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    • 42. 发明专利
    • ENERGY CONSERVATION CYCLE INTERNAL COMBUSTION ENGINE
    • JP2001221001A
    • 2001-08-17
    • JP2000338725
    • 2000-11-07
    • TANIGAWA HIROYASUTANIGAWA KAZUNAGA
    • TANIGAWA HIROYASUTANIGAWA KAZUNAGA
    • F01N5/02F01B21/00F02B3/06F02D19/02F02D19/12F02F1/00F02F3/00F02M25/022
    • PROBLEM TO BE SOLVED: To solve the problem in the existing reciprocating internal combustion engine in which a small gasoline engine with the maximum thermal energy rate at the top dead canter and non-rotation emission thermal energy loss about 50% has the lowest heat efficiency about 15%, while a marine large diesel engine with maximum delayed combustion and non-rotation emission thermal energy loss about 20% has heat efficiency of 55% at maximum, howere it is not applicable to an automobile or the like. SOLUTION: By two-stage combustion, the maximum combustion pressure is increased approximate eight times (16 MPa) as high as the compression pressure (2 MPa), and only the emission time of thermal energy is delayed to attain thermal efficiency about 70% by completely combusting with theoretical air fuel ratio in reduced-diameter main combustion chamber superheated steam injection separation combustion in substantially closed container. By heating exhaust temperature in 100 deg.C, in an enlarged-diameter combustion chamber very high speed mixing two-stage combustion and exhaust heat recovery heat exchanger, heat is recovered and fed to a reduced- diameter main combustion chamber heat exchanger repeatedly, thereby increasing heat recovery to the limit. Combustion gas such as CO2 or the like is dissolved, mixed and fixed in the cooled superheated steam condensed water and discharged so that exhaust of CO2 or the like is decreased to zero or a little.
    • 43. 发明专利
    • ENERGY RESERVING CYCLE ENGINE MOUNTING APPARATUS
    • JP2000234501A
    • 2000-08-29
    • JP33213399
    • 1999-11-24
    • TANIGAWA HIROYASUTANIGAWA KAZUNAGA
    • TANIGAWA HIROYASUTANIGAWA KAZUNAGA
    • F02B19/04F01B9/02F02B23/02F02B47/02F02F3/28F02M25/022F02M25/032
    • PROBLEM TO BE SOLVED: To decrease of NOx and increase an output by injecting steam from a steam injection valve 6 for a short time and at a suitable time to a wall surface of a diameter contracted main combustion chamber as well as carrying out combustion by mixing fuel with air in the combustion chamber. SOLUTION: A pair of diameter enlarged pistons 21 are continuously connected to a crankshaft 16, and respective pistons 21 are fitted to a pair of cylinder heads 15 disposed opposing to each other. A fuel injection valve 7B and an ignition device 8 are disposed to be faced to a diameter contracted main combustion chamber 1 partitioned into each cylinder head 15, air injected from an air flow path 9 and fuel injected from a fuel injection valve 7 are agitated and mixed with each other, and ignition combustion is carried out. Steam is injected from an outer periphery of a steam injection valve 6 through a steam supplying-out valve 4 and a steam, reservoir 5 at a suitable time and for high speed and super short time, and a combustion chamber wall surface is cooled to decrease the rate of NOx and increase an output. A turbo supercharger 12 is operated by energy of exhaust delivered from a diameter enlarged combustion chamber 10, and a rotary type supercharger 14 is operated by an electric motor 17 or the like, and intake air is supercharged.
