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    • 45. 发明专利
    • METHOD AND APPARATUS FOR CONTROLLING GAS TURBINE COMBUSTION DEVICE
    • JPH04203808A
    • 1992-07-24
    • JP32944590
    • 1990-11-30
    • HITACHI LTD
    • INOUE HIROSHITSUKAHARA SATOSHIIWAI KAZUMI
    • F02C9/00F01D17/08F23R3/26
    • PURPOSE:To enable the most suitable combustion to be always carried out at all combustion devices even in the case that a gas turbine has a plurality of combustion devices by a method wherein either a turbine discharged gas temperature distribution or a turbine discharging gas concentration distribution is measured and a controlling amount of an air distribution adjusting device of each of the combustion devices is shifted from this distribution. CONSTITUTION:An indicating temperature of each of thermo-couples 36 is compared with a mean temperature of all thermo-couples. In the event that there is a high displacement from the mean value, an amount of shift Xs of a degree of opening of an air distribution adjusting valve 18 of each of the combustion devices is set. This amount of shift Xs is added to a standard value Xo of a combustion control device 19 and then a degree of opening X signal of an air adjusting valve is sent to an adjusting valve driving device 21. Operation at this shifting amount Xs is continuously carried out at a specified time interval tau. Due to this fact, an air distribution of each of the combustion devices is always kept at its most suitable value during an operation of the gas turbine. NOx or Co in each of the combustion devices or a discharged hydrocarbon of it is detected with a discharged gas temperature distribution measuring thermocouple 36 being applied as a discharged gas sensor and a degree of opening shifting amount Xs of an air distribution adjusting valve 18 of each of the combustion devices is set and then an air distribution of each of the combustion devices is always kept at its most suitable state.
    • 46. 发明专利
    • FUEL SPRAYING DEVICE FOR GAS TURBINE COMBUSTOR
    • JPH04124519A
    • 1992-04-24
    • JP24401190
    • 1990-09-17
    • HITACHI LTD
    • HAYASHI NORIYUKITSUKAHARA SATOSHIKOBAYASHI SHIGEYOSHIIWAI KAZUMI
    • F23R3/00
    • PURPOSE:To shorten a time, in which a compressor installed in a different place is run, as much as possible and to improve the thermal efficiency of the whole of a gas turbine by a method wherein a part of air fed to a burner is branched, and a steam system is connected to an air system where atomization of liquid fuel is promoted by means of air pressurized by the compressor installed in a different place. CONSTITUTION:A nozzle core 11 through which liquid fuel 101 is atomized is located to the central part of a fuel nozzle 1, the liquid fuel 101 is atomized at a vortex chamber 12, and injected as spray through a nozzle hole 13. A cone 15 to form a spray air flow passage 14 is located to the outer periphery of the nozzle hole. Steam 106 the pressure of which is increased in an exhaust heat recovery boiler 53 produces a high speed swirl by means of a spray swirler 16, the swirl being discharged through the nozzle hole 13. Since atomization is promoted, even when a compressor 54 installed in a different place is stopped, the atomizing characteristics of the liquid fuel 101 is not lowered. Since steam 103 and steam 106 are used for atomization of liquid fuel grains, a mixing state of steam in a region where fuel reaction on the fuel nozzle side in a liner is active is improved and production of NOX is reduced by means of a less amount of steam.
