KR900010224A - Power generator, buoyancy and thrust generator and cooling system using fluid compression and flow increase device - Google Patents

Abstract

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Description

Power generator, buoyancy and thrust generator and cooling system using fluid compression and flow increase device

As this is a public information case, the full text was not included.

1 is a perspective view of a fluid compression and flow increase apparatus, FIG. 2 is a side cross-sectional view of the fluid compression and flow increase apparatus, and FIG. 3 is a bottom view of the fluid compression and flow increase apparatus.

Claims (37)

Suction port (1) of the rectangular channel section is a ladder-shaped rectangle with a long side, and the radius of curvature of the surface (5) on the upper side (short side) of the ladder side is bent constantly so that the fluid passing through the pipe flows along the surface and the centrifugal force And the curvature of the inner diameter surface 5 is gradually increased (the length from 52 to 2 'is the same as the length from 52 to 2 ", and the length from 52 to 5" is longer than the length from 52 to 5'). ) The inner diameter surface (5) and the outer diameter surface (2) gradually become close, but gradually widen to the side (3, 4) so that the flow path cross-sectional structure of the oil pipe inlet (1) and the outlet is reversed (inlet (1) The longer the side (3, 4) and the longer the exit (6), the shorter the side (7, 9) and the inner and outer surfaces (8, 10) are changed), and the inner wall of the milk pipe is smooth to minimize the frictional resistance of the fluid The cross-sectional area of the flow path is either constant from the inlet (1) toward the exit or gradually decreases When compressing the fluid, the flow path section is gradually reduced and when the flow velocity is faster, the flow path section is made constant or slightly enlarged and the flow path area is large so that the flow rate increases and the curvature radius of the pipe is too small. The frictional resistance is small and the flow rate at the suction port (1) is fast, the rate of change of the flow path wall (2, 3, 4, 5) is large, and the flow rate is slow (less the length of 3 and 9). Curvature (11) (at least R ≒ 5MM or more) to smooth out the conduit of the edges to reduce frictional resistance, and also to connect several short circuits of the same conduit (see Fig. 6) or to the inlet (1) or outlet (6) Connect the inlet or outlet of the compressor or the flower, and the difference between the length of the bottom side (two long sides) and the short side (5) of the ladder side of the duct suction port (1) is at least 1.5 times and the outlet (6) Each transition angle is angle similar to a structure compressed fluid and a flow rate of increase of the inlet device of the forming surface. The hydraulic and flow rate increasing device is connected with several short circuits (17-23 in FIG. 7), and the axial flow motor 16 and the output multi-stage turbines 11, 12, 13 and the generator 14 are mounted on the same shaft at both ends. The poly (15) is mounted to the rotating shaft of the rotary fan 16 to rotate the cross-sectional area of the flow path (17-23) inside the inlet (17) to the outlet (23) gradually reduced to a constant structure or turbine The flow path cross-sectional area between the blades of (11, 12, 13) is constant in all the zones (11, 12, 13), or the flow path cross-sectional area between the blades in (12) of the guide is gradually enlarged, and is constant inside the rotor blade, and the hydraulic pressure and the flow rate The cross-section structure of the canal inlet 18 is changed so that the direction of the curvature centripetal axis of the connecting pipe between each paragraph of the increasing device is perpendicular to each other (see FIG. 6), that is, the short side plate at the suction port 18 ( 19 ', 19) gradually longer and the length of the upper side (2) and lower side (5) gradually shorter 19, the power generation (power generation) and the cooling unit of the structure to connect the short-circuit. The hydraulic and flow rate increasing device (28, 29, 30 in FIG. 9) is connected in multiple stages (28-29), and the centrifugal compressor (25) and the axial turbines (34, 35, 36) are connected to the same shaft (34). , 35, 36 and the compressor 25 are integrally mounted, the generator and the motor 14 are mounted on the rotating shaft, and the guide vane 24 and the diffuser 33 are mounted at the outlet of the centrifugal compressor 25 and the tube is extended there. It is connected to the fluid compression and flow rate increasing devices (28, 29, 30) equipped with heat exchangers (26 and 27) to form a closed circuit, and the internal flow path area of the flow rate increasing devices (28, 29, 30) gradually decreases or becomes constant. The flow path area is enlarged in the turbine guide vane 35, the flow path area is constant in the rotor blades 34 and 36, and the flow path area is reduced in the compressor blades 25 and the diffuser 33, and the pulley 46 is rotated on the rotation axis of the generator 44. ) To rotate the blower 32 to circulate gas for supplying heat to the heat exchanger 26, or (26) to circulate the liquid to supply heat. Rotates the motor cum generator 14, the first equipped with a pipe (27) when the threshold speed power generation (power generation) and the cooling apparatus is also to stop the power supply operation voluntarily, using a self-developed current. 