CN115615247A - A digital electronic rain-enhancing anti-overhead rocket launch safety locker - Google Patents

Abstract

The invention discloses a digital electronic rain-increasing anti-overhead rocket launch safety locker, which comprises: a fuselage, a display is fixedly connected to the inner wall of the fuselage, a control panel is fixedly connected to the side surface of the fuselage, and a control panel is fixedly connected to the inner wall of the fuselage. The indicator light, the control panel is electrically connected to the display, the indicator light is electrically connected to the control panel, a safety device is provided on the surface of the fuselage, the safety device includes a protective mechanism, the protective mechanism is arranged on the side surface of the fuselage, the safety device includes a driving mechanism, and the driving mechanism The mechanism is set on the inner wall of the protection mechanism. The safety device includes a cleaning mechanism, which uses multiple structural components in the protection mechanism to continuously protect the device control button. Because the device control button is not directly exposed to the outside after being protected, it makes non-professional It is difficult for operators to operate through the equipment, which provides support for the safety of the equipment and realizes the ability of the equipment to seal and protect the control panel.

Description

A digital electronic rain-enhancing anti-overhead rocket launch safety locker

technical field

The invention relates to the technical field of rocket control equipment, in particular to a digital electronic rain-enhancing anti-overhead rocket launch safety locker.

Background technique

The method of artificial rainfall enhancement is a method of appropriately increasing or redistributing precipitation by using spreading technology for certain types of cloud systems and storm systems. Stoves, flame bombs and other tools send catalysts such as silver iodide and dry ice into the supercooled part of the cloud, increasing ice crystals and condensation nuclei in the cloud, causing more water vapor to form raindrops and fall to the ground. Strong catalysts (such as salt, calcium chloride, calcium oxide, urea, ammonium nitrate, etc.) promote cloud droplets to grow into raindrops, increasing the amount of precipitation. In addition, when rockets, antiaircraft guns and flame bombs explode in the cloud Shock waves are generated, which can accelerate the collision process between cloud droplets and cloud droplets, and merge and increase into raindrops to fall down, which plays a role in increasing rainfall; and due to the high launch altitude of the rocket, it is more suitable for areas with lower altitudes or higher zero-degree altitudes Therefore, whether it is in the south or the north of China, rocket operation systems are widely used in artificial rainfall enhancement operations, and rockets are used to sow artificial ice nuclei in the operation area. The monthly average isotherm of the local operation period -6~-12°C should be calculated in advance. The average height of the rocket is used as a reference for the rocket flame spreading level. At this time, the latent heat effect should also be considered. The temperature in the cloud (updraft area) is generally slightly higher than the ambient temperature.

The launch methods of rain-increasing rockets can be divided into: plane shooting: when the cumuliform cloud has a large horizontal scale, a small vertical scale, and weak updraft in the cloud, the plane shooting method is used to carry the silver iodide particles evenly The best catalytic height in the cloud layer enables the catalyst to act on a wide range of horizontal planes to achieve the maximum rain-enhancing effect; Trapezoidal shooting method, this three-dimensional shooting method uses different shooting angles and different orientations to bring silver iodide particles to different heights in the cloud layer, so that the catalyst can act on a large vertical surface to achieve maximum Rain effect.

However, the existing processing equipment has the following disadvantages:

In daily use, the rocket safety locker such as CN112540562A is found. Most of the existing equipment uses buttons as the main structure of the control panel. During the use of the equipment, the buttons of the equipment are mostly exposed to the air. The control panel is exposed and easy to be pressed and manipulated by non-professionals, which reduces the safety of the equipment during use.

So we have proposed a kind of digital electronic rain-enhancing anti-skyrocket launching safety locker, so that solve the problem mentioned above.

Contents of the invention

The purpose of the present invention is to provide a digital electronic rain-increasing anti-skyrocket launch safety locker, through the protective mechanism connected to the fuselage, using multiple structural components in the mechanism to continuously protect the equipment control button position, due to equipment control After the button is protected, it is not directly exposed to the outside world, making it difficult for non-professional operators to operate through the device, providing support for the safety of the device, and realizing the ability of the device to seal and protect the control panel to solve the above background technology. The problem.

