Jet propulsion type engine

Abstract

The invention discloses a jet propulsion type engine, relates to the field of jet propulsion type engines, and solves the problems that when an existing jet propulsion type engine is used, air flow is directly conveyed into the engine through a turbofan, impurities easily enter the engine, and the service life of the engine is influenced. The protection mechanism comprises a rotating cylinder, a fan-shaped blade and a control part, an output groove is formed in the shell, the protection mechanism controls the swing angle of the fan-shaped blade and adjusts the size of an opening in one end of the shell, the control part controls the rotating state of the rotating cylinder, and when impurities need to be blocked and thrown out, the rotating cylinder is controlled to rotate along with the turbofan; and when the impurities do not need to be blocked, the rotating cylinder is controlled to be limited, the angle of the fan-shaped blade is adjusted, and meanwhile the output groove is automatically closed, so that the gas completely flows into the shell through the turbofan, and the gas conveying amount is increased.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of jet propulsion engine, in particular to a jet propulsion engine. BACKGROUND

[0002] With the development of aviation technology, the performance requirements of jet propulsion engine are getting higher and higher. In the existing jet propulsion engine, the linkage control between each part plays a key role in the performance and efficiency of the engine. The principle is to draw gas into the body through the turbofan, and after pressurized combustion, high temperature and high pressure gas is obtained, which is ejected from the tail to produce reverse thrust.

[0003] The existing jet propulsion engine is generally directly provided with a turbofan at the front end for gas extraction. In extreme weather such as heavy rain and sandstorm, these impurities will directly enter the interior of the body through the turbofan, causing damage to the internal structure, especially when birds collide, the damage to the turbofan is particularly serious, and even major accidents can be caused. When the equipment is stopped for use, the turbofan is still exposed outside. When the external impurities are blown into the interior of the turbofan, starting the engine directly will cause damage to the turbofan, affecting the operation of the body. SUMMARY

[0004] The purpose of the present application is to provide a jet propulsion engine which is convenient for protecting the interior of the engine and prolonging the service life, so as to solve the problems raised in the background.

[0005] To achieve the above purpose, the present application provides the following technical scheme: a jet propulsion engine, comprising a shell and a protection mechanism, the shell is provided with a drive shaft, the outer wall of the drive shaft is provided with a turbofan, the protection mechanism comprises a rotating cylinder rotatably connected to one end of the drive shaft, the outer wall of the rotating cylinder is uniformly provided with a plurality of groups of fan-shaped leaves, an output slot is formed in the shell, and a control member is arranged in the shell for controlling the rotation state of the rotating cylinder, the protection mechanism can adjust the opening size of the position of one end of the shell by controlling the swing angle of the fan-shaped leaves, the rotation state of the rotating cylinder is controlled by the control member, when it is needed to block and throw out the impurities, the rotating cylinder is controlled to rotate with the turbofan, and the impurities are blocked and thrown to the output slot for output by the fan-shaped leaves, so as to avoid the impurities entering the interior of the turbofan, when it is not needed to block the impurities, the rotating cylinder is controlled to be limited, the angle of the fan-shaped leaves is adjusted, and the output slot is automatically closed, so that the gas completely flows into the interior of the shell through the turbofan, the stability of the gas flow conveying is improved, the conveying amount of the gas is increased, the interior of the engine is protected, and the service life is prolonged.

[0006] Preferably, the control piece comprises a rotating ring rotatably connected to the inner wall of the shell, the side surface of the rotating ring is fixedly connected with a first helical gear ring, the shell is provided with a storage cavity, the storage cavity is provided with a guide groove, the storage cavity is slidably connected with a second helical gear ring capable of being clamped with the first helical gear ring, the outer wall of the second helical gear ring is uniformly fixedly connected with a plurality of guide blocks, the guide blocks are slidably connected with the inner wall of the guide groove in the horizontal direction, and the storage cavity is provided with a driving piece for controlling the sliding state of the second helical gear ring and simultaneously controlling the opening and closing state of the output groove, so as to facilitate the control of the rotating state of the rotating cylinder.

