CN115615247A - Digital electronic rain-increasing and trumpet-preventing rocket launching safety locking device - Google Patents

Abstract

The invention discloses a digital electronic rain-increasing and trumpet-preventing rocket launching safety locker, which comprises: the fuselage, the inner wall fixedly connected with display of fuselage, the side surface fixedly connected with control panel of fuselage, the inner wall fixedly connected with pilot lamp of fuselage, control panel and display electrical connection, the pilot lamp is connected with control panel electrical connection, the surface of fuselage is provided with safety device, safety device includes protection machanism, protection machanism sets up the side surface at the fuselage, safety device includes actuating mechanism, actuating mechanism sets up the inner wall at protection machanism, safety device includes clearance mechanism, utilize a plurality of structural component in the protection machanism, continuously protect the equipment control button position, because of equipment control button is directly not exposed in the external world after being protected, make non-professional operating personnel be difficult to operate through equipment, support for the security of equipment provides, the ability that equipment can carry out the closed protection to controlling the panel position has been realized.

Description

Digital electronic rain-increasing and trumpet-preventing rocket launching safety locking device

Technical Field

The invention relates to the technical field of rocket control equipment, in particular to a digital electronic rainfall and campsis enhancing rocket launching safety locker.

Background

The artificial rain enhancement method is a method for properly increasing or redistributing rainfall by adopting a broadcasting technology for certain types of cloud systems and storm systems, and is a means for human to modify and utilize nature, such as using tools such as airplanes, rockets, cannons, combustion furnaces, flame bombs and the like to send catalysts such as silver iodide, dry ice and the like to supercooled parts in clouds to increase ice crystals and condensation nuclei in the clouds and promote more water vapor to form raindrops on the ground, and for warm clouds, broadcasting catalysts (such as salt, calcium chloride, calcium oxide, urea, ammonium nitrate and the like) with strong hygroscopicity to the clouds to promote the cloud drops to be increased into raindrops to fall off, so that the rainfall amount is increased, in addition, shock waves are generated when the rockets, the cannons, the flame bombs and the like explode in the clouds to accelerate the merging process, the cloud drops and the cloud drops to be merged and increased into raindrops to fall off, so that the rain enhancement effect is achieved; however, since the rocket has high launching height, the rocket is more suitable for areas with low altitude or spring and autumn seasons with high zero-degree layer height, so that the rocket operation system is widely used in artificial precipitation operation no matter in south or north China, the rocket sowing artificial ice core operation is carried out in the operation area, the average height of the average isotherm of-6 to-12 ℃ in the month in the local operation period is calculated in advance and used as the reference of the rocket flame sowing height layer, the latent heat effect is considered at the moment, and the temperature in cloud (updraft area) is generally slightly higher than the ambient temperature.

The launching method of the rain-increasing rocket comprises the following steps: plane shooting: when the horizontal size of the accumulated cloud is large, the vertical size of the accumulated cloud is small, and the ascending air flow in the cloud is weak, the operation is carried out in a plane shooting mode, silver iodide particles are uniformly carried to the cloud layer for optimal catalysis at a certain height by the method, so that the catalyst acts on a horizontal plane in a large range, and the effect of enhancing the rain to the maximum extent is achieved; trapezoidal shooting: when the vertical dimension of the cumulus cloud is large and the ascending airflow in the cloud is strong, the operation is carried out by adopting a trapezoidal shooting mode, the three-dimensional shooting method adopts different shooting angles and different directions to bring the silver iodide particles to different heights in the cloud layer, so that the catalyst acts on the vertical surface in a large range to achieve the effect of enhancing the rain to the maximum extent.

However, the existing treatment equipment has the following defects:

in daily use, such as a rocket safety lock of CN112540562A is found, most existing devices adopt a button as a main structure of a control panel, during the use of the device, the button of the device is mostly exposed to the air, and during the operation of the device, the safety of the device is reduced due to the fact that the existing control panel is exposed and is easily pressed and operated by unskilled persons.

Therefore, a digital electronic rain-increasing and trumpet-preventing rocket launching safety locker is provided so as to solve the problems.

Disclosure of Invention

The invention aims to provide a digital electronic precipitation-increasing and trumpet-preventing rocket launching safety locking device, which continuously protects the position of an equipment control button by a protection mechanism connected with a machine body and utilizing a plurality of structural components in the mechanism, and non-professional operators are difficult to operate through the equipment because the equipment control button is not directly exposed outside after being protected, so that support is provided for the safety of the equipment, the capability of the equipment for sealing and protecting the position of a control panel is realized, and the problems in the background art are solved.

