Integrated rotary piston gas turbine generator set

Abstract

The application discloses an integrated rotary piston gas turbine generator set, and relates to the technical field of internal combustion engines and generators, and solves the problems of complex structure, large volume and weight, and high price of existing power generation equipment. In the application, hot power is generated by burning gas or oil in a cylinder to drive rotary pistons to rotate, and then the rotary pistons drive a turbine to rotate; the rotating force of the pistons and the turbine drives a gas compression system to ensure the air intake and pressure of a combustion chamber and drives a coaxial generator to generate electric power. The integrated rotary piston gas turbine generator set has the same power as an existing internal combustion engine generator set, and the volume of the integrated rotary piston gas turbine generator set is only half of that of the internal combustion engine generator set; the efficiency of the integrated rotary piston gas turbine generator set is higher than that of a same-power gas turbine generator set; the structure is simplified, the volume and weight are reduced, the structure is simple, the integrated rotary piston gas turbine generator set is easy to manufacture, the price is low, the operation is reliable, the integrated rotary piston gas turbine generator set is solid and durable, the operation efficiency is relatively high, the integrated rotary piston gas turbine generator set is convenient to maintain, and the integrated rotary piston gas turbine generator set is more suitable for high-speed operation and use on mobile equipment.

Description

Technical Field

[0001] This invention relates to the technical field of internal combustion engines and generators, and more particularly to an integrated rotary piston gas turbine generator set. Background Technology

[0002] A generator set is a complete set of mechanical equipment that converts other forms of energy into electrical energy. It consists of a power system and a control system, driven by a water turbine, steam turbine, diesel engine, or other power machinery. It converts the energy generated by water flow, airflow, fuel combustion, or nuclear fission into mechanical energy, which is then transferred to a generator. The generator then converts this mechanical energy into electrical energy, which is output to electrical equipment. Existing generator sets for range-extended electric vehicles, electric agricultural machinery and tractors, fully electric boats, heavy-duty electric aircraft, and engineering sites without mains power are complex in structure, large in size and weight, and expensive, and urgently need to be upgraded or replaced.

[0003] In range-extended electric vehicles (REEVs), the range extender's operating speed and power are completely decoupled from the vehicle's overall speed, thus not being limited by vehicle speed. Automotive drive systems can be categorized into diesel engines, gasoline engines, electric motors, and hybrid systems. Common gasoline and diesel engines are reciprocating piston internal combustion engines, which convert the chemical energy of fuel into the mechanical energy of piston movement to output power. However, reciprocating piston internal combustion engines use a single type of fuel and suffer from problems such as large mass and significant space occupation during piston reciprocating motion.

[0004] An aircraft engine, also known as a flight engine, is a device that converts the thermal energy or other forms of energy of fuel into mechanical energy to provide power for aircraft such as airplanes and helicopters. It is a highly complex and precise thermodynamic machine that provides the power required for aircraft to fly. It has the advantage of being lightweight, but due to its low efficiency and high price, it is difficult to apply directly to electric vehicles.

[0005] In general, existing reciprocating piston engines used in automobiles, airplanes, ships, and tractors are relatively efficient and inexpensive, but their biggest drawback is their large size and heavy weight, limiting their application range. Aero engines (mostly used in aircraft, but also in ships and tanks) are essentially gas turbines. Compared to reciprocating piston engines, they lack pistons and other piston-like components, making them a type of rotary engine (turbomachinery). They can be made smaller and lighter for the same output power, but their disadvantages are lower efficiency and higher cost. At the same output power, reciprocating piston engines (generator sets) can achieve an efficiency of around 40%, while gas turbines (generator sets) struggle to reach 30%. Gas turbines weigh less than half that of reciprocating piston engines, and their price is about ten times that of reciprocating piston engines. Therefore, there is an urgent need for a high-efficiency, small-sized, lightweight, and low-cost generator set. Summary of the Invention

[0006] Based on the problems existing in the background technology, the present invention provides an integrated rotary piston gas turbine generator set that is highly efficient, small in size, light in weight, and low in cost.

[0007] To achieve the above objectives, the technical solution adopted by the present invention is as follows:

[0008] An integrated rotary piston gas turbine generator set includes: a generator rotor 1, a generator stator 2, a turbine mount 3, a rotary piston engine 4, and a turbine rotor 5. The rotary piston engine 4 includes: an engine housing 418, a blade rotor body 405, an eccentric main shaft 404, a bushing 408, and an intake-side eccentric shaft 410. The eccentric main shaft 404 is rotatably mounted within the engine housing 418. The blade rotor body 405 is disposed within the engine housing 418 and sleeved on the eccentric main shaft 404 via the bushing 408. The blade rotor body 405 is rotatable around the eccentric main shaft 404. One end of the air-side eccentric shaft 410 is connected to the air intake end of the eccentric main shaft 404; the generator stator 2 is connected to the air intake side outer wall of the engine housing 418; the generator rotor 1 includes: rotating blades 101, a surrounding belt 102 and permanent magnets 103, the rotating blades 101 are mounted on the air intake side eccentric shaft 410, the outer edge of the rotating blades 101 is connected to the surrounding belt 102, and a plurality of permanent magnets 103 are mounted around the surrounding belt 102; the turbine seat 3 is connected to the exhaust side outer wall of the engine housing 418, and the turbine rotor 5 is located in the turbine seat 3 and mounted on the eccentric main shaft 404.

