HIGH-EFFICIENCY TURBINE WITH A TIGHT CHAMBER STRUCTURE, HEAT EXCHANGER SYSTEM, AND OPERATING METHOD.
Patent Information
- Application Number
- TR202613949
- Authority / Receiving Office
- TR · TR
- Patent Type
- Applications
- Current Assignee / Owner
- Filing Date
- 2026-08-18
- Publication Date
- 2026-09-21
Smart Images
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Abstract
Description
1 TARIFF HIGH-EFFICIENCY TURBINE WITH A TIGHT-PROOF CHAMBER STRUCTURE, HEAT RECYCLING. CHANGER SYSTEM AND OPERATING METHOD Technical Area The invention consists of a high-efficiency turbine with a sealed chamber structure, a heat exchanger system, and 5 It relates to the operating method. State of the Art In natural gas power plants, which are widely used in energy production today turbines, high-powered turbines, consist of numerous angled blades arranged on a circular turbine housing. It operates on the principle of colliding with rapid, high-pressure combustion gases. This 10 structures that have gaps between turbine blades allowing gas to pass through It is inevitable. However, if the gas flow rate or pressure decreases, combustion will stop. Some of the gas escapes through these gaps without creating any torque. They are leaving the system, which is leading to a significant loss of efficiency. This structural problem... Due to limitations, the operating efficiency of current gas turbines is typically 35-45%. It remains limited in range, and the complex geometry, which includes numerous fins, is high. along with high-level engineering work, high production and maintenance costs It brings with it. In internal combustion engines based on piston-crank mechanisms, efficiency is even lower. and remains at levels of 25-35%. One of the main reasons for this low yield is, 20 continuous cooling of the engine block so that it can be prepared for the next compression cycle. This is a necessity; this situation leads to both a direct energy loss and exhaust fumes. It lowers the gas temperature to levels that will not allow for the regeneration process. Another structural constraint is the variable torque of the piston-crank system depending on the crank angle. It produces combustion gas. The maximum pressure of the combustion gas is at top dead center (Top Dead Center) 25 It is forming around this point, but the moment arm is at its shortest position at this point. Because of this, it is not possible to take efficient advantage of the high pressure. As the crankshaft angle increases, the moment arm reaches the desired length, but this time the cylinder volume increases. Due to the increase in pressure, the pressure has decreased. This physical paradox affects engine block cooling. As a result of the combination of these requirements, approximately 30% of the energy obtained from fuel comes from the engine. through cooling, 35% as exhaust gas heat, and 10% as piston-crank friction. 2 Heat losses occur in the system, resulting in a total efficiency of only around 25%. It can remain. As defined in application number TR2020 / 18190, which is included in the known state of the art. The structure is a chamber-forming valve used to create a high-pressure chamber. It includes. However, since this valve has a large surface area, it requires a high-pressure 5 important to counteract the force exerted by the fluid on the valve surface A considerable amount of power must be expended. The chamber-forming valve requires high pressure. the process of moving it downwards towards the fluid, against this force Because it is implemented, it requires a high energy input, which affects both the system as a whole. It negatively affects both the efficiency and the production of the valve mechanism and 10 This makes sizing difficult. Therefore, application number TR2020 / 18190, force imbalance that occurs during the creation of the high-pressure chamber a solution that leads to both energy loss and manufacturing difficulties It offers a complete solution to the efficiency problems mentioned above. It cannot produce. Therefore, in gas turbines and piston-crank engines 15 the encountered efficiency losses are due to the structural and mechanical properties of the current technique. improved sealing and exhaust that eliminates restrictions independently. A new solution is needed that allows for the regeneration of its energy. In conclusion, due to the negative aspects described above and the current solutions being the subject of discussion... Due to its shortcomings, an improvement in the relevant technical field is necessary. 20 It has been made. Purpose of the Invention The invention was created by drawing inspiration from existing situations and overcoming the aforementioned drawbacks. It aims to solve the problem. The main purpose of the invention is to create a positive pressure 25 at a temperature above 50°C. converting the kinetic and thermal energy of a fluid into torque, or circular motion. a technology that can convert with at least 30% higher efficiency compared to existing technology The aim is to present a system consisting of a turbine and an accompanying heat exchanger. This invention... The basic form of application, as embodied in the application, is the organic Rankine cycle. It is a basic mechanism in which the rotational movement obtained in the turbine rotor is converted into a generator. 