RU65141U1 - GAS TURBINE ENGINE - Google Patents

Abstract

The inventive utility model is intended for use in power engineering and transport.

The inventive gas turbine engine with reciprocating pistons is designed to convert the energy of combustion of fuel into the energy of the gas stream, and the energy of the gas into the mechanical energy of the driven unit. In our embodiment, the gas turbine engine contains an alternator drive to generate electricity.

The technical result of the claimed utility model is:

1. The increase in the resource of operation of a gas turbine engine.

2. Higher efficiency compared to a gas turbine engine adopted as a prototype.

3. Lower cost of 1 kW. hours of electricity generated by the proposed gas turbine engine compared to a gas turbine engine adopted as a prototype.

The technical result of a gas turbine engine in the claimed utility model is achieved by the fact that, compared with the invention adopted as a prototype, a gas turbine engine containing a combustion chamber, a shaft, a rotor with blades, a compressor, a feed system and an ignition system of a combustible mixture and a heat exchanger, in the claimed of a useful model, a gas turbine engine contains at least two combustion chambers, or multiple of two, and is equipped with a control system, a protection system, an indication and diagnostics unit, an alternator placed on the drive shaft of the output shaft on one side of the gas turbine and secured to it by means of a soft coupling, a controller and a receiver, the aforementioned power system provided with a hydrogen source and at least two, or multiple of two, cylinders for supplying fuel with working pistons, a shutter for protection against emergencies, a mixture accumulator with a double cylinder volume, a safety valve, as well as fuel intake and exhaust valves, are located respectively, in the inlet and exhaust pipes, each cylinder for supplying fuel, of the aforementioned power system, is equipped with a piston drive for the fuel supply cylinders, including a pneumatic cylinder containing an air cavity separated by a baffle with a stuffing box seal located in the center of the cylinder, with a rod installed in its opening, with the piston of the fuel supply cylinder mounted at the end and with the discharge pistons mounted on the rod located inside the pneumatic cylinders of the said actuator shnya fuel delivery cylinders, wherein the air chamber of each air cylinder actuator piston cylinder fuel supply from the fuel supply conduit via an air cylinder connected to the other air cavity of air cylinder

the drive of the piston of the fuel supply cylinder, and on the other side of the injection piston, the air cavity of the pneumatic cylinder of the piston of the fuel supply cylinder is connected through the air pipe, a check valve and an air filter to said receiver, while in the said ignition system the exhaust pipe of each combustion chamber is connected by an air pipe to the air the cavity of the other pneumatic cylinder of the piston drive of the fuel supply cylinder, and is also connected by the air pipe of the exhaust manifold to the said heat exchanger with a coil and with an exhaust pipe, while the said control system is equipped with four pneumatic cylinders for controlling exhaust valves, two pneumatic valves with electric actuators associated with electromagnetic valves for purging the combustion chambers, with a solenoid valve for starting the engine and the aforementioned receiver, and the said protection system is equipped with a coolant temperature sensor in said heat exchanger, air pressure sensors of the pneumatic cylinders of the piston drive of the fuel supply cylinder, pressure sensors the air of the pneumatic cylinders to control the exhaust valves, the air pressure sensor in the receiver, the fuel pressure sensor in the accumulator, the voltage sensor, the pressure sensor in the chamber of the hydrogen source, the water level sensor in the hydrogen source, the temperature sensor of the hydrogen source, tachometer, shutter for protection against emergency situations and a safety valve, as well as non-return valves, and the indicated display and diagnostic unit includes the mentioned controller, as well as interacting with m mentioned: the temperature sensor of the coolant in the heat exchanger, the air pressure sensors of the pneumatic cylinders of the piston of the fuel supply cylinder, the air pressure sensors of the pneumatic cylinders controlling the exhaust valves, the air pressure sensor in the receiver, the fuel pressure sensor in the storage device, the voltage sensor, the pressure sensor in the chamber of the hydrogen source , water level sensor in the source of hydrogen production, temperature sensor of the source of hydrogen production, tachometer, shutter for protection against emergency situations, safety an analysis valve, as well as non-return valves, wherein said controller is configured to interact with the aforementioned power supply, ignition systems, including with the possibility of interaction with pneumatic valves and pneumatic cylinders for controlling exhaust valves, as well as with an indication and diagnostics unit, and is configured to control the process of engine operation, including the control of actuators, including a gas turbine and with the possibility of control through the display and diagnostics unit and close current coupling by the alternator associated with a consumer of electricity.

