CN211893653U - Broken glass ball launching mechanism of pneumatic type based on unmanned aerial vehicle - Google Patents
Broken glass ball launching mechanism of pneumatic type based on unmanned aerial vehicle Download PDFInfo
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- CN211893653U CN211893653U CN202020105595.8U CN202020105595U CN211893653U CN 211893653 U CN211893653 U CN 211893653U CN 202020105595 U CN202020105595 U CN 202020105595U CN 211893653 U CN211893653 U CN 211893653U
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Abstract
The utility model relates to a broken glass bulb emitter, in particular to broken glass bulb emitter of pneumatic type based on unmanned aerial vehicle constructs, including the transmitter body, this internal power room and the transmission passageway of being provided with of transmitter, the power room is connected with air feeder, transmission passageway and exterior space intercommunication, the power room with be provided with shutoff mechanism between the transmission passageway, shutoff mechanism is used for control the power room with transmission passageway's intercommunication and/or wall make when power room and transmission passageway intercommunication, the broken glass bulb in the gaseous promotion transmission passageway of air feeder output is followed transmission passageway's axis direction output, promotes broken glass bulb through atmospheric pressure and is carried towards the stable direction, realizes treating the long-range broken tearing open of fixed point of broken glass, and principle and simple structure reduce emission mechanism's preparation cost and use cost.
Description
Technical Field
The utility model relates to a broken glass ball emitter, in particular to broken glass ball emitter of pneumatic type constructs based on unmanned aerial vehicle.
Background
Curtain walls, ceilings of high-rise buildings, windows of various vehicles and the like are usually made of toughened glass, and can be detached through a breaking tool when a fire disaster or other special conditions happen, so that access passages are provided for rescuers or trapped people.
However, when the toughened glass is broken at a short distance, glass fragments are easy to splash all around to hurt rescuers close to the broken glass, when a fire hazard and other critical conditions occur, the two side environments of the glass are different, flame deflagration is easy to occur when the glass is broken, and greater damage is brought to the rescuers close to the broken glass, at present, when emergency rescue, emergency escape and counter-terrorism outburst occur in the toughened glass conditions of curtain walls, vehicle windows and the like, a glass breaking high drill ball made of a high-hardness composite material is applied, the glass breaking high drill ball is thrown to break the toughened glass at a certain distance from the broken glass, in order to ensure smooth breaking and dismantling of the toughened glass, the glass breaking high drill ball has an irregular surface, when manual throwing is adopted, the requirement on the force of the rescuers is high, the aiming degree is low, when an instrument is thrown, the automation degree of the existing throwing instrument is low, the glass breaking high-speed drill ball is troublesome to use, and the throwing force and the throwing direction cannot be accurately controlled, so that the thrown glass breaking high-speed drill ball cannot smoothly break broken glass to be broken and disassembled, and trouble is brought to rescue work.
Therefore, a technical scheme is urgently needed at present to solve the technical problem that the existing glass breaking high-speed drill ball is not easy to be smoothly thrown and broken to break and disassemble toughened glass.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a: to the above-mentioned problem that the broken glass high brill ball of current glass meets at the in-process of throwing breaking open toughened glass, provides a broken glass ball launching mechanism of pneumatic type based on unmanned aerial vehicle.
In order to realize the purpose, the utility model discloses a technical scheme be:
the utility model provides a broken glass ball firing mechanism of pneumatic type based on unmanned aerial vehicle, includes the transmitter body, this internal power house and the transmission passageway of being provided with of transmitter, the power house is connected with air feeder, transmission passageway and exterior space intercommunication, the power house with be provided with shutoff mechanism between the transmission passageway, shutoff mechanism is used for control the power house with the intercommunication and/or the wall of transmission passageway.
