containing data characteristic of them, - at least one sensor ...  
WO/2003/068599A1
An aircraft light assembly comprises a light apparatus configured to be supported in a space on the body of an aircraft. The apparatus has one or more light emitting diodes (13) generating visible light and an outer structure overlying t...  
WO/2003/064919A1
A light cover has a transparent element (2) manufactured from polycarbonate and an infrared filter (12) angled so as to reflect infrared radiation emitted from a light source (16) away from both the transparent element (2) and the light ...  
WO/2003/058571A1
An airborne surveillance system for monitoring activity on an aircraft flight deck and in a passenger compartment of an aircraft or other form of mobile platform and relaying the images in real time to a remote monitoring location. The s...  
WO/2003/058586A1
The invention relates to a device and method for displaying luminous radiation on a shell of an aircraft, comprising at least one light source for producing luminous radiation, and at least one projection device for converting the lumino...  
WO2002028711A8
A dual mode light source unit (3) for an aircraft is configured to be secured into a socket for an incandescent navigation light bulb. The unit has electric circuitry configured to process the input current from the socket and based ther...  
WO/2003/055077A2
The disclosed electronic processing apparatus calculates and applies calibrations to sensors that produce quasi-sinusoidal, quadrature signals. The apparatus includes either or both of fixed and programmable electronic circuits. The appa...  
WO/2003/054831A1
The present invention achieves an accurate and quick centreline identification in a docking guidance system and further a verification of a centerline configuration. Heretofore, it is proposed to scan an apron in front of a docking stand...  
WO/2003/054775A2
The presend invention achieves an accurate and quick centreline identification in a docking guidance system and further a verification of a centreline configuration. Heretofore, it is proposed to scan (S1) an apron in front of a docking ...  
WO/2003/050581A1
The subject invention pertains to a method and apparatus for multiplexing in optical fiber communications. The subject invention relates to a method and apparatus for spatial domain modulation in optical wavelengths. In a specific embodi...  
WO/2003/050957A1
A solid state control switching and control system (200) for retractable landing lights. A control unit (208) uses an absolute position sensor (214) to monitor the position of the lighthead (210) of the retractable landing light, and act...  
WO/2003/050002A1
An electronically controlled retractable landing light (100) for use with aircraft. A controller (106) compares the commanded position of a lighthead (108) by means of a contactless absolute position sensor (212).Operation of a brake (11...  
WO2003021187A3
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/2003/045777A1
An aircraft monitoring system including the tracking and transmission of video images from cameras located at various points on the exterior and in the interior of an aircraft. The video images are transmitted in a continuous stream to v...  
WO/2003/043885A1
The invention concerns a remote-controlled flying craft, used in particular for aerial photography, comprising a nacelle (100) removably fixed to a levitating portion (1), the nacelle (100) including an elongated portion (101) which rece...  
WO/2003/039957A1
A multi-mode visible and infrared lighthead (100) for use as a landing light or searchlight. The mult-mode lighthead incorporates a modular design wherein at least one visible light source (200) and at least one infrared diode (302) are ...  
WO2002070343A3
A remote-control powered parafoil aircraft has an aircraft body (1) that is engine powered and hung with lines (2) from an air-expandable wing (3, 20). The lines include control lines (15) with which air flow and aerodynamic shape of the...  
WO/2003/024175A1
A design and installation method are provided to improve access to equipment mountable on aircraft equipment racks, including installing modified equipment rack framework on the aircraft, preassembling the equipment on a separate equipme...  
WO/2003/021187A2
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...  
WO2002095440A3
A closed loop radar power management system includes a radar sensor that transmits a terrain tracking signal and that receives a reflection of the terrain tracking signal. The radar sensor produces a terrain feature signal in response to...  
WO2002041276A3
A light emitting diode (LED) warning signal light and communication device comprising a controller for generating a first observable light signal and a second non-observable light signal within said first light signal. The second light s...  
WO/2002/102662A1
The invention relates to an anti-collision light for aircraft that is suitable for both daytime and night-time use. Prior art discloses separate daytime lights with a high light intensity and night-time lights with low infra-red radiatio...  
WO/2002/101289A2
An efficient redundant light distribution system includes redundant light generation enclosures providing light to a collector array 10, coupled to an ultraviolet to red converter 20, a combination array 30, a distribution array 40 and m...  
WO2001042932A3
Integrated Modular Avionics (101) can take advantage of faster modern processors and can run multiple existing avionics software applications (321) on a single processor (201) by using a two-layer operating system consisting of a system ...  
WO/2002/095440A2
A closed loop radar power management system includes a radar sensor that transmits a terrain tracking signal and that receives a reflection of the terrain tracking signal. The radar sensor produces a terrain feature signal in response to...  
WO/2002/075235A2
A stealth airborne suspended operating system, such as imaging sensor (camera 12), dusting sprinkling device etc., for suspension and operation beneath an aircraft (10), the system comprising a suspension device (14) of predetermined len...  
WO/2002/070343A2
A remote-control powered parafoil aircraft has an aircraft body (1) that is engine powered and hung with lines (2) from an air-expandable wing (3, 20). The lines include control lines (15) with which air flow and aerodynamic shape of the...  
WO/2002/068861A1
The invention relates to a lighting and signaling device (1) for motor vehicles or airplanes. The device comprises a light source (6) and means for focusing the radiation of said source onto the entry end of a transparent rod (2). Said r...  
WO/2002/068253A1
An electrical distribution system is disclosed that includes a gateway module (100) including logic (112) to interface to a vehicle management computer (VMC) (50) via a dual redundant standard data bus (1). The gateway module (100) has r...  
WO/2002/049915A1
A dual mode visible and infrared lighthead (100) for use as a landing light or searchlight. The dual mode lighthead incorporates a modular design wherein at least one visible light source (200) and at least one infrared diode (302)are mo...  
WO/2002/049917A1
An LED strobe light is disclosed. The strobe light (600) uses light emitting diodes (402) arranged about the circumference of an electrically insulative, thermally conductive disk (404) to form an LED light ring (400). LED Light rings (4...  
WO/2002/049916A1
An infrared LASER diode based high intensity light (100) for use as an aircraft landing light or searchlight in conjunction with night vision imaging systems. The high intensity light (100) uses infrared LASER diodes (110) installed into...  
WO2002028711A3
A dual mode light source unit (3) for an aircraft is configured to be secured into a socket for an incandescent navigation light bulb. The unit has electric circuitry configured to process the input current from the socket and based ther...  
WO/2002/041276A2
A light emitting diode (LED) warning signal light and communication device comprising a controller for generating a first observable light signal and a second non-observable light signal within said first light signal. The second light s...  
WO/2002/028711A2
A dual mode light source unit (3) for an aircraft is configured to be secured into a socket for an incandescent navigation light bulb. The unit has electric circuitry configured to process the input current from the socket and based ther...  
WO2001043308A3
A system for interfacing commercial satellite communications technology with military aircraft communications systems is disclosed. The system includes an off-board commercial transceiver and an onboard commercial transceiver for communi...  
WO2001032505A3
An aircraft orientation system that locates the earth's horizon, in order to determine the aircraft's attitude in the pitch and roll axes. The invention takes advantage of the fact that the earth's surface is typically warmer than the sk...  
WO/2001/099429A1
A video imaging apparatus for receiving, recording, and displaying images from a vehicle in which the video camera (568) connects to a lateral upper portion of a seat (566) in the vehicle. A member communicates light representative of an...  

Matches 1,001 - 1,050 out of 4,011