Description

The utility model is intended for use in power engineering and transport.

The inventive gas turbine engine with reciprocating pistons is designed to convert the energy of fuel combustion into the energy of the gas stream, and the gas energy into the mechanical energy of the driven unit, in our embodiment, the drive of an alternator.

A gas turbine engine comprising at least one combustion chamber, an output shaft of a turbine with blades, a power system and an ignition system is known from the prior art analogues (see Gas Turbine Engine, p. 101, Polytechnical Dictionary, Editor-in-Chief I. I. Artobolevsky. M. "Soviet Encyclopedia", 1977).

The disadvantages of a gas turbine engine adopted as a prototype are:

1. A small service life of the engine.

2. Lower efficiency compared to a gas turbine engine of the claimed utility model.

The closest in number of essential features, the prototype can be adopted "Gas turbine engine", containing combustion chambers, the output shaft of the turbine with blades, a compressor, systems for supplying and ignition of a combustible mixture and a heat exchanger with exhaust pipes (RU IPC 2161714, F02C 3/045, 7108, issued on the application for invention No. 97104082/06 03/18/1997, authors, applicants and patent holders Bahirev Viktor Serafimovich, Bahirev Igor Viktorovich, publication date: January 10, 2001, correspondence address 352400, Krasnodar Territory, Kurganinsk, ul. 76 quarter 1, quarter 20. Bahirev Sun.).

The disadvantages of the known invention are the following:

1. A small resource of operation of a gas turbine engine.

2. Lower efficiency compared with a gas turbine engine of the claimed utility model.

3. Higher cost of 1 kW. hours of energy generated by a gas turbine engine, compared with a gas turbine engine of the claimed utility model.

The technical result of the claimed utility model is:

1. The increase in the resource of operation of a gas turbine engine.

2. Higher efficiency compared to a gas turbine engine adopted as a prototype.

3. Lower cost of 1 kW. hours of energy generated by the proposed gas turbine engine compared to a gas turbine engine adopted as a prototype.

The technical result of a gas turbine engine in the claimed utility model is achieved by the fact that, compared with the invention adopted as a prototype, a gas turbine engine containing a combustion chamber, a shaft, a rotor with blades, a compressor, a feed system and an ignition system of a combustible mixture and a heat exchanger, in the claimed of a useful model, a gas turbine engine contains at least two combustion chambers, or multiple of two, and is equipped with a control system, a protection system, an indication and diagnostics unit, an alternator placed on the drive shaft of the output shaft on one side of the gas turbine and secured to it by means of a soft coupling, a controller and a receiver, the aforementioned power system provided with a hydrogen source and at least two, or multiple of two, cylinders for supplying fuel with working pistons, a shutter for protection against emergencies, a mixture accumulator with a double cylinder volume, a safety valve, as well as fuel intake and exhaust valves, are located respectively, in the inlet and exhaust pipes, each cylinder for supplying fuel, of the aforementioned power system, is equipped with a piston drive for the fuel supply cylinders, including a pneumatic cylinder containing an air cavity separated by a baffle with a stuffing box seal located in the center of the cylinder, with a rod installed in its opening, with the piston of the fuel supply cylinder mounted at the end and with the discharge pistons mounted on the rod located inside the pneumatic cylinders of the said actuator a cylinder of fuel supply cylinders, wherein the air cavity of each pneumatic cylinder of the piston for supplying fuel cylinders from the side of the fuel supply cylinder through the air pipe is connected to the air cavity of the other pneumatic cylinder of the piston drive of the fuel supply cylinder and, on the other side of the injection piston, the air cavity of the pneumatic cylinder of the piston drive of the fuel supply cylinder is connected through an air pipe, a check valve and an air filter with said receiver, while in said exhaust ignition system the nozzle of each combustion chamber is connected by an air pipe to the air cavity of the other pneumatic cylinder of the piston of the fuel supply cylinder, and also connected by an air pipe of the exhaust manifold with said heat exchanger with a coil and an exhaust pipe, while the said control system is equipped with four pneumatic cylinders for controlling exhaust valves, two pneumatic distributors with electric actuator associated with the solenoid valves for purging the combustion chambers, with the electromagnetic valve for starting the engine ator and said receiver, said system provided with a protection sensor coolant temperature in said heat exchanger, the air pressure sensors pneumatic actuator piston cylinder fuel supply, air pressure sensors pneumatic exhaust control valves, air pressure sensor in the receiver, dadatchikom