In order to achieve the above object, the present invention provides the following technical solutions: a digital electronic rain-increasing anti-overhead rocket launch safety locker, comprising: a fuselage, the inner wall of the fuselage is fixedly connected with a display, and the side surface of the fuselage is fixed A control panel is connected, an indicator light is fixedly connected to the inner wall of the fuselage, the control panel is electrically connected to the display, the indicator light is electrically connected to the control panel, and a safety device is provided on the surface of the fuselage;

The safety device includes a protection mechanism arranged on the side surface of the fuselage, the safety device includes a driving mechanism arranged on the inner wall of the protection mechanism, and the safety device includes a cleaning mechanism. The cleaning mechanism is arranged on the lower surface of the protection mechanism;

The protection mechanism includes a support frame, the support frame is fixedly connected to the lower surface of the fuselage, the side surface of the support frame is abutted with a baffle plate, and the side of the baffle plate close to the fuselage is fixedly connected with a sealing ring, The side surface of the baffle is fixedly connected with buckles, and multiple structural components in the mechanism are used to continuously protect the device control button. Because the device control button is not directly exposed to the outside world after being protected, non-professional operators It is difficult to operate through the equipment, providing support for the safety of the equipment, and realizing the ability of the equipment to seal and protect the control panel.

Preferably, the side surface of the fuselage is fixedly connected with a fixing frame, the surface of the fixing frame is clamped with a damping block, the lower surface of the supporting frame is fixedly connected with an identification panel, and the inner wall of the supporting frame is fixedly connected with The positioning clips can constrain the closed state of the baffle by the cooperation of the damping block and the buckle block.

Preferably, the baffle is in contact with the side surface of the fuselage, the sealing ring is in contact with the surface of the control panel, the number of the buckle blocks is two, and the two buckle blocks are left-right symmetrical with respect to the baffle It is provided that the buckle block abuts against the side surface of the fuselage, and the control panel can be closed by using the baffle to avoid operation by non-professionals.

Preferably, the number of the fixing brackets is two, and the two fixing brackets are symmetrically arranged about the fuselage, the surface of the buckle block is provided with a buckle groove, and the damping block is engaged with the inner wall of the buckle groove , the damping block abuts against the side surface of the fuselage, and the position of the damping block can be supported and fixed by the fixing frame to realize the constraint effect of the damping block.

Preferably, the drive mechanism includes a data mainboard, the data mainboard is fixedly connected to the inner wall of the supporting frame, the inner wall of the supporting frame is fixedly connected to a fingerprint reader, and the inner wall of the supporting frame is fixedly connected to a transmission motor, and the The cooperation between the identifier and the data mainboard can identify and store the fingerprint data of the operator.

Preferably, the driving end of the transmission motor is fixedly connected with a gear, the inner wall of the support frame is rotatably connected with a gear ring, the inner wall of the gear ring is fixedly connected with a rotating shaft, and the side surface of the rotating shaft is fixedly connected with a restraint block, The position of the baffle can be limited by the cooperation of the restraining block and the rotating shaft.

Preferably, the data mainboard is electrically connected to the fingerprint reader, the fingerprint reader is in contact with the identification panel, the transmission motor is electrically connected to the data mainboard, and the transmission motor is in contact with the side surface of the positioning bar. The gear ring can be driven by the cooperation of the transmission motor and the gear.

Preferably, the gear meshes with the tooth groove of the gear ring, the rotating shaft is arranged through the support frame, the side surface of the baffle is provided with an assembly groove, the rotating shaft abuts against the inner wall of the assembly groove, and the binding block It is clamped with the inner wall of the assembly groove, and the position of the rotating shaft can be constrained by the cooperation of the restraining block and the baffle.

Preferably, the cleaning mechanism includes a positioning sleeve, the positioning sleeve is fixedly connected to the lower surface of the support frame, the inner wall of the positioning sleeve is rotatably connected to a limiting shaft, and the lower surface of the limiting shaft is fixedly connected to a An adapter frame, the side surface of the adapter frame is abutted with a clasp, the surface of the clasp is fixedly connected with a latch, the inner wall of the clasp is provided with a mounting groove, and the clasp is located on the inner wall of the mounting groove and snapped with a The cleaning block can limit the position of the adapter frame by using the positioning sleeve and the limit shaft, and can restrain the rotation axis of the adapter frame at the same time.