    • 47. 发明专利
    • FUEL NOZZLE
    • JPH0484010A
    • 1992-03-17
    • JP19793690
    • 1990-07-27
    • HITACHI LTD
    • IWAI KAZUMIKOIZUMI HIROMIKOBAYASHI SHIGEYOSHIURUSHIYA HARUOIIZUKA NOBUYUKIMORITOMO YOSHIKAZU
    • F23D14/48F23D17/00F23R3/28
    • PURPOSE:To stabilize the flame and cool effectively the fuel nozzle by providing an air jet opening very close to a high calorie fuel jet opening. CONSTITUTION:Near a high calorie fuel jet opening 36, an air opening 60 is provided which leads a part of the air to be supplied to air rotating vanes 45 and the air supplied to the air opening 60 is introduced from an air intake port 61 at the outer circumference of a nozzle, and it crosses the inside of the nozzle and is jetted out from the front face of the nozzle with air rotation. This crossing flow channel cools the nozzle body. An oil fuel jet opening 36 is located at the center and fuel atomization air jet openings 40 are provided on its circumference. A main jet opening 44 of the coal gas which directly influences the flame stability is a little off the center at the position required for the flame stabilization. Air jet openings 60 for stabilizing the combustion of high calorie fuel 30, 40 are provided near the jet opening of the high calorie fuel. Air jet openings that contribute to the stabilization of the combustion of low calorie fuel 43, 44 are arranged on the outer circumference of the jet opening.
    • 48. 发明专利
    • BURNER
    • JPH0339821A
    • 1991-02-20
    • JP17275289
    • 1989-07-04
    • HITACHI LTDCENTRAL RES INST ELECT
    • MACHIDA TAKASHIMIYATA HIROSHINAKAKADO MASAAKIIWAI KAZUMIABE TOSHIOHISAMATSU NOBORU
    • F23R3/42F23D14/22
    • PURPOSE:To efficiently utilize the heat resistance of ceramics and suppress an increase in manufacturing man-hour, cost and weight by arranging ceramic layers in the given partial regions of the inner surface of an internal cylinder. CONSTITUTION:A burner is composed of an internal cylinder 1 and a tail cylinder 2 connected to the internal cylinder 1 in the direction of the length of the cylinder 1 or composed of at least the internal cylinder 1. At least one combustion air hole 3 is formed in the circumferential wall of the internal cylinder 1 and ceramic layers 6 are arranged on the inner surface of the internal cylinder 1. The ceramic layers 6 are arranged in at least given partial regions of the inner surface of the internal cylinder 1 whose temperatures are raised. For example, the ceramic layers are arranged only in the neighborhood of the combustion air hole 3 formed in the inner surface of the internal cylinder 1. The neighborhood of the ceramic layers 6 are the regions wherein the most violent combustion reaction is conducted and the maximum temperature 1500-2000 deg.C is locally generated. By arranging the ceramic layers 6 only in these regions, the cooling air can be reduced and an increase in manufacturing man-hour and weight can be suppressed.
    • 50. 发明专利
    • CATALYSTIC BURNER
    • JPS63101622A
    • 1988-05-06
    • JP24742986
    • 1986-10-20
    • HITACHI LTD
    • KOIZUMI HIROMIIWAI KAZUMIYOKOTA OSAMUWADA KATSUO
    • F23R3/40
    • PURPOSE:To provide a catalystic burner which is capable of burning completely an unburned fuel portion by providing a throttle at part of a flow passage of the high temperature gas which is generated from a pilot flame that is formed in the rear stage catalyst and mixing well an unburned portion which is generated at the front stage catalyst and the high temperature gas obtained from the pilot flame which is formed at the rear stage catalyst. CONSTITUTION:The concentration of a premixed gas upstream of a front stage catalyst 1 is always changing, and the catalyst is not always used at its optimum temperature. Accordingly, the combustion of the front stage catalyst 1 is not necessarily a complete combustion. But the temperature of the gas at the outlet of a rear stage catalyst 2 is always at optimum temperature for the catalyst and since a temperature over 1,000 deg.C can be obtained, a pilot flame 15 is formed behind the catalyst. Furthermore, by throttling at a throttle section 16 a burner liner 3 in order to promote the mixing of a high temperature gas which can be obtained from the pilot flame 15 at a short distance from it and an unburned portion other than the high temperature gas which is formed by the catalystic reaction the unburned portion generated by the catalystic reaction is mixed well with the pilot flame 15 after passing through the rear stage catalyst 2 and achieves complete combustion.