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Iden

Hiroshi Iden, Kanagawa JP

Patent application numberDescriptionPublished
20100203407FUEL CELL SYSTEM WITH REGENERATION OF ELECTRODE ACTIVITY DURING START OR STOP - A performance recovery operation for a fuel cell system effectively restores a fuel electrode such that, upon starting or stopping of operation of the fuel cell, both fuel and oxidizing electrodes are disposed in a hydrogen atmosphere and then the fuel electrode is maintained at a higher potential level than in a normal operation.08-12-2010

John Iden, Platte City, MO US

Patent application numberDescriptionPublished
20110094143Remote control decoy - A remote controlled decoy is provided. The remote control decoy operates using two propellers secured to a hull and remotely controlled by a radio frequency transmitter. A shell resembling a particular waterfowl is releasably coupled to a hull which serves as a watertight compartment for the receiver and the electronics associated with the propulsion of the decoy. The decoy may also be provided with strobe lights to draw attention to the decoy from passing waterfowl.04-28-2011

Mark C. Iden, Burien, WA US

Patent application numberDescriptionPublished
20090317587REINFORCED STIFFENERS AND METHOD FOR MAKING THE SAME - A composite stiffener is fabricated using preforms of laminated, unidirectional composite tape. The stiffener includes a void that is reinforced by a filler wrapped with a structural adhesive. The surfaces of the preforms surrounding the void include a layer of composite fabric which is bonded to the filler by the adhesive, thereby increasing the toughness of stiffeners around the void and improving pull-off strength of the stiffener.12-24-2009

Steven M. Iden, Dayton, OH US

Patent application numberDescriptionPublished
20090302153ELECTRICAL SYSTEM AND ELECTRICAL ACCUMULATOR FOR ELECTRICAL ACTUATION AND RELATED METHODS - An electrical system for driving flight control actuators, electrical accumulator, and methods for managing electrical power for an aircraft electrical system and methods of retrofitting an aircraft electrical system with an electrical accumulator are provided. The electrical system can include a bidirectional accumulator positioned in electrical communication with the plurality of flight control actuators to absorb excess electrical power regenerated by the plurality of flight control actuators and to provide supplemental power to the plurality of flight control actuators to thereby satisfy transient power requirements.12-10-2009

Tamon Iden, Nara JP

Patent application numberDescriptionPublished
20090034827Inspection device, inspection method, method of manufacturing color filter, and computer-readable storage medium containing inspection device control program - An inspection device of the present invention includes: a linear irregularity detecting section for detecting linear irregularities individually in an image L of dots on a substrate being inspected by projecting light from a first direction and in an image R of the dots by projecting light from a second direction, which differs from the first direction; a specific-cycle irregularity extracting section for extracting linear irregularities detected at predetermined intervals T in the individual mages L and R, the intervals being taken vertical to the linear irregularities on the substrate; and a detection-target-irregularity extracting section for extracting a linear irregularity detected in both the images L and R as a detection-target linear irregularity. The device therefore is capable of detecting only linear irregularities of a specific cycle which are caused by the presence of dots having irregular thickness when compared to a dot with normal thickness.02-05-2009
20090177428Method of Measuring Peripheral Tilt Angle, Method and Device for Inspecting Inspection Object Having Surface Mounds, Method of Determining Position of Illumination Means, Irregularity Inspection Device, and Light Source Position Determining Device - The method of measuring a peripheral tilt angle in accordance with the present invention, to address the problems, is a method of measuring a peripheral tilt angle on an inspection object having surface mounds, the method including: the step A of projecting light onto the inspection object; the step B of sensing distribution of light reflected off the inspection object; the step C of obtaining a feature point of the distribution of the reflected light from result of the sensing of the distribution of the reflected light; and the step D of obtaining a peripheral tilt angle which is a tilt angle near a periphery of each of the surface mounds based on an angle of projection of the light in step A to a position which, on the inspection object, corresponds to the feature point and an angle of sensing of the reflected light in step B off a position which, on the inspection object, corresponds to the feature point. Thus, the invention provides a method whereby a peripheral tilt angle, or a tilt angle of a surface mound near its periphery on an inspection object is obtained and also provides a method whereby deviation in height of the surface mound is precisely inspected based on the peripheral tilt angle.07-09-2009
20090303468Undulation Inspection Device, Undulation Inspecting Method, Control Program for Undulation Inspection Device, and Recording Medium - An undulation inspection device of the present invention includes: illumination means (line light source 12-10-2009