[0009] In the aforementioned integrated rotary piston gas turbine generator set, the end face of the combustion chamber cylinder 401 is a regular polygon, and the end face of the blade rotor 405 is petal-shaped. The number of petals of the blade rotor 405 is one less than the number of sides of the combustion chamber cylinder 401.

[0010] In the aforementioned integrated rotary piston gas turbine generator set, the engine housing 418 includes: a combustion chamber cylinder 401, an exhaust-side end cover 403, and an intake-side end cover 411. The exhaust-side end cover 403 is installed on one side of the combustion chamber cylinder 401, and the intake-side end cover 411 is installed on the other side of the combustion chamber cylinder 401. The intake-side end cover 411 has multiple air inlets 419, and the exhaust-side end cover 403 has multiple exhaust outlets 420.

[0011] The aforementioned integrated rotary piston gas turbine generator set, wherein the engine housing 418 further includes: spark plugs 416 and fuel injectors 417, and multiple spark plugs 416 and multiple fuel injectors 417 are installed at equal intervals along the outer wall of the combustion chamber cylinder 401, and the multiple spark plugs 416 and multiple fuel injectors 417 extend into the combustion chamber inside the combustion chamber cylinder 401.

[0012] The aforementioned integrated rotary piston gas turbine generator set includes a rotary piston engine 4 that further comprises a gear shaft 406, a key 407, and a large gear ring 412. The gear shaft 406 is connected and fixed to the blade rotor body 405 via the key 407. The large gear ring 412 is installed inside the intake side end cover 411 and meshes with the gear shaft 406.

[0013] The aforementioned integrated rotary piston gas turbine generator set, wherein the engine housing 418 further includes: a spring radial seal 402, wherein a plurality of spring radial seals 402 are installed at equal intervals along the inner wall of the combustion chamber cylinder 401, and at least one spark plug 416 and at least one fuel injector 417 are provided between any two adjacent spring radial seals 402.

[0014] The aforementioned integrated rotary piston gas turbine generator set includes a rotary piston engine 4 further comprising: an intake-side bearing housing 413, an intake-side bearing cover 414, and a rolling bearing 415. The intake-side bearing housing 413 is mounted on the intake-side end cover 411, and the rolling bearing 415 is installed inside the intake-side bearing housing 413. The intake-side eccentric shaft 410 and the intake-side bearing housing 413 are rotatably connected by at least one of the rolling bearings 415. The eccentric main shaft 404 and the turbine housing 3 are rotatably connected by at least one of the rolling bearings 415. The turbine-side bearing is placed in the lower temperature zone outside the turbine rotor 5.

[0015] The aforementioned integrated rotary piston gas turbine generator set includes a generator stator 2 comprising a silicon steel core coil 201, a generator stator base 202, and a motor stator end cover 203. One end of the generator stator base 202 is mounted on the intake side outer wall of the engine housing 418, and the other end of the generator stator base 202 is mounted with the motor stator end cover 203. The silicon steel core coil 201 is located on the inner wall of the generator stator base 202 and is installed inside the motor stator end cover 203. The silicon steel core coil 201 and the shroud 102 are located in the same vertical plane.

[0016] The aforementioned integrated rotary piston gas turbine generator set, wherein the rotary piston engine 4 further includes: an exhaust side cover 409, which is sleeved on the eccentric main shaft 404 and installed on the exhaust side end cover 403.

[0017] In the aforementioned integrated rotary piston gas turbine generator set, the end face of the rotor body 405 is petal-shaped, with each petal being a smoothly transitioning arc protruding outward; the number of petals can be 2 to 9.

[0018] The present invention, by adopting the above-mentioned technical solution, has the following positive effects compared with the prior art:

[0019] (1) In this invention, the heat generated by burning gas or oil in the cylinder drives the rotating piston to rotate, which in turn drives the turbine to rotate. The rotational force of the piston and turbine drives the compression system to ensure the intake and pressure of the combustion chamber and drives the coaxial generator to generate electricity. The integrated rotating piston gas turbine generator set with the same power as the existing internal combustion engine generator set has a volume of only 1 / 3 to 1 / 2 of the internal combustion engine generator set, and its efficiency is higher than that of the gas turbine generator set with the same power. It simplifies the structure, reduces the volume and weight, has a simple structure, is easy to manufacture, is inexpensive, reliable in operation, robust and durable, has high operating efficiency, is easy to maintain, and is more suitable for high-speed operation and use in mobile equipment. Compared with the reciprocating piston engine, the integrated rotating piston gas turbine generator set proposed in this invention has comparable efficiency and price, but the volume and weight of this invention are less than half of that of the reciprocating piston engine. The working efficiency of this invention can reach 40%.