The utility model discloses a broken glass bulb launching mechanism of pneumatic type based on unmanned aerial vehicle, through setting up shutoff mechanism, the intercommunication and/or the wall of control power room and launching channel, make when power room and launching channel intercommunication, the broken glass bulb in the gaseous promotion launching channel of air feeder output is along launching channel's axis direction output, promote broken glass bulb through atmospheric pressure and carry towards the steady direction, realize treating the long-range broken tearing of fixed point of breaking open glass, principle and simple structure, reduce launching mechanism's preparation cost and use cost.
As the utility model discloses a preferred scheme, be provided with the air vent on the shutoff mechanism, shutoff mechanism can remove to the messenger power house, air vent and launching channel communicate in proper order. When the power chamber, the vent hole and the launching channel are communicated, the air pressure output by the air supply device can push the glass breaking ball to launch along the launching channel, and the glass to be broken and dismantled is broken and dismantled in a long distance.
As the utility model discloses an optimal scheme, shutoff mechanism including can stretch into the body of rod of power house and with the end cap that the body of rod is connected, be provided with a plurality of air vents along broken glass ball transmission direction intercommunication power house and transmission passageway on the end cap, be connected with the sliding sleeve on the end cap, the sliding sleeve with the coaxial setting of the body of rod, the sliding sleeve can overlap and establish outside the wall of power house.
As the utility model discloses a preferred scheme, shutoff mechanism is connected with locking mechanism, locking mechanism is used for the restriction shutoff mechanism removes. The blocking mechanism is limited by the locking mechanism to move, so that the blocking mechanism can separate the power chamber and the launching channel, and the state of the broken glass ball to be launched is maintained.
As the preferred scheme of the utility model, be provided with reset spring on the shutoff mechanism. The reset spring is used for driving the plugging mechanism to reset after the broken glass ball is launched, and the partition of the power chamber and the launching channel is restored.
As the utility model discloses a preferred scheme still including the bullet passageway that fills who is used for the broken glass ball of splendid attire, the bullet passageway fill with launch the passageway intercommunication, shutoff mechanism can remove to the wall the bullet passageway fill with launch the passageway. The shot-filling channel can be used for containing a plurality of broken glass balls at the same time, the broken glass balls can be conveniently stored, and meanwhile, when the blocking mechanism moves to enable the power chamber to be communicated with the launching channel, the blocking mechanism simultaneously blocks the shot-filling channel and the launching channel, so that the launching mechanism launches one broken glass ball at a time, and the normal use of the launching mechanism is guaranteed.
As the preferred scheme of the utility model, be provided with in the bullet filling channel and be used for promoting broken glass ball and get into launch channel support the push mechanism. The pushing mechanism is adopted to push the broken glass balls to enter the launching channel, so that the broken glass balls automatically enter the launching channel, and the automatic loading effect of the launching mechanism is realized.
As the preferred scheme of the utility model, still include the casing, the transmitter body with air feeder all sets up in the casing. All parts are packaged by the shell to form the launching mechanism with an integral structure, so that the launching mechanism is convenient to carry and use.
As the utility model discloses a preferred scheme, the air feeder with be provided with the trigger piece between the power room, the trigger piece can be controlled the air feeder with the intercommunication and/or the wall of power room. Through setting up the trigger piece, when making broken glass ball be in the state of waiting to launch, air feeder and power room are in the non-connected state, guarantee the stability of shutoff mechanism position, further guarantee this launching mechanism's normal use.
As the utility model discloses an optimal scheme, fill out bullet passageway inner wall and broken glass ball appearance adaptation, launch passageway inner wall and broken glass ball appearance adaptation. The broken glass ball is stably contained in the bullet filling channel and can move towards the set direction after being output from the launching channel, the accuracy of the launching direction of the broken glass ball is guaranteed, and the precision of the launching mechanism is improved.
As the utility model discloses an optimal scheme, the transmitter body can be dismantled with unmanned aerial vehicle and be connected. Make unmanned aerial vehicle carry on transmitter body to eminence to carry out glass and break open, provide convenience for on-the-spot rescue work.