4. An open circuit according to claim 3, wherein the turbine (34, 35, 36 in FIG. 11) and the inlets (31, 41) of the compressors (24, 25) are not connected and there is no heat exchanger (26, 27 in FIG. 9). As a structure, a rod-shaped sound absorbing material (see FIG. 15) is attached to the suction port 37 and the discharge port 43, and the sequence of the column-shaped sound absorbing material (sponge, etc.) is alternately arranged ("B" in FIG. 15). The inlet 47 of the fluid compression and flow rate increasing device 45 is provided with the fluid flowing through the box suction port 37 so that the flow path becomes a zigzag shape and the sound absorbing material 40 such as a sponge is mounted on the inner wall. Power generation (power generation) and cooling device of the structure flowing through and discharged through the guide vane 24 of the compressor 25 is discharged through the mall outlet 43. The box according to claim 3, wherein the column-shaped sound absorbing materials are arranged at the inlets (37 in FIG. 12) and the outlets 43 so that the heats are alternately arranged ("B" in FIG. 15), and the sound absorbing materials 40 are attached to the inner wall. 39, and the blower 32 is rotated by the pulley 48 mounted on the rotating shaft of the generator 14, or the blower 32 is rotated by a separate electric motor to intake 37 and the box 39 A power generation (generation) and cooling device of such a structure that allows fluid flowing through the outlet (43) to heat and cool the heat exchanger (26). The fluid compression and flow rate increasing device (2 in Fig. 13) has a single short circuit and is wound in a spiral shape, and the exit (3) flow path cross section is arranged in a cylindrical shape. The high speed generator and the electric motor 6 are mounted on the rotary shaft of the centrifugal turbine / compressor 4 equipped with the axial turbine gear blade guiding blade 19 at the center, and the outlet (1) of the hydraulic and flow increase device 2 is discharged. 3) The flow path area to 3) is gradually reduced slightly, and the flow path area from the tip of the guide blade 19 to the tip 22 of the rotor blade 4 is slightly enlarged, and the flow path area inside the rotor blade of the turbine and compressor 4 is constant or slightly. The flow path cross-sectional area of the blade end 4 'is slightly smaller than or equal to the cross-sectional area of the inlet 1, and the blade angles and flow path cross-sectional structures of the guide blades 19 and the rotor blades 4 of the turbine-compressor 4 are axially impulsive. Of the turbine and recoil blade turbine It has the same angle and flow path structure, but the blade thickness of guide blades 19, rotary blades 4, and tip 22 is thin (similar to the tip of impulse blades) to reduce friction with fluid or impulse turbine turbine blades and structure. And the inlet and outlet angles have the same shape, and in the case of the impeller type wing structure, the flow path cross section of the blade tip portion 4 "is larger than the flow path cross section of the intermediate portion 4" ', and the flow path cross section of the distal end portion 4' is the blade tip portion 4 ") If the flow path area is the same and the rebound type wing structure is used, the tip end portion 4" and the middle portion 4 "'are the same as the impulse type, and the flow path area of the distal end 4' is the same as the middle portion 4" '. It is designed to reduce or further reduce the distance between the side plates (23, 24) in a constant structure in the first power to the generator and the motor (6) to rotate at high speed, and when the critical speed stops the power supply spontaneous operation is made Using the generated current to obtain a cooling fluid Force generation (power generation) and the cooling unit. The inlet / outlet (13, 14 in FIG. 14) and the inner wall (16) mounted on the hexahedral box (15) equipped with a sound absorbing material, and the fluid of the inlet (14) is the inlet of the hydraulic and flow increasing apparatus (2). 