阅读说明：本技术 发电型超高速推力矢量喷气发动机 (Power generation type ultrahigh-speed thrust vector jet engine ) 是由 林立 夏建国 于 2020-12-03 设计创作，主要内容包括：本发明一种发电型超高速推力矢量喷气发动机,它不需要涡轮,它是利用一种小型高速推力矢量喷气发动机来带动涡扇、发电机和压气机转动的,现在的涡轮喷气发动机,因为涡轮和轴制造需要大量的高性能的耐高温材料,这些材料贵如金,所以生产制造涡轮喷气发动机,它结构复杂,技术难度高,造成了加工难、制造难、维修难,是个世界性的难题,而本发明就解决了这个世界性的难题,它比现在的涡轮喷气发动机结构更简单、易加工、易制造、易维修、成本低,有发电机结构,不需另配发电机,节省了空间和成本,用电脑控制燃烧室内的温度和压气机的增压比,它能实现低噪音、低油耗、高效率、高可靠性、运转性能良好的发电型超高速推力矢量喷气发动机。(The invention relates to a power generation type super-high-speed thrust vector jet engine, which does not need a turbine, and utilizes a small-sized high-speed thrust vector jet engine to drive a turbofan, a generator and a gas compressor to rotate, the traditional turbojet engine has a complex structure and high technical difficulty because the turbine and a shaft are manufactured by a large amount of high-performance high-temperature-resistant materials which are expensive such as gold, so the turbojet engine is manufactured and manufactured, and has the worldwide problems of difficult processing, difficult manufacturing and maintenance, and the invention solves the worldwide problems The power generation type ultrahigh-speed thrust vector jet engine has low oil consumption, high efficiency, high reliability and good operation performance.)

1. A power generation type ultra-high-speed thrust vector jet engine comprises a shell (1), an adjustable air inlet (2), an outer turbofan (3), a force bearing frame (4), a small-sized high-speed thrust vector jet engine (5), an inner turbofan (6), a generator (7), a turbofan (8), an outer channel (9), an inner channel (10), a gas compressor (11), a swirler (12), a movable joint (13), an electric brush (14), a hollow shaft (15), a bearing (16), a high-pressure oil pipe (17), an oxygen supply and oil supply pipe (18), a boosting nozzle (19), a combustion chamber (20), a vector spray pipe (21), a rotator (22), an adjustable nozzle (23), a high-pressure oil pipe (24), a cable (25), a spark plug (26), an oil injector (27), a combustion chamber (28), a vector nozzle (29), a stator (30), a rotor (31), The small-sized high-speed thrust vector jet engine (5) is formed by combining an inner turbofan (6), a hollow shaft (15), a high-pressure oil pipe (24), a cable (25), a spark plug (26), an oil injector (27), a combustion chamber (28) and a vector nozzle (29) into a whole, and mainly used for driving the outer turbofan (3), the inner turbofan (6), a generator (7) and a compressor (11) to rotate, wherein the generator (7) is formed by a stator (30) and a rotor (31), the hollow shaft (15) is used for conveying fuel oil, the stator (30) is arranged on a shell of an outer channel (9), the rotor (31) is arranged on the turbofan (8), the stator (30) is matched with the rotor (31), and the cable (25) and the oil pipe (24) are hidden in a bearing frame (4), the resistance of the air inlet (2) can be reduced, the cable (25) and the oil pipe (24) are hidden in the blades of the inner turbofan (6), the resistance of air can be reduced, the appearance is attractive, two rectangular arc-shaped grooves are formed in the outer circle side surface of the inner turbofan (6) inwards and are used for mounting the small high-speed thrust vector jet engine (5), the engine (5) is designed to be an air cooling system, the power and the rotating speed of the engine (5) are not limited, the engine can be designed and manufactured according to requirements, the vector nozzle (29) of the engine (5) exhausts air towards the outer channel (9), the air entering the outer channel (9) dissipates heat of the engine (5), the generator (7), the compressor (11), the combustion chamber (20) and the vector jet pipe (21), the engine (5) is designed to be a square arc-shaped module, and the installation is facilitated, Dismantlement and maintenance, characterized by: the front part of a combustion chamber (20) of the power generation type ultra-high-speed thrust vector jet engine is provided with an adjustable air inlet (2), an outer turbofan (3), a bearing frame (4), a small-sized high-speed thrust vector jet engine (5), an inner turbofan (6), a power generator (7), a turbofan (8), an outer bypass (9), an inner bypass (10), a gas compressor (11), a swirler (12), a movable joint (13), an electric brush (14), a hollow shaft (15), a bearing (16), a high-pressure oil pipe (17), an oxygen supply and oil supply pipe (18) and a thrust augmentation nozzle (19); the rear part of the combustion chamber (20) is provided with a vector spray pipe (21), a rotator (22) and an adjustable nozzle (23) in a split charging way, when in starting, an oil injector (27) in a combustion chamber (28) of the small high-speed thrust vector jet engine (5) can automatically spray and burn mixed gas, a spark plug (26) can automatically ignite and explode, the generated high-temperature and high-pressure gas is discharged from the vector nozzle (29), so that reaction thrust is generated to push an inner turbofan (6) to rotate, the inner turbofan (6) rotates to drive a hollow shaft (15) to rotate, the hollow shaft (15) rotates to drive an outer turbofan (3) and a generator (7) to rotate together with a gas compressor (11) at high speed to convey air to the combustion chamber (20), at the moment, an afterburning nozzle (19) in the combustion chamber (20) can automatically spray and burn the mixed gas, the spark plug can automatically ignite and explode, and the generated high-temperature and high-pressure gas is discharged from the vector spray, thereby generating reaction thrust to the engine and pushing the airplane or missile to fly forwards at ultrahigh sonic speed.