[0007] Preferably, the driving piece comprises a plurality of stop blocks mounted in the output groove, the stop blocks are slidably connected with the inner wall of the shell, the stop blocks are fixedly connected with first tension springs fixedly connected with the shell, the side surface of the guide block is provided with a first inclined surface, and the side surface of the stop block is provided with a second inclined surface capable of being slidably attached to the first inclined surface. The shell is provided with a pressure piece for controlling the pressure in the storage cavity, so as to control the sliding state of the second helical gear ring and simultaneously control the opening and closing state of the output groove.

[0008] Preferably, the protection mechanism further comprises a plurality of rotating shafts rotatably connected to the outer wall of the rotating cylinder, one end of the rotating shaft away from the rotating cylinder is rotatably connected with the rotating ring, a plurality of the fan-shaped leaves are fixedly connected with the rotating shafts, the rotating cylinder is provided with a rotating piece for synchronously controlling the rotating angle of a plurality of the fan-shaped leaves, and the shell is provided with an output piece for outputting impurities blocked by the fan-shaped leaves into the output groove, so as to facilitate the rotation of the rotating cylinder with the turbofan when the impurities need to be blocked and thrown out, and the impurities are blocked and thrown to the output groove for output by the fan-shaped leaves, avoiding the impurities entering the inside of the turbofan. When the impurities do not need to be blocked, the rotating cylinder is controlled to be limited, the angle of the fan-shaped leaf is adjusted, and the output groove is automatically closed, so that the gas completely flows into the inside of the shell through the turbofan, and the stability of gas flow conveying is improved.

[0009] Preferably, the output piece comprises two fixed rings fixedly installed on the rotating ring, the shell is provided with a first annular groove, the rotating ring is provided with a second annular groove, the two fixed rings are fixedly connected with the two sides of the second annular groove respectively, the fixed ring is rotatably connected with the side surface of the first annular groove, one end of the output groove is in communication with the side surface of the first annular groove, and the other end is in communication with the outside. The rotating ring is uniformly provided with a plurality of communication holes in communication with the second annular groove, so as to facilitate the output of the impurities blocked by the fan-shaped leaves into the output groove.

[0010] Preferably, the rotating part comprises a driving motor fixedly installed in the rotating cylinder, the output end of the driving motor is coaxially and fixedly connected with a first bevel gear, one end of the rotating shaft is coaxially and fixedly connected with a second bevel gear, and a plurality of groups of the second bevel gears are engaged with the first bevel gear, so that the rotating angles of the plurality of groups of the fan-shaped leaves can be synchronously controlled.

[0011] Preferably, the fan-shaped leaf is provided with a rotating groove, a rotating net is rotatably connected in the rotating groove, and an electric telescopic rod is rotatably connected in the rotating groove, and the telescopic end of the electric telescopic rod is rotatably connected with the side surface of the rotating net, so that the gas flowing between the fan-shaped leaves can be preliminarily filtered.

[0012] Preferably, the pressure part comprises a conveying pump fixedly installed in the shell, the output end of the conveying pump is communicated with a connecting pipe, one end of the connecting pipe is communicated with the storage cavity, and the side surface of the second helical gear ring is fixedly connected with a second tension spring fixedly connected with the inner wall of the storage cavity, so that the pressure in the storage cavity can be controlled.

[0013] Preferably, the side surface of the fan-shaped leaf is uniformly provided with a plurality of groups of flow guide grooves, so that the impurities flowing close to the surface of the fan-shaped leaf can be guided to the output groove through the flow guide grooves.

[0014] Preferably, one end of the rotating cylinder is fixedly connected with a conical block, so that the resistance of the side surface of the rotating cylinder can be reduced.