Preferably, the adapter frame abuts against the lower surface of the support frame, and the lower surface of the adapter frame is provided with a limit hole, and the pin is engaged with the inner wall of the limit hole, and the number of the pins is two. The two pins are symmetrically arranged with respect to the buckle, the cleaning block abuts against the inner wall of the connecting frame, the cleaning block abuts against the surface of the identification panel, and the cleaning block is fixed on the joint by the cooperation of the pin and the buckle. inside the shelf.

Compared with prior art, the beneficial effect of the present invention is:

1. In the present invention, when rocket control is carried out by setting up a protective mechanism, the rocket launch parameters are set through the control panel, and the set parameters are displayed through the display. After the equipment is completed, the rocket launch can be carried out. Before operating the control panel, the designated operator will The unlocking finger is placed on the identification panel, and the drive mechanism drives the baffle after passing the identification. The blocking of the baffle is exposed, and then the equipment can be manipulated. By setting the protective mechanism, the control button of the equipment can be closed, thereby avoiding the problem of non-professionals operating the equipment, and further improving the safety of the equipment.

2. In the present invention, by setting the driving mechanism, when the designated operator's finger is placed on the identification panel, the fingerprint reader will identify the fingerprint and compare the fingerprint with the fingerprint data in the data main board. After the comparison is passed, the data main board Turn on the transmission motor, the transmission motor is energized to drive the gear, the gear drives the gear ring, the gear ring drives the rotating shaft, the rotation drives the restraint block, the restraint block drives the baffle to unfold, and then the deployment of the baffle is completed. By setting the drive mechanism, the protection mechanism needs It is unfolded under the fingerprint of the designated person, thereby reducing the probability of the protective mechanism being deployed by non-professionals, and improving the protection of the protective mechanism.

3. In the present invention, by setting the cleaning mechanism, after the fingerprint identification of the personnel is completed, the connecting frame is moved, the connecting frame drives the buckle, the buckle drives the cleaning block, the cleaning block moves and wipes the fingerprints remaining on the surface of the identification panel, and cleaning is required. When replacing the block, move the buckle downward, the buckle pulls the pin, the pin is forced out of the limit hole, the buckle loses the restraint of the pin and drives the cleaning block out of the connecting frame, and then the cleaning block can be replaced. The cleaning mechanism enables the fingerprint identification area of the device to be cleaned after the identification is completed, thereby reducing the probability of fingerprint identification errors and further improving the stability of fingerprint identification of the device.

Description of drawings

Fig. 1 is a three-dimensional view of the front view structure in a kind of digital electronic rain-enhancing and skyrocket-proof rocket launching safety locker of the present invention;

Fig. 2 is a three-dimensional view of the looking-up structure in a digital electronic rain-enhancing and skyrocket-proof rocket launching safety locker of the present invention;

Fig. 3 is a three-dimensional view of a cut-away structure of a digital electronic rain-enhancing anti-overhead rocket launching safety locker of the present invention;

Fig. 4 is a kind of digital electronic rain-increasing anti-overhead rocket launching safety locker of the present invention is the enlarged perspective view of the structure at A in Fig. 3;

Fig. 5 is an enlarged perspective view of the structure of the protection mechanism in a digital electronic rain-enhancing anti-overhead rocket launching safety locker of the present invention;

Fig. 6 is a digital electronic rain-increasing anti-overhead rocket launch safety locker of the present invention, which is an enlarged perspective view of the structure at B in Fig. 5;

Fig. 7 is an enlarged perspective view of the structure of the driving mechanism in a digital electronic rain-enhancing anti-overhead rocket launching safety locker of the present invention;

Fig. 8 is an enlarged perspective view of the structure of the cleaning mechanism in a digital electronic rain-increasing anti-overhead rocket launch safety locker of the present invention.

In the figure: 1. fuselage; 2. display; 3. control panel; 4. indicator light; 5. safety device; 51. protective mechanism; 511. support frame; 512. baffle; 515, fixed frame; 516, damping block; 517, identification panel; 518, positioning bar; 52, driving mechanism; 521, data main board; Gear ring; 526, rotating shaft; 527, binding block; 53, cleaning mechanism; 531, positioning sleeve; 532, limit shaft; 533, connecting frame; 534, clasp;

detailed description

The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described implementation regulations are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