30 via electrical energy or direct kinetic energy in vehicles The aim is to transform it. However, any of the turbines that are the subject of the invention... 3 The ability to convert positive pressure fluid into circular motion and torque with high efficiency. Due to its capabilities, it can be used in numerous different technical fields, as described below. This is among the objectives of the invention. One aim of the invention is to create a leak-proof structure between the turbine blade and the turbine housing. by creating a rotational moment of the fluid between the fins without creating a rotational moment. 5 to eliminate the voids through which it can escape and thus preserve the kinetic energy of the fluid The goal is to ensure that almost all of the energy is used to rotate the rotor. Thanks to its structural feature, unlike existing gas turbines, it is suitable for low and medium flow rates. obtaining at least 30% more power and energy without any loss of efficiency. The aim is to increase the number of current gas turbines by 35-45%. its efficiency remaining within the range of the organic Rankine cycle of heat energy in exhaust gas By means of regeneration, it can be increased by at least 100% to 80%. Raising it to that level constitutes another objective of the invention. Furthermore, the existing The turbines require a large number of blades and intensive engineering work. By eliminating the need for it, production and maintenance costs are reduced to the current 15%. The aim is also to reduce the energy consumption by at least 10 times compared to turbines. Another aim of the invention is to address the low efficiency observed in internal combustion piston-crank engines. The goal is to solve this problem with a new working principle and superior design. In this context, the combustion process takes place not inside the turbine, but in a separate chamber containing air from the compressor. The process of heating and expanding the fluid in the combustion chamber and transferring it to the turbine is carried out. 20 It is envisioned that the system will operate on the principle of a continuously rotating circular piston. This eliminates the need for engine block cooling. There is no pressure drop due to cooling, and the exhaust gas is recirculated. It can be stored at a temperature that allows for regeneration. This invention... In its application, instead of the up-down linear movement of the classic crank mechanism, 25 The aim is to use a continuously rotating circular design, which will enable the crankshaft the torque fluctuation that occurs depending on the angle, i.e., sinusoidal torque-crank angle eliminating the relationship and instead obtaining a flat torque-rotor angle characteristic. The aim is to achieve this. In this way, fluctuating torque in conventional internal combustion engines will be eliminated. The aim is also to prevent engine vibration caused by the graph. The 30 in question... Thanks to structural and functional improvements, piston-crank engines can achieve a 25-35% increase. Increasing the efficiency level, which remains at this level, to 85%, and therefore to 100%. up to 70% reduction in CO2 emissions along with an increase in efficiency Ensuring this is one of the important aims of the invention. 4 Another objective of the invention is to create a chamber-forming mechanism that is superior to the current state of the art. Unlike the structure described in application number TR2020 / 18190, the high-pressure fluid It is structured in such a way that it will not have to resist its force. For this purpose, The chamber-forming valve automatically closes as the vane moves, controlling the flow. stopping and relieving the high pressure, then the turbine rotor 5 As the vane advances, the valve's exhaust is ejected by means of a spring-loaded piston mechanism. evacuated from the cavity to the low-pressure zone with no opposing force It is expected to return without encountering anything. This ensures that the power required for valve movement is sufficient. significantly reducing the need and consequently increasing system efficiency. The aim is both to increase production and to overcome manufacturing and sizing difficulties. 10 The purposes regarding the areas of application of the invention can be listed as follows: subject of the invention The turbine, combined with a combustion mechanism, could replace existing internal combustion engines. It will be used as a highly efficient engine in propulsion systems for land, air, and sea vehicles. It is used in this way; thanks to its leak-proof operating mechanism, it is suitable for low and medium flow rates. Because it does not create efficiency loss even in flows, the existing steam in power plants is 15 replacing their turbines, with turbines that are 60% more efficient than today's steam turbines. Its use is due to its superior efficiency compared to existing gas turbines. Use of natural gas in energy production in thermal power plants; 30% at medium flow rates. Unlike existing hydroelectric turbines that operate with 60% efficiency, it achieves 95% efficiency at every flow rate. Thanks to its ability to function, it is used as an energy production turbine in hydroelectric power plants. its use; and to apply positive fluid pressure in the most efficient way to circular motion. Because it is a mechanism that can convert hydraulic oil pressure into circular motion. in hydraulic transmission systems that convert, especially mechanical gear transmissions transmission in vehicles such as construction machinery and locomotives that require high torque where it cannot be used It is used as an organ. 