To sum up, owing to adopted above-mentioned technical scheme, the utility model discloses a broken glass ball launching mechanism of pneumatic type based on unmanned aerial vehicle's beneficial effect is:
by arranging the plugging mechanism, the connection and/or the separation of the power chamber and the launching channel are controlled, so that when the power chamber is connected with the launching channel, the gas supply device outputs gas to push the broken glass balls in the launching channel to be output along the axis direction of the launching channel, the broken glass balls are pushed by the gas pressure to be conveyed towards the stable direction, the fixed-point remote breaking and dismantling of the glass to be broken and dismantled is realized, the principle and the structure are simple, and the preparation cost and the use cost of the launching mechanism are reduced.
Drawings
Fig. 1 is a schematic cross-sectional structure diagram of a pneumatic glass breaking ball launching mechanism based on an unmanned aerial vehicle in embodiment 1;
FIG. 2 is a schematic structural view showing a state in which the power chamber and the launching passage are shut off in embodiment 1;
FIG. 3 is a schematic structural view showing a state where the power chamber and the launching path communicate with each other in embodiment 1;
fig. 4 is a schematic structural diagram of a pneumatic glass breaking ball launching mechanism based on an unmanned aerial vehicle in embodiment 3.
Reference numerals
1-emitter body, 11-power chamber, 12-emission channel, 2-gas supply device, 3-blocking mechanism, 31-rod body, 32-plug, 33-vent hole, 34-sliding sleeve, 35-clamping groove, 4-locking mechanism, 41-locking rod, 42-trigger rod, 5-reset spring, 6-bullet filling channel, 7-pushing mechanism, 71-end cover, 72-spring, 8-shell, 9-trigger piece, 10-broken glass ball and 20-connecting mechanism.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention will be further described in detail with reference to the accompanying drawings and specific embodiments. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the invention.
Example 1
As shown in fig. 1-4, a broken glass bulb launching mechanism of pneumatic type based on unmanned aerial vehicle, including transmitter body 1, be provided with driver's cabin 11 and transmission passageway 12 in the transmitter body 1, driver's cabin 11 is connected with air feeder 2, transmission passageway 12 and exterior space intercommunication, driver's cabin 11 with be provided with shutoff mechanism 3 between the transmission passageway 12, be provided with air vent 33 on the shutoff mechanism 3, shutoff mechanism 3 can remove to the messenger driver's cabin 11, air vent 33 and transmission passageway 12 communicate in proper order, air feeder 2 with be provided with trigger 9 between the driver's cabin 11, trigger 9 can control air feeder 2 with the intercommunication and/or the wall of driver's cabin 11.
The broken glass bulb launching mechanism of a pneumatic type based on unmanned aerial vehicle of this embodiment, preferably set up the cavity as power house 11 in the emitter body 1 to set up and follow the launching path 12 that broken glass bulb launching direction communicates with power house 11, set up shutoff mechanism 3 between launching path 12 and power house 11, set up trigger 9 between power house 11 and air feeder 2, specifically, preferably air feeder 2 is the gas cylinder that contains high-pressure gas or can provide high-pressure draught's air pump, shutoff mechanism 3 including can stretch into power house 11 the body of rod 31 and with the end cap 32 that the body of rod 31 is connected, end cap 32 is located launching path 12 one side, be provided with on the end cap 32 along broken glass bulb launching direction for a plurality of air vents 33 of intercommunication power house 11 and launching path 12, when the body of rod 31 stretches into power house 11, end cap 32 laminating power house 11 opening, the air vent 33 on the plug 32 is staggered with the position of the power chamber 11, so that the plug 32 plugs the opening of the power chamber 11, and the power chamber 11 is separated from the launching channel 12, when the trigger 9 triggers the air supply device 2 to be communicated with the power chamber 11, the pressure in the power chamber 11 rises, the plugging mechanism 3 is pushed to move towards the launching channel 12, so that the power chamber 11, the air vent 33 and the launching channel 12 are communicated, the broken glass ball 10 in the launching channel 12 is launched along the launching channel 12 under the action of air pressure, the launching direction of the broken glass ball 10 is the extending direction of the launching channel 12, and the long-distance fixed-point accurate breaking of the broken glass ball 10 to broken glass is realized, in the embodiment, the air supply device 2 is preferably an air bottle, an air bottle connecting port detachably connected with the launcher body 1 is arranged, the trigger 9 is a ventilation cone capable of puncturing the opening of the air bottle and enabling, the launching mechanism has the advantages of simple principle and structure, good use effect, reduction of glass breaking cost and time, and great convenience for on-site rescue.