1) Power generation (power generation) and a cooling device having a structure in which the fluid of the compressor (4) and the outlet (5) is discharged to the mall (15) and the outlet (13). The compressor (2) of FIG. 15 is fitted with a guide vane (2) and a diffuser (8) and connected to the inlet port (1) of the hydraulic and flow increasing apparatus (2). To a closed circuit and to generate power by a circulator having a structure in which a heat exchanger 9 is installed in the middle of an oil pipe in a box as described in claim 7, and a blower 11 is installed at a box outlet 13. ) And chiller. Multi-stage hydraulic and flow increasers are connected in multiple stages (6-19 in Fig. 17), but the hydraulic and flow increasers of the multi-stage connected by changing the inlet flow paths (8, 10, 12, etc.) (see Fig. 8) On average, it is directed in one direction so that each paragraph does not incline more than about 40 degrees with respect to the lateral direction (average of synthesized directions) (26, 24, 25 for right angles 26, 24, 27 The hydraulic flow increase device of the multiple paragraphs (8-13) facing forward (in the direction of propulsion or buoyancy) to be below 40 degrees and the cylindrical tube (15, 17, 28) connected in a straight line towards the rear. Repeatedly connected in a short circuit so that the centrifugal force of the fluid (gas liquid) flowing through the fluid compression and flow rate increasing device (6-13, 16, 18) acts as a force toward the front 23, and has a large rotor rotation radius. Generator and electric motor with turbine (2, turbo centrifugal fan-like construction) (1) is connected to the turbine (6) and the entrance (6, 20) connected to the turbine and the current flower (2) which is sucked in the centripetal direction (21) and discharged in the centrifugal direction or vice versa (suction from the outside and discharged to the centripetal section). High speed direct current multi-phase or single-phase generator and motor equipped with a large portion (3) with a large blade radius of the rotor side plate of the blower (2) and a large mass and a generator-motor (1) equipped with a short-term contact commutator. (1) Power generating and buoyancy or thrust generating devices used as alternators and motors or coreless short-time contact commutator type generators and motors or coreless generators and motors. The flow path section of the fluid flows in a circular or rectangular tube with a constant curvature (1-2), again in the opposite direction (2-4) and again in the original direction (1-2) (4-6). The zigzag curved pipe structure is designed to be smooth, but the direction of propulsion (collective force in the direction of the centrifugal force of each curved pipe) and the average angle formed by the curved pipe are about 30 degrees or less on the left and right sides. At least about 30 degrees below the 12-17 straight line, and each curved surface has a constant radius of curvature, but the turning part (2, 4, 6, 8 in Fig. 18) does not have a corner angle. (R ≒ 5MM) The flow path is smooth and the direction to propel or float at the point (3,5,7,8) where the bend length is about 1/5 at the turning point (2,4,6,8) Draw a straight line at right angles and grasp the centripetal point (18, 19, 21 in Fig. 20) on the extension line. Propulsion and buoyancy generating device by centrifugal force in the direction of the fluid of the structure as the reference point of curvature. (See also 18-20.) A multi-parameter wing (1-5 in Fig. 21) of the same structure as the axial recoil turbine gear having a curvature similar to that of paragraph (10) should be installed in multiple stages. ) Wider (approximately 1 / 3-1 / 4 of the blade width) to smooth the flow path and reduce the curvature, and the blade thickness of the blade tip (12) and the tip (13) is thin (sharply at both ends). The frictional area is small and the flow path cross section between the blades is gradually reduced as the blade tip is wide and goes to the distal end. However, the faster the flow rate, the smaller the ratio of the flow path area between the blades in each short circuit Thrust and buoyancy generators () (see also 21 and 22) The thrust and buoyancy generator (Fig. 23) having the structure as described in claim 10 is connected to the outlet 2 of the fluid compressor 8 mounted on the rear fuselage of the propellant (aircraft, ship, automobile, etc.) and is wide. (13) A curved pipe 10 extending in proportion to the compression ratio of the compressor 8 in a structure in which it extends to the tip portion 6 through the square curved pipe 10 and the curvature radius is largely bent and then extends in a straight line toward the rear portion 5 and discharged. Thrust and buoyancy generators (Fig. 123, 24) of which the flow path cross-sectional area of the tube is gradually enlarged (16 is equal to 13 and 12 is longer than 11) and the flow path cross-sectional area of the straight pipe 20 is constant or slightly enlarged. 