阅读说明：本技术 梭镖型垂直起降高超音速飞机 (Shuttle dart type hypersonic aircraft capable of vertically taking off and landing ) 是由 林立 夏建国 于 2020-12-03 设计创作，主要内容包括：本发明一种梭镖型垂直起降高超音速飞机,它是用二台电磁型垂直起降喷气发动机和一台发电型超高速推力矢量喷气发动机来推动飞机垂直起降或飞行的。现在飞机用的涡轮喷气发动机,结构复杂、技术难度高,因涡轮制造需要大量的高性能的耐高温材料,这些材料贵如金,所以造成了加工难、制造难、维修难,是个世界性的难题,而本发明的飞机和喷气发动机,它体积小、重量轻、易加工、易制造、易维修,解决了这个世界性的难题,它比现在的喷气发动机结构更简单,去掉了涡轮和轴,去掉了阻力、降低了噪音,又有发电功能,它能控制燃烧室内的温度和压气机的增压比,提高了热效率和推进效率,它能实现低油耗、高效率、高可靠性、运转性能良好的梭镖型垂直起降高超音速飞机。(The invention relates to a dart type vertical take-off and landing hypersonic airplane, which uses two electromagnetic vertical take-off and landing jet engines and a power generation type hypersonic thrust vector jet engine to push the airplane to take off and land or fly vertically. The present invention relates to a turbojet engine for airplane, which is characterized by that its structure is complex, technical difficulty is high, and because the manufacture of turbine requires lots of high-temp. resistant material with high performance, and these materials are noble, such as gold, so that it is difficult to make, and repair, and is a worldwide problem.)

1. The utility model provides a dart type VTOL hypersonic aircraft, it includes organism (1), a chassis, preceding wing (2), perpendicular wing (3), back wing (4), cockpit (5), electromagnetic type VTOL jet engine (6), electricity generation type hypervelocity thrust vector jet engine (7), adjustable air inlet (8), vector spray tube (9), adjustable spout (10), preceding landing gear wheel, back landing gear wheel (11), high-pressure fuel pipe, high-pressure gas pipe, the cable conductor, the battery, the charger, the signal lamp, the radar, a computer, the display screen, the control rod, instrument and electronic switch, design into the dart type with the aircraft, the organism designs into stealthy streamlined, the engine designs into no turbine, the electricity generation type, make the aircraft more advanced, characterized by: a sharp nose with a round tip is arranged right ahead a machine body (1), a front wing (2) and a rear wing (4) are arranged on the periphery of a chassis of the machine body (1), a vertical wing (3) is arranged above the chassis of the machine body (1), the rear wing (4) can be folded upwards or folded on the front wing (2), air resistance can be reduced when the airplane vertically takes off, space can be saved when the airplane stops on the ground, a front landing gear wheel is arranged at the front part below the chassis of the machine body (1), two rear landing gear wheels (11) are arranged at the rear part, an electromagnetic vertical take-off and landing jet engine (6) or an electromagnetic turbofan is respectively arranged at two sides of a cockpit (5) of the machine body (1), a power generation type ultrahigh-speed thrust vector take-off jet engine (7) is arranged at the rear part of the chassis of the machine body (1), when the engine is vertical, a computer is started firstly, cover plates at two ends of the engine are opened, and the, the engine (7) will start, generate electricity to supply two electromagnetic vertical take-off and landing jet engines (6), at this time, the thrust augmentation nozzles in each combustion chamber of the two electromagnetic vertical take-off and landing jet engines (6) and the electricity generation type super-high speed thrust vector jet engine (7) will automatically spray and burn the mixed gas, the spark plug will automatically ignite and burst, the generated high-temperature and high-pressure gas is discharged from the adjustable nozzle (1.3) and the vector spray pipe (9) downwards through the adjustable nozzle (10), thereby generating the reaction thrust to the engine, pushing the airplane to ascend, controlling the air flow sprayed by each jet engine by the computer, ensuring the airplane to ascend in balance or suspend in the air immovable, when the airplane ascends to a certain safe height, retracting the front and rear landing frame wheels (11), closing the two electromagnetic vertical take-off and landing jet engines (6), closing the cover plates at both ends of the engine, the plane is formed by the body (1) and the chassis, the air resistance is reduced, the rear wing (4) is unfolded and locked, the airplane flies at hypersonic speed or flies on a rotary disk in the air, if the airplane flies to the space, only a rocket is needed to be arranged behind a vector spray pipe (9) and an adjustable nozzle (10) of a shuttle dart type hypersonic-speed airplane which vertically takes off and lands, and then a power generation type ultrahigh-speed thrust vector jet engine (7) is used for providing power and air for the rocket, because the fuel oil of the airplane is limited, the airplane is sent to the near space by a rocket, the rocket is automatically separated and falls off, then the airplane continuously rushes into the space by the power of the airplane, when the airplane flies in the space and needs to return, the airplane rushes into the atmosphere by the power of the airplane, when the airplane lands, cover plates at two ends of the engine are firstly opened, then two electromagnetic type vertical take-off jet engines (6) are started, and then the vector spray pipe (9) of the power generation type thrust vector jet engine The jet nozzles (10) are adjusted to discharge, so that reaction thrust on the engines is generated, the airplane is pushed to slowly descend, the air flow sprayed by each jet engine is controlled by a computer, the airplane is ensured to safely land vertically or land on a runway in a sliding way, and the hypersonic flight of the unmanned or manned airplane can be realized.

