CN113460305A - Six rotor crafts of overhead power grid fire control - Google Patents
Six rotor crafts of overhead power grid fire control Download PDFInfo
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- CN113460305A CN113460305A CN202110975076.6A CN202110975076A CN113460305A CN 113460305 A CN113460305 A CN 113460305A CN 202110975076 A CN202110975076 A CN 202110975076A CN 113460305 A CN113460305 A CN 113460305A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/36—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like adapted to receive antennas or radomes
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/54—Floats
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
- B64D47/04—Arrangements or adaptations of signal or lighting devices the lighting devices being primarily intended to illuminate the way ahead
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G1/00—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines
- H02G1/02—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for overhead lines or cables
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Abstract
The invention discloses an overhead power grid fire-fighting six-rotor aircraft which comprises an aircraft main body, wherein a fire-fighting calling mechanism is arranged on the outer surface of the upper end of the aircraft main body, an aircraft support is arranged on the outer surface of the lower end of the aircraft main body, an installation rod is arranged in the middle of the aircraft support, a multifunctional fire-fighting rescue mechanism is arranged on the outer surface of the lower end of the installation rod, and a water surface takeoff base is arranged on the outer surface of the lower end of the aircraft support. The aerial power grid fire-fighting six-rotor aircraft is provided with the fire-fighting calling mechanism, the water surface take-off base and the multifunctional fire-fighting rescue mechanism, can be used for calling and reminding fire-fighting rescue workers to trapped people, is convenient for the aircraft to take off and land on the water surface, can be used for continuously lighting the trapped area, and can be used for facilitating rescue workers to lift power grid wires to a high place, so that a better use prospect is brought.
Description
Technical Field
The invention relates to the field of aircrafts, in particular to an overhead power grid fire-fighting six-rotor aircraft.
Background
The six-rotor aircraft is an unmanned aircraft specially used for overhead power grid fire protection, can be conveniently used by people, and is simple in structure and convenient to operate.
There is certain drawback when using in the six rotor crafts of current built on stilts electric power electric wire netting fire control, at first, in the use, traditional aircraft does not have the function of calling out the warning, the fire rescue function singleness, secondly, can't take off and land on the surface of water, there is the restriction to the place of taking off, in addition, the fire rescue in-process at night, can't throw light on to the rescue region, certain adverse effect has been brought to people's use, for this reason, we propose a six rotor crafts of built on stilts electric power electric wire netting fire control.
Disclosure of Invention
The invention mainly aims to provide an overhead power grid fire-fighting six-rotor aircraft which can effectively solve the problems in the background technology.
In order to achieve the purpose, the invention adopts the technical scheme that:
the utility model provides an overhead power grid six rotor crafts of fire control, includes the aircraft main part, the upper end surface of aircraft main part is provided with fire control calling mechanism, the lower extreme surface of aircraft main part is provided with the aircraft support, the middle part of aircraft support is provided with the installation pole, the lower extreme surface of installation pole is provided with multi-functional fire rescue mechanism, the lower extreme surface of aircraft support is provided with the surface of water base of taking off.
The fire-fighting calling mechanism is mainly beneficial to the fire-fighting rescue personnel to call and remind the trapped personnel.
The water surface take-off base is mainly beneficial to take-off and landing of the aircraft on the water surface.
Multifunctional fire rescue mechanism is mainly favorable to carrying out the illumination of lasting light to stranded region, can also make things convenient for the rescue personnel to promote the eminence with electric power electric wire netting wire rod.
Preferably, the outer wall of aircraft main part is provided with the connecting rod, one side surface of connecting rod is provided with the promotion screw, the connecting rod is six groups with the quantity that promotes the screw.
Preferably, fire control calling mechanism includes megaphone wiring, signal reception line, threaded connection spare, fixed shell, signal transmission antenna and megaphone, the inner wall of fixed shell is provided with the megaphone, the upper end surface of fixed shell is provided with signal transmission antenna, the lower extreme surface of fixed shell is provided with threaded connection spare, threaded connection spare's lower extreme surface is provided with megaphone wiring and signal reception line, the megaphone wiring is located one side of signal reception line.
Preferably, the surface of water takes off the base and includes installation knob, blotter, cystosepiment, convenient mounting bracket, illumination fluting and handle groove, the upper end surface of blotter is provided with the cystosepiment, the upper end both sides of cystosepiment all are provided with convenient mounting bracket, the middle part of convenient mounting bracket is provided with the installation knob, illumination fluting and handle groove have all been seted up to the cystosepiment and the outer wall of blotter, the handle groove is located illumination slotted one side.
Preferably, multi-functional fire rescue mechanism includes group battery, LED banks, connects shell, mount and wire rod fixed hook, the both sides surface of connecting the shell all is provided with the wire rod fixed hook, the inner wall of connecting the shell is provided with the group battery, the lower extreme surface of connecting the shell is provided with the LED banks, the upper end surface of connecting the shell is provided with the mount.