[0020] (2) In this invention, the combustion chamber can burn gasoline, diesel, aviation kerosene, alcohol, natural gas, hydrogen and other fuels without structural modification. In particular, hydrogen combustion can achieve near-zero emissions and has lower requirements for hydrogen purity compared with fuel cells.

[0021] (3) In this invention, the reciprocating piston of the existing reciprocating piston internal combustion engine is replaced by a rotating piston, and turbocharging is performed by a turbine rotor. The combustion chamber cylinder and rotating piston have simple structures and are easy to manufacture in simple 2D.

[0022] (4) This invention integrates the advantages of reciprocating piston engines and gas turbines while eliminating their disadvantages, resulting in high efficiency, small size, light weight, and low cost. It effectively solves the problems of complex structure, large size, heavy weight, and high price of existing generator sets or equipment. This invention is more suitable for high-speed operation and mobile equipment. Attached Figure Description

[0023] Figure 1 This is a schematic diagram of the intake side structure of an integrated rotary piston gas turbine generator set according to the present invention.

[0024] Figure 2 This is a schematic diagram of the exhaust side structure of an integrated rotary piston gas turbine generator set according to the present invention.

[0025] Figure 3 This is an intake side view of an integrated rotary piston gas turbine generator set according to the present invention.

[0026] Figure 4 This is a side sectional view of an integrated rotary piston gas turbine generator set according to the present invention.

[0027] Figure 5This is an intake side view of the rotary piston engine of an integrated rotary piston gas turbine generator set according to the present invention.

[0028] Figure 6 This is an internal schematic diagram of the intake side of the rotary piston engine of an integrated rotary piston gas turbine generator set according to the present invention.

[0029] Figure 7 This is an exhaust side view of the rotary piston engine of an integrated rotary piston gas turbine generator set according to the present invention.

[0030] Figure 8 This is an internal schematic diagram of the exhaust side of the rotary piston engine of an integrated rotary piston gas turbine generator set according to the present invention.

[0031] Figure 9 This is an air intake side view of the blade rotor of an integrated rotary piston gas turbine generator set according to the present invention.

[0032] Figure 10 This is a side view of the blade rotor of an integrated rotary piston gas turbine generator set according to the present invention.

[0033] Figure 11 This is a top view of the blade rotor of an integrated rotary piston gas turbine generator set according to the present invention.

[0034] Figure 12 This is an exhaust side view of the blade rotor of an integrated rotary piston gas turbine generator set according to the present invention.

[0035] Figure 13 This is a schematic diagram of the structure of an integrated rotary piston gas turbine generator set of the present invention, which has a regular pentagonal combustion chamber cylinder with four petals.

[0036] Figure 14 The present invention relates to an integrated rotary piston gas turbine generator set with a regular pentagonal combustion chamber cylinder body and a cycloid equation with four petals.

[0037] Figure 15 This is a schematic diagram of the equilateral triangular combustion chamber cylinder of an integrated rotary piston gas turbine generator set of the present invention, with two petals.

[0038] Figure 16 The present invention relates to an integrated rotary piston gas turbine generator set with an equilateral triangular combustion chamber cylinder body and a cycloidal equation having two petals.

[0039] Figure 17 This is a side sectional view of the generator rotor of an integrated rotary piston gas turbine generator set according to the present invention.

[0040] Figure 18This is a schematic diagram of the generator rotor of an integrated rotary piston gas turbine generator set according to the present invention.

[0041] Figure 19 This is a schematic diagram of the structure of the eccentric main shaft and the intake-side eccentric shaft of an integrated rotary piston gas turbine generator set according to the present invention.

[0042] Figure 20 This is a schematic diagram showing the axial positions of the eccentric main shaft and the intake-side eccentric shaft of an integrated rotary piston gas turbine generator set according to the present invention.

[0043] In the attached diagram: 1. Generator rotor; 101. Rotating blade; 102. Surrounding belt; 103. Permanent magnet; 2. Generator stator; 201. Silicon steel core coil; 202. Generator stator frame; 203. Motor stator end cover; 3. Turbine mount; 4. Rotary piston engine; 401. Combustion chamber cylinder block; 402. Spring radial seal; 403. Exhaust side end cover; 404. Eccentric main shaft; 405. Blade rotor body ; 406, Gear shaft; 407, Flat key; 408, Bushing; 409, Exhaust side cover; 410, Intake side eccentric shaft; 411, Intake side end cover; 412, Large gear ring; 413, Intake side bearing housing; 414, Intake side bearing cover; 415, Rolling bearing; 416, Spark plug; 417, Fuel injector; 418, Engine housing; 419, Intake port; 420, Exhaust port; 5, Turbine rotor. Detailed Implementation

[0044] The present invention will be further described below with reference to the accompanying drawings and specific embodiments, but this is not intended to limit the scope of the invention.