fuel pressure in the drive, a voltage sensor, a pressure sensor in the chamber of the hydrogen source, a water level sensor in the hydrogen source, a temperature sensor for the hydrogen source, a tachometer, an emergency shutter and a safety valve, as well as non-return valves, and the said unit Indications and diagnostics includes the mentioned controller, as well as the ones mentioned interacting with it: heat carrier temperature sensor in the said heat exchanger, air pressure sensors cylinders for driving a piston of a fuel supply cylinder, air pressure sensors for pneumatic cylinders for controlling exhaust valves, an air pressure sensor in a receiver, a fuel pressure sensor in a storage device, a voltage sensor, a pressure sensor in a chamber of a hydrogen source, a water level sensor in a hydrogen source, a source temperature sensor hydrogen, a tachometer, a shutter for protection against emergency situations, a safety valve, as well as non-return valves, while the said controller is made with the possibility of interaction actions with the aforementioned power supply and ignition systems, including with the possibility of interacting with pneumatic valves and pneumatic cylinders for controlling exhaust valves, as well as with an indication and diagnostics unit, and is configured to control the engine operation process and, in particular, control actuators including gas a turbine and with the ability to control through the display and diagnostic unit and current feedback mentioned by the alternator connected with the consumer of electricity.

The utility model is illustrated by drawings, which depict:

Figure 1. Gas turbine engine, block diagram.

Figure 2. Gas turbine engine block diagram.

The essence of the utility model is a gas turbine engine. A gas turbine engine contains two combustion chambers 1 (Fig. 1), or two times, with water jackets (not shown in the drawing) for cooling the combustion chamber 1 (Fig. 1) and heating water for technical needs, made in the housing of the combustion chamber 1 (figure 1). The combustion chambers 1 (Fig. 1) contain spark plugs 2 (Figs. 1, 2), the intake valves 3 (Fig. 1) of the fuel supply and the exhaust valves 4 (Fig. 1) of the exhaust gas exhaust, as well as the inlet pipes 5 (Fig. .1) and exhaust pipes 6 (Fig. 1). The gas turbine engine contains a shaft 7 (Fig. 1) mounted on bearings 8 (Fig. 1), on which a turbine 9 (Fig. 1) is mounted with blades (not shown in the drawing) and is equipped with an alternator 10 (Fig. 1) ) located on the shaft 7 (Fig. 1) of the drive of the output shaft 7 (Fig. 1) on one side of the said gas turbine and fixed to it by means of a soft coupling 11 (Fig. 1). The gas turbine engine is equipped with a power system and an ignition system of the combustible mixture, a control system, a protection system, an indication and diagnostic unit, a receiver 12 (FIG. 1), a controller 13 (FIGS. 1, 2). The power system is equipped with a source of hydrogen 14 (Fig. 1) and at least two, or multiple of two, mentioned fuel supply cylinders 15 (Fig. 1) with working pistons 16 (Fig. 1), a shutter for protection against emergency situations 17 (FIG. 1), a combustible mixture accumulator 18 (FIG. 1) with a double cylinder volume, a safety valve 19 (FIG. 1) and fuel inlet valves 3 (FIG. 1) and exhaust exhaust valves 4 (FIG. 1) exhaust gases. The fuel supply cylinders 15 (FIG. 1) are equipped with working pistons 16 (FIG. 1), each of which includes a drive of the working piston 16 (FIG. 1) of the fuel supply cylinders 15 (FIG. 1), which includes a pneumatic cylinder 20 (FIG. 1) ), containing an air cavity separated by a baffle 21 located in the center of the cylinder (Fig. 1) with a stuffing box seal (not shown in the drawing), in the hole of which a rod 22 (Fig. 1) is installed, with a working piston 16 mounted at the end (Fig. 1) fuel supply cylinder 15 (Fig. 1) and with air pistons mounted on the stem 22 (Fig. 1) holes 23 (figure 1) located inside the pneumatic cylinders 20 (figure 1) drive the working piston 16 (figure 1) of the fuel supply cylinders 15 (figure 1). Sealing of the rod 22 (Fig. 1) in the baffle 21 (Fig. 1) and in the forcing air piston 23 (Fig. 1) is ensured by stuffing box seals (not shown in the drawing), and the working pistons 16 (Fig. 1) and forcing air pistons 23 (Fig. 1) are sealed with cast-iron and rubber rings (not shown in the drawing). The air receiver 12 (Fig. 1) is configured to be filled with air from each pneumatic cylinder 20 (Fig. 1) of the drive of the working piston 16 (Fig. 1) of the fuel supply cylinders 15 (Fig. 1) through the air pipelines 24 (Fig. 1) with the movement of the pumping air pistons 23 (Fig. 1) in each pneumatic cylinder 20 (Fig. 1). The air cavity of each pneumatic cylinder 20 (Fig.1) drive