Preferably, the inner wall of fixed shell and the outer wall fixed connection of megaphone, the upper end surface of fixed shell and the lower extreme surface fixed connection of signal transmission antenna, the lower extreme surface of fixed shell and the upper end surface fixed connection of threaded connection spare, the upper end surface of megaphone wiring runs through the inner wall and the inner wall electric connection of megaphone of threaded connection spare and fixed shell, the upper end surface of signal reception line runs through the inner wall of fixed shell and the inner wall electric connection of signal transmission antenna, the lower extreme surface of fire control calling mechanism passes through the upper end surface of threaded connection spare and aircraft main part and can dismantle and be connected.
Preferably, the upper end surface of blotter and the lower extreme fixed surface of cystosepiment are connected, the upper end both sides of cystosepiment all are connected with the lower extreme fixed surface of convenient mounting bracket, the middle part of convenient mounting bracket can be dismantled with the outer wall of installation knob and be connected, the quantity of handle groove is two sets of, the upper end surface of the surface of water base of taking off can be dismantled through the lower extreme surface of convenient mounting bracket and installation knob and aircraft support and be connected.
Preferably, the both sides surface of connecting the shell all with one side fixed surface connection of wire rod fixed hook, the inner wall of connecting the shell and the outer wall fixed connection of group battery, the lower extreme surface of connecting the shell can be dismantled with the upper end surface of LED banks and be connected, the upper end surface of connecting the shell can be dismantled with the lower extreme surface of mount and be connected, be provided with the power cord between group battery and the LED banks, the middle part electric connection of power cord and LED banks is passed through to one side surface of group battery, the upper end surface of multi-functional fire rescue mechanism can be dismantled through the outer wall of mount and installation pole and be connected.
Compared with the prior art, the invention has the following beneficial effects: the aerial power grid fire-fighting hexa-rotor aircraft is characterized in that a loudspeaker wiring and a signal receiving wire can be connected into an aircraft main body firstly through a fire-fighting calling mechanism, then a threaded connecting piece is installed at the upper end of the aircraft main body, fire rescue personnel can control the loudspeaker to play audio through a signal transmitting device during fire rescue, and can also call in real time to remind trapped people, so that the aerial power grid fire-fighting hexa-rotor aircraft is beneficial to use of fire rescue, a convenient installation frame can be installed at the lower end of an aircraft bracket through a water surface take-off base when the aerial power grid fire-fighting hexa-rotor aircraft needs to take off on the water surface, and then the aerial power grid fire-fighting hexa-rotor aircraft is fixed through rotating an installation knob, so that the overall buoyancy of the hexa-rotor aircraft can be improved by a foam plate to float on the water surface to take off and land, the use limitation of the hexa-rotor aircraft is reduced, and a cushion can also buffer impact force during landing, be favorable to six rotor crafts's use, the multi-functional fire rescue mechanism of setting, when the night fire rescue, can install the installation pole outer wall through the mount with connecting the shell, the group battery provides electric power for the LED banks and lasts the illumination to fire rescue region, the wire rod fixed hook can also make things convenient for the rescue personnel to promote the eminence with the electric power electric wire netting wire rod, carry out electric power electric wire netting and salvage, be favorable to improving fire rescue efficiency, whole six rotor crafts of overhead electric power electric wire netting fire control simple structure, high durability and convenient operation, the effect of using is better for traditional mode.
Drawings
Fig. 1 is a schematic overall structure diagram of an overhead power grid fire-fighting six-rotor aircraft according to the invention.
Fig. 2 is an enlarged view of the aircraft body 4 of fig. 1 of an overhead power grid fire-fighting six-rotor aircraft of the present invention.
Fig. 3 is an enlarged view of the aircraft pylon 3 of fig. 1 of an overhead power grid fire-fighting six-rotor aircraft of the present invention.
Fig. 4 is an enlarged view of the fire fighting call mechanism 5 of fig. 1 of an overhead power grid fire fighting six-rotor aircraft according to the present invention.
Fig. 5 is an enlarged view of the water takeoff base 1 in fig. 1 of the aerial power grid fire-fighting six-rotor aircraft according to the invention.
Fig. 6 is an enlarged view of the multifunctional fire rescue mechanism 2 of fig. 1 of an overhead power grid fire-fighting six-rotor aircraft according to the present invention.
In the figure: 1. a water surface takeoff base; 2. a multifunctional fire rescue mechanism; 3. an aircraft support; 4. an aircraft body; 5. a fire call mechanism; 6. a connecting rod; 7. lifting the propeller; 8. mounting a rod; 501. wiring of a loudspeaker; 502. a signal receiving line; 503. a threaded connection; 504. fixing the housing; 505. a signal transmitting antenna; 506. (ii) a 101. Installing a knob; 102. a cushion pad; 103. a foam board; 104. a convenient mounting rack; 105. lighting slotting; 106. a handle slot; 201. a battery pack; 202. an LED lamp group; 203. connecting the shell; 204. a fixed mount; 205. and (4) fixing the hook by the wire.