[0045] Please refer to Figures 1 to 20As shown, an integrated rotary piston gas turbine generator set is illustrated, comprising: a generator rotor 1, a generator stator 2, a turbine housing 3, a rotary piston engine 4, and a turbine rotor 5. The rotary piston engine 4 includes: an engine housing 418, a blade rotor body 405, an eccentric main shaft 404, a bushing 408, and an intake-side eccentric shaft 410. The eccentric main shaft 404 is rotatably mounted within the engine housing 418. The blade rotor body 405 is disposed within the engine housing 418 and sleeved on the eccentric main shaft 404 via the bushing 408. The blade rotor body 405 is rotatable around the eccentric main shaft 404. 4. Rotation: One end of the intake-side eccentric shaft 410 is connected to the intake end of the eccentric main shaft 404; the generator stator 2 is connected to the intake-side outer wall of the engine housing 418; the generator rotor 1 includes: rotating blades 101, a surrounding belt 102, and permanent magnets 103. The rotating blades 101 are mounted on the intake-side eccentric shaft 410, and the outer edge of the rotating blades 101 is connected to the surrounding belt 102. Multiple permanent magnets 103 are mounted around the surrounding belt 102; the turbine seat 3 is connected to the exhaust-side outer wall of the engine housing 418, and the turbine rotor 5 is located inside the turbine seat 3 and mounted on the eccentric main shaft 404.

[0046] Furthermore, in a preferred embodiment, the end face of the combustion chamber cylinder 401 is a regular polygon, and the end face of the blade rotor 405 is petal-shaped, with the number of petals of the blade rotor 405 being one less than the number of sides of the combustion chamber cylinder 401.

[0047] Furthermore, in a preferred embodiment, the engine housing 418 includes: a combustion chamber cylinder block 401, an exhaust-side end cover 403, and an intake-side end cover 411. The exhaust-side end cover 403 is installed on one side of the combustion chamber cylinder block 401, and the intake-side end cover 411 is installed on the other side of the combustion chamber cylinder block 401. The intake-side end cover 411 has a plurality of air inlets 419, and the exhaust-side end cover 403 has a plurality of exhaust outlets 420.

[0048] Furthermore, in a preferred embodiment, the engine housing 418 further includes: spark plugs 416 and fuel injectors 417, with multiple spark plugs 416 and multiple fuel injectors 417 installed at equal intervals along the outer wall of the combustion chamber cylinder 401, and the multiple spark plugs 416 and multiple fuel injectors 417 extending into the combustion chamber inside the combustion chamber cylinder 401.

[0049] Furthermore, in a preferred embodiment, the rotary piston engine 4 further includes: a gear shaft 406, a key 407, and a large gear ring 412. The gear shaft 406 is connected and fixed to the blade rotor body 405 via the key 407. The large gear ring 412 is installed inside the intake side end cover 411, and the large gear ring 412 meshes with the gear shaft 406.

[0050] Furthermore, in a preferred embodiment, the engine housing 418 further includes: a spring radial seal 402, a plurality of spring radial seals 402 are installed at equal intervals along the inner wall of the combustion chamber cylinder 401, and at least one spark plug 416 and at least one fuel injector 417 are provided between any two adjacent spring radial seals 402.

[0051] Furthermore, in a preferred embodiment, the rotary piston engine 4 further includes: an intake-side bearing housing 413, an intake-side bearing cover 414, and a rolling bearing 415. The intake-side bearing housing 413 is mounted on the intake-side end cover 411, and the rolling bearing 415 is installed inside the intake-side bearing housing 413. The intake-side eccentric shaft 410 and the intake-side bearing housing 413 are rotatably connected by at least one rolling bearing 415. The eccentric main shaft 404 and the turbine housing 3 are rotatably connected by at least one rolling bearing 415. The turbine-side bearing is placed in the lower temperature zone outside the turbine rotor 5.

[0052] Furthermore, in a preferred embodiment, the generator stator 2 includes: a silicon steel core coil 201, a generator stator frame 202, and a motor stator end cover 203. One end of the generator stator frame 202 is installed on the air intake side outer wall of the engine housing 418, and the other end of the generator stator frame 202 is equipped with the motor stator end cover 203. The silicon steel core coil 201 is disposed on the inner wall of the generator stator frame 202 and installed inside the motor stator end cover 203. The silicon steel core coil 201 and the surrounding belt 102 are located in the same vertical plane.

[0053] Furthermore, in a preferred embodiment, the rotary piston engine 4 further includes an exhaust-side cover 409, which is sleeved on the eccentric main shaft 404 and mounted on the exhaust-side end cover 403.

[0054] The above are merely preferred embodiments of the present invention and are not intended to limit the implementation methods and protection scope of the present invention.

[0055] In addition to the above, the present invention also has the following embodiments:

[0056] In a further embodiment of the present invention, an integrated rotary piston gas turbine generator set is disclosed, which consists of three parts: a generator, an internal combustion engine, and a turbine.