[0015] Compared with the prior art, the beneficial effects of the present application are: The jet propulsion engine provided by the present application solves the problem that in the prior art, the gas flow directly passes through the turbofan and is delivered to the inside of the engine, which easily causes impurities to enter and affect the service life of the engine. The swinging angle of the fan-shaped leaf is controlled by the protection mechanism, the size of the opening at one end of the shell is adjusted, the rotating state of the rotating cylinder is controlled by the control part, when it is needed to block and throw out the impurities, the rotating cylinder is controlled to rotate with the turbofan, the impurities are blocked by the fan-shaped leaf and thrown to the output groove for output, so that the impurities are prevented from entering the inside of the turbofan, when it is not needed to block the impurities, the rotating cylinder is controlled to be limited, the angle of the fan-shaped leaf is adjusted, and the output groove is automatically closed, so that the gas flow passes through the turbofan and flows into the inside of the shell, the stability of the gas flow delivery is improved, and the delivery amount of the gas is increased. The device is flexible to operate and can be applied to different occasions, has a good protection effect on the engine body, and effectively prolongs the service life of the engine. BRIEF DESCRIPTION OF DRAWINGS

[0016] Figure 1 It is a whole structure schematic view of the present application; Figure 2 It is an external structure schematic view of the present application; Figure 3 is a sectional view of the shell structure of the present application; Figure 4 is Figure 3 is an enlarged view of area A in the middle; Figure 5 is Figure 4 is an enlarged view of area B in the middle; Figure 6 is a schematic view of the internal structure of the shell of the present application; Figure 7 is Figure 6 is an enlarged view of area C in the middle; Figure 8 is a schematic view of the partial structure of the protection mechanism of the present application; Figure 9 is an exploded view of the partial structure of the output of the present application; Figure 10 is a schematic view of the partial structure of the rotating member of the present application; Figure 11 is an exploded view of the partial structure of the rotating member of the present application; Figure 12 is Figure 11 is an enlarged view of area D in the middle; Figure 13 is an exploded view of the partial structure of the protection mechanism of the present application; Figure 14 is Figure 13 is an enlarged view of area E in the middle.

[0017] In the figure: 1 - shell; 2 - drive shaft; 3 - turbofan; 4 - protection mechanism; 5 - rotating cylinder; 6 - fan-shaped blade; 7 - output slot; 8 - control member; 9 - rotating ring; 10 - first helical tooth ring; 11 - storage cavity; 12 - guide slot; 13 - second helical tooth ring; 14 - guide block; 15 - driving member; 16 - stop block; 17 - first tension spring; 18 - first inclined surface; 19 - second inclined surface; 20 - pressure member; 21 - rotating shaft; 22 - rotating member; 23 - output member; 24 - fixed ring; 25 - first annular groove; 26 - second annular groove; 27 - communication hole; 28 - drive motor; 29 - first bevel gear; 30 - second bevel gear; 32 - rotating slot; 33 - rotating net; 34 - electric telescopic rod; 35 - delivery pump; 36 - connecting pipe; 37 - second tension spring; 38 - flow guide slot; 39 - conical block; 40 - suction device. DETAILED DESCRIPTION

[0018] The technical solutions in the embodiments of the present application will be described clearly and completely below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those skilled in the art without creative labor fall within the protection scope of the present application.