13. A straight pipe (euro cross-sectional area) according to claim 12, wherein a curved pipe (Figs. 11-13) connected in multiple paragraphs is mounted in a propulsion or buoyancy direction (17) and (11) is reversed (180 switching) again. Same as the outlet 11, and repeats the structure that extends to a straight square tube having a constant structure and connects again to the curved tube 18-9 of the multi-stage and is directed to the upper portion 17. (14) and straight pipes connected to the rear end are also connected by several paragraphs (8, 10, 15), and the cross-sectional structure of the oil pipe of the distal end 4 is modified so that the cross-sectional structure is the same and the cross-sectional structure is circular, so that the blade rotation radius is It connects to the centrifugal inlet 12 of the large centrifugal compressor 1, and connects the outlet 15 of the compressor 1 with the curved end inlet 13, and thickens the large part of the rotational radius of the side plate of the compressor 1. (3) Make the wheel work and the motor (2) mounted on the rotating shaft of the compressor (1) at high speed DC motor with a commutator mounted contact or a coreless motor or thrust and the buoyancy of a structure to the AC motor generator (see Fig. 25 and 26) A square plate (4) having a curved surface (Fig. 27) forming a flow path as described in claim 10 is mounted on the outer diameter of the cylinder through which the centripetal part is formed so that its width is radial and its length is axially, and the outer side is covered with a cylindrical side plate. The curved pipe of the cylindrical tube has a structure surrounding the outer diameter of the cylinder, and a centrifugal compressor having a large blade rotation radius is mounted on the lower portion of the cylinder, and the inlet port (3) is connected to the cylindrical center space and the outlet pipe (4) flow path is mounted on the outer periphery of the cylinder ( 13) and a semi-spherical groove-shaped flow path connected in the form of a short-circuit with the central portion of the bottom of the head 9 forming a curved pipe flow outlet 8 at the upper part of the curved pipe, which protrudes into a conical shape. The upper surface (outer side) has a curvature conical shape, which is connected to the inlet port 3 and the cylindrical core flow path 10 of the high-speed centrifugal compressor 2, and the outlet port 13 is curved in curvature. It is connected to the thrust and buoyancy device of A buoyancy and thrust generating device in which the structure of the shaft blade (2) side plate (11) and the motor has the same structure as in claim 9. 15. An open circuit according to claim 14, which is connected to a centrifugal compressor (2 in FIG. 29) and a curved tube flow path 5 so as to have an open circuit (8) formed at an outer side thereof with an annular hemispherical groove-shaped flow path 17 formed at an outer side thereof. The suction port 18 of the centripetal part of 2) is sucked from the bottom to the upper part, and the rotor blade radius of the compressor is large, and the upside buoyancy that the structure of the blade side plate 11 and the motor 11 can be the same as that of claim 9 and Thrust generator (See also 29, 30 degrees) The structure different from that of claim 15 is the same, but the structure of the curved pipe flow path (11-15 in FIG. 31) is not connected, and the multi-stage blade shape (as in claim 11) is large, the radius of rotation of the compressor 2 is large, high speed, and the blade side plate 11 ) And the upward buoyancy and thrust generating device of which the structure of the motor 1 can be the same as that of claim 9 (see also 31 and 32). 17. The flow path structure of the end vane (32, 35 degrees 15) outlet flow path structure of the upper portion 916, as in the flow path structure of claim 14, is connected to the flow path of the central portion 21 in the shape of a hemispherical groove and the compressor (2). ) Upward buoyancy and thrust generator having a structure in which the inlet port 22 and the centripetal flow channel 23 are connected, and the outlet 19 flow path is connected to the thrust and the buoyancy device and the closed circuit (32, 33 degrees). Reference) High speed motor 1 equipped with a centrifugal compressor having a large blade rotation radius (2 in FIG. 34), and a multi-stage gear-type flow path 4-9 and an outlet 10 radially mounted in a diameter of a large and short cylindrical cylinder. The annular hemispherical groove 11 flow path is formed in the upper part of the cylinder, and the volume of the cylindrical center portion 18 is discharged into a large closed space, and the upper surface of the cylinder is sealed in a smooth cone shape and the compressor (2) center suction port 912) An upward buoyancy and thrust generating device, in which the structure of the compressor blade (2) side plate (3) and the electric motor (1) can have the same structure as in claim 9 in the circulation device which is re-sucked through. 