CN109236494B

CN109236494B - Ultrahigh-speed thrust vector jet engine

Info

Publication number: CN109236494B
Application number: CN201811337130.9A
Authority: CN
Inventors: 夏丰
Original assignee: Individual
Current assignee: Individual
Priority date: 2018-11-01
Filing date: 2018-11-01
Publication date: 2022-09-23
Anticipated expiration: 2038-11-01
Also published as: CN109236494A

Abstract

The invention relates to a shaftless turbofan type superspeed thrust vector jet engine, which does not need a turbine and completely changes the structure of the existing jet engine, and comprises a shell, an adjustable air inlet, a ring gear, a turbofan, a force bearing frame, a gas compressor, a swirler, an oxygen supply and oil supply pipe, a thrust augmentation nozzle, a combustion chamber, a spark plug, a shaftless turbofan engine, a gear, a force transmission shaft, a vector spray pipe and an adjustable nozzle, wherein when the jet engine is started, the turbofan rotates to drive the shaft and the gas compressor to operate at high speed to convey air to the combustion chamber, the thrust augmentation nozzle in the combustion chamber can automatically spray oil, the spark plug can automatically ignite and explode, the generated high-temperature and high-pressure gas flows backwards through the shaftless turbofan engine, part of the internal energy expands in the ring rotor to drive blades to be mechanical energy, the ring rotor rotates at high speed to drive the turbofan to rotate at high speed through the force transmission shaft group, so that the continuous operation is started, then the huge gas flow is discharged from the vectoring nozzle and the adjustable nozzle to push and control the airplane and the missile to fly at ultrahigh speed.

Description

Ultrahigh-speed thrust vector jet engine

Technical Field

The invention relates to a shaftless turbofan type ultrahigh-speed thrust vector jet engine.

Background

The existing jet engines on the market are all jet engines with turbine structures, which are complex in structure, difficult to manufacture and maintain, small in thrust, large in noise, low in efficiency, high in oil consumption and high in cost, the turbine is driven to rotate by high-temperature and high-pressure gas flow generated by explosion in a combustion chamber, a shaft, a fan and a compressor are driven to work by the rotation of the turbine, a turbine disc is large in volume, occupies space in the jet engine, generates resistance, generates noise, consumes huge fossil energy, and loses a large amount of gas energy, so that the efficiency, the oil consumption, the noise and the speed of the jet engine are high, the resistance can be removed only by removing the turbine and the shaft behind the combustion chamber, the structure is simple, the volume is small, and the manufacture is easy, the efficiency, thrust and speed can be improved, and the oil consumption and noise can be reduced. At present, fossil energy is exhausted day by day, energy is short, oil price is expensive, and only a strong innovation is made, energy is saved, and the natural environment is protected. Today, I invented a novel thrust vector jet engine, which completely changed the structure of the existing jet engine, and its structure is simpler and more scientific, the thermal efficiency and the propulsion efficiency are better, the thrust vector manipulation performance is better, its efficiency is higher, the oil consumption is lower, the noise is smaller, the thrust is bigger, the speed is faster, the cost is lower, the maintenance operation is simpler, and the manufacture is easier. The production and manufacture of a shaftless turbofan type ultrahigh-speed thrust vector jet engine is characterized in that a jet engine part and a shaftless turbofan engine part are combined into a whole, and the jet engine part comprises the following components: the engine comprises a shell, an outer duct, an adjustable air inlet, a ring gear, a bearing frame, a turbofan, an air compressor, a flow applier, an oxygen supply and oil supply pipe, a boosting nozzle, a combustion chamber, a vector spray pipe, a stepping motor, a vector control rod, a universal joint, an adjustable nozzle, a spark plug, a generator, a charger, a storage battery, a starter, a computer, an electric wire, an instrument, an electronic switch and a shaftless turbofan engine part: the invention relates to a novel thrust vector jet engine, which can revolutionize the industry for manufacturing the jet engine, realize the green and environment-friendly jet engine with low oil consumption, low pollution, low emission, low noise, high efficiency, high reliability and good running performance, is digitally controlled by a computer, can be started manually or automatically, has huge commercial development value, can bring huge social efficiency and economic benefit for human beings, and can make great contribution to saving energy for human beings and protecting natural environment.