[0019] Please refer to Figures 1-14 The application provides a technical solution: a jet propulsion engine, comprising a shell 1 and a protection mechanism 4, the shell 1 is provided with a driving shaft 2, the outer wall of the driving shaft 2 is provided with a turbofan 3, the protection mechanism 4 comprises a rotating cylinder 5 rotatably connected to one end of the driving shaft 2, one end of the rotating cylinder 5 is fixedly connected with a conical block 39, the outer wall of the rotating cylinder 5 is uniformly provided with a plurality of groups of fan-shaped leaves 6, the shell 1 is provided with an output slot 7, the shell 1 is provided with a control member 8 for controlling the rotating state of the rotating cylinder 5, the protection mechanism 4 can adjust the opening size of the position of one end of the shell 1 by controlling the swing angle of the fan-shaped leaves 6, the rotating state of the rotating cylinder 5 is controlled by the control member 8, when it is needed to block and throw out impurities, the rotating cylinder 5 is controlled to rotate with the turbofan 3, and the impurities are blocked and thrown to the output slot 7 for output by the fan-shaped leaves 6, so that the impurities are prevented from entering the inside of the turbofan 3, when it is not needed to block the impurities, the rotating cylinder 5 is controlled to be limited, the angle of the fan-shaped leaves 6 is adjusted, and the output slot 7 is automatically closed at the same time, so that the gas completely flows into the inside of the shell 1 through the turbofan 3, the stability of the gas flow conveying is improved, and the conveying amount of the gas is increased.

[0020] The control member 8 comprises a rotating ring 9 rotatably connected to the inner wall of the shell 1, the side surface of the rotating ring 9 is fixedly connected with a first bevel gear ring 10, the shell 1 is provided with a storage cavity 11, the storage cavity 11 is provided with a guide groove 12, the storage cavity 11 is slidably connected with a second bevel gear ring 13 capable of being clamped with the first bevel gear ring 10, the outer wall of the second bevel gear ring 13 is uniformly fixedly connected with a plurality of groups of guide blocks 14, the guide blocks 14 are slidably connected with the inner wall of the guide groove 12 in the horizontal direction, and the storage cavity 11 is provided with a driving member 15 for controlling the sliding state of the second bevel gear ring 13 and simultaneously controlling the opening and closing state of the output slot 7.

[0021] The driving member 15 comprises a plurality of groups of stop blocks 16 mounted in the output slot 7, the stop blocks 16 are slidably connected with the inner wall of the shell 1, the stop blocks 16 are fixedly connected with first tension springs 17 fixedly connected with the shell 1, the side surface of the guide block 14 is provided with a first inclined surface 18, the side surface of the stop block 16 is provided with a second inclined surface 19 capable of being slidably attached with the first inclined surface 18, the shell 1 is provided with a pressure member 20 for controlling the pressure of the storage cavity 11, the pressure member 20 comprises a delivery pump 35 fixedly mounted in the shell 1, the output end of the delivery pump 35 is communicatively connected with a connecting pipe 36, one end of the connecting pipe 36 is in communication with the storage cavity 11, and the side surface of the second bevel gear ring 13 is fixedly connected with a second tension spring 37 fixedly connected with the inner wall of the storage cavity 11.

[0022] The protection mechanism 4 further comprises a plurality of rotating shafts 21 rotatably connected to the outer wall of the rotating cylinder 5, one end of the rotating shaft 21 away from the rotating cylinder 5 is rotatably connected to the rotating ring 9, a plurality of sector leaves 6 are fixedly connected to the rotating shafts 21 respectively, a plurality of guide grooves 38 are uniformly arranged on the side surface of the sector leaf 6, the rotating cylinder 5 is provided with a rotating part 22 for synchronously controlling the rotating angle of the plurality of sector leaves 6, the shell 1 is provided with an output part 23 for outputting the impurities blocked by the sector leaf 6 into the output slot 7, the rotating part 22 comprises a driving motor 28 fixedly installed in the rotating cylinder 5, the model of the driving motor 28 is preferably YYHS-40, the output end of the driving motor 28 is coaxially fixedly connected with a first bevel gear 29, one end of the rotating shaft 21 is coaxially fixedly connected with a second bevel gear 30, and the plurality of second bevel gears 30 are meshed with the first bevel gear 29.