19. The upward buoyancy and thrust generating device according to claim 18, wherein the upstream buoyancy and thrust generating device has a curved flow path (like 14) connected to the flow path structure (15, 19 in FIG. 37). Stable curvature Cone shape vertically connects several short jaws with a constant flow path area where the edges and grooves (11, 12, 15, and 18 in Fig. 39) are connected up and down at the outer edge of the gently curved structure. The fluid flows to the upper portion 9 by centrifugal force acting on the wall of the flow path by mounting the flow path side plate 11 of the shape of enclosing the chain cone shape. The outlet 4 of the centrifugal compressor 3 having a large rotation radius is connected to the lower portion 34 of the structure generating the thrust, and the flow path is connected. 45 degrees with a straight line 28-19 drawn in the direction of the driving force or buoyancy of the outer flow path surface (see FIG. 45) in the structure connected to the compressor 3 in the center inlet 2 Less than (each 19, 28, 30 is 45 degrees or less) The curvature of the horn outer surface is such that the straight line (20-22) drawn in the direction of propulsion and the angle (24, 32, 31) are at least about 90 degrees or less. (14) When the compressor (3) is rotated at a high speed so that the angle formed by the straight line drawn in the direction of the propulsion and buoyancy is small (close to the straight line) so as not to be excessively curved, the force of the centrifugal force of the fluid generates upward thrust. An upward buoyancy and thrust generating device capable of having the structure of the compressor blade (3) and the side plate and the motor (1) as described in claim 9. (See also 39-42) 21. The structure according to claim 20, wherein a flow path that reverses at the exit of the curved flow path (9 in FIG. 43) and flows back to the lower part is connected to the central inlet port 2 of the compressor 3 by passing through the central port 17 of the cone. The upward buoyancy and thrust of the structure which forms an annular hemispherical groove-shaped flow path at the upper curved flow path exit 9 to make the flow path cross section constant and form a smooth smooth flow path at the compressor 3 and the suction port 2. Generator (see also 43-45) The structure of an isobar in which the flow of the external fluid flowing into the inlet port 2 of the fluid flowing in the centrifugal direction by the centrifugal compressor (1 in FIG. 46) having a large blade radius of high speed is achieved. When the turbine passes through the turbines (4, 5, 6) while being refracted and collected by the opposite flow path (15), the turbine rotates, and the motor and generator (7) mounted on the same shaft as the turbine rotates and the compressor In the structure in which the compressor (1) is rotated by the structure connected integrally with (1) of the turbine (4, 5, 6), the inlet area of the flow path of the inlet (16) gradually decreases slightly from the tip (4 ') of the turbine rotation. It gradually expands to the end blades 6 and the outlet 8 or has a structure in which the flow path area is constant within the rotor blades 4 and 6 and only extends inside the guide blades 5, and the suction port 2 of the centrifugal compressor 1 The flow path cross section is larger than the turbine inlet (at least about 1.5 times) The centrifugal compressor (1), the larger the blade radius and rotation speed, the larger the fluid inlet (2) cross-sectional area than the outlet (16) cross-sectional area, the compressor blade (1) internal flow path (19, 20) cross-sectional area is the outer periphery 20 It is gradually enlarged toward (19) and mounted on the box 14 of the cube with sound absorbing material installed at the entrance and exit ports 9 and 10 and the inner wall 13, and the passage cross-sectional area between the compressor blades 1 is gradually moved from the tip of the core to the exit. It is slightly reduced or made constant, and the inlet 16 flow path cross-sectional area is gradually reduced toward the turbine memory tip 4 '. The first motor and generator 7 are rotated at high speed, and when the critical speed is stopped, the turbine is integrally connected. Power generation (generator) and cooling systems using the current generated in generation (7) and obtaining cooling fluid discharged to the turbine (4,5,6) outlet (8) while continuing to operate with power generated at (4, 5, 6) . 23. The turbine (4,5,6) outlet (8) and compressor (1) inlet port according to claim 22, wherein the outlet of the centrifugal compressor (1 in FIG. 47) and the inlet port 2 are connected in a smooth curvature (12). (2), but a heat exchanger (15) is attached to the oil pipe (17) connecting the turbine outlet (8) and the compressor inlet (2) to heat the fluid ejected to the turbine outlet (8) and recirculate. The flow path cross-sectional area from the turbine outlet 8 to the inlet 9 is not reduced, and the cross-sectional area of the compressor 1 and the outlet 11 to the inlet 10 is constant, and is connected to the turbine outlet 8. The power generation (power generation) and cooling device of the structure connected to the compressor (1), the centrifugal