25 The overall aim of the invention is to overcome the structural limitations encountered in the known state of the art, leak-proof structure, independent of yield losses and high production / maintenance costs. And thanks to the principle of continuous circular motion, it provides energy in a wide range of applications. significantly increasing conversion efficiency, reducing fuel consumption and emission values The goal is to develop a turbine and heat exchanger system that reduces heat loss. 30 The structural and characteristic features and all the advantages of the invention are given in the figures below. This becomes clearer thanks to the detailed explanation written with references to these figures. This will be understood, and therefore the evaluation should also take these forms and detailed explanations into consideration. It needs to be done by taking precautions. Figures that will help understand the invention. Figure 1 shows the system used to generate circular motion using the organic Rankine cycle. This is a general overview of its components. 5 Figure 2 shows a general view of the turbine. Figure 3 shows a general view of the rotor. Figure 4 shows a general view of the injection, exhaust, and chambering valves. Figure 5 shows the views of the working fluid voids inside the chambers and on the rotor. Figure 6 shows a cross-sectional view of the turbine rotor. 10 Figure 7 shows a cross-sectional view of the turbine rotor. Figure 8 shows a cross-section and perspective of a dual-channel aluminum extrusion heat exchanger. They are appearances. Figure 9 shows different angles and perspective views of the heat exchanger tube head. Figure 10 shows a cross-section and perspective view of a double-channel aluminum extrusion heat exchanger tube. 15 They are appearances. Figure 11 shows the inside of a double-channel aluminum extrusion heat exchanger tube. They are the appearances of fluids. Explanation of Part References 1 Turbine 20 2 Condensers 3 Mechanical fluid pumps 4 Evaporators Working fluid 6 Working fluid inlet channel 25 7. Working fluid inlet channel - left injection valve connection. 8. Working fluid inlet channel - right injection valve connection. 9 Right turbine housing Left turbine body 11 Rotors 30 12 Rotor connections 13 Right injection, exhaust and chambering valve 14 Left injection, exhaust and chambering valve 6 Right spring piston 16 Left spring piston 17 Right exhaust outlet 18 Left exhaust outlet 19 Right winglet 5 Left winglet 21 Valve injection channels 22 Valve exhaust duct 23 Valve contact surface 24 High pressure chamber 10 exhaust chamber 26 Heat exchanger tubes 27 Heat exchanger tube header 28 Header mounting bolts 29 Heat source fluid inlet 15 Working fluid inlet 31 Fins that increase heat transfer 32 Heat source fluid advancement channel 33 Working fluid advancement channel Detailed Description of the Invention 20 This detailed description explains the invention, which features a high-efficiency, leak-proof chamber structure. The turbine, heat exchanger system, and operating method are the preferred configurations, only. This is explained to facilitate a better understanding of the subject. The invention describes the extraction of energy from any fluid with a temperature above 50°C. with a turbine (1) which obtains rotational moment in an efficient circular motion. It consists of a high-efficiency heat exchanger feeding the turbine (1). The invention The system in question is a mechanism that operates on the principle of the organic Rankine cycle. The rotational motion obtained in the turbine (1) is embodied by means of a generator. electrical energy or kinetic energy for direct use in vehicles It is converted. The basic operation of the system is that the heat source fluid in the evaporator (4) is converted into 30 transfer of the heat energy it possesses to the working fluid (5), this fluid By vaporizing and being pressurized, it is fed into the turbine (1) in pressurized condition and the rotor (11) its rotation, the fluid that has completed its work is re-condensed in the condenser (2) and 7 based on the principle of sending the fluid back to the evaporator (4) by means of a mechanical fluid pump (3). It is based on the fact that the working fluid (5) has a low boiling temperature. Therefore, isopentane was preferred, and isopentane boils at approximately 35°C. it passes into the gas phase and with the pressure energy it has in this phase, it drives the turbine (1) It operates. 