[0057] In a further embodiment of the present invention, the integrated rotary piston gas turbine generator set is a whole. All fixed parts of the whole are defined as the stator part, which is a component of the integrated rotary piston gas turbine generator set. All rotatable parts of the whole are defined as the rotor part, which is a component fixed on a crankshaft. The crankshaft consists of an intake-side eccentric shaft 410 and an eccentric main shaft 404. The intake-side eccentric shaft 410 and the eccentric main shaft 404 are fixed together by a pin connection. One end of the crankshaft on the rotor part is rotatably connected to the intake-side bearing seat 413 of the stator part through two rolling bearings 415. The other end of the crankshaft on the rotor part is rotatably connected to the turbine seat 3 of the stator part through one rolling bearing 415. The stator part, rotor part, intake-side end cover 411 and exhaust-side end cover 403 are connected together by three bearings to form an integrated structure.

[0058] In a further embodiment of the present invention, an integrated rotary piston gas turbine generator set includes a stator section. The stator section is internally provided with a generator stator base 202, a combustion chamber cylinder 401, a silicon steel core coil 201, an intake side bearing cover 414, an intake side end cover 411, and an intake side bearing seat 413. The silicon steel core coil 201 is composed of a generator core and a coil. The intake side end cover 411 is equipped with a positioning planetary gear set large gear ring 412. The intake side bearing seat 413 and the turbine seat 3 are respectively equipped with front and rear rolling bearings 415. The rolling bearings 415 support the rotor section. The rotor section is composed of compressor rotating blades 101 on the same crankshaft, a generator permanent magnet 103 on the shroud 102, a turbine rotor 5, a rotating piston rotating in the crank section, and a positioning planetary gear set gear shaft 406. The rotating piston is also known as the blade rotor body 405.

[0059] In a further embodiment of the present invention, which relates to the field of internal combustion engine and generator technology, the invention proposes a method where the combustion of gas or oil in a cylinder generates heat to drive a rotating piston rotor 405, which in turn drives a turbine rotor 5. The rotational force of the rotor 405 and the turbine rotor 5 drives a compression system to ensure the intake and pressure of the combustion chamber, and drives a coaxial generator to produce electricity. By replacing the reciprocating piston of the existing reciprocating piston internal combustion engine with a rotating piston and using the turbine rotor 5 for turbocharging, the mass and size of the engine are reduced. A rotating piston gas turbine generator set with the same power output has a volume of only about 1 / 3 to 1 / 2 that of an existing internal combustion engine generator set, and its efficiency is higher than that of a gas turbine generator set with the same power output. It has a simple structure, is easy to manufacture, inexpensive, reliable in operation, robust and durable, and has high operating efficiency, making it more suitable for high-speed operation.

[0060] In a further embodiment of the present invention, a rotary piston replaces the reciprocating piston of the existing reciprocating piston internal combustion engine, and a turbine rotor 5 is used for turbocharging. Compared with the existing internal combustion engine, the volume and mass of the rotary piston gas turbine generator set are halved, while the power generation efficiency is the same.

[0061] In a further embodiment of the present invention, the integrated rotary piston gas turbine generator set proposed in this patent generates heat by burning gas or oil in the cylinder to drive the blade rotor 405 to rotate, which in turn drives the turbine rotor 5 to rotate. The rotational force of the blade rotor 405 and the turbine rotor 5 drives the compression system to ensure the intake and pressure of the combustion chamber, and drives the coaxial generator to generate electricity. By replacing the reciprocating piston of the existing reciprocating piston internal combustion engine with a rotary piston and using the turbine rotor 5 for turbocharging, the mass is reduced while the engine size is reduced. The rotary piston gas turbine generator set with the same power is only about 1 / 3 to 1 / 2 the size of the existing internal combustion engine generator set, and the efficiency is higher than that of the gas turbine generator set with the same power. It has a simple structure, is easy to manufacture, is inexpensive, reliable in operation, robust and durable, and has high operating efficiency, making it more suitable for high-speed operation.

[0062] In a further embodiment of the present invention, based on the cycloidal curve equation, a series of rotary piston propulsion systems with different numbers of combustion chambers are given, such as... Figures 13 to 16 As shown, compared to existing internal combustion engine units, this design increases the pressure in the gas turbine combustion chamber without a linkage mechanism. The generator rotor blades 101 and the compressor impeller shroud 102 are integrated into one unit, and the generator rotor 1, generator stator 2, and intake side end cover 411 are connected together by two rolling bearings 415. This integrated structure solves the problems of complex structure, large size, heavy weight, and high price of existing power generation equipment, making it more suitable for high-speed operation and use in mobile equipment.

[0063] In further embodiments of the present invention, such as Figures 13 to 16 As shown, based on the cycloidal equation constrained by the gear ratio of the internal and external gears in a specific positioning planetary gear set (n:n-1, n≥3 integers), multiple regular polygons with 3 sides, 4 sides, 5 sides, etc., and corresponding petal shapes with 2 petals, 3 petals, 4 petals, etc., can be derived. The number of petals is also called the number of leaves, which equals the number of sides minus one. Regular polygons and petal shapes can be used as the stator and rotor of the rotary piston engine 4, respectively. The regular polygons can be placed sideways on the stator, and the petal shapes can be placed sideways on the rotor, such as... Figures 5 to 8 As shown, the petal-shaped blades can also be placed on the stator, and the regular polygonal blades on the rotor. Because of the even number of power strokes, an even number series of blades (2, 4, 6...) is preferred. One combustion chamber is placed on each side or vertex of the corresponding regular polygon, so the number of combustion chambers equals the number of sides, i.e., an odd number of combustion chambers (3, 5, 7...). Placing the combustion chambers on the stator side offers more advantages.