Disclosure of Invention

The invention aims to provide a novel super-high-speed thrust vector jet engine which is simple in structure, high in efficiency, low in oil consumption, large in thrust, high in speed, small in noise, small in size, low in cost, easy to manufacture, easy to operate, green and environment-friendly. The production and manufacture of a shaftless turbofan type ultrahigh-speed thrust vector jet engine is characterized in that a jet engine part and a shaftless turbofan engine part are combined into a whole, and the jet engine part comprises the following components: the device comprises a shell, an outer duct, an adjustable air inlet, a ring gear, a force bearing frame, a turbofan, an air compressor, a swirler, an oxygen supply and oil supply pipe, a boosting nozzle, a combustion chamber, a vector spray pipe, a stepping motor, a vector control rod, a universal joint, an adjustable nozzle, a spark plug, a generator, a charger, a storage battery, a starter, a computer, an electric wire, an instrument and meter, an electronic switch and a shaftless turbofan engine part: the ultrahigh-speed thrust vector jet engine comprises a sealing movable joint, a ring rotor, a ring gear, a ring bearing, blades, a gear, a force transmission shaft, a bearing seat, a gear and a sealing protective cover, has a simpler and more scientific structure, lower oil consumption, higher thrust, higher speed, lower noise, lower cost, simpler maintenance and operation and easier manufacture compared with the conventional jet engine with a turbine, can be started manually or automatically by using computer numerical control, and can realize low oil consumption, low pollution, low emission, low noise, high efficiency, high reliability and good running performance.

The technical scheme of the invention is realized as follows: a shaftless turbofan type ultrahigh-speed thrust vector jet engine is formed by combining a jet engine part and a shaftless turbofan engine part into a whole, wherein the jet engine part comprises: the device comprises a shell, an outer duct, an adjustable air inlet, a ring gear, a force bearing frame, a turbofan, an air compressor, a swirler, an oxygen supply and oil supply pipe, a boosting nozzle, a combustion chamber, a vector spray pipe, a stepping motor, a vector control rod, a universal joint, an adjustable nozzle, a spark plug, a generator, a charger, a storage battery, a starter, a computer, an electric wire, an instrument and meter, an electronic switch and a shaftless turbofan engine part: including sealed loose joint, ring rotor, ring gear, ring bearing, blade, gear, biography power axle, bearing frame, gear, sealed protection casing, characterized by: the front part of the jet engine combustion chamber is provided with an adjustable air inlet, a ring gear, a turbofan, an air compressor, a swirler, an oxygen supply and oil supply pipe and a thrust augmentation nozzle; the rear part is provided with a sealing movable joint, a ring rotor, a ring gear, a ring bearing, a vector spray pipe, a stepping motor, a vector control lever, a universal joint and an adjustable spray nozzle, the ring rotor, the ring gear and the ring bearing are radiated by air of an outer duct, two small holes are formed in the casing of the thrust vector jet engine and are used for mounting the gear and transmitting power, a sealing protective cover is arranged, blades are arranged in the ring rotor, the ring gear is arranged in the middle part of the outer part of the ring rotor, the ring bearings are arranged at two ends of the outer part of the ring rotor, the ring bearing is formed by combining an annular outer casing, an annular inner casing, circular marbles and an annular marble isolating device into a whole, and a marble groove, a convex body and a concave groove are formed in the annular outer casing; the ring bearing is assembled by loading the ring bullet separator into the ring inner shell, loading the round bullet, injecting high temperature resistant lubricating grease, loading the ring outer shell which is cut into two halves, welding the ring outer shell which is cut into two halves by modern high-tech welding technology into a seamless whole, using the new technology, the method is characterized in that a ring bearing is manufactured, a plurality of round marbles are filled in the ring bearing, the bearing capacity is large, the practical service life is long, when a vector spray pipe is manufactured, a machine is used for rotating a long strip-shaped steel sheet while lapping half steel sheets to press the steel sheet, a pressing ring is manufactured into the vector spray pipe, the vector spray pipe can stretch and retract like a steel sheet spring pipe and can bend 90 degrees in any direction, one end of a vector control rod is provided with a screw, the other end of the vector control rod is connected with a universal joint, the vector control rod is matched with a stepping motor, and one stepping motor or one stepping motor is respectively arranged above or below an air jet engine and matched with an upper stepping motor and a lower stepping motor; when the stepping motor on the left side or the right side of the jet engine rotates, the stepping motor rotates leftwards or rightwards to drive the vector control lever to push leftwards or rightwards, the vector control lever pushes leftwards or rightwards to drive the universal joint to push leftwards or rightwards, the universal joint pushes leftwards or rightwards to drive the vector spray pipe to bend leftwards or rightwards, and meanwhile, the adjustable nozzle is driven to spray leftwards or rightwards; when the stepping motor above the jet engine rotates, the stepping motor rotates leftwards or rightwards to drive the vector control lever to push leftwards or rightwards, the vector control lever pushes leftwards or rightwards to drive the universal joint to push leftwards or rightwards, the universal joint pushes leftwards or rightwards to drive the vector spray pipe to bend upwards or downwards and simultaneously drive the adjustable spray nozzle to spray upwards or downwards, in sum, the vector spray pipe and the adjustable spray nozzle on the jet engine can exhaust upwards or downwards or leftwards and rightwards, and the jet engine thrust vector can be directly adopted to control an airplane or a missile to fly. When the jet engine is started, a computer is started, a switch is pressed down, a starter is started, a turbofan of the jet engine rotates to drive a shaft and a gas compressor to run at a high speed to convey air to a combustion chamber, an afterburning nozzle in the combustion chamber can automatically spray oil, a spark plug can automatically ignite and explode, generated high-temperature and high-pressure gas flows backwards through the shaftless turbofan engine, part of internal energy expands in a ring rotor to push blades to be mechanical energy, the ring rotor is driven to rotate at a high speed, the ring rotor rotates at a high speed to drive a ring gear to rotate at a high speed, the ring gear rotates at a high speed to drive a gear to rotate at a high speed, the gear rotates at a high speed to drive a force transmission shaft to rotate at a high speed, the gear rotates at a high speed to drive the turbofan and the shaft and the gas compressor to rotate at a high speed, so that the jet engine can continuously run, and then huge gas flow flows from a vector spray pipe, The nozzle discharge can be adjusted to push and control the airplane and missile to fly at ultrahigh speed.