In order to achieve the purpose, the invention provides the following technical scheme: a digital electronic rain-increasing and trumpet-preventing rocket launching safety locker comprises: the display device comprises a machine body, a display is fixedly connected to the inner wall of the machine body, a control panel is fixedly connected to the side surface of the machine body, an indicator lamp is fixedly connected to the inner wall of the machine body, the control panel is electrically connected with the display, the indicator lamp is electrically connected with the control panel, and a safety device is arranged on the surface of the machine body;

the safety device comprises a protection mechanism, wherein the protection mechanism is arranged on the side surface of the machine body and comprises a driving mechanism, the driving mechanism is arranged on the inner wall of the protection mechanism, and the safety device comprises a cleaning mechanism. The cleaning mechanism is arranged on the lower surface of the protection mechanism;

protection machanism includes the support frame, the support frame is connected with the lower fixed surface of fuselage, the side surface butt of support frame has the baffle, the baffle is close to one side fixedly connected with sealing washer of fuselage, the side surface fixedly connected with buckle of baffle utilizes a plurality of structural component in the mechanism, continuously protects the equipment control button position, because of equipment control button is not directly exposed in the external world after being protected for non-professional operating personnel are difficult to operate through equipment, provide support for the security of equipment, have realized that equipment can carry out the ability of sealing the protection to controlling the panel position.

Preferably, the side surface fixedly connected with mount of fuselage, the surperficial joint of mount has the damping piece, the lower fixed surface of support frame is connected with identification panel, the inner wall fixed link of support frame has the locator card strip, utilizes the damping piece to retrain with detaining the closed state of piece.

Preferably, the baffle is in butt joint with the side surface of fuselage, the sealing washer is in butt joint with control panel's surface, the quantity of detaining the piece is two, two detain the piece and be bilateral symmetry setting about the baffle, detain the side surface butt of piece and fuselage, utilize the baffle to seal control panel in order to avoid non-professional's operation.

Preferably, the quantity of mount is two, two the mount is bilateral symmetry setting about the fuselage, the catching groove has been seted up on the surface of knot piece, the damping piece is connected with the inner wall looks joint of catching groove, the damping piece supports with the side surface looks butt of fuselage, utilizes the mount to support the position of damping piece and fixes the restraint effect in order to realize the damping piece.

Preferably, actuating mechanism includes the data mainboard, the inner wall fixed connection of data mainboard and support frame, the inner wall fixedly connected with fingerprint identification ware of support frame, the inner wall fixedly connected with drive motor of support frame utilizes the cooperation of fingerprint identification ware and data mainboard to discern and store operating personnel's fingerprint data.

Preferably, the driving end of the transmission motor is fixedly connected with a gear, the inner wall of the supporting frame is rotatably connected with a toothed ring, the inner wall of the toothed ring is fixedly connected with a rotating shaft, a binding block is fixedly connected to the side surface of the rotating shaft, and the position of the baffle can be limited by the aid of the matching of the binding block and the rotating shaft.

Preferably, the data mainboard is electrically connected with the fingerprint recognizer, the fingerprint recognizer is abutted against the recognition panel, the transmission motor is electrically connected with the data mainboard, the transmission motor is abutted against the side surface of the positioning clamp strip, and the gear ring can be driven by the matching of the transmission motor and the gear.

Preferably, the gear meshes with the tooth's socket of ring gear mutually, the pivot runs through the support frame setting, the assembly groove has been seted up to the side surface of baffle, the pivot is with the inner wall looks butt in assembly groove, the constraint piece is with the inner wall looks joint in assembly groove, utilizes the cooperation of constraint piece and baffle to retrain the position of pivot.

Preferably, the clearance mechanism includes the position sleeve, the lower fixed surface of position sleeve and support frame is connected, the inner wall of position sleeve rotates and is connected with spacing axle, the lower fixed surface of spacing axle is connected with links up the frame, the side surface butt that links up the frame has the buckle, the fixed surface of buckle is connected with the bolt, the mounting groove has been seted up to the inner wall of buckle, the inner wall joint that the buckle is located the mounting groove has the cleaning piece, utilizes position sleeve and spacing axle can restrict the position that links up the frame, but retrains the rotation axis that links up the frame simultaneously.