[0023] The output part 23 comprises two sets of fixed rings 24 fixedly installed on the rotating ring 9, the shell 1 is provided with a first annular groove 25, the rotating ring 9 is provided with a second annular groove 26, the two sets of fixed rings 24 are fixedly connected to the two sides of the second annular groove 26 respectively, the fixed ring 24 is rotatably connected to the side surface of the first annular groove 25, one end of the output slot 7 is in communication with the side surface of the first annular groove 25, and the other end is in communication with the outside.

[0024] The sector leaf 6 is provided with a rotating groove 32, the rotating groove 32 is rotatably connected with a rotating net 33, and the rotating groove 32 is rotatably connected with an electric telescopic rod 34, and the telescopic end of the electric telescopic rod 34 is rotatably connected with the side surface of the rotating net 33.

[0025] In the embodiment, the driving motor 28 drives the first bevel gear 29 to rotate, so that the plurality of second bevel gears 30 are synchronously rotated, the rotating angle of the rotating shaft 21 is changed, the sector leaf 6 is driven to rotate, when the engine is in a stationary state, the plurality of sector leaves 6 are driven to rotate to the state that the side surfaces are mutually attached, the function of preliminarily closing one end of the shell 1 is realized, some floating impurities (such as plastic bags) are prevented from being blown into the turbofan 3 together with the wind, and then the running state of the engine is affected, and the safety hazard is caused, so that the engine in the stationary state can be better protected, and foreign matters are prevented from entering the engine.

[0026] When the engine is normally rotating, at this time the delivery pump 35 pushes hydraulic oil into the storage cavity 11, the second bevel gear ring 13 gradually slides to one side of the first bevel gear ring 10, until the second bevel gear block is clamped with the first bevel gear ring 10, after that the rotating cylinder 5 cannot continue to rotate with the rotating of the turbofan 3, at the same time the first inclined surface 18 on the guide block 14 and the second inclined surface 19 on the block 16 will be in close contact during the sliding of the second bevel gear ring 13, gradually lifting the block 16, the first tension spring 17 is stretched, the block 16 gradually slides into the output groove 7, blocking the output groove 7, a sealing ring can be arranged around the block 16 to improve the sealing process of the output groove 7, after that the driving motor 28 adjusts the inclination angle of the plurality of fan-shaped leaves 6, so that the fan-shaped leaves 6 are limited when the air flow thrust is the smallest, at this time the resistance of the fan-shaped leaves 6 to the air flow is the smallest, and the air flow will be directly delivered to the turbofan 3 after passing through the fan-shaped leaves 6 to reach the inside of the engine, so that the input air flow is maximized, this scene is suitable for weather suitable and no obstacles, some large obstacles will be blocked by the fan-shaped leaves 6, to avoid directly entering the inside of the turbofan 3.

[0027] When the weather is abnormal and the impurities in the airflow are more, the fan-shaped leaf 6 is adjusted to the required inclination angle by the driving motor 28, and then the hydraulic oil in the storage cavity 11 is pumped out by the delivery pump 35, the second bevel gear ring 13 is driven by the second tension spring 37 to move away from the first bevel gear ring 10, gradually releasing the clamping and limiting of the first bevel gear ring 10, at the same time, under the pulling of the first tension spring 17, the block 16 slides reversely, so that the block 16 releases the blockage of the middle part of the output groove 7, and then in the process of rotating the turbofan 3, the input airflow will push the inclined surface of the fan-shaped leaf 6 to make the fan-shaped leaf 6 rotate the rotating cylinder 5 together, since the driving force of the fan-shaped leaf 6 is pushed by the airflow, most of the airflow entering the turbofan 3 will flow through the surface of the fan-shaped leaf 6, and after being guided by the guide groove 38, the rainwater and other impurities will be adsorbed in the guide groove 38 and thrown to the surrounding, then transported to the second annular groove 26 through the communication hole 27, and then transported to the output groove 7 through the first annular groove 25 for output, the outer end of the output groove 7 is connected with the outside, and the end is located in the arc region of the outer surface of the shell 1, the airflow outside the shell 1 will help to suck out the impurities in the output groove 7 and flow with the outside airflow in the process of flowing backward, thereby effectively avoiding the impurities entering the engine, and at the same time, since the inner opening of the communication hole 27 is larger than the outer opening, the airflow can more smoothly pass through the communication hole from the fan-shaped leaf 6 to the output groove 7, and the airflow in the output groove 7 is prevented from flowing reversely to the position of the fan-shaped leaf 6, and the auxiliary suction device 40 (such as a impeller rotating structure) can be arranged in the output groove 7 to improve the driving force of the airflow from the communication hole to the output groove 7, and the structure can be linked and controlled with the running state of the block 16 through a sensor or a control switch, so that when the block 16 moves up to block the output groove 7, the suction device 40 stops running, and when the block 16 moves down to open the communication state of the output groove 7, the suction device 40 starts to run at high speed, and the impurities at the communication hole 27 are sucked into the output groove 7 and discharged from the other end of the output groove 7.