The invention has the advantages that: the invention is novel, the practicability is strong, the invention creates the shaftless turbofan type ultra-high speed thrust vector jet engine, the structure of the existing jet engine is completely changed, the structure is simpler and more scientific, the efficiency is higher, the oil consumption is lower, the thrust is higher, the speed is faster, the noise is lower, the cost is lower, the maintenance operation is simpler, the manufacture is easier, the computer control is adopted, the engine can be started manually or automatically, the invention has huge commercial development value, and the invention is the most advanced ultra-high speed thrust vector jet engine which is initiated in the world at present.

Description of the drawings:

FIG. 1 is a schematic view of the construction of a shaftless turbofan ultra high speed thrust vector jet engine of the present invention;

FIG. 2 is a schematic view of a shaftless turbofan engine of the present invention;

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

FIG. 4 is a schematic view of a ring bearing of the present invention;

fig. 5 is a side view schematic of fig. 4:

the specific implementation mode is as follows:

as shown in fig. 1, 2, 3, 4 and 5, a shaftless turbofan type ultrahigh-speed thrust vector jet engine is formed by combining a jet engine part and a shaftless turbofan engine part into a whole, wherein the jet engine part comprises: the device comprises a shell 1, an outer duct, an adjustable air inlet 2, a ring gear 3, a force bearing frame, a turbofan 4, an air compressor 5, a swirler 6, an oxygen supply and oil supply pipe 7, a boost nozzle 8, a combustion chamber 9, a vector spray pipe 22, a stepping motor, a vector control rod, a universal joint 23, an adjustable nozzle 15, a spark plug, a generator, a charger, a storage battery, a starter, a computer, an electric wire, an instrument and a meter, an electronic switch and a shaftless turbofan engine part: the device comprises a sealing movable joint 10, a ring rotor 11, a ring gear 12, a ring bearing 13, blades 14, a gear 16, a force transmission shaft 17, a bearing 18, a bearing seat 19, a gear 20 and a sealing protective cover 21, and is characterized in that: the front part of a jet engine combustion chamber 9 is provided with an adjustable air inlet 2, a ring gear 3, a turbofan 4, a gas compressor 5, a swirler 6, an oxygen supply and oil supply pipe 7 and a thrust augmentation nozzle 8; the rear part is provided with a sealing movable joint 10, a ring rotor 11, a ring gear 12, a ring bearing 13, a vector spray pipe 22, a stepping motor, a vector control lever, a universal joint 23 and an adjustable nozzle 15, the ring rotor 11, the ring gear 12 and the ring bearing 13 are radiated by air of an external duct, two small holes are formed in the casing of the jet engine and used for mounting gears 16 and 20 and transmitting power, a sealing protective cover 21 is arranged, blades 14 are arranged in the ring rotor 11, the ring gear 12 is arranged in the middle part of the outer part of the ring rotor 11, the ring bearings 13 are arranged at two ends of the outer part of the ring rotor 11, the ring bearings 13 are formed by combining an annular outer casing 24, an annular inner casing 25, a circular marble 26 and an annular marble isolating device 27 into a whole, and a marble groove 28, a convex body 29 and a concave groove 31 are formed in the annular outer casing 24; the ring-shaped inner shell 25 is also provided with a marble groove 28, a concave body 30 and a concave groove 31, the marble groove 28 is used for containing the round marble 26, the convex body 29 is matched with the concave body 30 and is used for sealing and dust-proof, the concave groove 31 is used for containing the ring-shaped marble isolator 27, the ring-shaped marble isolator 27 is provided with a hole for isolating the round marble 26, the ring-shaped marble isolator 27 can rotate or not rotate, a wire cutting