[0064] In a further embodiment of the present invention, preferably, the end face of the combustion chamber cylinder 401 is a regular polygon, the end face of the blade rotor 405 is petal-shaped, and the number of blades of the blade rotor 405 is equal to the number of sides of the combustion chamber cylinder 401 minus one.

[0065] In a further embodiment of the present invention, preferably, the generator rotating blades 101 and the compressor impeller shroud 102 are integrated into one unit.

[0066] In a further embodiment of the present invention, preferably, a rolling bearing 415 is installed inside the turbine housing 3, and the turbine housing 3 and the eccentric main shaft 404 are rotatably connected by the rolling bearing 415. The turbine-side rolling bearing 415 is placed in the lower temperature zone outside the turbine.

[0067] In a further embodiment of the present invention, a turbine rotor 5 is provided between the turbine-side rolling bearing 415 and the exhaust-side end cover 403. The turbine-side rolling bearing 415 is mounted on the eccentric main shaft 404 and is as far away from the blade rotor body 405 as possible. The exhaust-side end cover 403 is provided with a plurality of exhaust ports 420. By increasing the distance between the turbine-side rolling bearing 415 and the exhaust-side end cover 403, the turbine-side rolling bearing 415 is placed in the lower temperature zone outside the turbine, reducing the temperature influence on the turbine-side rolling bearing 415 and extending the service life of the turbine-side rolling bearing 415.

[0068] In a further embodiment of the present invention, the integrated rotary piston gas turbine generator set with the same power output has a volume that is only 1 / 3 to 1 / 2 that of an internal combustion engine generator set, and its efficiency is higher than that of a gas turbine generator set with the same power output. It simplifies the structure, reduces size and weight, is inexpensive, and is easy to maintain. It is more suitable for high-speed operation and use in mobile equipment.

[0069] In a further embodiment of the present invention, the combustion chamber of the integrated rotary piston gas turbine generator set can burn fuels such as gasoline, diesel, aviation kerosene, alcohol, natural gas, and hydrogen without structural modifications. In particular, hydrogen combustion can achieve near-zero emissions, and compared with fuel cells, the requirements for hydrogen purity are not high.

[0070] In a further embodiment of the present invention, a rotary piston replaces the reciprocating piston of a conventional reciprocating piston internal combustion engine, and a turbine rotor 5 is used for turbocharging. The rotary piston rotor body 405 is as follows: Figures 9 to 12 As shown, the combustion chamber cylinder block 401 and the rotary piston have a simple structure and are easy to manufacture in simple 2D.

[0071] In a further embodiment of the present invention, a generator rotor 1 and a generator stator 2 are provided on the intake side of the rotary piston engine 4. The generator rotor 1 is driven to rotate in the generator stator 2 by the rotary piston engine 4. A silicon steel core coil 201 is provided in the generator stator 2. The permanent magnet 103 on the generator rotor 1 continuously cuts the magnetic field lines to realize the power generation function.

[0072] In a further embodiment of the present invention, a combustion chamber is provided inside the rotary piston engine 4, that is, multiple partitioned combustion chambers are provided between the inner wall of the combustion chamber cylinder 401 and the outer wall of the vane rotor 405. Fuel is injected into the combustion chamber through the fuel injector 417 and ignited by the spark plug 416, driving the vane rotor 405 to rotate. The vane rotor 405 drives the eccentric position of the eccentric main shaft 404 to move within the engine housing 418. The gear shaft 406 and the large gear ring 412 mesh, causing the gear shaft to... 406 moves along the internal teeth of the large gear ring 412. Under the action of the large gear ring 412, the blade rotor body 405 and the eccentric main shaft 404 rotate synchronously but in opposite directions. The blade rotor body 405 drives the eccentric main shaft 404 to rotate. The intake side eccentric shaft 410 and the eccentric main shaft 404 are connected and fixed by a pin. The generator rotor 1 is mounted on the intake side eccentric shaft 410, and the turbine rotor 5 is mounted on the eccentric main shaft 404. The generator rotor 1 and the turbine rotor 5 are located on the same axis. Figure 20 As shown, the rotary piston engine 4 and the turbine rotor 5 drive the generator rotor 1 to rotate synchronously.

[0073] In a further embodiment of the present invention, the generator rotor 1 is composed of rotating blades 101 and a surrounding belt 102. Permanent magnets 103 are arranged along the surrounding belt 102 for generating electricity. The rotating blades 101 rotate with the intake side eccentric shaft 410, continuously inputting air into the rotary piston engine 4, thereby increasing the working efficiency of the rotary piston engine 4.