[0028] It is worth noting that when encountering sand and dust weather, the aircraft needs to filter the solid particle impurities in the airflow during take-off and landing to avoid impurities entering the engine, the rotating net 33 is pushed out by controlling the electric telescopic rod 34, and the rotating net 33 is rotated to an angle perpendicular to the fan-shaped leaf 6, at this time, the gas flowing between the fan-shaped leaves 6 will be filtered by the rotating net 33, some relatively large sandstones are blocked, and in the process of rotation, the sandstones are thrown into the communication hole 27 by centrifugal force, and then discharged through the output groove 7, after use, the rotating net 33 is reversely turned over to the rotating groove 32 by the electric telescopic rod 34 for storage, the device has large resistance to airflow, and the engine speed needs to be increased during use to improve the thrust, which is only suitable for special weather use and plays an emergency role to avoid a large amount of impurities entering the engine and affecting the service life of the engine.

[0029] It has to be noted that, in the present document, the terms "first", "second", etc. merely serve to identify a subject or action, without necessarily requiring or implying any such actual relationship or order between such subjects or actions. Moreover, the terms "comprises", "comprising", or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but can include other elements not expressly listed or inherent to such process, method, article, or apparatus.

[0030] While embodiments of the present application have been shown and described, it is to be understood that various modifications, substitutions, combinations, and variations of the embodiments can be undertaken without departing from the spirit and scope of the present application, which is defined by the appended claims and their equivalents.

Claims

1. A jet propulsion engine, characterized in that, include: A housing (1) is provided inside the housing (1), and a turbine fan (3) is provided on the outer wall of the drive shaft (2). Also includes: The protective mechanism (4) includes a rotating cylinder (5) rotatably connected to one end of the drive shaft (2). The outer wall of the rotating cylinder (5) is uniformly provided with multiple sets of fan-shaped blades (6). An output slot (7) is provided inside the housing (1). A control component (8) for controlling the rotation state of the rotating cylinder (5) is provided inside the housing (1). The protective mechanism (4) can adjust the opening size at one end of the housing (1) by controlling the swing angle of the fan-shaped blades (6), and control the rotation of the rotating cylinder (5) through the control component (8). In the dynamic state, when it is necessary to block and throw out impurities, the rotating cylinder (5) is controlled to rotate with the turbine fan (3), and the impurities are blocked and thrown to the output slot (7) through the fan blade (6) for output, so as to prevent impurities from entering the turbine fan (3). When it is not necessary to block impurities, the rotating cylinder (5) is controlled to limit the position, the angle of the fan blade (6) is adjusted, and the output slot (7) is automatically closed at the same time, so that the gas flows completely through the turbine fan (3) into the housing (1), improving the stability of airflow and increasing the gas delivery volume.