Preferably, a locking mechanism 4 is connected to the blocking mechanism 3, and the locking mechanism 4 is used for limiting the movement of the blocking mechanism 3. The locking mechanism 4 is configured to maintain a relatively static state of the plugging mechanism 3 and the power chamber 11 when the power chamber 11 and the emission channel 12 are in a blocking state, in this embodiment, preferably, the locking mechanism 4 includes a locking rod 41, the locking rod 41 is detachably connected to the emitter body 1, a clamping groove 35 adapted to the locking rod 41 is provided on the plugging mechanism 3, when the locking rod 41 is connected to the clamping groove 35 in a matching manner, the plugging mechanism 3 is limited by the locking rod 41 to maintain the blocking of the power chamber 11 and the emission channel 12, specifically, preferably, the locking mechanism 4 further includes a trigger rod 42, the trigger rod 42 is configured to drive the locking rod 41 to rotate relative to the emitter body 1, so that the locking rod 41 is disconnected from the clamping groove 35, and the plugging mechanism 3 can move under the air pressure action of the power chamber 11 to achieve communication between the power chamber 11 and the emission channel 12, the structure is simple, the moving state of the plugging mechanism 3 is easily controlled, and the communication state of the power chamber 11 and the launching channel 12 is controlled.
Preferably, a return spring 5 is arranged on the blocking mechanism 3. In this embodiment, it is preferable that a sliding sleeve 34 is connected to the plug 32 of the plugging mechanism 3, the sliding sleeve 34 and the rod body 31 are coaxially arranged, the sliding sleeve 34 can be sleeved outside the wall of the power chamber 11, the moving direction of the plugging mechanism 3 is ensured, meanwhile, the clamping groove 35 is arranged on the sliding sleeve 34, the locking rod 41 is arranged on the outer wall of the emitter body 1 corresponding to the power chamber 11, the sliding sleeve 34 is sleeved with the return spring 5, the return spring 5 applies a force to the plugging mechanism 3 to move towards the power chamber 11, the rod body 31 maintaining the plugging mechanism 3 extends into the power chamber 11, an opening between the power chamber 11 and the emission channel 12 is plugged, and the partition of the power chamber 11 and the emission channel 12 is recovered.
Preferably, the transmitter body 1 can be detachably connected with the unmanned aerial vehicle. In this embodiment, preferably be provided with coupling mechanism 20 that is used for connecting unmanned aerial vehicle on transmitter body 1 outer wall, make unmanned aerial vehicle can promote or carry on transmitter body 1 to the high department and carry out broken of glass and tear open, provide convenience for on-the-spot rescue work, coupling mechanism 20 corresponds the design according to unmanned aerial vehicle's model, transmitter body 1 appearance, makes transmitter body 1 can be easier be connected with unmanned aerial vehicle.
Example 2
As shown in fig. 1 to 4, the structure of the pneumatic type glass breaking ball launching mechanism based on the unmanned aerial vehicle of the present embodiment is the same as that of embodiment 1, except that: the glass ball breaking device is characterized by further comprising a ball filling channel 6 used for containing the broken glass ball 10, the ball filling channel 6 is communicated with the launching channel 12, the blocking mechanism 3 can move to block the ball filling channel 6 and the launching channel 12, and a pushing mechanism 7 used for pushing the broken glass ball 10 to enter the launching channel 12 is arranged in the ball filling channel 6.