Technical Field

The invention relates to a power generation type ultrahigh-speed thrust vector jet engine, which is a power generation type ultrahigh-speed thrust vector jet engine without a turbine structure and utilizes a small-sized high-speed thrust vector jet engine to drive a turbofan, a generator and a gas compressor to rotate.

Background

The jet engines on the market at present do not have a structure with a generator, all the jet engines are jet engines with a turbine structure, and the turbine and the shaft are manufactured by a large amount of high-temperature-resistant materials which are expensive such as gold, so that the turbine jet engines are manufactured, have complex structures and high technical difficulty, and cause difficult processing, manufacturing and maintenance, thereby being a worldwide problem. The existing turbojet engine is an oil slot, the turbine is pushed to rotate by high-temperature and high-pressure gas generated by explosion of mixed gas in a combustion chamber, the turbine rotates to drive a shaft, a fan and a gas compressor to rotate together, the turbine generates resistance, noise and partial energy for discharging the high-temperature gas, and the turbojet engine is low in efficiency, high in oil consumption, low in thrust, large in noise, large in size, difficult to machine, manufacture, maintain and high in cost. Because the high-temperature turbine, the air compressor and the fan are arranged on the same shaft, the gas temperature in the combustion chamber and the pressure ratio of the air compressor cannot be regulated, and the heat efficiency and the propulsion efficiency of the turbojet engine cannot be improved. In order to improve the thermal efficiency and the propulsion efficiency of the jet engine, resistance and noise reduction need to be removed, and the resistance and noise reduction can only be realized by removing a turbine and a shaft behind a combustion chamber of the jet engine, so that the gas temperature in the combustion chamber and the pressure ratio of a gas compressor can be regulated and controlled, the thermal efficiency and the propulsion efficiency can be improved, the structure of a generator can be realized, and the structure is simple, easy to process, manufacture and maintain, small in size, light in weight and low in cost. At present, fossil energy is gradually exhausted, energy is short, oil price is high, only great innovation is made, and the novel machine is invented, so that energy is saved, efficiency is improved, and natural environment is protected. Through years of research, the invention provides a power generation type ultrahigh-speed thrust vector jet engine which does not need an additional generator, saves space and cost, completely changes the structure of the prior turbine jet engine, is a power generation type non-turbine structure and utilizes a small-sized high-speed thrust vector jet engine to drive a turbofan, a generator and a gas compressor to rotate. The small high-speed thrust vector jet engine is formed by combining an inner turbofan, a hollow shaft, a high-pressure oil pipe, a cable, a spark plug, an oil sprayer, a combustion chamber and a vector nozzle into a whole, is arranged in an air inlet shell of the power generation type ultrahigh-speed thrust vector jet engine and effectively combines the turbofan, a generator and a gas compressor, is customized, is a seamless combination, is an unexpected technical effect, can realize the regulation and control of the gas temperature in the combustion chamber and the pressurization ratio of the gas compressor, is advanced compared with the conventional turbine jet engine, can generate power, has simpler and more scientific structure, higher thermal efficiency and propulsion efficiency, removes resistance, reduces noise, has small volume, light weight, easy processing, easy manufacture, easy maintenance, low cost and better operation performance, and solves the worldwide problem. The power generation type superhigh speed thrust vector jet engine includes casing, adjustable air inlet, outer turbofan, bearing frame, small high speed thrust vector jet engine, inner turbofan, power generator, turbofan, outer duct, inner duct, gas compressor, swirler, union, brush, hollow shaft, bearing, high pressure oil pipe, oxygen supply and oil supply pipe, thrust augmentation nozzle, combustion chamber, vector jet pipe, rotator, adjustable nozzle, high pressure oil pipe, cable, spark plug, oil sprayer, combustion chamber, vector nozzle, stator, rotor, coil, charger, accumulator, computer, instrument and electronic switch The engine has the advantages of easy maintenance and low cost, can realize the power generation type ultra-high-speed thrust vector jet engine with low noise, low oil consumption, high efficiency, high reliability and good operation performance, is digitally controlled by a computer, can regulate and control the gas temperature in a combustion chamber and the pressure ratio of a gas compressor, can start the engine manually or automatically, has huge commercial development value, brings huge social benefit and economic benefit, and makes huge contribution to saving energy, improving efficiency and protecting natural environment for human beings.