Please refer to Figures 1-8, the present invention provides a technical solution: a digital electronic rain-enhancing anti-overhead rocket launch safety locker, comprising: a fuselage 1, the inner wall of the fuselage 1 is fixedly connected with a display 2, the fuselage The side surface of 1 is fixedly connected with a control panel 3, the inner wall of the fuselage 1 is fixedly connected with an indicator light 4, the control panel 3 is electrically connected with the display 2, the indicator light 4 is electrically connected with the control panel 3, and the surface of the fuselage 1 is provided with a safety Device 5, safety device 5 includes protection mechanism 51, and protection mechanism 51 is arranged on the side surface of fuselage 1, and safety device 5 includes drive mechanism 52, and drive mechanism 52 is arranged on the inner wall of protection mechanism 51, and safety device 5 includes cleaning mechanism 53. The cleaning mechanism 53 is arranged on the lower surface of the protection mechanism 51 .

As shown in Figures 5-6, the protection mechanism 51 includes a support frame 511, which is fixedly connected to the lower surface of the fuselage 1, and the side surface of the support frame 511 abuts against a baffle 512, which is close to the bottom of the fuselage 1. One side is fixedly connected with a sealing ring 513, and the side surface of the baffle 512 is fixedly connected with buckles. Multiple structural components in the mechanism are used to continuously protect the device control button, because the device control button is not directly exposed after being protected. In the outside world, it makes it difficult for non-professional operators to operate through the equipment, providing support for the safety of the equipment, and realizing the ability of the equipment to seal and protect the control panel.

As shown in Figures 5-6, the side surface of the fuselage 1 is fixedly connected with a fixed frame 515, the surface of the fixed frame 515 is clamped with a damping block 516, the lower surface of the support frame 511 is fixedly connected with an identification panel 517, and the support frame 511 The inner wall is fixedly connected with a positioning clip 518 , and the closed state of the baffle 512 can be constrained by the cooperation of the damping block 516 and the buckle block 514 .

As shown in Figures 5-6, the baffle 512 is in contact with the side surface of the fuselage 1, the sealing ring 513 is in contact with the surface of the control panel 3, and the number of buckle blocks 514 is two, and the two buckle blocks 514 are connected to the baffle plate 512 is arranged symmetrically on the left and right, and the buckle 514 abuts against the side surface of the fuselage 1 , and the control panel 3 can be closed by the baffle 512 to avoid operation by non-professionals.

As shown in Figures 5-6, there are two fixed mounts 515, and the two fixed mounts 515 are symmetrically arranged with respect to the fuselage 1. The surface of the buckle block 514 is provided with a buckle groove, and the damping block 516 is in contact with the inner wall of the buckle groove. Clamping, the damping block 516 abuts against the side surface of the fuselage 1 , and the position of the damping block 516 can be supported and fixed by the fixing frame 515 to realize the constraint effect of the damping block 516 .

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

As shown in FIG. 7 , the driving end of the transmission motor 523 is fixedly connected with a gear 524 , the inner wall of the support frame 511 is rotatably connected with a gear ring 525 , the inner wall of the gear ring 525 is fixedly connected with a rotating shaft 526 , and the side surface of the rotating shaft 526 is fixedly connected with a shackle. Block 527 , the position of the baffle 512 can be limited by the cooperation of the binding block 527 and the rotating shaft 526 .

As shown in Figure 7, the data mainboard 521 is electrically connected to the fingerprint reader 522, the fingerprint reader 522 is in contact with the identification panel 517, the transmission motor 523 is electrically connected to the data mainboard 521, and the transmission motor 523 is in contact with the side surface of the positioning bar 518 Then, the gear ring 525 can be driven by the cooperation of the transmission motor 523 and the gear 524 .

As shown in Figure 7, the gear 524 meshes with the tooth groove of the gear ring 525, the rotating shaft 526 is set through the support frame 511, the side surface of the baffle plate 512 is provided with an assembly groove, the rotating shaft 526 is in contact with the inner wall of the assembly groove, and the binding block 527 The position of the rotating shaft 526 can be constrained by the cooperation of the binding block 527 and the baffle plate 512 by engaging with the inner wall of the assembly groove.

As shown in Figure 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 the limit shaft 532, and the lower surface of the limit shaft 532 is fixed. An adapter frame 533 is connected, the side surface of the adapter frame 533 is abutted with a clasp 534, the surface of the clasp 534 is fixedly connected with a latch 535, and the inner wall of the clasp 534 is provided with a mounting groove, and the clasp 534 is located on the inner wall of the mounting groove and snapped into place. There is a cleaning block 536, the position of the adapter frame 533 can be limited by the positioning sleeve 531 and the limit shaft 532, and the center of the rotation axis 526 of the adapter frame 533 can be restricted at the same time.