2. An electromagnetic vertical take-off and landing jet engine comprises a shell (1), a stator (2), a rotor (3), a turbofan (4), a shaft (5), a gas compressor (6), a swirler (7), a high-pressure oil pipe (8), a high-pressure air pipe (9), a thrust augmentation nozzle (10), a combustion chamber (11), an air inlet (12) and an air outlet (13), wherein the electromagnetism consists of an armature and a permanent magnet and is used for pushing the permanent magnet to rotate by means of a moving magnetic field generated by current, when the engine is started, the moving magnetic field generated by the current in the stator (2) pushes the rotor (3) to rotate, the rotor (3) rotates to drive the turbofan (4) and the shaft (5) to rotate, the shaft (5) rotates to drive the gas compressor (6) to rotate at high speed to convey air to the combustion chamber (11), the thrust augmentation nozzle (10) in the combustion chamber (11) can automatically spray and burn mixed gas, and a spark plug can, the generated high-temperature and high-pressure fuel gas is discharged from the exhaust port (13), so that the reaction thrust to the engine is generated, and the airplane is pushed to ascend.

3. 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 sprayer (27), a combustion chamber (28) and a vector nozzle (29) into a whole and is used for driving the outer turbofan (3), the inner turbofan (6), a generator (7) and a gas compressor (11) to rotate, when the small-sized high-speed thrust vector jet engine is started, the oil sprayer (27) in the combustion chamber (28) of the small-sized high-speed thrust vector jet engine (5) can automatically spray and burn mixed gas, the spark plug (26) can automatically ignite and burst, the generated high-temperature high-pressure gas is discharged from the vector nozzle (29), so that reaction thrust is generated 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) to rotate together at a high speed to convey air to the combustion chamber (20), at the moment, the boosting nozzle (19) in the combustion chamber (20) can automatically spray and burn mixed gas, the spark plug can automatically ignite and explode, and the generated high-temperature and high-pressure fuel gas is discharged from the vectoring nozzle (21) through the adjustable nozzle (23), so that reaction thrust on the engine is generated, and the airplane is pushed to fly at a high supersonic speed.

Technical Field

The invention relates to a dart type vertical take-off and landing hypersonic aircraft, an electromagnetic type vertical take-off and landing jet engine and a power generation type ultrahigh-speed thrust vector jet engine.