2. The jet propulsion engine according to claim 1, characterized in that: The control component (8) includes a rotating ring (9) rotatably connected to the inner wall of the housing (1). A first helical toothed ring (10) is fixedly connected to the side of the rotating ring (9). A storage cavity (11) is provided inside the housing (1). A guide groove (12) is provided inside the storage cavity (11). A second helical toothed ring (13) that can engage with the first helical toothed ring (10) is slidably connected inside the storage cavity (11). Multiple sets of guide blocks (14) are evenly fixedly connected to the outer wall of the second helical toothed ring (13). The guide blocks (14) are slidably connected to the inner wall of the guide groove (12) in the horizontal direction. A drive component (15) is provided inside the storage cavity (11) for controlling the sliding state of the second helical toothed ring (13) and simultaneously controlling the opening and closing state of the output groove (7).

3. A jet propulsion engine according to claim 2, characterized in that: The drive unit (15) includes multiple sets of stops (16) installed in the output slot (7). The stops (16) are slidably connected to the inner wall of the housing (1). A first tension spring (17) is fixedly connected to the stops (16) and fixedly connected to the housing (1). A first inclined surface (18) is provided on the side of the guide block (14). A second inclined surface (19) is provided on the side of the stops (16) that can slide against the first inclined surface (18). A pressure member (20) is provided inside the housing (1) for controlling the pressure in the storage cavity (11).

4. A jet propulsion engine according to claim 2, characterized in that: The protective mechanism (4) also includes multiple sets of rotating shafts (21) rotatably connected to the outer wall of the rotating cylinder (5). The end of the rotating shaft (21) away from the rotating cylinder (5) is rotatably connected to the rotating ring (9). Multiple sets of fan blades (6) are fixedly connected to the rotating shafts (21). The rotating cylinder (5) is provided with a rotating component (22) for synchronously controlling the rotation angle of multiple sets of fan blades (6). The housing (1) is provided with an output component (23) for outputting the impurities blocked by the fan blades (6) into the output slot (7).

5. A jet propulsion engine according to claim 4, characterized in that: The output component (23) includes two sets of fixed rings (24) fixedly installed on the rotating ring (9). The housing (1) has a first annular groove (25) and the rotating ring (9) has a second annular groove (26). The two sets of fixed rings (24) are fixedly connected to both sides of the second annular groove (26) respectively. The fixed rings (24) are rotatably connected to the side of the first annular groove (25). One end of the output groove (7) is connected to the side of the first annular groove (25), and the other end is connected to the outside. The rotating ring (9) has multiple sets of connecting holes (27) evenly opened to communicate with the second annular groove (26).

6. A jet propulsion engine according to claim 4, characterized in that: The rotating component (22) includes a drive motor (28) fixedly installed inside the rotating cylinder (5). The output end of the drive motor (28) is coaxially fixedly connected to a first bevel gear (29), and one end of the rotating shaft (21) is coaxially fixedly connected to a second bevel gear (30). Multiple sets of second bevel gears (30) mesh with the first bevel gear (29).

7. A jet propulsion engine according to claim 1, characterized in that: The fan-shaped blade (6) is provided with a rotating groove (32), a rotating net (33) is rotatably connected in the rotating groove (32), and an electric telescopic rod (34) is rotatably connected in the rotating groove (32). The telescopic end of the electric telescopic rod (34) is rotatably connected to the side of the rotating net (33).

8. A jet propulsion engine according to claim 3, characterized in that: The pressure component (20) includes a delivery pump (35) fixedly installed in the housing (1). The output end of the delivery pump (35) is connected to a connecting pipe (36). One end of the connecting pipe (36) is connected to the storage cavity (11). The side of the second helical toothed ring (13) is fixedly connected to a second tension spring (37) which is fixedly connected to the inner wall of the storage cavity (11).

9. A jet propulsion engine according to claim 1, characterized in that: Multiple sets of guide grooves (38) are evenly provided on the side of the fan-shaped blade (6).

10. A jet propulsion engine according to claim 1, characterized in that: A conical block (39) is fixedly connected to one end of the rotating cylinder (5).

Images