portion (2) is gradually reduced by being combined with the inlet (9). An axial flow compressor (6 in FIG. 50) is mounted in the cylindrical flow paths 20 and 21 in the rotational axis direction, connected to the radial flow path 5 having the same cross-sectional area as the flow path of the compressor 6, and the radial flow path 5 and the axial compressor 6 ), The inlet port (19) and the inlet port (16) and the turbine (2,3,4) are connected to the inlet port (21) to form a closed circuit, and the inlet port (19) is formed so that external fluid can be sucked into the central part of the inlet port (21). , 3,4) The inner flow passage has the same structure as in claim 22, and the lateral flow passage 20 has a cross-sectional area slightly larger than the radial flow passage cross-sectional area 5, 5 'and the compressor 6 in the radial direction 5 + 5'. ), The flow path area to the inlet (7 + 7 ') is constant and the flow path area of the compressor inlet (21) is equal to the sum of the cross-sectional area of the radial flow path (5,5') and the cross section of the external fluid inlet (19). When the generator and the motor 1 are rotated at high speed, the turbines 2, 3, and 4 are rotated by the fluid flowing into the turbine inlet 16 by the rotation of the compressor 6. Power generation to operate the generator 1 while operating the generator blade 1 while rotating the compressor blade 6 by the power, to use the generated current, and to obtain the cooling fluid of the turbine 2, 3, 4 outlet 8 ( Power generation) and chiller. A heat exchanger (12, 13) is mounted in the middle of the oil pipe connecting the turbine (2, 3, 4) outlet 8 and the external fluid inlet (19) of the FIG. Power generation (generation) and cooling device of the structure that the flow path area from the turbine outlet (8) to the inlet (19) is not reduced to the structure for supplying heat in the structure. Radial flow paths 23 and 23 'of the centrifugal compressor (4 in FIG. 52) have a large blade radius and a constant flow path area is formed inside the blade 4, and the compressor 4, the outlet 22 and the suction port 15 are formed. The flow path area is constant from the inlet port 15 to the outlet 22, so that the flow path cross section is smooth (not curved), and the turbine is a centrifugal multistage turbine (16-20). The blade structure and the blade angle are similar to the axial impulse or recoil turbine blade structure and the blade angle of the entrance and exit (foam structures such as 1,2,3,4,5 in Fig. 59), but the blade thickness of the blade tip is thin. The inlet 1 of the circular flow path cross section is formed so that the external fluid flows into the central part of the flow paths 2, 2 'connected to the compressor outlet 22 to the suction port of the compressor 4, and thus connected to the compressor outlet 22. Flow path cross-sectional area is gradually added to the compressor 4 and the centrifugal portion 15 in combination with the flow paths 2 and 2 '. It is designed to be reduced in size, mounted on a hexahedral box 14 equipped with sound absorbing materials at the entrances and exits 3 and 10 and the inner wall 13, and is used as a generator and a high speed to the rotary shaft 25 of the turbine 16-20 and the compressor 4. Power generating (electric power generation) and cooling device that generates electric power by self-operation when power is interrupted at the critical speed by initially supplying power to motor and generator (9) with the structure equipped with electric motor (9). 27. The fluid ejected from the compressor (4 in FIG. 53) outlet 22 without the passage tube connected to the outside and into a space 27 enclosed with the outside. Power generation (power generation) and cooling device of the structure which is made to flow through the inlet (2) formed in the. 27. The pump (14) and suction port (3) of claim 26 having a structure in which a diffuser 28 is mounted at an outlet of a turbine (16-20 in FIG. 56) and a heat exchanger 26 is mounted on an oil pipe 29. Power generation (power generation) and cooling system by a circulator to allow the fluid to flow through the outside of the heat exchanger (26) to supply heat and exit through the outlet (10). 27. The fluid at the compressor outlet (4 in FIG. 57) is separated separately and spouted to a separate outlet (21) and sucked through an external inlet (3) separated therefrom. Power generation (power generation) and cooling device of the structure that ejects to the outlet (10) of the box. 27. The fluid ejected through the compressor (4) and the centripetal fluid outlet (24) using the turbine as a centrifugal multistage turbine (16-20 in FIG. 58) is centripeted through an outflow passage (12). The inlet 12 of the outside of the turbine 16-20 is introduced into the inlet 12 and the blade structure is the same as the axial turbine blade type as described in claim 26, but the inlet angle of the blade tip of the outermost blade 16 is radial