the working piston 16 (Fig. 1) of the fuel supply cylinders 15 (Fig. 1) from the side of the fuel supply cylinder 15 (Fig. 1) is connected through the air pipe 24 (Fig. 1) to the air cavity of another actuator pneumatic cylinder 20 (Fig. 1) the working piston 16 (FIG. 1) of the fuel supply cylinder 15 (FIG. 1), and on the other hand the injection piston 23 (FIG. 1) the air cavity of the pneumatic cylinder 20 (FIG. 1) of the drive of the working piston 16 (FIG. 1) of the supply cylinder fuel 15 (FIG. 1) is connected through an air pipe 24 (FIG. 1), check valves 25 (FIG. 1) and an air filter 26 (FIG. 1) with an air receiver 12 (FIG. .one). In the ignition system, the exhaust pipe 6 (Fig. 1) of each combustion chamber 1 (Fig. 1) is connected by an air pipe 24 (Fig. 1) to the air cavity of another pneumatic cylinder 20 (Fig. 1) of the drive of the working piston 16 (Fig. 1) of the cylinder fuel supply 15 (Fig. 1), and is also connected by an air pipe 24 (Fig. 1) of the exhaust pipe to the heat exchanger 27 (Fig. 1) with a coil 28 (Fig. 1) and with an exhaust pipe 29 (Fig. 1). The control system is equipped with four pneumatic control cylinders of the exhaust valves 30 (Fig. 1), connected by air pipelines 24 (Fig. 1) with two pneumatic distributors 31 (Fig. 1) with an electric actuator connected to the electromagnetic valves 32 (Figs. 1, 2) of purging the chambers combustion 1 (Fig. 1), with an electromagnetic valve for starting the engine 33 (Figs. 1, 2). The exhaust control cylinders 30 (FIG. 1) are connected on one side by exhaust air pipes 24 (FIG. 1) to the intake valves 3 (FIG. 1) of the fuel supply of the combustion chambers 1 (FIG. 1), and on the other hand, are connected to the pneumatic valves 31 (Fig. 1) with electric drives, which are configured to control the pneumatic control cylinders of the exhaust valves 30 (Fig. 1), interacting with the inlet 3 (Fig. 1) and the exhaust valves 4 (Fig. 1), overlapping the openings, respectively, of the inlet pipe 5 (figure 1) and exhaust pipe 6 (f ig. 1). The protection system is equipped with a temperature sensor coolant 34 (figure 2) in the heat exchanger 27 (figure 1), air pressure sensors 35 (figure 2) of the pneumatic cylinders 20 (figure 1) of the piston drive 16 (figure 1) of the fuel supply cylinder 15 ( 1), air pressure sensors 36 (FIG. 2) of the pneumatic cylinders for controlling exhaust valves 30 (FIG. 1), an air pressure sensor 37 (FIG. 2) in the receiver 12 (FIG. 1), a fuel pressure sensor 38 (FIG. 2) in the drive of the combustible mixture 18 (figure 1) with a double cylinder volume, a current feedback sensor 39 (figure 2), a voltage sensor 40 (figure 2), a pressure sensor 41 (f Ig.2) in the chamber of the source of hydrogen 14 (Fig. 1), the water level sensor 42 (figure 2) in the source of hydrogen 14 (Fig. 1), the temperature sensor 43 (figure 2) in the source of hydrogen 14 ( figure 1), a tachometer 44 (figure 2), a shutter for protection against emergency situations 17 (figure 1) and a safety valve 19 (figure 1), as well as check valves 25 (figure 1). The display and diagnostic unit includes the mentioned controller 13 (Fig. 1), as well as the mentioned ones interacting with it: temperature sensor of the heat carrier 34 (Fig. 2) in the heat exchanger

