CN215155769U - Multifunctional bullet hanging guarantee equipment - Google Patents
Multifunctional bullet hanging guarantee equipment Download PDFInfo
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- CN215155769U CN215155769U CN202120841659.5U CN202120841659U CN215155769U CN 215155769 U CN215155769 U CN 215155769U CN 202120841659 U CN202120841659 U CN 202120841659U CN 215155769 U CN215155769 U CN 215155769U
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Abstract
The utility model relates to a multifunctional bullet hanging support device, which comprises a front panel, a rear panel, a left closing plate and a right panel, wherein the front panel is provided with a laser and a radar sensing probe; the left sealing plate is provided with an SD manual lifting handle, an YL bullet hanging lifting device control area, an SD bullet hanging lifting device control area, a charging interface, a line change-over switch, an intelligent display screen, a charging state indication area and an alarm; the right panel is provided with an YL manual lifting handle and an embedded remote controller storage box; an YL missile placement posture universal device, an SD missile placement posture universal device and an emergency stop button are arranged above the device; the rear part of the device is provided with a PLC encoder, a battery box, a receiver and a controller. The YL hanging spring lifting device realizes the up-and-down lifting through an YL wired/wireless remote controller 8/5; the SD bullet hanging and lifting device realizes the up-and-down lifting through an SD wired/wireless remote control 9/5. The utility model has the advantages of small volume, small turning radius, flexible and convenient taking and transferring and wide application range.
Description
Technical Field
The utility model belongs to the technical field of hang bullet guarantee equipment, concretely relates to multi-functional bullet guarantee equipment of hanging.
Background
The bullet hanging protection equipment in the prior art has the following two problems:
1) after the lifting system is lifted, the space stability is poor, the personnel operation is complex, and the working efficiency is low;
2) the guarantee equipment is bulky, and the chassis is low, and the dead weight is great, and the transition degree of difficulty increases.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the above problem, provide a volume is less, turning radius is little, take the nimble convenient, the wide multi-functional bullet support equipment of hanging of accommodation of transition.
In order to achieve the above object, the utility model provides a following technical scheme:
a multifunctional bullet hanging guarantee device comprises a front panel, a rear panel, a left sealing plate and a right panel, and is characterized in that a laser and a radar sensing probe are arranged on the front panel; the left sealing plate is provided with an SD manual lifting handle, an YL bullet hanging lifting device control area, an SD bullet hanging lifting device control area, a charging interface, a line change-over switch, an intelligent display screen, a charging state indication area and an alarm; the right panel is provided with an YL manual lifting handle and an embedded remote controller storage box;
an YL missile placement posture universal device, an SD missile placement posture universal device and an emergency stop button are arranged above the device;
the rear part of the device is provided with a PLC encoder, a battery box, a receiver and a controller.
Further, the battery case includes battery clamp, power battery 1/2, battery stopper, I/O module.
Further, the YL hanging spring lifting device realizes the up-and-down lifting thereof through an YL wired/wireless remote controller 8/5; the SD bullet hanging and lifting device realizes the up-and-down lifting through an SD wired/wireless remote control 9/5.
Furthermore, the SD missile placement posture universal device and the YL missile placement posture universal device are respectively a platform bottom plate and a slider fixing plate arranged above the platform bottom plate, an upper moving base and a lower moving base, a first slider, a second slider, a first guide rail and a second guide rail are arranged above the platform bottom plate, the upper moving base is connected with the first slider and forms a certain moving range with the first guide rail, the first guide rail is connected with the lower moving base, and the upper moving base and the lower moving base form linear motion through the first slider and the first guide rail; the lower moving base is connected with the second guide rail and forms a certain moving range with the second sliding block, and the second sliding block is connected with the platform bottom plate; the upper moving base and the lower moving base are connected with a bullet supporting frame through turntable bearings, a turntable base bottom plate and a pitching swinging connecting block, rollers are arranged on a bullet supporting frame beam part above the bullet supporting frame, and bearings and bearing baffles are arranged on side plates of the bullet supporting frame.
