Abstract: A gas turbine combustor is provided with a nozzle extension tube having an inclination outward in a diameter direction of a combustor inner cylinder and in a peripheral direction of the combustor inner cylinder. As a result, the premixed gas is transformed to a spiral flow passing into a combustion chamber while turning, i.e., an outward turning flow, thereby sufficiently mixing the premixed gas while the premixed gas is flowing in the combustion chamber.

Abstract: A method for forming a dielectric thin film includes a film deposition step of spraying a material solution onto a heated substrate under a reduced pressure by a two-fluid technique using an inert gas to deposit a thin film. The material solution is supplied at a rate that is greater than the vaporization rate of the solvent in the film deposited on the substrate. The supply of the material solution is stopped and the solvent remaining in the film is vaporized remaining solvent. Then, the film is heat-treated in an oxidizing atmosphere. The substrate is heated to a temperature in the range of about 100° C. to about 300° C. Thus, a dielectric thin film having reliability can be formed even if the film thickness is small.

Abstract: A method for forming a dielectric thin film includes a film deposition step of spraying a material solution onto a heated substrate under a reduced pressure by a two-fluid technique using an inert gas to deposit a thin film. The material solution is supplied at a rate that is greater than the vaporization rate of the solvent in the film deposited on the substrate. The supply of the material solution is stopped and the solvent remaining in the film is vaporized remaining solvent. Then, the film is heat-treated in an oxidizing atmosphere. The substrate is heated to a temperature in the range of about 100° C. to about 300° C. Thus, a dielectric thin film having reliability can be formed even if the film thickness is small.

Abstract: A gas turbine combustor is provided with a nozzle extension tube having an inclination outward in a diameter direction of a combustor inner cylinder and in a peripheral direction of the combustor inner cylinder. As a result, the premixed gas is transformed to a spiral flow passing into a combustion chamber while turning, i.e., an outward turning flow, thereby sufficiently mixing the premixed gas while the premixed gas is flowing in the combustion chamber.

Abstract: A gas turbine combustor is provided with a nozzle extension tube having an inclination outward in a diameter direction of a combustor inner cylinder and in a peripheral direction of the combustor inner cylinder. As a result, the premixed gas is transformed to a spiral flow passing into a combustion chamber while turning, i.e., an outward turning flow, thereby sufficiently mixing the premixed gas while the premixed gas is flowing in the combustion chamber.

Abstract: A digital synchronization circuit 1000 according to the present invention includes: a polyphase clock generation circuit outputting a plurality of clock signals having the sane frequency and different phases; a selection circuit selecting and outputting one of the plurality of clock signals in accordance with the selection signal; and a selection control circuit outputting a selection signal in accordance with a clock selection signal and the plurality of clock signals. The timing at which a value of the selection signal changes from the first value to the second value is in the period in which potential levels of the clock signals respectively represented by the first and second values are the same. Thus, an output clock signal without any hazard is output which is in synchronization with an input data signal of a plurality of clock signals.

Abstract: A high level synthesis method for generating a logic circuit of a register transfer level from an operation description includes a control data flowgraph generation stage; a scheduling stage; an allocation stage; a data path generation stage; and a control logic generation stage. When generating a thread sharing a common memory with another thread operating in parallel therewith, a memory access request is represented by a node of a control data flowgraph so as to perform scheduling, and a control logic is generated. The control logic outputs a memory access request signal to a common memory interface in a state corresponding to a step to which the node is scheduled, and keeps the state until a memory access request acceptance signal from the common memory interface is changed to be active.

Abstract: A pilot nozzle of a gas turbine combustor comprises a first structure, provided near a main nozzle of a combustor that injects fuel oil, having a flow channel for a fuel gas and an outlet for the fuel gas. The first structure diffusion-injecting the fuel gas obliquely forward through the outlet to maintain a flame and to aid ignition of the fuel oil injected from the main nozzle. There is further provided a second structure which circulates in whirls a combustion gas generated due to the combustion of the fuel gas.

Abstract: A combustor includes a burner and a combustion chamber including a heat chamber to which fuel is supplied from the burner. The burner includes a nozzle having a fuel discharge outlet from which the fuel is discharged into the combustion chamber; and the nozzle includes a plurality of discharge openings around the fuel discharge outlet from which cooling water is discharged toward inside surfaces of the heat chamber. The plurality of discharge openings may be disposed so that the directions of the cooling water discharged from the discharge openings differ in the radial direction.

Abstract: A high-level synthesis method comprising the steps of converting an operating description describing one or more operations to a control data flow graph (CDFG) including one or more nodes representing the one or more operations and one or more I/O branches representing a flow of data, scheduling the CDFG obtained by the converting step, and allocating one or more logic circuits required for executing the CDFG obtained by the scheduling step. A portion of the CDFG in the converting step is subjected to logical synthesis in advance to generate a node, and the portion of the CDFG is replaced with that node.

Abstract: A method for forming a dielectric thin film includes a film deposition step of spraying a material solution onto a heated substrate under a reduced pressure by a two-fluid technique using an inert gas to deposit a thin film. The material solution is supplied at a rate that is greater than the vaporization rate of the solvent in the film deposited on the substrate. The supply of the material solution is stopped and the solvent remaining in the film is vaporized remaining solvent. Then, the film is heat-treated in an oxidizing atmosphere. The substrate is heated to a temperature in the range of about 100° C. to about 300° C. Thus, a dielectric thin film having reliability can be formed even if the film thickness is small.