    • 44. 发明专利
    • ENERGY CONVERSION METHOD INCLUDING MAGNETIC POWER TRANSMISSION AND DEVICE THEREFOR
    • JPH1018860A
    • 1998-01-20
    • JP20404896
    • 1996-06-28
    • TANIGAWA HIROYASUTANIGAWA KAZUNAGA
    • TANIGAWA HIROYASUTANIGAWA KAZUNAGA
    • F01D1/24F02C3/067F02C7/36H02K49/10
    • PROBLEM TO BE SOLVED: To improve thermal efficiency sharply while obtaining a large output and a large torque with a simple structure by connecting an inner and outer moving blade shaft devices to each other through magnetic power transmission devices which rotate in a direction reverse to each other with an optimal rotational ratio. SOLUTION: An all moving blade turbo jet engine provided with a double inversion all moving blade gas turbine, is provided with an outside compressor moving blade barrel device provided with a first step moving blade group 1, an odd number step moving blade group 2, and a final step moving blade group 3 from a cylindrical outside moving blade barrel 11 having a taper slightly inward in a radial direction. The engine is provided with an outside turbine moving blade barrel device having a first step moving blade group 4 and a final step moving blade group 6, or an odd number step moving blade group 5 and the final step turbine moving blade group 6. A shaft device is extended from the first step moving blade group 1 to connect to an upstream magnetic power transferring device, an outside shaft device is extended from the moving blade groups 3, 4 and to connect to an intermediate magnetic power transmission, and a turbine engine is constituted by interposing a combustor between an annular compressor outlet 7 and an annular turbine inlet nozzle 8.
    • 46. 发明专利
    • ENERGY CONVERTOR INCLUDING SPECIAL GAS TURBINE
    • JPH09291831A
    • 1997-11-11
    • JP14339096
    • 1996-04-30
    • TANIGAWA HIROYASUTANIGAWA KAZUNAGA
    • TANIGAWA HIROYASUTANIGAWA KAZUNAGA
    • F02C3/30F02C6/18F02C7/232F23R3/00F23R3/42
    • PROBLEM TO BE SOLVED: To improve thermal efficiency by lowering turbine inlet temperature at the finishing point of a superheating stroke, to turbine heat resistant limit temperature or below in the super-heating stroke while pressure ratio is increased in the compression stroke of a gas turbine cycle and/or supply heat quantity is increased in the superheating stroke after the compression stroke. SOLUTION: In a Brayton cycle equipped with a compressor 1, a combustor 2 and a turbine 3, water and steam is supplied to the inside of the combustor 2 through a water introducing pipe 4 and a steam pipe 6. Even through water supplied to the inside of this combustor 2 is vaporized by heat of combustion, and heat of vaporization at that time is taken away from a supply heat quantity, thereby the compression ratio of the compressor 1 is set considerably higher than the conventional case, turbine inlet gas temperature can be suppressed lower than turbine resistant heat limit temperature. Also, steam vaporized in the combustor 2 is sent on a steam turbine 8 side after separated from water, therefore combustion gas temperature in the combustor 2 is energy- converted unlimitedly as heat of vaporization, and output outputted by the turbine 3 is increased.
    • 47. 发明专利
    • FUEL INJECTION TYPE INTERNAL COMBUSTION ENGINE WITH REVOLVING ENGINE BODY
    • JPH0893491A
    • 1996-04-09
    • JP27192894
    • 1994-09-28
    • TANIGAWA HIROYASUTANIGAWA KAZUNAGA
    • TANIGAWA HIROYASUTANIGAWA KAZUNAGA
    • F02B75/28F02B57/00
    • PURPOSE: To reduce the thermal load of a cylinder by communicating an output combustion chamber to use the energy of low pressure and low temperature with a contracted main combustion chamber to generate the combustion gas and superheated steam of high pressure and low temperature, and separating these combustion chambers before and after the top and bottom dead centers of the output piston. CONSTITUTION: Head parts of output pistons 3a, 3b are contracted ones 24a, 24b, and the sectional area in the radial direction is determined so that a cylinder may be of the same diameters 25a, 25b corresponding to the center contracted piston of e.g. 1/16 of the output piston. A contracted and small reciprocation piston of the diameter 25 same as the contracted diameter 24 is constituted immediately before the output piston reaches the top dead center, and the total air in the center output combustion chamber of 15/16 of the area is compressed and injected from near-path non-return valves 96a, 96b side through the difference of the compression ratio into the center contracted main combustion chamber 98 of 1/16 of the area before the top dead center. The fuel and water injected from an all-around fuel injection valve 20b is stirred, compressed, ignited, expanded and vaporized at high speed to prevent the reverse flow to the center output combustion chamber side by the near-path non-return valve. The volume increase of the center contracted main combustion chamber 98 when the output piston is moved to the bottom dead center side is 1/16 of the normal value.