Further, the roller and a roller shaft at the center of the roller are arranged on a bullet support vertical plate above the bullet support cross beam part, and the bullet support vertical plate and the bullet support cross beam part provide support for the bullet body; a quick positioning pin is arranged on one side of the bullet supporting frame, and a positioning pin fixing groove matched and connected with the quick positioning pin is arranged below the quick positioning pin; a guide rail shock pad is connected above the platform bottom plate, and an upper moving base limiting block and a lower moving base limiting block are respectively arranged between the upper moving base, the lower moving base and the platform bottom plate; the lower moving base and the platform form linear motion through a second sliding block and a second guide rail, the sliding distance is determined by the limiting block of the lower moving base and the effective length of the second guide rail, and the horizontal position of the projectile body is adjustable through the horizontal movement of the lower moving base; go up and remove base stopper and move base stopper bottom down and be equipped with respectively and move base stopper shock pad down.
Furthermore, pitching swinging movement with a deflection angle of 8 degrees is arranged between the pitching swinging connecting block and the bullet support frame beam component, angular deflection is generated between the upper component and the lower component through rotation of the turntable bearing, the turntable bearing is connected with the upper accessory and the lower accessory, 360-degree rotation without dead angles is realized, and angles in four directions of the horizontal plane of the bullet body are adjusted in real time.
Furthermore, the bottom of the bottom plate of the SD missile placement posture universal device platform is also provided with a fixed frame, and a servo motor and a speed reducer are arranged in the fixed frame.
Preferably, the charging interface adopts a clamshell structure.
Preferably, the laser is an infrared cross laser.
Preferably, the top of the bullet hanging protection device is provided with a wire control interface, and the bottom of the bullet hanging protection device is provided with four universal wheels.
Compared with the prior art, the beneficial effects of the utility model reside in that:
the utility model discloses it is spacing that equipment operating system elevating gear is equipped with four directions to elevating gear is the back and forth movement in the vertical direction, removes the process and can not squint, and the platform that rises is stable, reliable, and easy operation adopts wired/wireless operating handle to operate, and the quantity can be hung to the single nature is 2, improves work efficiency.
The equipment has the advantages of small volume, small turning radius, flexible and convenient field carrying and transition and wide application range.
The power supply system of the equipment adopts a principle of 'one-by-one' to ensure that a certain work (task) period is finished.
Drawings
In order to more clearly illustrate the technical solution of the embodiment of the present invention, the drawings required to be used in the description of the embodiment will be briefly introduced below, it is obvious that the drawings in the following description are only for more clearly illustrating the embodiment of the present invention or the technical solution in the prior art, and for those skilled in the art, other drawings can be obtained according to the drawings without any creative effort.
Fig. 1 is a left side view of the present invention;
FIG. 2 is a front view of the present invention;
fig. 3 is a right side view of the present invention;
fig. 4 is a top view of the present invention;
fig. 5 is a rear view of the present invention;
FIG. 6 is a diagram of the YL wired remote control of the present invention;
FIG. 7 is a structural diagram of the SD wired remote controller of the present invention;
fig. 8 is a diagram of the structure of the YL wireless remote controller of the present invention;
FIG. 9 is a structural diagram of the SD wireless remote controller of the present invention;
in the figure: a-a left sealing plate, B-a front panel, C-a right panel, a D-YL missile placement attitude universal device and an E-SD missile placement attitude universal device; 1-a guide rail shock pad, 2-a slider fixing plate, 3-an upper moving base stopper shock pad, 4-an upper moving base stopper, 5-an upper moving base, 6-a first slider, 7-a first guide rail, 8-a turntable bearing, 9-a turntable base bottom plate, 10-a pitching connecting block, 11-a carriage beam member, 12-a roller shaft, 13-a roller, 14-a bearing, 15-a lower moving base, 16-a bearing baffle, 17-a carriage riser, 18-a lower moving base stopper, 19-a quick positioning pin, 20-a positioning pin fixing groove, 21-a lower moving base stopper shock pad, 22-a second slider, 23-a second guide rail, 24-a platform bottom plate, 25-an SD manual lifting operation handle, 26-YL hanging bomb lifting device control area, 27-SD hanging bomb lifting device control area, 28-emergency stop button, 29-charging interface, 30-line change-over switch, 31-intelligent display screen, 32-charging state indication area, 33-alarm, 34-universal wheel, 35-infrared cross laser, 36-radar sensing probe, 39-YL manual lifting handle, 40-PLC encoder, 42-battery hoop, 43-power battery 1/2, 44-battery limiting block, 45-I/O module, 46-receiver, 47-controller, 48-YL wired remote controller, 49-SD wired remote controller, 51-embedded remote controller storage box, 52-YL wireless remote controller, 53-SD wireless remote controller, 54-servo motor, 55-reducer, 56-fixed frame.