Disclosure of Invention

The invention aims to provide a power generation type ultrahigh-speed thrust vector jet engine which has the advantages of simple structure, easiness in processing, easiness in manufacturing and maintenance, low oil consumption, high efficiency, high thrust, high speed, low noise, small volume, light weight, low cost, easiness in operation and capability of generating power. The power generation type superhigh speed thrust vector jet engine includes casing, adjustable air inlet, outer turbofan, bearing frame, small high speed thrust vector jet engine, inner turbofan, power generator, turbofan, outer duct, inner duct, compressor, swirler, union, brush, hollow shaft, bearing, high pressure oil pipe, oxygen supply and oil supply pipe, thrust boosting nozzle, combustor, vector jet pipe, rotator, adjustable nozzle, high pressure oil pipe, cable, spark plug, oil sprayer, combustor, vector nozzle, stator, rotor, coil, charger, accumulator, computer, instrument and electronic switch The engine has the advantages of low cost, better operating performance, digital control by a computer, realization of regulation and control of the gas temperature in the combustion chamber and the pressure ratio of the gas compressor, manual or full-automatic starting, and realization of the power generation type ultra-high-speed thrust vector jet engine with low oil consumption, low noise, high efficiency, high reliability and good operation performance.

The technical scheme of the invention is realized as follows: a power generation type ultrahigh-speed thrust vector jet engine comprises a shell, an adjustable air inlet, an outer turbofan, a force bearing frame, a small-sized high-speed thrust vector jet engine, an inner turbofan, a generator, a turbofan, an outer duct, an inner duct, a gas compressor, a swirler, a movable joint, an electric brush, a hollow shaft, a bearing, a high-pressure oil pipe, an oxygen supply and oil supply pipe, a boosting nozzle, a combustion chamber, a vector spray pipe, a rotator, an adjustable nozzle, a high-pressure oil pipe, a cable conductor, a spark plug, an oil injector, a combustion chamber, a vector nozzle, a stator, a rotor, a coil, a charger, a storage battery, a computer, an instrument and an electronic switch The generator and the compressor rotate, the generator is composed of a stator and a rotor, a hollow shaft is used for conveying fuel oil, the stator is arranged on a shell of an outer channel, the rotor is arranged on a turbofan, the stator and the rotor are matched, a cable wire and an oil pipe are hidden in a bearing frame, the resistance of an air inlet is reduced, the cable wire and the oil pipe are hidden in blades of the inner turbofan, the resistance of air is reduced, the appearance is attractive, two rectangular arc-shaped grooves are inwards formed in the outer circle side surface of the inner turbofan and are used for installing a small high-speed thrust vector jet engine, the engine is designed into an air cooling system, the power and the rotating speed of the engine are not limited, the engine can be designed, produced and manufactured according to requirements, a vector nozzle of the engine exhausts air towards the outer channel, and the air entering the outer channel dissipates heat of the engine, the generator, the compressor, a combustion chamber and the shell of the vector jet pipe, the engine is designed into a rectangular arc module, which is beneficial to installation, disassembly and maintenance, and the front part of a combustion chamber of the power generation type ultrahigh-speed thrust vector jet engine is provided with an adjustable air inlet, an outer turbofan, a force bearing frame, a small-sized high-speed thrust vector jet engine, an inner turbofan, a power generator, a turbofan, an outer channel, an inner channel, a gas compressor, a swirler, a movable joint, an electric brush, a hollow shaft, a bearing, a high-pressure oil pipe, an oxygen supply and oil supply pipe and a force application nozzle; the rear part of the combustion chamber is provided with a vector spray pipe, a rotator and an adjustable nozzle, when the engine is started, an oil sprayer in the combustion chamber of the small high-speed thrust vector jet engine can automatically spray and combust mixed gas, a spark plug can automatically ignite and burst, the generated high-temperature high-pressure gas is discharged from the vector nozzle, so that reaction thrust is generated, the inner turbofan is pushed to rotate, the inner turbofan rotates to drive the hollow shaft to rotate, the hollow shaft rotates to drive the outer turbofan, the generator and the air compressor to rotate together at high speed to convey air to the combustion chamber, at the moment, the thrust nozzle in the combustion chamber can automatically spray and combust the mixed gas, the spark plug can automatically ignite and burst, the generated high-temperature high-pressure gas is discharged from the vector spray pipe through the adjustable nozzle, so that the reaction thrust to the engine is generated, and an airplane or.