Preferably, the linking frame is abutted against the lower surface of the support frame, the lower surface of the linking frame is provided with a limiting hole, the bolts are clamped with the inner walls of the limiting hole, the number of the bolts is two, the two bolts are arranged in bilateral symmetry about the retaining ring, the cleaning block is abutted against the inner wall of the linking frame, the cleaning block is abutted against the surface of the identification panel, and the cleaning block is fixed in the linking frame by the cooperation of the bolts and the retaining ring.

Compared with the prior art, the invention has the beneficial effects that:

1. according to the invention, by arranging the protection mechanism, when rocket control is carried out, rocket launching parameters are set through the control panel, the set parameters are displayed through the display, rocket launching can be carried out after equipment is finished, before the control panel is operated, an unlocking finger of a designated operator is placed on the identification panel, the driving mechanism identifies the back driving baffle plate, the baffle plate drives the buckling block, the buckling block is driven to be separated from the damping block, the baffle plate is driven to be unfolded, the sealing ring is driven to be separated from the control panel by the baffle plate, meanwhile, the control panel loses the blocking exposure of the baffle plate, then, equipment control can be carried out, and by arranging the protection mechanism, the equipment can seal the control button, so that the problem that non-professionals operate the equipment is avoided, and the safety of the equipment is further improved.

2. According to the fingerprint identification device, the driving mechanism is arranged, when the finger of an appointed operator is placed on the identification panel, the fingerprint identification device identifies the fingerprint, the fingerprint is compared with fingerprint data in the data main board, after the comparison is passed, the data main board opens the transmission motor, the transmission motor is electrified to drive the gear, the gear drives the gear ring, the gear ring drives the rotating shaft to rotate and drive the binding block, the binding block drives the baffle to be unfolded, the unfolding operation of the baffle is completed immediately, the driving mechanism is arranged, the protection mechanism needs to be unfolded under the fingerprint of the appointed operator, the probability that the protection mechanism is unfolded by non-professionals is reduced, and the protection performance of the protection mechanism is improved.

3. According to the invention, the cleaning mechanism is arranged, after fingerprint identification of a person is completed, the connecting frame is shifted, the connecting frame drives the retaining ring, the retaining block drives the cleaning block, the cleaning block moves and wipes fingerprints remained on the surface of the identification panel, when the cleaning block needs to be replaced, the retaining ring is shifted downwards, the retaining ring pulls the bolt, the bolt is forced to be separated from the limiting hole, the retaining ring loses the constraint of the bolt and drives the cleaning block to be separated from the connecting frame, and then the cleaning block can be replaced.

Drawings

FIG. 1 is a perspective view of a front view structure of a digital electronic rainfall enhancement and campsis prevention rocket launching safety locker;

FIG. 2 is a perspective view of a bottom view of a digital electronic rain-increasing and trumpet-preventing rocket launching safety lock in accordance with the present invention;

FIG. 3 is a perspective view of a cross-sectional structure of a digital electronic rain-increasing and trumpet-preventing rocket launching safety locker of the present invention;

FIG. 4 is an enlarged perspective view of the structure at A in FIG. 3 of a digital electronic rain-increasing and trumpet-preventing rocket launching safety locker of the present invention;

FIG. 5 is an enlarged perspective view of a protection mechanism in the digital electronic rainfall enhancement and campsis prevention rocket launching safety locker of the invention;

FIG. 6 is an enlarged perspective view of the digital electronic rain-increasing and trumpet-preventing rocket launching safety locker at the position B in FIG. 5;

FIG. 7 is an enlarged perspective view of a structure of a driving mechanism in the digital electronic rain-increasing and trumpet-preventing rocket launching safety locker of the invention;

fig. 8 is an enlarged perspective view of a cleaning mechanism in the digital electronic rain enhancement and trumpet creeper prevention rocket launching safety locker of the invention.