Detailed Description
In order to make the technical solution of the present invention better understood by those skilled in the art, the present invention will be further described with reference to the following specific embodiments, which are provided as illustration only and are not intended to limit the present invention.
As shown in fig. 1-4, the multifunctional bullet hanging safeguard device includes a front panel B, a rear panel, a left sealing plate a and a right panel C, wherein a laser 35 and a radar sensing probe 36 are arranged on the front panel B; the left sealing plate A is provided with an SD manual lifting handle 25, an YL bullet hanging lifting device control area 26, an SD bullet hanging lifting device control area 27, a charging interface 29, a line change-over switch 30, an intelligent display screen 31, a charging state indication area 32 and an alarm 33; the right panel C is provided with an YL manual lifting handle 39 and an embedded remote controller storage box 51; the YL hanging spring lifting device realizes the up-and-down lifting through an YL wired/wireless remote controller 48/52; the SD bullet hanging and lifting device realizes the up-and-down lifting through an SD wired/wireless remote control 49/53.
An YL missile placement attitude universal device D, an SD missile placement attitude universal device E and an emergency stop button 28 are arranged above the device; the back of the device is provided with a PLC encoder 40, a battery box, a receiver 46 and a controller 47. The battery box comprises a battery hoop 42, a power battery 1/243, a battery limiting block 44 and an I/O module 45.
And (3) functional classification of ascending and descending of the projectile body:
manual operation: 1. the purpose of raising and lowering the projectile body can be achieved by clockwise/anticlockwise rotation of the SD manual operation handle 25;
electric driving: 1. the purposes of ascending and descending the projectile body can be realized through a servo motor system and a speed reducer;
2. the projectile body is supported in a four-point tangent structure mode, supporting points are tangent points of four rollers above the platform, namely tangent planes, and 360-degree rotation of the projectile body can be realized through supporting point support;
3. the ammunition supporting frame vertical plate 17 and the ammunition supporting frame beam part 11 provide effective stability for supporting the ammunition.
4. And a pitching swinging motion with an offset angle of 8 degrees is formed between the pitching swinging connecting block 10 and the bullet-supporting frame beam part 11. The rotation of the bearing 14 causes the upper and lower parts to swing angularly; the bearing baffle 16 limits the displacement of the bearing caused by axial force, and the integral adjustment of the front and back deflection of the projectile body is realized.
5. The turntable bearing 8 is connected with upper and lower accessories, so that 360-degree rotation without dead angles is realized, and angles in four directions of a horizontal plane of the projectile body are adjusted in real time.
6. The upper moving base 5 is connected with the first sliding block 6, a certain moving range is formed between the upper moving base 5 and the first guide rail 7, the first guide rail 7 is connected with the lower moving base 15, namely the upper moving base 5 and the lower moving base 15 form linear motion through the first sliding block 6 and the first guide rail 7, the sliding limit distance is determined by the effective length of the upper moving base limiting block 4, the upper moving base limiting fixing block and the first guide rail 7, and the longitudinal movement of the upper moving base 5 enables the longitudinal position of the projectile body to be adjustable.
7. The lower moving base 15 is connected with the second guide rail 23, a certain moving range is formed between the lower moving base 15 and the second sliding block 22, the second sliding block 22 is connected with the platform bottom plate 24, the guide rail shock pad 1 is connected with the platform bottom plate 24, namely the lower moving base 15 and the platform form linear motion through the second sliding block 22 and the second guide rail 23, the sliding distance is determined by the effective length of the lower moving base limiting block 18 and the effective length of the second guide rail 23, and the horizontal position of the projectile body is adjustable through the horizontal movement of the lower moving base 15.
