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11. 发明专利

JPH11218033A GAS TURBINE 失效
公开(公告)号：JPH11218033A
公开(公告)日：1999-08-10
申请号：JP5567798
申请日：1998-01-30
申请人： MURAYAMA YOSHINOBU
发明人： MURAYAMA YOSHINOBU
IPC分类号： F02C3/045 , F02C5/12 , F02C7/08 , F02C7/26 , F02C7/266 , F02C7/27
摘要： PROBLEM TO BE SOLVED: To provide a gas turbine which is vibration-free, simplified structure, and sasy to start, and which exceeds a reciprocating engine in the performance, cost, fuel consumption, and exhaust gas-components, as a prime mover for traveling or stationary type various types of industial machines. SOLUTION: A cover 1 with a ring-like inlet reservoir 2 and a cylinder 4 with a ring-like combustion chamber 5 are fastened to each other while a bulkhead 3 with an inlet port 47 are put between them. When an inlet valve 48 closing an inlet hole is pressed to be opened, fuel in a pump room 32 is pressed by a piston 34 to be injected from a fuel injection nozzle hole 50 to touch the inlet air and the red heat part of an electric heating plug 52 to be ignited to explode. The inlet valve is closed by explosion pressure, and the explosion pressure does not reach a compression blade. Explosion gas are adiabatically expands in the ring-like combustion chamber to blow against a double flow driving blade 8 and turn it, and turn an axial flow compression blade 10 in the cylinder and a shaft 30. The explosion gas is straightened by a reversed axial flow blade 13 with an angle of attack to be reversed by straightening resistance, and to reverse a reversed compression blade 15 inside the cylinder to straightening- compress the inlet air. The straightened explosion gas turns an axial flow driving blade 60, and turns an axial flow compression blade 62 and the shaft 30.

12. 发明专利

JPH0742501A INTERNAL COMBUSTION ENGINE 失效
公开(公告)号：JPH0742501A
公开(公告)日：1995-02-10
申请号：JP22636693
申请日：1993-07-27
申请人： MURAYAMA YOSHINOBU
发明人： MURAYAMA YOSHINOBU
IPC分类号： F01B13/06 , F02B3/06
摘要： PURPOSE:To provide an interbal combustion engine which is light, compact, at a low cost, with high performance, and in which environmental deterioration component of exhaust gas is smaller, comparing with a prior diesel engine or a gasoline engine, as a prime mover used in each field. CONSTITUTION:Main and auxiliary cylinder blocks in which 2 to 6 cylinders 5 arranged radially and cymmetrically in relation to a center are integrated by a dish-like disc are fixed on an axis in the same phase, and balls 7, 38 which slide airtightly in a cylinder are rolled by centrifugal force on an elliptical orbit in the main cylinder block, and on an eccentric circular orbit in the auxiliary cylinder block. In the main cylinder block, respective 7, 38 complete reciprocating motion twice every time the shaft turns once, and four cycle operation is completed. On the other hand, in the auxiliary cylinder block, respective balls 7, 38 complete one reciprocating motion, mixture air is sucked and compressed, and injected into air compressed in a main cylinder hole and an ignition hole 27 at a bottom dead center so as to carry out ignition explosion. The cooling fin 24 of each cylinder is formed as the impeller of an centrifugal pump, lubricating oil and air in a case are circulated so as to transmit heat from the inside of the cooling fin of the inside/outside of the case to the outside. It is thus possible to eliminate necessity of a radiator and the like since the case is cooled by wind of the cooling fan 23 provided on an axis end.

13. 发明专利

JPH10227228A GAS TURBINE 失效
公开(公告)号：JPH10227228A
公开(公告)日：1998-08-25
申请号：JP6886597
申请日：1997-02-13
申请人： MURAYAMA YOSHINOBU
发明人： MURAYAMA YOSHINOBU
IPC分类号： F02C3/08 , F02B61/04 , F02C5/02 , F02C5/12 , F02C7/00 , F02C7/232
摘要： PROBLEM TO BE SOLVED: To provide a small gas turbine which is low in cost, less in vibration, and simple in structure as a prime mover of industrial machinery. SOLUTION: Sucked air entered by press-opening a leaf spring 7 which clogs an air intake port 6 opened in a partition wall-34 which divides a chamber 20 into an annular air intake reservoir 33 in which the mixture of fuel and air compressed by a compression blade 2 is stored and a combustion chamber 20 touches the red hot part of an electric heating plug 4, ignited, and exploded. The leaf spring 7 is closed by the pressure, and high temperature gas is blown on an impeller 10 which is commonly tightened by several stages to the compression blade 2 and guided to a guide vane 11 of several stages commonly tightened to a ring 23 and cases 21, 22, and 25 so as to rotate the impeller 10. Also air from an air hole 6 provided at the axis of a needle valve 5 which is slid tightly in a cylinder provided in the case 21 is mixed with fuel from a fuel hole so as to assist in atomizing fuel, the mixture is passed through a fuel hole in a shaft 1, and injected from a canopy part of the shaft 1 to the compression blade 2 by a centrifugal force. When the speed of the shaft 1 becomes excessive, a pressure inside a cylinder in which a spring is stored is reduced, a spring is pressed, and a needle valve 5 limits fuel so as to lower the speed of a turbine.

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