27 (FIG. 1), air pressure sensors 35 (FIG. 2) of the pneumatic cylinders 20 (FIG. 1) of the piston drive 16 (FIG. 1) of the fuel supply cylinder 15 (FIG. 1), air pressure sensors 36 (FIG. 2) exhaust control cylinders 30 (FIG. 1), air pressure sensor 37 (FIG. 2) in the receiver 12 (FIG. 1), fuel pressure sensor 38 (FIG. 2) in the combustible mixture storage 18 (FIG. 1) with a double cylinder volume, current feedback sensor 39 (figure 2), voltage sensor 40 (figure 2), pressure sensor 41 (figure 2) in the chamber of the source of hydrogen 14 (figure 1), water level sensor 42 (figure .2) at the source of odoroda 14 (figure 1), a temperature sensor 43 (figure 2) in the source of hydrogen 14 (figure 1), a tachometer 44 (figure 2), a shutter for protection against emergency situations 17 (figure 1) and a safety valve 19 (FIG. 1), as well as check valves 25 (FIG. 1). The proposed gas turbine engine allows the accumulation, and then the consumption of fuel hydrogen combustible mixture, which prevents the accumulation of the mixture in dangerous volumes. The proposed gas turbine engine has a protection system, a diagnostic system consisting of the above sensors and a control controller 13. (Fig.1).

The operation of a gas turbine engine is as follows.

Starting a gas turbine engine is as follows. A compressor or pump (not shown in the drawing) pumps air into the receiver 12 to create pressures of up to 5 atmospheres, set the working pistons 16 in the fuel supply cylinders 15 to the leftmost position (Fig. 1), and then turn on the voltage to the controller 13 and the source hydrogen production 14, after which the cavity of the fuel supply cylinders 15 begin to be filled with hydrogen fuel mixture. Filling the fuel supply cylinders 15 with hydrogen fuel mixture, the command from the controller 13 opens the valve of the air pressure sensor 37 in the receiver 12 into the air cavity of the pneumatic cylinder 20 of the drive of the working piston 16 of the fuel supply cylinder 15 (Fig. 1). When the pressure piston 23 of the pneumatic cylinder 20 and, accordingly, the working piston 16 move in the fuel supply cylinders 15 by means of the working rod 16, the fuel mixture is supplied to the combustion chamber 1 through the open intake valve 3 and the intake pipe 5, the fuel mixture in the combustion chamber 1 reaches 5 atmospheres while the exhaust valve 4 exhaust gas is closed. After the fuel hydrogen fuel mixture has been supplied, the intake valve 3 is closed, the spark plugs 2 are ignited, the fuel mixture in the combustion chamber 1 is ignited and, having reached a pressure of 15-20 atmospheres, the exhaust exhaust valve 4 opens. Through the open exhaust valve 4 of the exhaust gas exhaust 4, the gases ignite, gaining pressure, rush through the exhaust pipes 6 to the blades of the gas turbine 9, while the gases from the high pressure zone enter the pneumatic cylinders 20 to pump the hydrogen fuel mixture into another combustion chamber 1 and return pistons 16 feed cylinders

fuel 15 of the combustion chamber 1, and air is also pumped into the receiver 12. The incoming gases under high pressure on the blades of the gas turbine 9 cause the turbine shaft 7 to rotate, on the shaft 7 of which the alternator 10 is rotated through the coupling 11, in the proposed embodiment, or other mechanisms. After the camera K1 is triggered, other K2 cameras begin to work, these processes are gradually repeated in antiphase. The response frequency depends on the load on the shaft of the gas turbine 9. Combustion chambers work in antiphase, the number of chambers depends on the need for power, but always even. Valves are driven by pneumatic cylinders for controlling exhaust valves 30, and pneumatic cylinders for controlling exhaust valves 30 are controlled by pneumatic valves 31 and controller 13. Pneumatic valves 31 with electric actuators control pneumatic cylinders for controlling exhaust valves 30 interacting with inlet 3 and exhaust valves 4 of exhaust gases that overlap the inlet openings respectively of the inlet 5 and exhaust pipe 6. For controlling the ignition, pneumatic valves, power system, feedback, diagnostics and security system is the controller 13 of the control. The compression ratio is regulated by the pressure of the fuel mixture by the pressure sensor 41 in the chamber of the source of hydrogen 14. The gas turbine engine can operate on the proposed fuel mixture, liquefied gas, low-pressure natural gas and gasoline; at the same time, the fuel system and the security system change somewhat; they are not indicated in the diagram and description. The protection system is equipped with a coolant temperature sensor 34 in the heat exchanger 27, air pressure sensors 35 pneumatic cylinders 20 of the piston drive 16 of the fuel supply cylinder 15, air pressure sensors 36 pneumatic cylinders for controlling the exhaust valves 30, an air pressure sensor 37 in the receiver 12, a fuel pressure sensor 38 in the combustible drive a mixture of 18 with a double cylinder volume, a current feedback sensor 39, a voltage sensor 40, a pressure sensor 41 in the chamber of the hydrogen source 14, a water level sensor 42 in the source hydrogen 14, a temperature sensor 43 in the source of hydrogen 14, a tachometer 44.