The operation area is divided into two types: YL hanging bomb lifting device control area 26 and SD bomb body posture regulation area 27.
When no-load elastic body needs to be placed on the device, the quick positioning pin 19 needs to be inserted into the positioning pin fixing groove 20, and all the parallel components on the limiting device move and displace; only when the projectile needs to be adjusted, the quick positioning pin 19 is detached to adjust the position and posture of the projectile, and when the adjustment is not needed, the quick positioning pin 19 must be inserted into the positioning pin fixing groove 20.
4 universal casters 34 are arranged below the security equipment, so that the motion of the security equipment in four directions, namely front, back, left and right is realized.
Four emergency stop buttons 28 are arranged on the upper surface of the security equipment, and when an emergency occurs, any one of the emergency stop buttons 28 can be pressed nearby to stop the current operation task.
The right panel C is provided with an embedded wired/wireless remote controller storage box 51; the remote controller is stored when the equipment is used, so that the phenomenon of loss is prevented.
The front panel B is provided with an infrared cross laser 35, and when the equipment approaches the airplane for a certain distance, the equipment can be aligned according to the position of a cross cursor.
Front panel B is equipped with radar sensor 36, can respond to corresponding distance positional information when the assurance equipment is close the aircraft, and when the dangerous position, the assurance equipment takes place to report to the police, and alarm 33 sets up on left shrouding A.
The charging interface 29 adopts a flip structure, is dustproof and waterproof, and avoids short circuit caused by rainwater; during charging, the intelligent display screen 31 displays the electric quantity percentage and the voltage condition of the battery during charging, the intelligent display screen 31 has a charging compensation function, the battery can not feed electricity because of over charging or over discharging, and the buzzer is set by the alarm voltage. Parameters displayed during charging or heavy current discharging fluctuate with time; when the battery is low, the red lightning energy symbol of the display area can flash and give an alarm. An external NTC temperature detection sensor; the charging state and the full-charge state can also be confirmed by the corresponding indicator lamp.
The power supply of the guarantee equipment adopts a principle of one use and one standby, two sets of power supply sources are arranged, and the left sealing plate A is provided with a circuit change-over switch 30 to switch a main battery and a standby battery so as to ensure the completion of the guarantee task.
As shown in fig. 6 to 9, two specifications of a wired remote controller and a wireless remote controller are provided outside, and the two specifications are divided into two types according to different functions: namely an YL wired remote controller 48, an SD wired remote controller 49, an YL wireless remote controller 52, and an SD wireless remote controller 53. The SD multifunctional hanging bomb lifting device is lifted up and down by an SD wired/wireless remote controller 49/53, and the YL multifunctional hanging bomb lifting device is lifted up and down by an YL wired/wireless remote controller 48/52.
The SD missile placement posture universal device E and the YL missile placement posture universal device D are both a platform bottom plate 24 and a slider fixing plate 2 arranged above the platform bottom plate 24, an upper moving base and a lower moving base, a first slider, a second slider, a first guide rail and a second guide rail are arranged above the platform bottom plate 24, the upper moving base 5 is connected with the first slider 6, a certain moving range is formed between the upper moving base and the first guide rail 7, the first guide rail 7 is connected with the lower moving base 15, and the upper moving base 5 and the lower moving base 15 form linear motion through the first slider 6 and the first guide rail 7; the lower moving base 15 is connected with a second guide rail 23, a certain moving range is formed between the lower moving base and a second sliding block 22, and the second sliding block 22 is connected with a platform bottom plate 24; the upper portion of the upper moving base 5 and the upper portion of the lower moving base 15 are connected with a bullet supporting frame through a turntable bearing 8, a turntable base bottom plate 9 and a pitching swinging connecting block 10, rollers 13 are arranged on a bullet supporting frame beam part 11 above the bullet supporting frame, and a bearing 14 and a bearing baffle 16 are arranged on a side plate of the bullet supporting frame. The bottom of the platform bottom plate 24 of the SD missile placement attitude universal device E is further provided with a fixed frame 56, and a servo motor 54 and a speed reducer 55 are arranged in the fixed frame 56. The top of the bullet hanging guarantee equipment is provided with a wire control interface 50, and the bottom of the bullet hanging guarantee equipment is provided with four universal wheels 34.