Drawings

FIG. 1 is a schematic view of a super high speed thrust vector jet engine of the power generation type of the present invention;

FIG. 2 is a schematic side view of the structure of FIG. 1;

FIG. 3 is a side view schematic of the structure of FIG. 2;

FIG. 4 is a side view schematic of the structure of FIG. 1;

the specific implementation mode is as follows:

as shown in figures 1, 2, 3 and 4, the power generation type ultra-high speed thrust vector jet engine comprises a shell 1, an adjustable air inlet 2, an outer turbofan 3, a force bearing frame 4, a small high speed thrust vector jet engine 5, an inner turbofan 6, a generator 7, a turbofan 8, an outer bypass 9, an inner bypass 10, a compressor 11, a swirler 12, a movable joint 13, an electric brush 14, a hollow shaft 15, a bearing 16, a high pressure oil pipe 17, an oxygen supply and oil supply pipe 18, an afterburning nozzle 19, a combustion chamber 20, a vector spray pipe 21, a rotator 22, an adjustable nozzle 23, a high pressure oil pipe 24, a cable 25, a spark plug 26, an oil injector 27, a combustion chamber 28, a vector spray nozzle 29, a stator 30, a rotor 31, a coil, a charger, a storage battery, a computer, instruments and electronic switches, wherein the small high speed thrust vector jet engine 5 comprises the inner turbofan 6, the hollow shaft 15, the high pressure oil pipe, The electric cable 25, the spark plug 26, the fuel injector 27, the combustion chamber 28 and the vector nozzle 29 are combined into a whole, the electric cable is mainly used for driving the outer turbofan 3, the inner turbofan 6, the generator 7 and the compressor 11 to rotate, the generator 7 is composed of a stator 30 and a rotor 31, a hollow shaft I5 is used for conveying fuel oil, the stator 30 is arranged on the shell of the outer channel 9, the rotor 31 is arranged on the turbofan 8, the stator 30 and the rotor 31 are matched, the electric cable 25 and the oil pipe 24 are hidden in a bearing frame, the resistance of the air inlet 2 can be reduced, the electric cable 25 and the oil pipe 24 are hidden in blades of the inner turbofan 6, the resistance of air can be reduced, the appearance is attractive, two rectangular arc grooves are inwards formed on the outer side surface of the inner turbofan 6 and are used for installing the small high-speed thrust vector jet engine 5, the engine 5 is designed as an air cooling system, and the power of the engine 5 is large or small-size, The speed of the rotating speed is not limited, the design, the production and the manufacture can be carried out according to the requirement, a vector nozzle 29 of the engine 5 exhausts towards the outer duct 9, the air entering the outer duct 9 is used for radiating the shell of the engine 5, the generator 7, the compressor 11, the combustion chamber 20 and the vector spray pipe 21, the engine 5 is designed into a rectangular arc module which is beneficial to installation, disassembly and maintenance, the front part of the combustion chamber 20 of the power generation type ultra-high speed thrust vector jet engine is provided with an adjustable air inlet 2, an outer turbofan 3, a force bearing frame 4, a small-sized high speed thrust vector jet engine 5, an inner turbofan 6, a generator 7, a turbofan 8, the outer duct 9, an inner duct 10, the compressor 11, a swirler 12, a movable joint 13, an electric brush 14, a hollow shaft 15, a bearing 16, a high-pressure oil pipe 17, an oxygen supply and stressing nozzle 18 and a stress application nozzle 19; the rear portion of the combustion chamber 20 is separately provided with a vectoring nozzle 21, a rotator 22 and an adjustable nozzle 23, and at the time of starting, the fuel injector 27 in the combustion chamber 28 of the small high-speed thrust vector jet engine 5 automatically injects and burns the mixed gas, the spark plug 26 automatically ignites and explodes, the generated high-temperature and high-pressure fuel gas is discharged from the vector nozzle 29, thereby generating reaction thrust to push the inner turbofan 6 to rotate, the inner turbofan 6 rotates to drive the hollow shaft 15 to rotate, the hollow shaft 15 rotates to drive the outer turbofan 3, the generator 7 and the compressor 11 rotate together at high speed to convey air to the combustion chamber 20, at this time, the boosting nozzle 19 in the combustion chamber 20 automatically sprays and burns the mixed gas, the spark plug automatically ignites and explodes, the generated high-temperature and high-pressure gas is discharged from the vector spray pipe 21 through the adjustable nozzle 23, thereby generating reaction thrust to the engine and pushing the airplane or missile to fly forwards at ultrahigh sonic speed.