In the figure: 1. a body; 2. a display; 3. a control panel; 4. an indicator light; 5. a safety device; 51. a protection mechanism; 511. a support frame; 512. a baffle plate; 513. a seal ring; 514. buckling blocks; 515. a fixed mount; 516. a damping block; 517. identifying a panel; 518. positioning the clamping strip; 52. a drive mechanism; 521. a data main board; 522. a fingerprint identifier; 523. a drive motor; 524. a gear; 525. a toothed ring; 526. a rotating shaft; 527. a tie block; 53. a cleaning mechanism; 531. positioning the sleeve; 532. a limiting shaft; 533. a linking frame; 534. a retaining ring; 535. a bolt; 536. and (4) cleaning the block.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Referring to fig. 1-8, the present invention provides a technical solution: a digital electronic rainfall and campsis enhancing rocket launching safety locker comprises: fuselage 1, the inner wall fixedly connected with display 2 of fuselage 1, the side surface fixedly connected with control panel 3 of fuselage 1, the inner wall fixedly connected with pilot lamp 4 of fuselage 1, control panel 3 and display 2 electrical connection, pilot lamp 4 is connected with control panel 3 electrical connection, the surface of fuselage 1 is provided with safety device 5, safety device 5 includes protection machanism 51, protection machanism 51 sets up the side surface at fuselage 1, safety device 5 includes actuating mechanism 52, actuating mechanism 52 sets up the inner wall at protection machanism 51, safety device 5 includes clearance mechanism 53. The cleaning mechanism 53 is provided on the lower surface of the guard mechanism 51.

According to fig. 5-6, the protection mechanism 51 comprises a support frame 511, the support frame 511 is fixedly connected with the lower surface of the machine body 1, a baffle 512 is abutted to the side surface of the support frame 511, a sealing ring 513 is fixedly connected to one side of the baffle 512, which is close to the machine body 1, and a buckle is fixedly connected to the side surface of the baffle 512.

According to fig. 5-6, a fixing frame 515 is fixedly connected to a side surface of the body 1, a damping block 516 is clamped on a surface of the fixing frame 515, an identification panel 517 is fixedly connected to a lower surface of the supporting frame 511, a positioning clamping strip 518 is fixedly connected to an inner wall of the supporting frame 511, and the closed state of the baffle 512 can be restrained by matching the damping block 516 with the buckling block 514.

According to fig. 5-6, the baffle 512 abuts against the side surface of the body 1, the sealing ring 513 abuts against the surface of the control panel 3, the number of the buckling blocks 514 is two, the two buckling blocks 514 are symmetrically arranged left and right relative to the baffle 512, the buckling blocks 514 abut against the side surface of the body 1, and the control panel 3 can be closed by the baffle 512 to avoid operation of non-professionals.

According to the illustration in fig. 5-6, the number of the fixing frames 515 is two, the two fixing frames 515 are arranged in bilateral symmetry with respect to the machine body 1, the surface of the fastening block 514 is provided with a fastening groove, the damping block 516 is clamped with the inner wall of the fastening groove, the damping block 516 is abutted with the side surface of the machine body 1, and the position of the damping block 516 can be supported and fixed by the fixing frames 515 to achieve the constraint effect of the damping block 516.

As shown in fig. 7, the driving mechanism 52 includes a data main board 521, the data main board 521 is fixedly connected to an inner wall of the supporting frame 511, a fingerprint identifier 522 is fixedly connected to the inner wall of the supporting frame 511, a transmission motor 523 is fixedly connected to the inner wall of the supporting frame 511, and the fingerprint data of the operator can be identified and stored by the cooperation of the fingerprint identifier 522 and the data main board 521.

According to fig. 7, a gear 524 is fixedly connected to a driving end of the transmission motor 523, a gear ring 525 is rotatably connected to an inner wall of the support frame 511, a rotating shaft 526 is fixedly connected to an inner wall of the gear ring 525, a binding block 527 is fixedly connected to a side surface of the rotating shaft 526, and the position of the baffle 512 can be limited by the matching of the binding block 527 and the rotating shaft 526.

As shown in fig. 7, the data main board 521 is electrically connected to the fingerprint identifier 522, the fingerprint identifier 522 is in contact with the identification panel 517, the transmission motor 523 is electrically connected to the data main board 521, the transmission motor 523 is in contact with the side surface of the positioning strip 518, and the gear ring 525 can be driven by the cooperation of the transmission motor 523 and the gear 524.

According to the illustration of fig. 7, the gear 524 is engaged with the tooth socket of the gear ring 525, the rotating shaft 526 is arranged to penetrate through the supporting frame 511, the side surface of the baffle plate 512 is provided with an assembling groove, the rotating shaft 526 is abutted against the inner wall of the assembling groove, the binding block 527 is clamped with the inner wall of the assembling groove, and the position of the rotating shaft 526 can be constrained by the matching of the binding block 527 and the baffle plate 512.