The roller 13 and the roller shaft 12 at the center thereof are arranged on a bullet-supporting frame vertical plate 17 above the bullet-supporting frame beam part 11, and the bullet-supporting frame vertical plate 17 and the bullet-supporting frame beam part 11 provide support for a bullet body; a quick positioning pin 19 is arranged on one side of the bullet supporting frame, and a positioning pin fixing groove 20 which is matched and connected with the quick positioning pin 19 is arranged below the quick positioning pin 19; a guide rail shock pad 1 is connected above the platform bottom plate 24, and an upper moving base limiting block 4 and a lower moving base limiting block 18 are respectively arranged between the upper moving base 5, the lower moving base 15 and the platform bottom plate 24; the lower moving base 15 and the platform form a linear motion through a second sliding block 22 and a second guide rail 23, the sliding distance is determined by the effective lengths of the lower moving base limiting block 18 and the second guide rail 23, and the horizontal position of the projectile body is adjustable through the horizontal movement of the lower moving base 15; the bottoms of the upper moving base limiting block 4 and the lower moving base limiting block 18 are respectively provided with an upper moving base limiting block damping pad 3 and a lower moving base limiting block damping pad 21.
Pitching swinging movement with a deflection angle of 8 degrees is arranged between the pitching swinging connecting block 10 and the bullet supporting frame beam part 11, angular deflection is generated between an upper part and a lower part through rotation of the turntable bearing 8, the turntable bearing 8 is connected with an upper accessory and a lower accessory, 360-degree rotation without dead angles is realized, and angles in four directions of a horizontal plane of a bullet body are adjusted in real time.
The utility model discloses it is spacing that equipment operating system elevating gear is equipped with four directions to elevating gear is the back and forth movement in the vertical direction, removes the process and can not squint, and the platform that rises is stable, reliable, and easy operation adopts wired/wireless operating handle to operate, and the quantity can be hung to the single nature is 2, improves work efficiency.
The equipment has the advantages of small volume, small turning radius, flexible and convenient field carrying and transition and wide application range.
The power supply system of the equipment adopts the principle of 'using one for one' and ensuring that a certain work (task) period is finished.
The present invention is not described in detail in the prior art.
The above description is only a preferred embodiment of the present invention, and should not be taken as limiting the invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (10)
1. A multifunctional bullet hanging guarantee device comprises a front panel (B), a rear panel, a left sealing plate (A) and a right panel (C), and is characterized in that a laser (35) and a radar sensing probe (36) are arranged on the front panel (B); the left sealing plate (A) is provided with an SD manual lifting handle (25), an YL bullet hanging lifting device control area (26), an SD bullet hanging lifting device control area (27), a charging interface (29), a line change-over switch (30), an intelligent display screen (31), a charging state indication area (32) and an alarm (33); an YL manual lifting handle (39) and an embedded remote controller storage box (51) are arranged on the right panel (C);
an YL missile placing posture universal device (D), an SD missile placing posture universal device (E) and an emergency stop button (28) are arranged above the equipment;
the back of the device is provided with a PLC encoder (40), a battery box, a receiver (46) and a controller (47).
2. The multifunctional hanging bomb security device of claim 1, wherein the battery box comprises a battery clamp (42), a power battery 1/2(43), a battery stopper (44), and an I/O module (45).
3. The multifunctional hanging bomb safeguard equipment as claimed in claim 1, wherein the YL hanging bomb lifting device is lifted up and down by a YL wired/wireless remote controller (48/52); the SD bullet hanging lifting device realizes the up-and-down lifting through an SD wired/wireless remote controller (49/53).