As shown in Figure 8, the connecting frame 533 abuts against the lower surface of the support frame 511, the lower surface of the connecting frame 533 is provided with a limiting hole, and the latch 535 is engaged with the inner wall of the limiting hole, and the number of the latch 535 is two. The two bolts 535 are left and right symmetrically arranged with respect to the buckle 534, the cleaning block 536 abuts against the inner wall of the connecting frame 533, the cleaning block 536 abuts against the surface of the identification panel 517, and the cleaning block 536 is abutted against the surface of the identification panel 517 by cooperation of the bolt 535 and the buckle 534. fixed in the adapter frame 533.

The effect achieved by the whole mechanism is: when performing rocket control, the rocket launch parameters are set through the control panel 3, and the set parameters are displayed on the display 2. After the equipment is completed, the rocket launch can be carried out. Before operating the control panel 3, the The unlocking finger of the designated operator is placed on the identification panel 517, and the driving mechanism 52 drives the baffle 512 after the recognition passes, the baffle 512 drives the buckle 514, the buckle 514 is driven away from the damping block 516, the baffle 512 is driven to expand, and the sealing ring 513 Driven by the baffle 512, the control panel 3 is separated from the control panel 3. At the same time, the control panel 3 loses the blocking of the baffle 512 and is exposed, and then the equipment can be controlled. By setting the protection mechanism 51, the equipment can close the control button, thereby avoiding non-professional The problem of personnel operating the equipment and further improving the safety of the equipment;

At the same time, by setting the drive mechanism 52, when the designated operator's finger is placed on the identification panel 517, the fingerprint reader 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 The main board 521 turns on the transmission motor 523, the transmission motor 523 is energized to drive the gear 524, the gear 524 drives the gear ring 525, the gear ring 525 drives the rotating shaft 526, and the rotation drives the binding block 527, which drives the baffle 512 to unfold, and then the baffle 512 is completed. The deployment operation, by setting the drive mechanism 52, the protection mechanism 51 needs to be deployed under the fingerprint of the designated person, thereby reducing the probability that the protection mechanism 51 is deployed by non-professionals, and improving the protection of the protection mechanism 51;

In addition, by setting the cleaning mechanism 53, after the personnel fingerprint identification is completed, the connecting frame 533 is moved, the connecting frame 533 drives the buckle 534, the buckle block 514 drives the cleaning block 536, and the cleaning block 536 moves and removes the residual fingerprint on the identification panel 517 surface. Wipe, when the cleaning block 536 needs to be replaced, move the buckle 534 downward, the buckle 534 pulls the pin 535, the pin 535 is forced out of the limit hole, the buckle 534 loses the constraint of the pin 535 and drives the cleaning block 536 to disengage Then the cleaning block 536 can be replaced. By setting the cleaning mechanism 53, the fingerprint recognition area of the device can be cleaned after the recognition is completed, thereby reducing the probability of fingerprint recognition errors and further improving the stability of fingerprint recognition of the device. sex.

Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art can still modify the technical solutions described in the aforementioned embodiments, or perform equivalent replacements for some of the technical features. Within the spirit and principles of the present invention, any modifications, equivalent replacements, improvements, etc., shall be included in the protection scope of the present invention.

Claims (10)