According to fig. 8, the cleaning mechanism 53 includes a positioning sleeve 531, the positioning sleeve 531 is fixedly connected to the lower surface of the support frame 511, the inner wall of the positioning sleeve 531 is rotatably connected to a limiting shaft 532, the lower surface of the limiting shaft 532 is fixedly connected to a linking frame 533, a retaining ring 534 is abutted to the side surface of the linking frame 533, a bolt 535 is fixedly connected to the surface of the retaining ring 534, a mounting groove is formed in the inner wall of the retaining ring 534, a cleaning block 536 is clamped to the inner wall of the retaining ring 534 located in the mounting groove, the position of the linking frame 533 can be limited by the positioning sleeve 531 and the limiting shaft 532, and the center of the rotating shaft 526 of the linking frame 533 can be restrained.

As shown in fig. 8, the engaging frame 533 abuts against the lower surface of the supporting frame 511, a limiting hole is formed in the lower surface of the engaging frame 533, the pins 535 are clamped against the inner wall of the limiting hole, the number of the pins 535 is two, the two pins 535 are symmetrically arranged about the retaining ring 534, the cleaning block 536 abuts against the inner wall of the engaging frame 533, the cleaning block 536 abuts against the surface of the identification panel 517, and the cleaning block 536 is fixed in the engaging frame 533 by the cooperation of the pins 535 and the retaining ring 534.

The effect that its whole mechanism reaches does: during rocket control, rocket launching parameters are set through the control panel 3, the set parameters are displayed through the display 2, rocket launching can be carried out after equipment is completed, before the control panel 3 is operated, unlocking fingers of an appointed operator are placed on the identification panel 517, the driving mechanism 52 identifies the rear driving baffle 512, the baffle 512 drives the buckle block 514, the buckle block 514 is driven to be separated from the damping block 516, the baffle 512 is driven to be unfolded, the sealing ring 513 is driven to be separated from the control panel 3 by the baffle 512, meanwhile, the control panel 3 loses the blocking exposure of the baffle 512, then, equipment can be controlled, and the equipment can seal a control button through the arrangement of the protection mechanism 51, so that the problem that non-professionals operate the equipment is solved, and the safety of the equipment is further improved;

meanwhile, by arranging the driving mechanism 52, when the finger of a designated operator is placed on the identification panel 517, the fingerprint identifier 522 identifies the fingerprint and compares the fingerprint with the fingerprint data in the data main board 521, after the comparison is passed, the data main board 521 opens the transmission motor 523, the transmission motor 523 is electrified to drive the gear 524, the gear 524 drives the toothed ring 525, the toothed ring 525 drives the rotating shaft 526 to rotate and drive the binding block 527, the binding block 527 drives the baffle 512 to expand, and then the expansion operation of the baffle 512 is completed, and by arranging the driving mechanism 52, the protection mechanism 51 needs to be expanded under the fingerprint of the designated operator, so that the probability that the protection mechanism 51 is expanded by non-professional personnel is reduced, and the protection performance of the protection mechanism 51 is improved;

in addition, by arranging the cleaning mechanism 53, after the fingerprint identification of a person is completed, the connecting frame 533 is shifted, the connecting frame 533 drives the retaining ring 534, the buckling block 514 drives the cleaning block 536, the cleaning block 536 moves and wipes the residual fingerprint on the surface of the identification panel 517, when the cleaning block 536 needs to be replaced, the retaining ring 534 is shifted downwards, the retaining ring 534 pulls the bolt 535, the bolt 535 is forced to be separated from the limiting hole, the retaining ring 534 loses the constraint of the bolt 535 and drives the cleaning block 536 to be separated from the connecting frame 533, the cleaning block 536 can be replaced immediately, and by arranging the cleaning mechanism 53, the fingerprint identification area of the device can be cleaned after the identification is completed, so that the probability of fingerprint identification errors is reduced, and the stability of the fingerprint identification of the device is further improved.

Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for some of the features thereof, and any modifications, equivalents, improvements and the like made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.

Claims (10)

1. A digital electronic rain-increasing and trumpet-preventing rocket launching safety locker is characterized in that: the method comprises the following steps: the portable electronic device comprises a machine body (1), wherein a display (2) is fixedly connected to the inner wall of the machine body (1), a control panel (3) is fixedly connected to the side surface of the machine body (1), an indicator lamp (4) is fixedly connected to the inner wall of the machine body (1), the control panel (3) is electrically connected with the display (2), the indicator lamp (4) is electrically connected with the control panel (3), and a safety device (5) is arranged on the surface of the machine body (1);

the safety device (5) comprises a protection mechanism (51), the protection mechanism (51) is arranged on the side surface of the machine body (1), the safety device (5) comprises a driving mechanism (52), the driving mechanism (52) is arranged on the inner wall of the protection mechanism (51), the safety device (5) comprises a cleaning mechanism (53), 2, the cleaning mechanism (53) is arranged on the lower surface of the protection mechanism (51); protection machanism (51) are including support frame (511), the lower fixed surface of support frame (511) and fuselage (1) is connected, the side surface butt of support frame (511) has baffle (512), one side fixedly connected with sealing washer (513) that baffle (512) are close to fuselage (1), the side surface fixedly connected with buckle of baffle (512).