direction. And power generation (generation) and cooling arrangements (such as the blade tip of the first paragraph of FIG. 59) with the direction of the blade tip passage radially away from the centroid. The turbine blades with a small blade width and a short distance between the blades and the adjacent blades are fitted with multiple short-circuits at the center of the centrifugal compressor blades (6 in Figs. 59-62 degrees) with a large blade radius, but fixed to the rotor blades (1, 3, 5). (Guide) blades (2,4) or by connecting the bearing (46 of Fig. 61) and the generator rotor 44 of the guide blades (2,4) integrally to operate the separate generator (44,45) It is a turbine composed only of a rotor blade with no fixed blades and all rotors move relative to each other.The turbine blades (1-5) have the same structure as the axial flow impulse and recoil turbine blade structure. Thinner, less friction with the fluid, the flow path inlet angle of the tip blade (1) has a radial structure so that the direction of the fluid flowing outward from the centripet (9) to the outside is easy to flow in the radial direction and the end turbine blade (5) ) Widen the gap between the outlet and the compressor blade (6) The furnace cross-sectional area is kept constant (the 16-part flow path area of Fig. 61 and the 14-way flow path area are the same), and the blade angle of the compressor blade 6 is inclined as much as possible in the circumferential direction. The width of the blade is wider, and the linear distance between the tip and the end of the blade is more than 2.5 times the linear distance between the tip and the tip of the turbine blade, and the distance between the blade and the adjacent blade is gradually expanded from the tip of the blade to the end. (27 in Fig. 62 is less than 28), and the flow path cross-sectional area is gradually reduced and the distance between the left and right wing side plates is gradually closer (14 is greater than 15 in Fig. 61) and the compressor blade 6 is centrifugal It may be of a structure (a centrifugal fan structure with many blades similar to the axial turbine blades), and the cross-sectional area of the flow path between each blade of the turbine blades (1-5) may be the impeller type blade structure. The flow path cross sections of 17, 19, 21, 23, 25 at 62 degrees are larger than the cross-sectional areas of the vane middle portions 17 ', 19', 21 ', 23', 25 'and the blade ends 18, 20, 22, The flow path cross section of 24, 26 is the same as that of the blade tips 17, 19, 21, 23, 25, and in the case of a reactionary wing structure, the blade tips 17, 19, 21, 23, 25 The flow path cross sectional area is larger than the flow path cross sections of the blade middle portions 17 ', 19', 21 ', 23', 25 'and the flow cross section of the blade ends 18, 20, 22, 24, and 26 is the middle portion of the blade flow path. Is less than or equal to and the distance between the blade plates (47-11 'in Fig. 61) is constant from the tip bladehead (1) to the end bladehead (5) and the distance between the compressor blades (6) is small and the number of blades is small. If the turbine blades have a large number of short circuits, the distance between the end turbine blades (5) and the compressor blades (6) is large, the space passage (7) is long, the blade width of the compressor blades (6) is longer, and the radius of rotation is large. Part of side plate To thicken (11) to act as a wheel, to install a short-term contact commutator on the generator and motor 10 side, input the generator 10 output to the storage battery and connected to use the output to initially the generator and motor (10) When the external power is turned on and the critical speed is reached, the compressor 6 rotates by the power generated by itself even when the power is turned off, and thus the cooling fluid at the outlet of the compressor 6 can be used by using the generated current by operating the generator 10. Power generation and cooling device. The outermost compressor blade (4 in Fig. 63) has the same structure as the compressor blade of claim 31, and is equipped with (1, 2, 3) of a compressor with a narrow wing width of several stages at the center, but the distance between the blade and the adjacent blade And the widths of the gaps (1 ', 2', 3 ') between each paragraph are narrow so that the blades of each paragraph are adjacent to each other, and the flow path area between the respective blades is as shown in the compressor blades (6) of claim 31, respectively. Centrifugal multistage compressor with a structure where the flow path area at the tip of the blade is smaller than the flow path area at the tip of the blade of the blade, that is, gradually reduced. 32. The guide blade (33) and the diffuser (34) are installed at the exit of the compressor blade (6), and the oil pipe is extended to be connected to the centripetal inlet (9) via a heat exchanger (37) to form a circulation device. A power generating and cooling device for a closed circuit having a flow path area of the oil pipe (36) extending from the side 35) that is enlarged or constant without being reduced. 