CN212006954U - Glass blasting unmanned aerial vehicle - Google Patents
Glass blasting unmanned aerial vehicle Download PDFInfo
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- CN212006954U CN212006954U CN201921064496.3U CN201921064496U CN212006954U CN 212006954 U CN212006954 U CN 212006954U CN 201921064496 U CN201921064496 U CN 201921064496U CN 212006954 U CN212006954 U CN 212006954U
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Abstract
The utility model discloses an unmanned aerial vehicle for blasting glass, which comprises a flight control and graph transmission device (1), an fpv lens (2), an explosive mounting bin (3), a composite explosive (4), an igniter (5), a first aircraft connector (6), a second aircraft connector (7), a third aircraft connector (8), a first mounting bin interface (9), a second mounting bin interface (10) and a third mounting bin interface (11); the head of the flight control and graph transmission (1) is provided with an fpv lens (2); it has overcome among the prior art commercial zhongting top skylight, office building outer wall etc. and these glass materials are all unusually firm, and toughness is also very strong, the difficult broken shortcoming has the advantage of reacing fast with the help of unmanned aerial vehicle, carries on directional blasting device, carries out directional blasting to the glass of conflagration department all around and market zhongting top for fire rescue efficiency.
Description
Technical Field
The utility model relates to go to market atrium top glass blasting, the high-rise glass blasting technical field of large-scale office building, more specifically be glass blasting's unmanned aerial vehicle.
Background
In the modern society, along with the improvement of living standard of people, various high-rise buildings and superstores stand up, wherein most buildings are applied to glass structures, such as top skylights of commercial courtyards, outer walls of office buildings and the like, and the glass materials are extremely firm, have high toughness and are not easy to break; the fire-fighting supporting facilities of the buildings are generally perfect, special smoke-discharging and fire-extinguishing pipelines are arranged after a fire disaster occurs, the fire is often insufficient when the fire is too big, and if the glass can be opened, the glass is greatly helpful for smoke discharging, fire fighting outside water-hitting fire extinguishing and the like. In case of fire, people are busy to escape from the site, few people think of breaking the glass, but some glass cannot be broken at all, and at the moment, the glass needs to be removed by adopting an explosion device.
Disclosure of Invention
The utility model aims to overcome the weak point of above-mentioned background art, and propose blasting glass's unmanned aerial vehicle.
The utility model aims at being implemented through the following technical scheme: the unmanned aerial vehicle for blasting glass comprises a flight control and graph transmission device, an fpv lens, an explosive mounting bin, composite explosives, a detonating device, a first aircraft connector, a second aircraft connector, a third aircraft connector, a first mounting bin interface, a second mounting bin interface and a third mounting bin interface;
the head of the flight control and graph transmission is provided with an fpv lens, the bottom of the flight control and graph transmission is provided with a composite explosive and a detonation device, and the flight control and graph transmission is fixedly connected with the composite explosive and the detonation device through an explosive mounting bin.
In the above technical scheme: the front end of the flight control and graph transmission is provided with a first aircraft connector, and the rear end of the flight control and graph transmission is provided with a second aircraft connector and a third aircraft connector; the front end of the explosive mounting bin is provided with a third mounting bin interface, and the rear end of the explosive mounting bin is provided with a first mounting bin interface and a second mounting bin interface; the first aircraft connector and the third mounting bin connector are screwed up through screws, and the second aircraft connector and the third aircraft connector are arranged at the left end and the right end and are fixedly connected with the first mounting bin connector and the second mounting bin connector through screws respectively.
In the above technical scheme: the flight control and the image transmission are made of carbon fiber structures.
The utility model has the advantages of as follows: 1. the utility model belongs to special unmanned aerial vehicle high altitude blasting glass equipment carries out directional blasting device with the help of the advantage that unmanned aerial vehicle reachd fast, reaches the glass at court top in the market to conflagration department all around for fire rescue efficiency.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention.
Fig. 2 is a split view of the present invention.
In the figure: the system comprises a flight control and image transmission lens 1, an fpv lens 2, an explosive mounting bin 3, a composite explosive 4, a detonating device 5, a first aircraft connector 6, a second aircraft connector 7, a third aircraft connector 8, a first mounting bin interface 9, a second mounting bin interface 10 and a third mounting bin interface 11.