In the pneumatic broken glass ball launching mechanism based on the unmanned aerial vehicle of the embodiment, preferably, the bullet filling channel 6 is communicated with the bullet filling channel 6 along the direction perpendicular to the axis of the launching channel 12, the end of the bullet filling channel 6, which is far away from the launching channel 12, is provided with the pushing mechanism 7 including the end cover 71 and the spring 72, so that the opening of the bullet filling channel 6, which is far away from the launching channel 12, is sealed by the end cover 71, the broken glass ball 10 is conveniently supplemented, the spring 72 pushes the broken glass ball 10 into the launching channel 12, and the automatic loading of the broken glass ball 10 is realized, meanwhile, in the embodiment, preferably, the opening of the bullet filling channel 6, which is communicated with the launching channel 12, is close to the power chamber 11, so that when the sealing mechanism 3 moves to communicate the power chamber 11 and the launching channel 12, the sealing mechanism 3 also plays a role in separating the bullet filling channel 6 and the launching channel 12, so that the launching mechanism can only launch, ensuring the normal use of the launching mechanism.
Preferably, the inner wall of the bomb filling channel 6 is matched with the shape of the broken glass ball 10, and the inner wall of the launching channel 12 is matched with the shape of the broken glass ball 10. In this embodiment, it is preferable that the broken glass ball 10 has an irregular-shaped surface formed by combining a plurality of pointed cone protrusions, the inner wall of the bullet filling channel 6 is provided with a groove adapted to the irregular-shaped surface on the broken glass ball 10, so that the broken glass ball 10 can only move towards a set direction in the bullet filling channel 6 and cannot rotate at will, the stable arrangement of the broken glass ball 10 in the bullet filling channel 6 is ensured, meanwhile, the inner wall of the launching channel 12 is provided with a plurality of grooves, the change of the launching direction caused by the impact of the irregular-shaped surface on the broken glass ball 10 on the inner wall of the launching channel 12 is avoided, and the precision of the launching mechanism is improved.
Example 3
As shown in fig. 1 to 4, the structure of the pneumatic type glass breaking ball launching mechanism based on the unmanned aerial vehicle of the present embodiment is the same as that of embodiment 2, except that: still include casing 8, emitter body 1 with air supply unit 2 all sets up in casing 8.
The pneumatic broken glass ball launching mechanism based on the unmanned aerial vehicle preferably adopts a shell 8 to integrally encapsulate components including a launcher body 1, an air supply device 2, a structural component provided with a bullet filling channel 6 and the like, and particularly, in the embodiment, a trigger rod 42 used for triggering the separation of a locking rod 41 and a clamping groove 35 on a sliding sleeve 34 of the blocking mechanism 3 extends out of the shell 8, so that the movement control of the blocking mechanism 3 can be realized through the trigger rod 42, the launching mechanism with an integral structure is formed, the structural appearance is simple, the launching mechanism is convenient to carry and use, according to actual conditions, the trigger rod 42 can be remotely or electrically driven by a driving mechanism to act, the locking rod 41 is controlled to be separated from the clamping groove 35 on the blocking mechanism 3, when the air supply device 2 is communicated with a power chamber 11, the air pressure in the power chamber 11 rises, and the blocking mechanism 3 is pushed to move towards the launching channel 12, the power chamber 11 is communicated with the launching channel 12 to realize the remote control launching of the broken glass ball 10 in the launching channel 12, and preferably, the driving mechanism is a relay, a switching device and the like with a matched control circuit.