machine or a laser cutting machine is used for cutting two halves or only one opening is cut and expanded for containing the round marble 26, the cut is ground and polished by a grinding machine to realize butt joint without a gap, when the ring bearing 13 is assembled, the ring-shaped marble isolator 27 is firstly arranged in the ring-shaped inner shell 25, then the round marble 26 is filled, high-temperature resistant lubricating grease is filled, finally the ring-shaped outer shell 24 which is cut into two halves is arranged, the ring-shaped outer shell 24 which is cut into two halves is welded into a seamless whole by using the modern high-tech welding technology, when the vector spray pipe 22 is manufactured, a machine is used for rotating a long strip-shaped steel sheet while pressing a half steel sheet on the steel sheet, and a pressing ring is manufactured into the vector spray pipe 22 which can stretch and retract like a steel sheet spring pipe and bend 90 degrees in any direction, one end of the vector control rod is provided with a screw, the other end of the vector control rod is connected with a universal joint 23, the vector control rod is matched with a stepping motor, and one stepping motor or one stepping motor is respectively arranged above or below the jet engine and matched with an upper stepping motor and a lower stepping motor; when the stepping motor on the left side or the right side of the jet engine rotates, the stepping motor rotates leftwards or rightwards to drive the vector control lever to push leftwards or rightwards, the vector control lever pushes leftwards or rightwards to drive the universal joint 23 to push leftwards or rightwards, the universal joint 23 pushes leftwards or rightwards to drive the vector spray pipe 22 to bend leftwards or rightwards, and simultaneously, the adjustable nozzle 15 is driven to spray air leftwards or rightwards; when the stepping motor above the jet engine rotates, the stepping motor rotates leftwards or rightwards to drive the vector control lever to push leftwards or rightwards, the vector control lever pushes leftwards or rightwards to drive the universal joint 23 to push leftwards or rightwards, the universal joint 23 pushes leftwards or rightwards to drive the vector spray pipe 22 to bend upwards or downwards and simultaneously drive the adjustable spray nozzle 15 to spray upwards or downwards, in conclusion, the vector spray pipe 22 and the adjustable spray nozzle 15 on the jet engine can exhaust upwards or downwards or leftwards and rightwards, and the jet engine thrust vector can be directly adopted to control an airplane or a missile to fly. When the jet engine is started, a computer is started, a switch is pressed, a starter is started, a jet engine turbofan 4 rotates to drive a shaft and a gas compressor 5 to run at a high speed to convey air to a combustion chamber 9, boosting nozzles 8 in the combustion chamber 9 can automatically spray oil, spark plugs can automatically ignite and explode, generated high-temperature and high-pressure gas flows backwards through the shaftless turbofan engine, part of internal energy expands in a ring rotor 11 to push blades 14 to be mechanical energy, the ring rotor 11 is driven to rotate at a high speed, the ring rotor 11 rotates at a high speed to drive a ring gear 12 to rotate at a high speed, the ring gear 12 rotates at a high speed to drive a gear 16 to rotate at a high speed, the gear 16 rotates at a high speed to drive a force transmission shaft 17 to rotate at a high speed, the force transmission shaft 17 rotates at a high speed to drive a gear 20 to rotate at a high speed, the gear 20 rotates at a high speed to drive the ring gear 3 to drive the turbofan 4 to rotate with the shaft and the gas compressor 5 at a high speed, the continuous operation is started, and then the huge gas flow is discharged from the vectoring nozzle 22 and the adjustable nozzle 15 to push and operate the airplane and the missile to fly at a high speed.