Detailed Description
The following detailed description of the embodiments of the present invention will be made with reference to the accompanying drawings, which are not intended to limit the present invention, but are merely exemplary; while the advantages of the invention will be apparent and readily appreciated by the description.
Referring to FIGS. 1-2: the unmanned aerial vehicle for blasting glass comprises a flight control and image transmission 1, a fpv lens 2, an explosive mounting bin 3, a composite explosive 4, a detonating device 5, a first aircraft connector 6, a second aircraft connector 7, a third aircraft connector 8, a first mounting bin interface 9, a second mounting bin interface 10 and a third mounting bin interface 11;
the head of the flight control and graph transmission 1 is provided with fpv lenses 2, the bottom of the flight control and graph transmission 1 is provided with a compound explosive 4 and a detonating device 5, and the flight control and graph transmission 1 and the compound explosive 4 and the detonating device 5 are fixedly connected through an explosive mounting bin 3.
The front end of the flight control and graph transmission device 1 is provided with a first aircraft connector 6, and the rear end of the flight control and graph transmission device is provided with a second aircraft connector 7 and a third aircraft connector 8; the front end of the explosive mounting bin 3 is provided with a third mounting bin interface 11, and the rear end is provided with a first mounting bin interface 9 and a second mounting bin interface 10; the first aircraft connector 6 and the third mounting bin connector 11 are screwed tightly through screws, and the second aircraft connector 7 and the third aircraft connector 8 arranged at the left end and the right end are respectively fixedly connected with the first mounting bin connector 9 and the second mounting bin connector 10 through screws; the flight control and the graph transmission 1 are made of carbon fiber structures.
The above-mentioned parts not described in detail are prior art.
Claims (3)
1. Glass blasting's unmanned aerial vehicle, its characterized in that: the explosive loading device comprises a flight control and image transmission device (1), an fpv lens (2), an explosive loading bin (3), a composite explosive (4), a detonation device (5), a first aircraft connector (6), a second aircraft connector (7), a third aircraft connector (8), a first loading bin interface (9), a second loading bin interface (10) and a third loading bin interface (11);
the head of the flight control and graph transmission device (1) is provided with an fpv lens (2), the bottom of the flight control and graph transmission device (1) is provided with a composite explosive (4) and a detonating device (5), and the flight control and graph transmission device (1) is fixedly connected with the composite explosive (4) and the detonating device (5) through an explosive mounting bin (3).
2. The unmanned aerial vehicle for blasting glass of claim 1, wherein: the front end of the flight control and graph transmission (1) is provided with a first aircraft connecting port (6), and the rear end of the flight control and graph transmission (1) is provided with a second aircraft connecting port (7) and a third aircraft connecting port (8); the front end of the explosive mounting bin (3) is provided with a third mounting bin interface (11), and the rear end of the explosive mounting bin (3) is provided with a first mounting bin interface (9) and a second mounting bin interface (10); the first aircraft connector (6) and the third mounting bin connector (11) are screwed up through screws, and the second aircraft connector (7) and the third aircraft connector (8) are arranged at the left end and the right end and are fixedly connected with the first mounting bin connector (9) and the second mounting bin connector (10) through screws respectively.
3. The glass blasting drone of claim 1 or 2, characterized in that: the flight control and graph transmission (1) is made of a carbon fiber structure.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921064496.3U CN212006954U (en) | 2019-07-09 | 2019-07-09 | Glass blasting unmanned aerial vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921064496.3U CN212006954U (en) | 2019-07-09 | 2019-07-09 | Glass blasting unmanned aerial vehicle |
Publications (1)
Publication Number | Publication Date |
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CN212006954U true CN212006954U (en) | 2020-11-24 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201921064496.3U Active CN212006954U (en) | 2019-07-09 | 2019-07-09 | Glass blasting unmanned aerial vehicle |
Country Status (1)
Country | Link |
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CN (1) | CN212006954U (en) |
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2019
- 2019-07-09 CN CN201921064496.3U patent/CN212006954U/en active Active
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