32. The suction port 20 and the outlet of the fluid flowing outside the heat exchanger 13 are mounted with the sound absorbing material 25 on the inner wall of the hexahedral box (24 of FIG. 69). 23, but equipped with a centrifugal multi-feeder at the outlet 23 to be connected to the inlet of the turbine (1-5) to install the hydraulic and flow increasing device (16) and to the heat exchanger outlet (14) (16 '). Power generation (power generation) and cooling device by a circulator which allows the fluid discharged to the compressor (11) outlet (11) to flow into the heat exchanger (13) and the suction port (12). The blades of the turbo type centrifugal compressor (2 of 70 and 71 degrees) having a large blade rotation angle and the circumference 33 are extremely small (average angle of about 20 degrees or less). The distance between the wing and the adjacent wing (2 ") is farther away, the width of the blade is larger, the total number of blades is smaller, and the channel cross-sectional area of the blade tip 35 is equal to or slightly narrower than that of the blade end 34. ') And the adjacent blade (2 ") is farther away from the blade tip end portion 35 than the blade tip end portion 35, and the distance between the blade side plates (36,37) is the blade tip (34) at the blade tip (35) The centrifugal turbine (5, 7) is installed in the lateral direction adjacent to the compressor (2), and the turbine (5, 7) has no guide vane. Rotation in the opposite direction to each other, the blade radius of the rotor blades of the advanced turbine (5) is the radius of rotation of the compressor (2) The turbine blade structure is the same as the recoil or impulse blade of the axial turbine, but the blade thickness at the tip of the blade is thin (sharp) to reduce friction with the fluid and the flow path in the turbine blades (5, 7). The cross-sectional area of the blade tip end portion 17 of the blade 73 is larger than the cross-sectional area of the blade middle portion 17 ', and the cross-sectional area of the blade end portion 16 is equal to the blade middle portion 17' (recoil) or blade Like the tip 17 (impulsive), the blade inlet or outlet angle has the same structure as the axial turbine blade, and the shaft plate 19 of the centripet 16 protrudes with curvature so that the shaft of rotation of the turbine of each paragraph is It is connected to the generator (10, 11), but connects the rotary shaft of the tip turbine (5) of the centrifugal with the rotary shaft (11 ') of the generator and the end turbine (7) and the rotary shaft (9) and the external stator (10) of the generator Connected to each other and rotated in opposite directions. When the motor 1 is rotated at a high speed, the core 2 is formed by the compressor 2 at a high speed (the flow path structure of the compressor shaft and the turbine shaft is the same) and the cross-sectional area of the end turbine 7 is larger than that of the advanced turbine. 3) The fluid introduced into the vortex rotates and expands while rotating the turbines 5 and 7, and flows out to the outlet 14, and the number of short circuits of the turbine can be increased. It rotates at high speed and thickens the side plates 37, 38, and 39 of the large portion of the rotation radius of the compressor 2 and the turbines 5 and 7, so that the inertia is increased, and the wheels are actuated. It is a gravity generator and a motor equipped with a short-term contact commutator in the motor (1). When the power is first supplied to the motor (1), the compressor (2) rotates to become a critical speed. 10,11 rotates and the generated current is used in the motor (1). And interrupt the power supply for power generation (power generation) and the cooling apparatus continues to operate while the rotary compressor 2 as a self-developed current. 36. The apparatus according to claim 35, wherein the apparatus is mounted in a box (28) having rod-shaped sound absorbing materials (31, 32) attached to an inlet (23 of FIG. 71) and an outlet (30) and a sound absorbing material (29) attached to an inner wall. A power generation (power generation) and cooling device having a structure in which a nozzle (27) is attached to the inlet port (4) of the) and is connected thereto to mount a fluid compression and flow increase device (25). 37. The fluid according to claim 36, wherein the inlet 24 of the hydraulic and flow increaser 25 of the device and the outlets 8 of the turbines 5, 7 are connected in a conduit with a heat exchanger interposed therebetween and a fluid flowing outside the heat exchanger. Power generation (power generation) and cooling apparatus by a circulator of a structure (see FIG. 69) that supplies heat by means of (gas, liquid) and causes the fluid to cool. (See also 70-73) ※ Note: The disclosure is based on the initial application.