5 The heat exchanger used in the system is a double-channel heat exchanger manufactured using the aluminum extrusion method. It has a modular structure consisting of heat exchanger tubes (26). Heat exchanger tubes (26), heat located in the inner channels and produced by aluminum extrusion method. It has an increased heat transfer surface area thanks to the fins (31) that increase heat transfer. and thus a higher heat transfer compared to heat exchangers in current technology. The coefficient is obtained. Multiple heat exchanger tubes (26) have heat located at their ends. by means of changer pipe heads (27) without mixing the internal channels These connecting bolts can be joined together in a leak-proof manner. (28) is fixed. Thanks to this modular structure, the required heat transfer Depending on its capacity, multiple heat exchanger tubes (26) can be combined to form a multi-15 A cellular heat exchanger block can be formed. According to the operating principle of the heat exchanger, the heat source fluid is the heat source fluid. from the inlet (29) it enters the heat exchanger tube (26) and is located in the middle part of the tube The heat source fluid moves through the advancement channel (32). Working fluid (5) enters the system from the working fluid inlet (30) and is located on the outside of the pipe 20 The field working fluid flows through the fluid advancement channel (33). Both fluids It exchanges heat by contacting the fins (31) which increase heat transfer, In this way, heat transfer efficiency is maximized while minimizing heat loss to the outside. The modifier can withstand temperatures up to approximately 350°C, during which time the aluminum maintains its structural stability. with heat source fluids at temperatures such as hot water, hot oil, exhaust combustion gas 25 or is configured to operate with hot steam; the heat source fluid As the temperature increases, the working fluid (5) becomes more pressurized and this situation The heat exchanger increases the energy production efficiency obtained from the turbine (1). The heat exchanger is the second in the cycle. It can also function as a condenser (2) in this stage, in which case it is the heat source Cold water fed from the fluid inlet (29) feeds the hot isopentane coming out of the turbine (1) 30 It is used for the purpose of concentration. When we look at the structural details of the turbine (1), the inlet of the working fluid (5) to the turbine There is a working fluid inlet channel (6) which provides working fluid and this channel is divided into two inside the turbine. 8 separated into working fluid inlet channel-right injection valve connection (8) and working fluid inlet channel-right injection valve connection (8) respectively. the right and left of the turbine via the fluid inlet channel-left injection valve connection (7). It provides power to its sections. The turbine body consists of right and left sides that function independently. two symmetrical sections, namely the turbine body (9) and the left turbine body (10) It consists of the right turbine housing (9) and the left turbine housing (10), both of which are under pressure 5 forming the side and top walls of the chamber, the rotor (11) and on the rotor (11) centering the located vanes (19, 20), so that the vane (19, 20) is related to high-pressure fluid between injection, exhaust and chamber forming valve (13, 14) It forms a closed chamber that allows the rotor (11) to rotate. Right turbine Two separate rotor parts located inside the body (9) and the left turbine body (10), rotor 10 By connecting them through the link (12) they are made into a single piece rotor (11), right vane (19) and left vane with an angular position difference of 180 degrees on this rotor (11). There are two vanes (20). Rotor (11), right vane (19) and left vane on it. (20) obtains rotational motion thanks to the pressure force acting on its surface and this It is the main component that transmits motion to a generator or a power transmission unit. 15 There is one injection, one exhaust, and one chamber formation valve on each of the right and left sections of the turbine. (13, 14) are located. Right injection, exhaust and chambering valve (13), rotor (11) and sealed to the right turbine housing (9) wall via the valve contact surface (23) it is in contact with the high pressure coming from the supply channel (7) on its left side. working fluid (5) through valve injection channel (21) into high pressure chamber (24) 20 It transfers the exhaust through the valve exhaust channel (22) located at the bottom. It discharges the fluid accumulated in the (low pressure) chamber (25). Left injection, exhaust and the chamber forming valve (14) performs the same function symmetrically for the left section. These valves (13, 14) provide leak-proof contact with the rotor (11) when closed. by separating the high pressure chamber (24) from the exhaust (low pressure) chamber (25) with a 25 It functions as a chamber boundary, and in the open position, the relevant vane (19, 20) has high pressure. It allows him to move freely within the chamber (24). The valves (13, 14) The element that provides a watertight contact with the rotor (11) passes through the turbine body (9, 10). The right spring piston (15) and the left spring piston left (16) are the elements connected to the valve (13, 14); By pushing the valve (13, 14) upwards, the vane (19, 20) on the rotor (11) pushes these spring pistons 30 (15, 16) is set up by spontaneous tension, the wing (19, 20) rotates away then returns the valve (13, 14) to its leak-proof position. From the turbine discharged low-pressure fluid, right exhaust outlet (17) and left exhaust outlet (18) It leaves the system via its channels and is directed to the condenser (2). 