[0074] In a further embodiment of the present invention, the rotary piston engine 4 employs an eccentric main shaft 404, on which a vane rotor 405 is mounted. A gear shaft 406 is mounted on the vane rotor 405, and a large gear ring 412 is mounted on the intake side end cover 411. The gear shaft 406 and the large gear ring 412 mesh. After the vane rotor 405 rotates and drives the eccentric portion of the eccentric main shaft 404 to move within the engine housing 418, the movement is achieved through the gear shaft 406 and the large gear ring 412. Figures 5 to 8 The equation of motion for the cycloid is shown in the figure.

[0075] In a further embodiment of the present invention, the exhaust-side end cap 403 and the eccentric main shaft 404 are sealed by the exhaust-side small cover 409.

[0076] In a further embodiment of the present invention, the combustion chamber is connected to the outer wall of the blade rotor body 405, thereby increasing the working efficiency of the rotary piston engine 4.

[0077] In a further embodiment of the present invention, the spring radial seal 402 is used to separate the combustion chamber, and a spring plate is provided thereon to facilitate the rotation of the blade rotor 405 within the combustion chamber cylinder 401.

[0078] In a further embodiment of the present invention, the blade rotor body 405 is as follows: Figures 9 to 12 As shown, the intake side has an intake chamber communicating with its outer wall, and the exhaust side has an exhaust chamber communicating with its outer wall. The blade rotor 405 is sleeved on the eccentric main shaft 404 through the bushing 408, and the gear shaft 406 is sleeved on the eccentric main shaft 404. The blade rotor 405 and the gear shaft 406 are connected by a flat key 407. After the rotary piston engine 4 is running, the fuel injector 417 injects fuel into the combustion chamber in the combustion chamber cylinder 401 and ignites it through the spark plug 416, which drives the blade rotor 405 to rotate in the combustion chamber cylinder 401. During the rotation of the blade rotor 405, air is introduced into the combustion chamber through the intake chamber on its intake side, and the next blade of the blade rotor 405 compresses the air in the combustion chamber. After fuel is injected through the fuel injector 417 and ignited by the spark plug 416, the exhaust gas after combustion is discharged through the exhaust chamber on its exhaust side. At the same time, the discharged exhaust gas is used to drive the turbine rotor 5 to rotate in the turbine mount 3.

[0079] In a further embodiment of the present invention, the blade rotor body 405 is sleeved on the eccentric position of the eccentric main shaft 404 through the bushing 408, so that the blade rotor body 405 can compress the combustion chamber in the combustion chamber cylinder block 401 during rotation. At the same time, the gear shaft 406 meshes with the large gear ring 412 assembled on the intake side end cover 411, realizing the rotation of the eccentric main shaft 404, and the rotation direction of the eccentric main shaft 404 is opposite to that of the blade rotor body 405.

[0080] In a further embodiment of the present invention, the generator rotor 1 is composed of rotating blades 101, a surrounding belt 102, and permanent magnets 103. The rotating blades 101 are mounted on the intake-side eccentric shaft 410, and the outer edge of the rotating blades 101 is connected to the surrounding belt 102. A plurality of permanent magnets 103 are mounted around the surrounding belt 102, such as... Figure 17 and Figure 18 As shown.

[0081] In a further embodiment of the present invention, the eccentric main shaft 404 and the intake side eccentric shaft 410 are connected by pins. The eccentric main shaft 404 and the intake side eccentric shaft 410 form a crankshaft with both ends located on the same axis. The rotating blades 101 are mounted on the intake side eccentric shaft 410. After the crankshaft is driven to rotate by the rotary piston engine 4 and the turbine rotor 5, it drives the generator rotor 1 to rotate. The generator stator 2 is provided with a silicon steel core coil 201. The permanent magnet 103 on the generator rotor 1 continuously cuts the magnetic field lines to achieve the power generation function. At the same time, it drives the rotating blades 101 of the generator rotor 1 to rotate, continuously inputting air into the rotary piston engine 4 and increasing the working efficiency of the rotary piston engine 4.

[0082] In a further embodiment of the present invention, the blade rotor body 405 is sleeved on the eccentric main shaft 404 by a bushing 408, and the eccentric main shaft 404 can rotate freely within the blade rotor body 405 by setting the bushing 408.

[0083] In a further embodiment of the present invention, the rotary piston gas turbine generator set consists of three parts: a generator, an internal combustion engine, and a turbine. The generator rotor 1 is driven to rotate within the generator stator 2 by the rotary piston engine 4 and the turbine rotor 5 to achieve the power generation function. At the same time, air is input to the rotary piston engine 4 through the rotating blades 101 of the generator rotor 1, increasing the working efficiency of the rotary piston engine 4. By replacing the reciprocating piston of the existing reciprocating piston internal combustion engine with a rotary piston and using the turbine rotor for turbocharging, the structure is simplified and the volume and weight are reduced. Its volume is only 1 / 3 to 1 / 2 of that of an internal combustion engine generator set, and its efficiency is higher than that of a gas turbine generator set of the same power. This solves the problems of complex structure, large size, heavy weight, and high price of existing power generation equipment.