Background

Jet engines for supersonic aircraft in the market at present are all jet engines with turbine structures without structures with generators, and also need to be additionally provided with generators for supplying power, and also occupy another space. The prior turbojet engine is an oil tiger, the turbine is pushed to rotate by high-temperature and high-pressure gas generated by explosion of fuel gas mixture in a combustion chamber, the turbine rotates to drive a shaft, a fan and a gas compressor to rotate together, the turbine generates resistance and noise for discharging the high-temperature gas and also consumes part of energy, so that the turbojet engine has high oil consumption, low efficiency, low thrust, high noise, large volume, difficult processing, manufacture, maintenance and high cost, and the high-temperature turbine, the gas compressor and the fan are arranged on the same shaft, so that the temperature of the gas in the combustion chamber and the pressure ratio of the gas compressor cannot be regulated and controlled, the thermal efficiency and the propulsion efficiency of the turbojet engine cannot be improved, and the thermal efficiency and the propulsion efficiency of the turbojet engine need to be improved, the resistance and the noise are reduced, and the efficiency is improved only by removing the turbine and the shaft behind the combustion chamber of the turbojet engine, the novel aircraft and the novel aircraft are scientific, can achieve resistance removal and noise reduction, can achieve regulation and control of gas temperature in a combustion chamber and the pressure ratio of a gas compressor, can achieve improvement of heat efficiency and propulsion efficiency, can achieve the structure of a generator, can achieve the purposes that the aircraft and the engine are simple in structure, easy to machine, easy to manufacture and easy to maintain, and can achieve the purposes of low oil consumption, high efficiency, large thrust, high speed, low noise and low cost. Through years of research, the dart type vertical take-off and landing hypersonic aircraft, the electromagnetic type vertical take-off and landing jet engine and the power generation type ultrahigh-speed thrust vector jet engine are invented, the structures of the existing aircraft and engines are completely changed, a turbine and a shaft are removed from the jet engine, the dart type vertical take-off and landing hypersonic jet engine is simpler in structure, lower in oil consumption, higher in efficiency, higher in thrust, higher in speed, lower in noise, smaller in volume, lighter in weight, lower in cost, easy to machine, manufacture and maintain, can generate power, the temperature of gas in a combustion chamber and the pressure ratio of a gas compressor can be controlled by a computer, so that the thermal efficiency and the propulsion efficiency are higher, the operation performance is better, and the worldwide problem is solved. A dart type vertical take-off and landing hypersonic aircraft is produced and manufactured, which comprises a body, a chassis, a front wing, a vertical wing, a rear wing, a cockpit, an electromagnetic vertical take-off and landing jet engine, a power generation type hypersonic thrust vector jet engine, an adjustable air inlet, a vector spray pipe, an adjustable nozzle, a front landing gear wheel, a rear landing gear wheel, a high-pressure oil pipe, a high-pressure air pipe and a cable, the invention relates to a storage battery, a charger, a signal lamp, a radar, a computer, a display screen, an operating rod, an instrument and an electronic switch, a novel dart type vertical take-off and landing hypersonic aircraft, an electromagnetic type vertical take-off and landing jet engine and a power generation type ultrahigh-speed thrust vector jet engine, which inevitably brings a revolution to the manufacturing industry of the aircraft and the engine and can realize the dart type vertical take-off and landing hypersonic aircraft with low oil consumption, low pollution, low emission, low noise, high efficiency, high reliability and good flight performance. The aircraft is designed into a dart type, the aircraft body is designed into a stealthy streamline shape, the aircraft has high speed, small resistance, large lift force, large load capacity and long flight time, can take off and land vertically or slide, can suspend in the air and fly immovably or cruise, can realize unmanned or manned full-automatic piloting and operating of the aircraft, has huge commercial development value, must bring huge social and economic benefits for human, and must make great contribution to the aviation industry of human.

Disclosure of Invention

The invention aims to provide a dart type hypersonic airplane capable of vertically taking off and landing, which has the advantages of simple structure, low oil consumption, high efficiency, large thrust, high speed, easiness in processing, manufacture and maintenance, small noise, small volume, light weight, low cost and easiness in operation. The dart type vertical take-off and landing hypersonic aircraft comprises a machine body, a chassis, a front wing, a vertical wing, a rear wing, a cockpit, an electromagnetic vertical take-off and landing jet engine, a power generation type ultrahigh-speed thrust vector jet engine, an adjustable air inlet, a vector spray pipe, an adjustable nozzle, a front landing gear wheel, a rear landing gear wheel, a high-pressure oil pipe, a high-pressure air pipe, a cable wire, a storage battery, a charger, a signal lamp, a radar, a computer, a display screen, a control rod, an instrument and an electronic switch, has simpler structure, lower oil consumption, higher efficiency, higher thrust, higher speed, lower noise, lower cost, easy processing, easy manufacture, easy maintenance and power generation compared with the prior vertical take-off and landing hypersonic aircraft, can regulate the gas temperature in a combustion chamber and the pressurization ratio of a gas compressor by the computer, can be piloted by no person or someone, the dart type vertical take-off and landing hypersonic aircraft can realize low oil consumption, low pollution, low emission, low noise, high efficiency, high reliability and good flight performance.