Abstract: A combustor section is disposed downstream of a nozzle section. The combustor section extends from a downstream end of the nozzle section to an entrance of a gas turbine and supplies a combustion gas which is generated by combusting a pre-mixed gas to a gas turbine. The combustor section is formed by an inner tube and a tail tube unitarily. The combustor is provided with a wall cooling apparatus for cooling a wall surface of the combustor. On the inner wall of the combustor section, grooves are formed. An entrance for introducing an air for cooling action is disposed on the outer wall of the combustor section. The introduced air performs a film cooling and convective cooling in a combined manner. By doing this, the temperature of the combustion gas may be high, and a highly efficient gas turbine is realized.

Abstract: The present invention relates to a scheduling method and apparatus for high-level synthesis of a circuit which is represented by an operation description. The method includes calculating a probability for each of a plurality of nodes included in a control flow graph to be assigned to a time step and calculating a sum of the probabilities for each time step. For each node having a scheduling candidate in a time step for which the sum of probabilities is maximum, an estimated value of an area of the circuit is calculated with the node having been temporarily assigned to the scheduling candidate and a combination of a node and a scheduling candidate for which the estimated value is maximum is retrieved. Finally, a list of scheduling candidates of the node in the combination is narrowed down by excluding the scheduling candidate in the combination from the list of scheduling candidates of the node in the combination.

Abstract: A circuit synthesis method includes the steps of converting a behavioral description describing a behavior of calculation processing into a control data flowgraph; assigning a plurality of calculations, at least one input and at least one output in the control data flowgraph into a plurality of prescribed time slots; assigning the plurality of calculations, a plurality of data dependency edges, the at least one input and the at least one output respectively to a plurality of calculation devices, at least one register, at least one input pin and at least one output pin; generating a plurality of paths corresponding to the plurality of data dependency edges; detecting a feedback loop formed of at least two of the plurality of paths and at least one of the plurality of calculation devices; and re-assigning one calculation, which has been assigned to a first calculation device included in the feedback loop, to a second calculation device among the plurality of calculation devices, so as to delete the feedback loo

Abstract: A high level synthesis method for generating a logic circuit of a register transfer level from an operation description includes a control data flowgraph generation stage; a scheduling stage; an allocation stage; a data path generation stage; and a control logic generation stage. When generating a thread sharing a common memory with another thread operating in parallel therewith, a memory access request is represented by a node of a control data flowgraph so as to perform scheduling, and a control logic is generated. The control logic outputs a memory access request signal to a common memory interface in a state corresponding to a step to which the node is scheduled, and keeps the state until a memory access request acceptance signal from the common memory interface is changed to be active.

Abstract: A pilot nozzle of a gas turbine combustor comprises a first structure, provided near a main nozzle of a combustor that injects fuel oil, having a flow channel for a fuel gas and an outlet for the fuel gas. The first structure diffusion-injecting the fuel gas obliquely forward through the outlet to maintain a flame and to aid ignition of the fuel oil injected from the main nozzle. There is further provided a second structure which circulates in whirls a combustion gas generated due to the combustion of the fuel gas.

Abstract: A gas turbine combustor is provided with a nozzle extension tube having an inclination outward in a diameter direction of a combustor inner cylinder and in a peripheral direction of the combustor inner cylinder. As a result, the premixed gas is transformed to a spiral flow passing into a combustion chamber while turning, i.e., an outward turning flow, thereby sufficiently mixing the premixed gas while the premixed gas is flowing in the combustion chamber.

Abstract: A circuit synthesis method includes the steps of converting a behavioral description describing a behavior of calculation processing into a control data flowgraph; assigning at least one calculation, at least one input and at least one output in the control data flowgraph into prescribed time slots; assigning the at least one calculation, a plurality of data dependency edges, the at least one input and the at least one output respectively to at least one calculation device, at least one register, at least one input pin and at least one output pin; generating a plurality of paths corresponding to the plurality of data dependency edges; and detecting a first false path among the plurality of paths.

Abstract: A gas turbine combustor improves the fuel distribution from a main fuel nozzle, suppressing fluctuations of internal pressure and elevation of inner tube metal temperature, and enhancing the combustion stability and durability of the combustor. The gas turbine combustor is a multi-nozzle type premixing combustor with a nozzle outer tube (7) for forming and injecting a premixed gas of main fuel and combustion air divided and disposed in plural sections around a cone (4) for forming a diffusion flame by reaction between pilot fuel and combustion air disposed in a center of a section of a combustor inner tube (1). Nozzle holes (5a) of a main fuel nozzle (5) are formed in three positions at equal intervals on the nozzle main body wall, and one of them is disposed at the outer periphery of the combustor inner tube (1) on a diametral line linking between the center of the combustor inner tube (1) and the center of the main fuel nozzle (5), whereby the fuel distribution to the outer periphery is decreased.

Abstract: A high-level synthesis apparatus for receiving operational descriptions includes synchronous communication instructions between threads which operate in parallel, and for synthesizing a product circuit based on the received operational descriptions. The high-level synthesis apparatus includes: an extractor for analyzing the received operational descriptions and extracting consecutive synchronous communication instructions which are of the same kind from among the received operational descriptions; a scheduler for generating scheduling for each thread by bundling together the extracted synchronous communication instructions into one arithmetic operation; and a circuit generator for generating the product circuit based on results of the scheduling, the product circuit being capable of commencing the bundled synchronous communication instructions with the same level of priority based on handshaking.