[0084] The above are merely preferred embodiments of the present invention and are not intended to limit the implementation methods and protection scope of the present invention. Those skilled in the art should recognize that any equivalent substitutions and obvious changes made based on the description and illustrations of the present invention should be included within the protection scope of the present invention.

Claims

1. An integrated rotary piston gas turbine generator set, characterized in that, include: The generator rotor (1), generator stator (2), turbine mount (3), rotary piston engine (4), and turbine rotor (5) are included. The rotary piston engine (4) includes: engine housing (418), blade rotor body (405), eccentric main shaft (404), bushing (408), and intake side eccentric shaft (410). The eccentric main shaft (404) is rotatably mounted inside the engine housing (418). The blade rotor body (405) is located inside the engine housing (418) and is sleeved on the eccentric main shaft (404) through the bushing (408). The blade rotor body (405) can rotate around the eccentric main shaft (404). One side of the intake side eccentric shaft (410) is... The generator stator (2) is connected to the intake end of the eccentric main shaft (404); the generator rotor (1) is connected to the intake side outer wall of the engine housing (418); the generator rotor (1) includes: rotating blades (101), a shroud (102) and permanent magnets (103), the rotating blades (101) are mounted on the intake side eccentric shaft (410), the outer edge of the rotating blades (101) is connected to the shroud (102), and a plurality of permanent magnets (103) are mounted around the shroud (102); the turbine seat (3) is connected to the exhaust side outer wall of the engine housing (418), and the turbine rotor (5) is located in the turbine seat (3) and mounted on the eccentric main shaft (404); The end face of the combustion chamber cylinder block (401) is a regular polygon, and the end face of the blade rotor body (405) is petal-shaped. The number of petals of the blade rotor body (405) is one less than the number of sides of the combustion chamber cylinder block (401). The rotary piston engine (4) further includes: an intake side bearing housing (413), an intake side bearing cover (414), and a rolling bearing (415). The intake side bearing housing (413) is mounted on the intake side end cover (411). The rolling bearing (415) is installed inside the intake side bearing housing (413). The intake side eccentric shaft (410) and the intake side bearing housing (413) are rotatably connected by at least one of the rolling bearings (415). The eccentric main shaft (404) and the turbine housing (3) are rotatably connected by at least one of the rolling bearings (415). The turbine side bearing is placed in the lower temperature zone outside the turbine rotor (5). The generator stator (2) includes: a silicon steel core coil (201), a generator stator frame (202), and a motor stator end cover (203). One end of the generator stator frame (202) is installed on the outer wall of the engine housing (418) on the air intake side. The other end of the generator stator frame (202) is equipped with the motor stator end cover (203). The silicon steel core coil (201) is located on the inner wall of the generator stator frame (202) and installed inside the motor stator end cover (203). The silicon steel core coil (201) and the shroud (102) are located in the same vertical plane.

2. The integrated rotary piston gas turbine generator set according to claim 1, characterized in that, The engine housing (418) includes: a combustion chamber cylinder block (401), an exhaust side end cover (403), and an intake side end cover (411). The exhaust side end cover (403) is installed on one side of the combustion chamber cylinder block (401), and the intake side end cover (411) is installed on the other side of the combustion chamber cylinder block (401). The intake side end cover (411) has multiple air inlets (419), and the exhaust side end cover (403) has multiple exhaust outlets (420).

3. The integrated rotary piston gas turbine generator set according to claim 2, characterized in that, The engine housing (418) further includes: spark plugs (416) and fuel injectors (417). Multiple spark plugs (416) and multiple fuel injectors (417) are installed at equal intervals along the outer wall of the combustion chamber cylinder (401). The multiple spark plugs (416) and multiple fuel injectors (417) extend into the combustion chamber inside the combustion chamber cylinder (401).

4. The integrated rotary piston gas turbine generator set according to claim 3, characterized in that, The rotary piston engine (4) also includes: a gear shaft (406), a key (407) and a large gear ring (412). The gear shaft (406) is connected and fixed to the blade rotor body (405) via the key (407). The large gear ring (412) is installed inside the intake side end cover (411) and meshes with the gear shaft (406).

5. The integrated rotary piston gas turbine generator set according to claim 3, characterized in that, The engine housing (418) further includes: a spring radial seal (402), a plurality of spring radial seals (402) are installed at equal intervals along the inner wall of the combustion chamber cylinder (401), and at least one spark plug (416) and at least one fuel injector (417) are provided between any two adjacent spring radial seals (402).

6. The integrated rotary piston gas turbine generator set according to claim 1, characterized in that, The rotary piston engine (4) further includes an exhaust side cover (409), which is sleeved on the eccentric main shaft (404) and installed on the exhaust side end cover (403).

7. The integrated rotary piston gas turbine generator set according to claim 1, characterized in that, The integrated rotary piston gas turbine generator set has a petal-shaped end face of the blade rotor body (405), with each petal being a smoothly transitioning arc shape that protrudes outward; the number of petals is 2 to 9.

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