1. A digital electronic rain-increasing anti-skyrocket launch safety locker, characterized in that it includes: a fuselage (1), the inner wall of the fuselage (1) is fixedly connected with a display (2), and the fuselage ( The side surface of 1) is fixedly connected with a control panel (3), the inner wall of the fuselage (1) is fixedly connected with an indicator light (4), the control panel (3) is electrically connected with the display (2), and the indicator The lamp (4) is electrically connected to the control panel (3), and the surface of the fuselage (1) is provided with a safety device (5); The safety device (5) includes a protection mechanism (51), the protection mechanism (51) is arranged on the side surface of the fuselage (1), the safety device (5) includes a driving mechanism (52), and the driving mechanism (52) is set on the inner wall of the protection mechanism (51), and the safety device (5) includes a cleaning mechanism (53), 2. The cleaning mechanism (53) is set on the lower surface of the protection mechanism (51); the protection The mechanism (51) includes a support frame (511), the support frame (511) is fixedly connected to the lower surface of the fuselage (1), and the side surface of the support frame (511) is abutted against a baffle plate (512), so A sealing ring (513) is fixedly connected to the side of the baffle (512) close to the fuselage (1), and a buckle is fixedly connected to the side surface of the baffle (512). 2. The digital electronic rain-increasing anti-skyrocket launch safety locker according to claim 1, characterized in that: the side surface of the fuselage (1) is fixedly connected with a fixing frame (515), and the fixing frame (515 ) is clamped with a damping block (516), the lower surface of the support frame (511) is fixedly connected with an identification panel (517), and the inner wall of the support frame (511) is fixedly connected with a positioning clip (518). 3. The digital electronic rain-increasing anti-skyrocket safety locker according to claim 1, characterized in that: the baffle (512) abuts against the side surface of the fuselage (1), and the sealing ring (513 ) is in contact with the surface of the control panel (3), the number of the buckle blocks (514) is two, and the two buckle blocks (514) are left and right symmetrically arranged with respect to the baffle (512), and the buckle blocks ( 514) abuts against the side surface of the fuselage (1). 4. The digital electronic rain-increasing anti-skyrocket launch safety locker according to claim 2, characterized in that: the number of the fixing frames (515) is two, and the two fixing frames (515) are about the fuselage (1) It is symmetrically arranged on the left and right. The surface of the buckle block (514) is provided with a buckle groove, and the damper block (516) is engaged with the inner wall of the buckle groove. ) are in contact with the side surfaces. 5. The digital electronic rain-increasing anti-skid rocket launch safety locker according to claim 2, characterized in that: the driving mechanism (52) includes a data main board (521), and the data main board (521) is connected to the support frame ( 511) is fixedly connected to the inner wall, the fingerprint reader (522) is fixedly connected to the inner wall of the support frame (511), and the transmission motor (523) is fixedly connected to the inner wall of the support frame (511). 6. The digital electronic rain-increasing anti-overhead rocket launch safety locker according to claim 5, characterized in that: the driving end of the transmission motor (523) is fixedly connected with a gear (524), and the support frame (511) The inner wall of the gear ring (525) is rotatably connected with a gear ring (525), the inner wall of the gear ring (525) is fixedly connected with a rotating shaft (526), and the side surface of the rotating shaft (526) is fixedly connected with a binding block (527). 7. The digital electronic rain-increasing and skyrocket launch safety locker according to claim 6, characterized in that: the data mainboard (521) is electrically connected to the fingerprint reader (522), and the fingerprint reader (522) It abuts against the identification panel (517), the transmission motor (523) is electrically connected to the data mainboard (521), and the transmission motor (523) abuts against the side surface of the positioning clip (518). 8. The digital electronic rain-increasing and skyrocket launch safety locker according to claim 6, characterized in that: the gear (524) meshes with the tooth groove of the gear ring (525), and the rotating shaft (526) runs through The support frame (511) is set, the side surface of the baffle (512) is provided with an assembly groove, the rotating shaft (526) is in contact with the inner wall of the assembly groove, and the binding block (527) is locked with the inner wall of the assembly groove catch. 9. The digital electronic rain-increasing anti-skid rocket launch safety locker according to claim 2, characterized in that: the cleaning mechanism (53) includes a positioning sleeve (531), and the positioning sleeve (531) is connected to the support The lower surface of the frame (511) is fixedly connected, the inner wall of the positioning sleeve (531) is rotatably connected with the limit shaft (532), and the lower surface of the limit shaft (532) is fixedly connected with the connecting frame (533). The side surface of the connecting frame (533) is abutted with a clasp (534), the surface of the clasp (534) is fixedly connected with a pin (535), and the inner wall of the clasp (534) is provided with a mounting groove. The clasp (534) is located on the inner wall of the installation groove and is snapped with a cleaning block (536). 10. The digital electronic rain-increasing anti-skyrocket safety locker according to claim 9, characterized in that: the adapter frame (533) abuts against the lower surface of the support frame (511), and the adapter frame (533 ) is provided with a limit hole on the lower surface, and the pin (535) is engaged with the inner wall of the limit hole. The number of the pin (535) is two. ) are symmetrically arranged left and right, the cleaning block (536) abuts against the inner wall of the connecting frame (533), and the cleaning block (536) abuts against the surface of the identification panel (517).

Images