4. The multifunctional missile hanging guarantee equipment according to claim 1, wherein the SD missile placing posture universal device (E) and the YL missile placing posture universal device (D) are respectively a platform bottom plate (24) and a slider fixing plate (2) arranged above the platform bottom plate, an upper moving base, a lower moving base, a first slider, a second slider, a first guide rail and a second guide rail are arranged above the platform bottom plate (24), the upper moving base (5) is connected with the first slider (6) and forms a certain moving range with the first guide rail (7), the first guide rail (7) is connected with the lower moving base (15), and the upper moving base (5) and the lower moving base (15) form linear motion through the first slider (6) and the first guide rail (7); the lower moving base (15) is connected with a second guide rail (23) and forms a certain moving range with a second sliding block (22), and the second sliding block (22) is connected with a platform bottom plate (24); the upper moving base (5) and the lower moving base (15) are connected with a bullet supporting frame through a turntable bearing (8), a turntable base bottom plate (9) and a pitching swinging connecting block (10), rollers (13) are arranged on a bullet supporting frame beam part (11) above the bullet supporting frame, and a bearing (14) and a bearing baffle (16) are arranged on a side plate of the bullet supporting frame.
5. The multifunctional ammunition hanging support equipment as claimed in claim 4, wherein the roller (13) and the roller shaft (12) at the center of the roller are mounted on a ammunition carrier vertical plate (17) above a ammunition carrier transverse beam part (11), and the ammunition carrier vertical plate (17) and the ammunition carrier transverse beam part (11) provide support for ammunition bodies; a quick positioning pin (19) is arranged on one side of the bullet supporting frame, and a positioning pin fixing groove (20) which is matched and connected with the quick positioning pin (19) is arranged below the quick positioning pin (19); a guide rail shock pad (1) is connected above the platform bottom plate (24), and an upper moving base limiting block (4) and a lower moving base limiting block (18) are respectively arranged between the upper moving base (5), the lower moving base (15) and the platform bottom plate (24); the lower moving base (15) and the platform form linear motion through a second sliding block (22) and a second guide rail (23), the sliding distance is determined by the effective lengths of a lower moving base limiting block (18) and the second guide rail (23), and the horizontal position of the projectile body is adjustable through the horizontal movement of the lower moving base (15); the bottoms of the upper moving base limiting block (4) and the lower moving base limiting block (18) are respectively provided with an upper moving base limiting block shock pad (3) and a lower moving base limiting block shock pad (21).
6. The multifunctional missile hanging support device according to claim 4, wherein a pitching swinging motion with a deflection angle of 8 degrees is formed between the pitching swinging connecting block (10) and the missile supporting frame beam part (11), an angle deflection is generated between the upper part and the lower part through rotation of the turntable bearing (8), the turntable bearing (8) is connected with the upper part and the lower part, 360-degree rotation without dead angles is realized, and four direction angles of a horizontal plane of a missile body are adjusted in real time.
7. The multifunctional missile hooking and ensuring equipment according to claim 4, wherein the bottom of the platform bottom plate (24) of the SD missile placing posture universal device (E) is further provided with a fixed frame (56), and a servo motor (54) and a speed reducer (55) are arranged in the fixed frame (56).
8. The multifunctional hanging ammunition security device as claimed in claim 1, wherein the charging interface (29) is of a clamshell type structure.
9. A multifunctional hanging ammunition security device according to claim 1, characterized in that the laser (35) is an infrared cross laser.
10. The multifunctional hanging and bullet ensuring device as claimed in any one of claims 1 to 9, wherein the hanging and bullet ensuring device is provided with a wire control interface (50) at the top and four universal wheels (34) at the bottom.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120841659.5U CN215155769U (en) | 2021-04-23 | 2021-04-23 | Multifunctional bullet hanging guarantee equipment |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120841659.5U CN215155769U (en) | 2021-04-23 | 2021-04-23 | Multifunctional bullet hanging guarantee equipment |
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| CN215155769U true CN215155769U (en) | 2021-12-14 |
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| CN202120841659.5U Active CN215155769U (en) | 2021-04-23 | 2021-04-23 | Multifunctional bullet hanging guarantee equipment |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114455093A (en) * | 2022-04-13 | 2022-05-10 | 北京航天和兴科技股份有限公司 | Guided missile hanger device |
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2021
- 2021-04-23 CN CN202120841659.5U patent/CN215155769U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114455093A (en) * | 2022-04-13 | 2022-05-10 | 北京航天和兴科技股份有限公司 | Guided missile hanger device |
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