9 When the working principle of the turbine (1) is examined, it is seen that 1 atmosphere evaporates in the evaporator (4). The working fluid (5) pressurized on it, from the working fluid inlet channel (6) to the turbine (1) fed from here working fluid inlet channel-right injection valve connection (8) and through the working fluid inlet channel-left injection valve connection (7) to the relevant valves (13, 14) reaches and passes through the valve injection channel (21) into the high pressure chamber (24) 5 It enters. In the right section, the right injection, exhaust and chambering valve (13) enters the rotor. (11) makes a leak-proof contact with the valve contact surface (23), while the right vane (19) The working fluid (5) trapped between the rotor (11) surface acts on the vane (19) surface by creating a force, the rotor (11) rotates freely and continuously around its axis clockwise. It causes it to rotate in the direction of the previous 10. By rotating the flap (19, 20), the previous 10 The fluid remaining behind the fins (19, 20) from the cycle exits the exhaust (low pressure) chamber. (25) enters the valve exhaust channel (22), from there through the exhaust outlet (17, 18) to the turbine It leaves and reaches the condenser (2). In the condenser (2), it works with the help of cold water. Isopentane, heat source fluid, advancing through the fluid advancement channel (33) It condenses into the liquid phase by exchanging heat with the cold water passing through the channel (32) and 15 It reaches the mechanical fluid pump (3). The mechanical fluid pump (3), By pushing the condensed isopentane back into the evaporator (4), it restarts the cycle. The vane (19, 20) should be aligned with the relevant injection, exhaust and chambering valve (13, 14). with its arrival, the inclined back surface valve (13, 14) of the vane (19, 20) on the rotor (11) It lifts up automatically. When the valve (13, 14) is lifted up, it hits the turbine (1) wall 20 It stops the flow by fitting tightly and relieves the pressure in that area. It rises, during this movement the spring piston (15, 16) is stretched spontaneously It is being established. During this time, the rotation of the rotor (11) is not interrupted; because the right an angular position difference of 180 degrees between the left wing (19) and the left wing (20) Since it is located, the right injection, exhaust and chambering valve (13) is closed to the 25 position. When passed, the left injection, exhaust and chambering valve (14) is in the open position. is located and the working fluid (5) pressure is instantaneous on the left vane (20). effectively ensuring that the rotor (11) continues to rotate without any significant loss of torque. In this process, the right injection, exhaust and chamber forming valve (13) provides the right injection, exhaust and chamber forming valve (13). With the help of the spring piston (15), it returns to its original sealed position. Same 30 The working principle also applies in the reverse direction: left injection, exhaust, and chamber formation. When valve (14) is closed, this time the right injection, exhaust and chambering valve (13) opening up and the rotor (11) continues to rotate over the right vane (19) This is provided. This sequence between the right turbine housing (9) and the left turbine housing (10) and thanks to the continuous transmission, the rotor (11) is crank-independent, fixed and 35 a maximum torque is produced, in traditional piston-crank mechanisms The observed torque fluctuation and the resulting vibration are eliminated. The rotor (11) The continuous circular motion obtained by this principle, when the rotor (11) is connected to a generator when connected to electrical power, a transmission or powertrain It is directly converted into kinetic energy. 5 The turbine in question (1) is an application of the organic Rankine cycle as described above. The sequence involves converting any positive pressure fluid into circular motion with high efficiency. Thanks to its ability to transform, it can also be used in different technical fields. According to the turbine (1), when combined with a combustion chamber and compressor, it heats up as a result of combustion. an external combustion engine by feeding the expanding gas directly to the turbine (1) 10 It can be used as an engine block, unlike existing piston-crank engines. Since cooling is not needed, the exhaust gas temperature allows for regeneration. It remains at a level where it can be recognized. Similarly, the turbine (1) is used in natural gas power plants. It can be used as a replacement for existing multi-blade gas turbines and operates leak-proof. Thanks to its mechanism, efficiency loss is minimized even at low and medium flow rates. no problems occur. The turbine (1) can operate with high efficiency at every flow rate, in addition It also allows for its use as a water turbine in hydroelectric power plants.