2. The digital electronic rain enhancement and trumpet launching safety locker of claim 1, characterized in that: the side surface fixedly connected with mount (515) of fuselage (1), the surperficial joint of mount (515) has damping piece (516), the lower fixed surface of support frame (511) is connected with identification panel (517), the inner wall fixed connection of support frame (511) has location card strip (518).

3. The digital electronic rain enhancement and trumpet launching safety locker of claim 1, characterized in that: baffle (512) and the side surface looks butt of fuselage (1), sealing washer (513) and control panel (3)'s surface looks butt, the quantity of detaining piece (514) is two, two detain piece (514) and be bilateral symmetry setting about baffle (512), detain the side surface looks butt of piece (514) and fuselage (1).

4. The digital electronic rainfall enhancement and campsis prevention rocket launching safety locker of claim 2, characterized by that: the quantity of mount (515) is two, two mount (515) are bilateral symmetry setting about fuselage (1), the catching groove has been seted up on the surface of knot piece (514), damping piece (516) and the inner wall looks joint of catching groove, damping piece (516) and the side surface looks butt of fuselage (1).

5. The digital electronic rain enhancement and trumpet launching safety locker of claim 2, characterized in that: the driving mechanism (52) comprises a data main board (521), the data main board (521) is fixedly connected with the inner wall of the support frame (511), the inner wall of the support frame (511) is fixedly connected with a fingerprint identifier (522), and the inner wall of the support frame (511) is fixedly connected with a transmission motor (523).

6. The digital electronic rain enhancement and trumpet launching safety locker of claim 5, characterized in that: the drive end fixedly connected with gear (524) of transmission motor (523), the inner wall rotation of support frame (511) is connected with ring gear (525), the inner wall fixedly connected with pivot (526) of ring gear (525), the side surface fixedly connected with constraint piece (527) of pivot (526).

7. The digital electronic rain enhancement and trumpet launching safety locker of claim 6, characterized in that: the data main board (521) is electrically connected with the fingerprint identifier (522), the fingerprint identifier (522) is abutted against the identification panel (517), the transmission motor (523) is electrically connected with the data main board (521), and the transmission motor (523) is abutted against the side surface of the positioning clamping strip (518).

8. The digital electronic rain enhancement and trumpet launching safety locker of claim 6, characterized in that: gear (524) and the tooth's socket of ring gear (525) mesh mutually, pivot (526) run through support frame (511) and set up, the assembly groove has been seted up to the side surface of baffle (512), pivot (526) and the inner wall looks butt in assembly groove, restraint piece (527) and the inner wall looks joint in assembly groove.

9. The digital electronic rainfall enhancement and campsis prevention rocket launching safety locker of claim 2, characterized by that: the cleaning mechanism (53) comprises a positioning sleeve (531), the positioning sleeve (531) is fixedly connected with the lower surface of the support frame (511), the inner wall of the positioning sleeve (531) is rotatably connected with a limiting shaft (532), the lower surface of the limiting shaft (532) is fixedly connected with a linking frame (533), the side surface of the linking frame (533) is abutted with a retaining ring (534), the surface of the retaining ring (534) is fixedly connected with a bolt (535), the inner wall of the retaining ring (534) is provided with a mounting groove, and the inner wall of the retaining ring (534) in the mounting groove is connected with a cleaning block (536).

10. The digital electronic rain enhancement and trumpet launching safety locker of claim 9, characterized in that: the multifunctional cleaning tool is characterized in that the connecting frame (533) is abutted against the lower surface of the support frame (511), a limiting hole is formed in the lower surface of the connecting frame (533), the bolts (535) are clamped with the inner wall of the limiting hole, the number of the bolts (535) is two, the two bolts (535) are symmetrically arranged in the left-right direction relative to the retaining ring (534), the cleaning block (536) is abutted against the inner wall of the connecting frame (533), and the cleaning block (536) is abutted against the surface of the identification panel (517).

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