The above embodiments are only used to illustrate the present invention and not to limit the technical solutions of the present invention, and although the present invention has been described in detail with reference to the above embodiments, the present invention is not limited to the above embodiments, therefore, any modifications or equivalent replacements of the present invention can be made, and all technical solutions and modifications without departing from the spirit and scope of the present invention should be covered by the claims of the present invention.
Claims (10)
1. The utility model provides a broken glass bulb launching mechanism of pneumatic type based on unmanned aerial vehicle, a serial communication port, including transmitter body (1), be provided with power house (11) and transmission passageway (12) in transmitter body (1), power house (11) are connected with air feeder (2), transmission passageway (12) and exterior space intercommunication, power house (11) with be provided with between transmission passageway (12) shutoff mechanism (3), shutoff mechanism (3) are used for control power house (11) with the intercommunication and/or the wall of transmission passageway (12).
2. The pneumatic type glass breaking ball launching mechanism based on the unmanned aerial vehicle as claimed in claim 1, wherein a vent hole (33) is formed in the blocking mechanism (3), and the blocking mechanism (3) can move to enable the power chamber (11), the vent hole (33) and the launching channel (12) to be communicated in sequence.
3. The pneumatic type glass breaking ball launching mechanism based on the unmanned aerial vehicle as claimed in claim 2, wherein a locking mechanism (4) is connected to the blocking mechanism (3), and the locking mechanism (4) is used for limiting the movement of the blocking mechanism (3).
4. The pneumatic type glass breaking ball launching mechanism based on the unmanned aerial vehicle as claimed in claim 2, wherein a return spring (5) is arranged on the blocking mechanism (3).
5. A pneumatic type broken glass ball launching mechanism based on unmanned aerial vehicle as claimed in claim 2, further comprising a filling channel (6) for containing broken glass balls (10), wherein the filling channel (6) is communicated with the launching channel (12), and the blocking mechanism (3) can move to block the filling channel (6) and the launching channel (12).
6. The pneumatic type glass breaking ball launching mechanism based on the unmanned aerial vehicle as claimed in claim 5, wherein a pushing mechanism (7) for pushing the glass breaking ball (10) into the launching channel (12) is arranged in the bullet filling channel (6).
7. The pneumatic broken glass ball launching mechanism based on the unmanned aerial vehicle as claimed in claim 5, wherein the inner wall of the filling channel (6) is matched with the shape of the broken glass ball (10), and the inner wall of the launching channel (12) is matched with the shape of the broken glass ball (10).
8. The pneumatic type glass breaking ball launching mechanism based on the unmanned aerial vehicle as claimed in any one of claims 1-7, further comprising a housing (8), wherein the launcher body (1) and the gas supply device (2) are both arranged in the housing (8).
9. The pneumatic type glass breaking ball launching mechanism based on the unmanned aerial vehicle as claimed in claim 8, wherein a trigger (9) is arranged between the air supply device (2) and the power chamber (11), and the trigger (9) can control the communication and/or the partition of the air supply device (2) and the power chamber (11).
10. The pneumatic type glass breaking ball launching mechanism based on the unmanned aerial vehicle as claimed in claim 8, wherein the launcher body (1) can be detachably connected with the unmanned aerial vehicle.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020105595.8U CN211893653U (en) | 2020-01-17 | 2020-01-17 | Broken glass ball launching mechanism of pneumatic type based on unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202020105595.8U CN211893653U (en) | 2020-01-17 | 2020-01-17 | Broken glass ball launching mechanism of pneumatic type based on unmanned aerial vehicle |
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| CN211893653U true CN211893653U (en) | 2020-11-10 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114295001A (en) * | 2021-12-30 | 2022-04-08 | 平裕（成都）科技有限公司 | Aiming method of glass breaking equipment |
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- 2020-01-17 CN CN202020105595.8U patent/CN211893653U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114295001A (en) * | 2021-12-30 | 2022-04-08 | 平裕（成都）科技有限公司 | Aiming method of glass breaking equipment |
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