Claims

1. A shaftless turbofan type superspeed thrust vector jet engine is formed by combining a jet engine part and a shaftless turbofan engine part into a whole, wherein the jet engine part comprises: including casing (1), outer duct, adjustable air inlet (2), first ring gear (3), load frame, turbofan (4), compressor (5), swirler (6), oxygen suppliment and fuel feed pipe (7), afterburning nozzle (8), combustion chamber (9), vector spray tube (22), step motor, vector control pole, universal joint (23), adjustable spout (15), spark plug, generator, charger, battery, starter, computer, electric wire, instrument and meter, electronic switch, shaftless turbofan engine part: including sealed union (10), ring rotor (11), second ring gear (12), ring bearing (13), blade (14), first gear (16), biography power axle (17), bearing (18), bearing frame (19), second gear (20), sealed protection casing (21), characterized by: the front part of a jet engine combustion chamber (9) is provided with an adjustable air inlet (2), a first ring gear (3), a turbofan (4), a gas compressor (5), a swirler (6), an oxygen supply and oil supply pipe (7) and a thrust augmentation nozzle (8); the rear part is provided with a sealing movable joint (10), a ring rotor (11), a second ring gear (12), a ring bearing (13), a vector spray pipe (22), a universal joint (23) and an adjustable nozzle (15), the ring rotor (11), the second ring gear (12) and the ring bearing (13) are radiated by the air of an external duct, the shell of the jet engine is provided with two small holes for installing a first gear (16) and a second gear (20) and transmitting power and provided with a sealing protective cover (21), a blade (14) is arranged in the ring rotor (11), the second ring gear (12) is arranged in the middle part of the outer part of the ring rotor (11), the ring bearings (13) are arranged at the two ends, the ring bearings (13) are combined into a whole by an annular outer shell (24), an annular inner shell (25), a circular marble (26) and an annular marble isolator (27), and a vector control lever is matched with a stepping motor, installing a stepping motor above or below the jet engine or installing a stepping motor respectively to be matched with the upper stepping motor and the lower stepping motor; when the stepping motor on the left side or the right side of the jet engine rotates, the stepping motor rotates leftwards or rightwards to drive the vector control lever to push leftwards or rightwards, the vector control lever pushes leftwards or rightwards to drive the universal joint (23) to push leftwards or rightwards, the universal joint (23) pushes leftwards or rightwards to drive the vector spray pipe (22) to bend leftwards or rightwards, and meanwhile, the adjustable spray nozzle (15) is driven to spray leftwards or rightwards; when a stepping motor above the jet engine rotates, the stepping motor rotates leftwards or rightwards to drive a vector control lever to push leftwards or rightwards, the vector control lever pushes leftwards or rightwards to drive a universal joint (23) to push leftwards or rightwards, the universal joint (23) pushes leftwards or rightwards to drive a vector spray pipe (22) to bend upwards or downwards and simultaneously drive an adjustable nozzle (15) to spray upwards or downwards, when the jet engine is started, a computer is started firstly, a switch is pressed down, a starter is started, a jet engine turbofan (4) rotates to drive a shaft and a gas compressor (5) to run at high speed to convey air to a combustion chamber (9), a boosting nozzle (8) in the combustion chamber (9) automatically sprays oil, a spark plug automatically ignites and explodes, generated high-temperature and high-pressure gas flows backwards through the shaftless turbofan engine, and part of the internal energy expands in a ring rotor (11) to drive blades (14) to be mechanical energy, the ring rotor (11) is driven to rotate at a high speed, the ring rotor (11) rotates at a high speed to drive the second ring gear (12) to rotate at a high speed, the second ring gear (12) rotates at a high speed to drive the first gear (16) to rotate at a high speed, the first gear (16) rotates at a high speed to drive the force transmission shaft (17) to rotate at a high speed, the force transmission shaft (17) rotates at a high speed to drive the second gear (20) to rotate at a high speed, the second gear (20) rotates at a high speed to drive the first ring gear (3) to rotate at a high speed, the first ring gear (3) rotates at a high speed to drive the turbofan (4), the shaft and the compressor (5) to rotate together at a high speed, the continuous operation is started, then huge gas flow is discharged from the vector spray pipe (22) and the adjustable nozzle (15), and planes and missiles are pushed and controlled to fly at a high speed.