The technical scheme of the invention is realized as follows: a dart type vertical take-off and landing hypersonic aircraft comprises a aircraft body, a chassis, a front wing, a vertical wing, a rear wing, a cockpit, an electromagnetic vertical take-off and landing jet engine, a power generation type ultrahigh-speed thrust vector jet engine, an adjustable air inlet, a vector spray pipe, an adjustable nozzle, a front landing gear wheel, a rear landing gear wheel, a high-pressure oil pipe, a high-pressure air pipe, a cable wire, a storage battery, a charger, a signal lamp, a radar, a computer, a display screen, a control lever, an instrument and an electronic switch, wherein the vector spray pipe is used for regulating and controlling the direction, the aircraft body is designed into a dart type, the aircraft body is designed into a hidden streamline type, the engine is designed into a non-turbine type and a power generation type, the aircraft is more advanced, a sharp nose with a round tip is arranged right in front of the aircraft body, the front wing and the rear wing are arranged on the periphery of the, the back wing can be folded upwards or folded on the front wing, the air resistance can be reduced when the airplane vertically takes off, the space can be saved when the airplane stops on the ground, a front landing gear wheel is arranged at the front part of the lower part of a body chassis, two back landing gear wheels are arranged at the back part of the lower part of the body chassis, an electromagnetic type vertical take-off and landing jet engine or an electromagnetic type turbofan is respectively arranged at two sides of a body cockpit, a power generation type super-high speed thrust vector jet engine is arranged at the back part of the body chassis, a computer is started firstly during vertical take-off, cover plates at two ends of the engine are opened, the power generation type super-high speed thrust vector jet engine is started simultaneously, the engine can be started and generate power to be used by the two electromagnetic type vertical take-off and landing jet engines, at the moment, the boosting nozzles in each combustion chamber of the two electromagnetic type vertical take-off and landing jet engines and the power, the spark plug will automatically ignite and burst, the generated high-temperature and high-pressure gas is discharged from the adjustable nozzle and the vector jet pipe downwards through the adjustable nozzle, thereby generating reaction thrust to the engine, pushing the airplane to ascend, controlling the air flow sprayed by each jet engine by a computer, ensuring the balanced ascent or suspension of the airplane, when the airplane ascends to a certain safe height, retracting the front and rear landing gear wheels, closing the two electromagnetic vertical take-off and landing jet engines, closing the cover plates at the two ends of the engines, enabling the body and the chassis to form a plane, reducing air resistance, unfolding the rear wing and locking, the airplane flies forwards or revolves at the hypersonic speed in the air, if the airplane flies to the space, only a section of thrust needs to be arranged behind the vector jet pipe of the shuttle dart type vertical take-off and landing hypersonic airplane and the adjustable nozzle, and then the electricity generation type ultrahigh-speed vector jet engine is used for providing electricity and air for the rocket, because the fuel oil of the airplane is limited, a rocket is used for sending the airplane into a near space, the rocket is automatically separated from the airplane and falls off, then the airplane continuously rushes into the space by using the self power, when the airplane needs to return after flying in the space for a period of time, the airplane rushes into the atmosphere by using the self power, when the airplane lands, the cover plates at two ends of the engine are firstly opened, then two electromagnetic vertical take-off and landing jet engines are started, and then the vector jet pipe of the power generation type ultrahigh-speed thrust vector jet engine is regulated and controlled to downwards discharge through the adjustable nozzle, so that the reaction thrust to the engine is generated, the airplane is pushed to slowly descend, the air flow sprayed by each jet engine is controlled by a computer, the airplane is ensured to safely vertically land or land on a runway in a sliding way, and the airplane can.