Claims
11 REQUESTS 1. A turbine (1) that converts the energy of a positive pressure fluid into circular motion. feature; a rotor (11) that can rotate around the rotor linkage (12), On the rotor (11), 5 with an angular position difference of 180 degrees relative to each other. at least one right winglet (19) and one left winglet (20) are installed, centering the rotor (11) and the vanes (19, 20); relating to vane (19, 20) a pressure chamber between injection, exhaust and chamber forming valve (13, 14) forming the right turbine housing (9) and the left turbine housing (10), The rotor (11) is in leak-proof contact with a valve contact surface (23) 10 turbine bodies that have open and closed positions and are located on the right and left. (9, 10) each containing one injection, exhaust and chamber formation valve (13, 14), located above the injection, exhaust and chambering valve (13, 14), 15 that enables the transfer of the working fluid (5) to the high pressure chamber (24). a valve injection channel (21) and the rotor (11) rotate in the exhaust chamber (25) a valve exhaust channel that allows the discharge of the remaining working fluid (5). (22), Passing through the turbine body (9, 10) to injection, exhaust and chamber formation connected to the valve (13, 14) and the injection, exhaust and chambering valve 20 (13, 14) spring piston (15, 16) which provides a sealed contact with the rotor (11), providing the entry of the working fluid (5) into the turbine (1) and the right and left a working fluid inlet channel (6) which branches off to injection valve connections (7, 8) It includes the winglet (19, 20) and the related injection, exhaust and chamber formation. As it approaches the line of the valve (13, 14), the inclined ridge on the vane (19, 20) 25 by automatically lifting the surface valve (13, 14) up to the wall of the turbine (1) sealing it tightly so that it temporarily restricts flow and pressure in that section. stopping, during which time the spring piston (15, 16) is set up by itself; Thanks to the 180-degree angular position difference between the winglets (19, 20) side injection, exhaust and chambering valve (13, 14) closed 30 while in this position, the injection, exhaust and chambering valve on the other side (13, 14) By remaining in the open position, the rotor (11) continues to rotate uninterruptedly. 12 The injection, exhaust and chambering valve (13, 14) is spring-loaded and closed. It is the return of the piston (15, 16) to its initial sealed position with the help of a piston.
2. A turbine (1) conforming to claim 1, whose characteristic is that the working fluid (5) has a low boiling point. It is isopenta that has a certain temperature.
3. A turbine (1) conforming to claim 1 or 2, with the following features: an evaporator (4), a condenser 5 (2) and an organic Rankine cycle system together with a mechanical fluid pump (3). The evaporator (4) transfers the heat from the heat source fluid to the working fluid (5) by transferring and evaporating the working fluid (5) coming out of the turbine (1) of the condenser (2) re-condensation with the help of cold water and mechanical fluid pump (3) It is to feed the condensed working fluid (5) back to the evaporator (4). 10 4. A turbine (1) conforming to claim 3, whose characteristic is that the evaporator (4) and / or condenser (2), It consists of a double channel heat exchanger tube (26) and heat in the inner channel of this tube It includes wingers (31) who increase the transfer.