Claims (1)

A gas turbine engine comprising combustion chambers, a shaft, a rotor with vanes, a compressor, a feed system and an ignition system of a combustible mixture, and a heat exchanger, characterized in that the gas turbine engine contains at least two combustion chambers, or a multiple of two, and is equipped with a system control system, protection system, display and diagnostic unit, alternator placed on the output drive shaft on one side of the gas turbine and secured to it by a soft coupling with the controller and receiver, moreover the wrinkled power system is equipped with a source of hydrogen production and at least two, or multiple of two, cylinders for supplying fuel with working pistons, a shutter for protection against emergency situations, a combustible mixture accumulator with a double cylinder volume, a safety valve, and also fuel inlet valves and exhaust valves for exhaust gases located respectively in the inlet and exhaust pipes, each cylinder for supplying fuel, said power system, is equipped with a piston cylinder fuel supply core including a pneumatic cylinder, separated by a partition located in the center of the cylinder with a stuffing box seal, in the hole of which a rod is installed, with the piston of the fuel supply cylinder mounted at the end and with pressure pistons mounted on the rod located inside the pneumatic cylinders of the said piston drive fuel supply cylinders, the air cavity of each pneumatic cylinder driving the piston of the fuel supply cylinders from the side of the fuel supply cylinder and through the air pipe is connected to the air cavity of the other pneumatic cylinder of the piston drive of the fuel supply cylinder, and on the other side of the injection piston, the air cavity of the pneumatic cylinder of the piston drive of the fuel supply cylinder is connected through the air pipe, check valve and air filter to the aforementioned receiver, while in the said ignition system the exhaust pipe of each combustion chamber is connected by an air pipe to the air cavity of another pneumatic cylinder for driving the piston of the fuel supply cylinder, and it is also connected by an exhaust manifold air pipe to the aforementioned heat exchanger with a coil and an exhaust pipe, the control system being provided with four pneumatic control cylinders for exhaust valves, two pneumatic control valves with an electric actuator connected to electromagnetic valves for purging the combustion chambers, with an electromagnetic valve for starting the engine and the aforementioned receiver, moreover, the said protection system is equipped with a temperature sensor of the coolant in said heat exchanger, the pressure sensors I of the air of the pneumatic cylinders of the drive of the piston of the fuel supply cylinder, air pressure sensors of the pneumatic cylinders controlling the exhaust valves, air pressure sensor in the receiver, fuel pressure sensor in the fuel mixture with a double cylinder volume, voltage sensor, pressure sensor in the chamber of the hydrogen source, water level sensor in a hydrogen source, a temperature sensor for a hydrogen source, a tachometer, a shutter for emergency protection and a safety valve, as well as valves, and the indicated display and diagnostic unit includes the controller, as well as the ones mentioned: the temperature sensor for the heat carrier in the heat exchanger, the air pressure sensors of the pneumatic cylinders of the piston of the fuel supply cylinder, the air pressure sensors of the pneumatic cylinders for controlling the exhaust valves, the air pressure sensor in the receiver , fuel pressure sensor in the fuel mixture with a double cylinder volume, voltage sensor, pressure sensor in the chamber of the source an orode, a water level sensor in a hydrogen production source, a temperature sensor for a hydrogen production source, a tachometer, a shutter for protection against emergency situations, a safety valve, and also non-return valves, while the said controller is configured to interact with the mentioned power supply and ignition systems, including including, with the possibility of interaction with pneumatic distributors and pneumatic cylinders for controlling exhaust valves, as well as with an indication and diagnostic unit, and is configured to control the work process motor, and including control actuators, comprising a gas turbine and to control over the display and the diagnosis and current feedback, said alternator associated with a consumer of electricity.