The invention relates to an electromagnetic vertical take-off and landing jet engine which comprises a shell, a stator, a rotor, a turbofan, a shaft, a gas compressor, a swirler, a high-pressure oil pipe, a high-pressure air pipe, a thrust augmentation nozzle, a combustion chamber, an air inlet and an air outlet.

The invention relates to a power generation type ultra-high-speed thrust vector jet engine, which 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 power 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 thrust augmentation nozzle, a combustion chamber, a vector spray pipe, a rotator, 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, wherein the small-sized high-speed thrust vector jet engine is formed by combining the inner turbofan, the hollow shaft, the high-pressure oil pipe, a cable, a spark plug, a fuel injector, the combustion chamber and the vector nozzle into a whole and is mainly used for driving the outer turbofan, the inner turbofan, when the small-sized high-speed thrust vector jet engine is started, an oil sprayer in a combustion chamber of the small-sized high-speed thrust vector jet engine can automatically spray and burn mixed gas, a spark plug can automatically ignite and explode, the generated high-temperature high-pressure gas is discharged from a vector nozzle, so that reaction thrust is generated, the inner turbofan is pushed to rotate, the inner turbofan rotates to drive a hollow shaft to rotate, the hollow shaft rotates to drive an outer turbofan, a generator and a gas compressor to rotate together at a high speed to convey air to the combustion chamber, at the moment, an afterburner nozzle in the combustion chamber can automatically spray and burn the mixed gas, the spark plug can automatically ignite and explode, and the generated high-temperature high-pressure gas is discharged from a nozzle with the adjustable vector nozzle diameter, so that the.

Drawings

FIG. 1 is a schematic illustration of a dart-type VTOL hypersonic aircraft of the present invention;

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

FIG. 3 is a schematic diagram of an electromagnetic VTOL jet engine of the present invention;

FIG. 4 is a side view schematic of the structure of FIG. 3;

FIG. 5 is a schematic view of a super high speed thrust vector jet engine of the power generation type of the present invention;

FIG. 6 is a side view schematic of the structure of FIG. 5;

FIG. 7 is a side view schematic of the structure of FIG. 6;

FIG. 8 is a side view schematic of the structure of FIG. 5;

the specific implementation mode is as follows:

as shown in fig. 1 and 2, a dart type vertical take-off and landing hypersonic aircraft comprises a body 1, a chassis, a front wing 2, a vertical wing 3, a rear wing 4, a cockpit 5, an electromagnetic vertical take-off and landing jet engine 6, a power generation type ultrahigh-speed thrust vectoring jet engine 7, an adjustable air inlet 8, a vectoring nozzle 9, an adjustable nozzle 10, a front landing gear wheel, a rear landing gear wheel 11, a high-pressure oil pipe, a high-pressure air pipe, a cable, a storage battery, a charger, a signal lamp, a radar, a computer, a display screen, a control lever, an instrument and an electronic switch, wherein the vectoring nozzle 10 is used for regulating and controlling the direction, the aircraft is designed into a dart type, the body is designed into a stealthy streamline type, the engine is designed into a non-turbine type and a power generation type, the aircraft is more advanced, a sharp nose with a round point is arranged right in front of the body 1, the front wing 2 and, a door and a window are arranged on a machine body 1, a vertical wing 3 is arranged at the rear part of the machine body 1, a rear wing 4 can be folded upwards or folded on a front wing 2, air resistance can be reduced when the airplane vertically takes off, space can be saved when the airplane stops on the ground, a front landing gear wheel is arranged at the front part below a chassis of the machine body 1, two rear landing gear wheels 11 are arranged at the rear part, an electromagnetic vertical take-off and landing jet engine 6 or an electromagnetic turbofan is respectively arranged at two sides of a cockpit 5 of the machine body 1, a power generation type super-high-speed thrust vector jet engine 7 is arranged at the rear part of the chassis of the machine body 1, a computer is started firstly during vertical take-off, cover plates at two ends of the engine are opened, the power generation type super-speed thrust vector jet engine 7 is started at the same time, the engine 7 can be started and generate power for the two electromagnetic vertical take-off and landing jet engines 6, and each combustion chamber of the two electromagnetic vertical take-off and landing The internal boosting nozzle can automatically spray and burn mixed gas, the spark plug can automatically ignite and explode, the generated high-temperature and high-pressure fuel gas is discharged from the adjustable nozzle 13 and the vector spray pipe 9 downwards through the adjustable nozzle 10, so that the reaction thrust to the engine is generated, the airplane is pushed to ascend, the air flow sprayed by each jet engine is controlled by a computer, the balanced ascending of the airplane or the static suspension in the air is ensured, when the airplane ascends to a certain safe height, the front and rear landing frame wheels 11 are retracted, the two electromagnetic vertical lifting jet engines 6 are closed, the cover plates at the two ends of the engines are closed, the body 1 and the chassis form a plane, the air resistance is reduced, the rear wing 4 is unfolded and locked, the airplane flies forwards at high supersonic speed in the air or flies on a rotary disk, if the airplane flies to the space, only one section is needed to be arranged behind the vector spray pipe 9 and the adjustable nozzle 10 of the shuttle-type vertical lifting hypersonic airplane, the power generation type ultrahigh-speed thrust vector jet engine 7 is used for supplying power and air to the rocket, because the fuel of the airplane is limited, therefore, the airplane is sent into the near space by a rocket, the rocket is automatically separated and falls off, then the airplane continuously rushes into the space by the self power, when the airplane needs to return after flying in the space for a period of time, the airplane flies in the atmosphere by using the self power, when the airplane lands, the cover plates at the two ends of the engine are firstly opened, then the two electromagnetic vertical take-off and landing jet engines 6 are started, then the vector spray pipe 9 of the power generation type ultrahigh-speed thrust vector jet engine 7 is regulated and controlled to be discharged downwards through the adjustable nozzle 10, thus, the thrust of reaction to the engine is generated to push the airplane to slowly descend, the computer is used for controlling the airflow sprayed by each jet engine, the airplane is ensured to safely land vertically or land on a runway in a sliding way, and unmanned or manned control of the airplane for flying can be realized.

As shown in fig. 3 and 4, an electromagnetic vertical take-off and landing jet engine comprises a shell 1, a stator 2, a rotor 3, a turbofan 4, a shaft 5, a compressor 6, a swirler 7, a high-pressure oil pipe 8, a high-pressure air pipe 9, a thrust augmentation nozzle 10, a combustion chamber 11, an air inlet 12 and an air outlet 13, wherein the electromagnetism is composed of an armature and a permanent magnet and is used for pushing the permanent magnet to rotate by means of a moving magnetic field generated by current, when the engine is started, the rotor 3 is pushed to rotate by the moving magnetic field generated by the current in the stator 2, the turbofan 4 and the shaft 5 are driven to rotate by the rotation of the rotor 3, the shaft 5 drives the compressor 6 to rotate at high speed to convey air to the combustion chamber 11, the thrust augmentation nozzle 10 in the combustion chamber 11 can automatically spray and combust mixed gas, a spark plug can automatically ignite and explode, and the generated high-temperature and high-pressure gas is, pushing the airplane to ascend.

As shown in figures 5, 6, 7 and 8, 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 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 device is mainly used for driving the outer turbofan 3, the inner turbofan 6, the generator 7 and the compressor 11 to rotate, the hollow shaft 15 is used for conveying fuel oil, when the device is started, the fuel injector 27 in the combustion chamber 28 of the small-sized high-speed thrust vector jet engine 5 automatically sprays and combusts mixed gas, the spark plug 26 automatically ignites and explodes, the generated high-temperature high-pressure fuel gas is discharged from the vector nozzle 29, so that a reaction thrust force is generated 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 and the generator and the compressor 11 to rotate together at a high speed to convey air to the combustion chamber 20, at the moment, the boosting nozzle 19 in the combustion chamber 20 automatically sprays and combusts the mixed gas, the spark plug automatically ignites and explodes, the generated high-temperature high-pressure fuel, thereby generating reaction thrust to the engine and pushing the airplane to fly forwards at hypersonic speed.