5. A turbine (1) conforming to claim 4, whose characteristic is that the heat exchanger tube (26), in the middle a heat source fluid advancement channel (32) located in the part and 15 located in the outer part The area contains a working fluid flow advance channel (33) and multiple heat heat exchanger tube (26), heat exchanger tube caps (27) and cap fitting modularly sealed together with the help of bolts (28) It is the ability to connect.
6. A turbine (1) that conforms to any of requirements 3 to 5, and its characteristic is; heat source 20 the fluid must have a temperature between 50°C and 350°C and be hot water, hot The oil is selected from exhaust combustion gas or hot steam.
7. A turbine (1) that meets any of the previous requirements and whose characteristic is; right turbine two separate rotor parts located inside the body (9) and the left turbine body (10) It consists of a rotor (11) formed by connecting it to a rotor link (12). 25 8. A turbine (1) that meets any of the previous requirements and whose characteristic is; exhaust to ensure that the working fluid in the room (25) is discharged from the system, The right exhaust outlet (17) and the left exhaust corresponding to the right and left turbine housings (9, 10) The output is that it includes (18) channels. 13 9. Method of operating a turbine (1) that conforms to any of claims 1 to 8. feature; a pressurized working fluid (5), through the working fluid inlet channel (6) to the right and left injection valve connections (7, 8) and from there to the respective injection, feeding to the exhaust and chamber forming valve (13, 14), 5 the working fluid (5) passes through the valve injection channel (21) to the turbine transfer to the high pressure chamber (24) located inside the body (9, 10), the working fluid (5) in the high pressure chamber (24), the relevant vane (19, 20) by applying a force to its surface, it rotates the rotor (11) clockwise, The working fluid remaining from the previous cycle is 10 as the rotor (11) rotates. from the exhaust chamber (25) to the valve exhaust channel (22) and from there discharge from the system being done, the relevant injection, exhaust and chambering valve (13, 14) of the vane (19, 20) as it approaches the line, the inclined ridge surface on the winglet (19, 20) by raising the injection, exhaust and chambering valve (13, 14) turbine 15 (1) to fit it tightly into the wall and at the same time the spring piston (15, 16) by being spontaneously established, the flow and pressure in that section are temporarily reduced. cutting, Thanks to the 180-degree angular position difference between the fins (19, 20), one side injection, exhaust and chambering valve (13, 14) closed 20 when it switches to that position, the injection, exhaust and chamber formation on the opposite side. by keeping the valve (13, 14) in the open position, the rotor (11) does not experience any torque loss. continued uninterrupted rotation, the closing injection, exhaust and chamber forming valve (13, 14), spring piston (15, 16) with the help of the initial 25 which makes sealed contact with the rotor (11) again. returned to its position It includes the steps of the process.
10. This method complies with claim 9 and its characteristic is; a heat source fluid to heat the working fluid (5) in the evaporator (4). by transferring the working fluid (5) evaporation and pressurization 30 ensuring, 14 working fluid (5) coming out of the turbine (1), cold water in the condenser (2) condensing it back into the liquid phase by cooling it with the help of the condensed working fluid (5), with the mechanical fluid pump (3) repeating the cycle by pressing it back into the evaporator (4) It includes the steps of the process. 5 11. A method conforming to claim 10, characterized by the fact that the heat source fluid is a heat source fluid. heat source located in the middle part of the heat exchanger tube (26) from the inlet (29) the fluid is passed through the advance channel (32); the working fluid (5) is the working fluid. working fluid located outside of the same pipe (26) from the fluid inlet (30) passing the fluid through the advance channel (33) and heat transfer between the two fluids 10 Heat exchange is achieved by bringing the fins (31) into contact with the increasing heat.
12. The method conforming to any of claims 9 to 11 is characterized by its working fluid (5) isopenta is used as the source and isopenta is stored at approximately 35°C. It is vaporization.