| Patent application number | Description | Published |
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| 20100059176 | Multilayer Information Recording Medium, and Apparatus and Method for Manufacturing Same - The present invention provides an apparatus for fabricating a multi-layer information recording medium including a substrate, plural information recording layers placed on the aforementioned substrate, resin intermediate layers placed between adjacent information recording layers and a resin protective layer placed on all the information recording layers at the side opposite from the aforementioned substrate, the apparatus including an ejecting unit including ink jet nozzles operable to drip minute resin liquid drops onto the aforementioned substrate or the aforementioned information recording layers; and a control unit operable to control the aforementioned ejecting unit, whereby resin layers which form said resin intermediate layers or said resin protective layer are formed on the aforementioned substrate or the aforementioned information recording layers. | 03-11-2010 |
| 20110069599 | OPTICAL INFORMATION RECORDING AND/OR REPRODUCING APPARATUS, OPTICAL INFORMATION RECORDING AND/OR REPRODUCING METHOD, OPTICAL INFORMATION RECORDING MEDIUM, AND SOLID IMMERSION LENS - An optical information recording and/or reproducing apparatus comprises: a focusing unit ( | 03-24-2011 |
| 20120013675 | MULTILAYER INFORMATION RECORDING MEDIUM, AND APPARATUS AND METHOD FOR MANUFACTURING SAME - The present invention provides an apparatus for fabricating a multi-layer information recording medium including a substrate, plural information recording layers placed on the aforementioned substrate, resin intermediate layers placed between adjacent information recording layers and a resin protective layer placed on all the information recording layers at the side opposite from the aforementioned substrate, the apparatus including an ejecting unit including ink jet nozzles operable to drip minute resin liquid drops onto the aforementioned substrate or the aforementioned information recording layers; and a control unit operable to control the aforementioned ejecting unit, whereby resin layers which form said resin intermediate layers or said resin protective layer are formed on the aforementioned substrate or the aforementioned information recording layers. | 01-19-2012 |
| Patent application number | Description | Published |
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| 20080289341 | Combustor of Gas Turbine - A combustor | 11-27-2008 |
| 20090202339 | PLATFORM COOLING STRUCTURE FOR GAS TURBINE MOVING BLADE - A platform cooling structure for a gas turbine moving blade is provided which is capable of improving cooling performance of a platform and of improving reliability of a moving blade in such a manner that a portion in the vicinity of a side edge of the platform which is away from moving blade cooling passageways and is easily influenced by thermal stress caused by high-temperature combustion gas, that is, an upper surface of the side edge is effectively cooled by guiding high-pressure cooling air, flowing to the moving blade cooling passageways, to a discharge opening formed in a surface of the platform in the vicinity of the side edge of the platform without particularly attaching an additional member such as a cover plate to the platform. A moving blade cooling passageway | 08-13-2009 |
| 20100047065 | BLADE STRUCTURE OF GAS TURBINE - To reduce secondary flow loss and to improved turbine efficiency, a section located radially outward of a border section | 02-25-2010 |
| 20100196154 | TURBINE BLADE CASCADE ENDWALL - Provided is a turbine blade cascade endwall that is capable of suppressing a vortex generated on a suction surface of a turbine stator blade and that is capable of reducing secondary-flow loss due to this vortex. A turbine blade cascade endwall that is positioned on a tip side of a plurality of turbine stator blades arranged in a ring form is provided with a pressure gradient alleviating part that alleviates a pressure gradient generated in the blade height direction at a suction surface of the turbine stator blades due to a clearance leakage flow, leaking out of a gap between a tip of a turbine rotor blade located on the upstream side of the turbine stator blades and a tip endwall disposed facing the tip of this turbine rotor blade. | 08-05-2010 |
| 20100217540 | METHOD FOR ESTIMATING PHYSICAL PROPERTY OF CERAMIC, METHOD FOR ESTIMATING PHYSICAL PROPERTY OF THERMAL BARRIER COATING, METHOD FOR ESTIMATING REMAINING LIFETIME OF THERMAL BARRIER COATING, METHOD FOR ESTIMATING REMAINING LIFETIME OF HIGH-TEMPERATURE MEMBER, AND PHYSICAL PROPERTY ACQUIRING APPARATUS - A method is provided by which physical properties, in particular, the Young's modulus and thermal conductivity of a ceramic layer of a thermal barrier coating formed on a high-temperature member are accurately estimated in a short period of time. A method for estimating a physical property of a ceramic includes a step of calculating the Larson-Miller parameter from the time for which and the temperature at which the ceramic is heated; a step of acquiring the porosity of the ceramic corresponding to the calculated Larson-Miller parameter, based on the calculated Larson-Miller parameter and a diagram correlating the Larson-Miller parameter and the porosity obtained from samples having the same composition as the ceramic; and a step of acquiring the physical property of the ceramic corresponding to the acquired porosity, based on the acquired porosity and a diagram correlating the porosity and the physical property obtained from samples having the same composition as the ceramic. | 08-26-2010 |
| 20100284818 | TURBINE BLADE CASCADE ENDWALL - Provided is a turbine blade cascade endwall that is capable of reducing crossflow and is capable of reducing secondary-flow loss that occurs in association with the crossflow, therefore being capable of achieving enhanced turbine performance. A convex portion ( | 11-11-2010 |
| 20110262770 | THERMAL BARRIER COATING MATERIAL, THERMAL BARRIER COATING, TURBINE MEMBER, AND GAS TURBINE - A thermal barrier coating material that exhibits superior high-temperature crystal stability to YSZ, as well as a high degree of toughness and an excellent thermal barrier effect. Also provided are a thermal barrier coating, which has a ceramic layer formed using the thermal barrier coating material and exhibits excellent durability to heat cycling, and a turbine member and a gas turbine which are each provided with the thermal barrier coating. The thermal barrier coating material comprises mainly ZrO | 10-27-2011 |
| 20120014832 | Ni-BASED SINGLE CRYSTAL SUPERALLOY - The Ni-based single crystal alloy disclosed here is a single crystal and has a chemical composition containing, as % by mass,
| 01-19-2012 |
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| 20090013204 | INFORMATION PROCESSING DEVICE AND MOBILE PHONE - An information processing device, for use in a mobile terminal unable to obtain power consumption information from an external source, which can estimate, based on an actual performance value, a battery life, power consumption for processing that changes depending on the usage by the user, and so on, and ensures execution of processing specified by the user for a specified period of time, the information processing device comprising a power consumption calculating unit which calculates, for each processing executed by the information processing device, power consumption information concerning an amount of power consumed by executing each processing; a request generating unit which compares the amount of power indicated by the power consumption information and a remaining amount of power of the information processing device, and generates a request to execute predetermined processing according to a result of the comparison; and a request processing unit which executes the predetermined processing in response to the generated request. | 01-08-2009 |
| 20120005687 | SYSTEM ACTIVATION METHOD IN MULTI-TASK SYSTEM - When a multi-task system is powered on, the following steps are respectively executed: a first step in which hardware components are initialized; a second step in which sections are initialized; and a third step in which an operating system is initialized. In the third step, a task/object is statically generated when an initial access time of the task/object is at most a predefined threshold value but the task/object is dynamically generated after activation of the multi-task system is completed when the initial access time of the task/object is larger than the predefined threshold value. | 01-05-2012 |