Detailed Description
In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the invention is further described with the specific embodiments.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, such as "connected," which may be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
As shown in fig. 1-6, an overhead power grid fire-fighting six-rotor aircraft comprises an aircraft body 4, a fire-fighting calling mechanism 5 is arranged on the outer surface of the upper end of the aircraft body 4, an aircraft support 3 is arranged on the outer surface of the lower end of the aircraft body 4, an installation rod 8 is arranged in the middle of the aircraft support 3, a multifunctional fire-fighting rescue mechanism 2 is arranged on the outer surface of the lower end of the installation rod 8, and a water surface takeoff base 1 is arranged on the outer surface of the lower end of the aircraft support 3.
Further, the outer wall of aircraft main part 4 is provided with connecting rod 6, and one side surface of connecting rod 6 is provided with promotes screw 7, and connecting rod 6 is six groups with the quantity that promotes screw 7.
Further, the fire fighting call mechanism 5 comprises a loudspeaker wiring 501, a signal receiving line 502, a threaded connector 503, a fixed housing 504, a signal transmitting antenna 505 and a loudspeaker 506, wherein the loudspeaker 506 is arranged on the inner wall of the fixed housing 504, the signal transmitting antenna 505 is arranged on the outer surface of the upper end of the fixed housing 504, the threaded connector 503 is arranged on the outer surface of the lower end of the fixed housing 504, the loudspeaker wiring 501 and the signal receiving line 502 are arranged on the outer surface of the lower end of the threaded connector 503, and the loudspeaker wiring 501 is located on one side of the signal receiving line 502.
Further, surface of water base 1 of taking off includes installation knob 101, blotter 102, cystosepiment 103, convenient mounting bracket 104, illumination fluting 105 and handle groove 106, the upper end surface of blotter 102 is provided with cystosepiment 103, the upper end both sides of cystosepiment 103 all are provided with convenient mounting bracket 104, the middle part of convenient mounting bracket 104 is provided with installation knob 101, illumination fluting 105 and handle groove 106 have all been seted up to cystosepiment 103 and the outer wall of blotter 102, handle groove 106 is located one side of illumination fluting 105.
Further, multi-functional fire rescue mechanism 2 includes group battery 201, LED banks 202, connects shell 203, mount 204 and wire rod fixed hook 205, and the both sides surface of connecting shell 203 all is provided with wire rod fixed hook 205, and the inner wall of connecting shell 203 is provided with group battery 201, and the lower extreme surface of connecting shell 203 is provided with LED banks 202, and the upper end surface of connecting shell 203 is provided with mount 204.
Further, the inner wall of the fixed housing 504 is fixedly connected with the outer wall of the loudspeaker 506, the outer surface of the upper end of the fixed housing 504 is fixedly connected with the outer surface of the lower end of the signal transmitting antenna 505, the outer surface of the lower end of the fixed housing 504 is fixedly connected with the outer surface of the upper end of the threaded connecting piece 503, the outer surface of the upper end of the loudspeaker wiring 501 penetrates through the threaded connecting piece 503 and the inner wall of the fixed housing 504 and is electrically connected with the inner wall of the loudspeaker 506, the outer surface of the upper end of the signal receiving wire 502 penetrates through the inner wall of the fixed housing 504 and is electrically connected with the inner wall of the signal transmitting antenna 505, and the outer surface of the lower end of the fire-fighting calling mechanism 5 is detachably connected with the outer surface of the upper end of the aircraft body 4 through the threaded connecting piece 503.
Further, the upper end surface of blotter 102 and the lower extreme external surface fixed connection of cystosepiment 103, the upper end both sides of cystosepiment 103 all are connected with the lower extreme external surface fixed connection of convenient mounting bracket 104, the middle part of convenient mounting bracket 104 can be dismantled with the outer wall of installation knob 101 and be connected, the quantity of handle groove 106 is two sets of, the upper end surface of the surface of water base 1 of taking off can be dismantled through convenient mounting bracket 104 and installation knob 101 and aircraft support 3's lower extreme surface and be connected.
Further, the both sides surface of connecting shell 203 all is connected with one side surface fixed connection of wire rod fixed hook 205, the inner wall of connecting shell 203 and the outer wall fixed connection of group battery 201, the lower extreme surface of connecting shell 203 and the upper end surface of LED banks 202 can be dismantled and be connected, the upper end surface of connecting shell 203 and the lower extreme surface of mount 204 can be dismantled and be connected, be provided with the power cord between group battery 201 and the LED banks 202, the middle part electric connection of power cord and LED banks 202 is passed through to one side surface of group battery 201, the upper end surface of multi-functional fire rescue mechanism 2 passes through the outer wall of mount 204 and installation pole 8 and can dismantle and be connected.
The invention is to be noted that, the invention is an aerial power grid fire-fighting six-rotor aircraft, when in use, the fire call mechanism 5, the multifunctional fire rescue mechanism 2 and the water surface takeoff base 1 can be installed on the six-rotor aircraft according to requirements, when in use, an operator can control the six-rotor aircraft to ascend and descend through a remote controller, the fire call mechanism 5 is arranged, before the six-rotor aircraft is used, the loudspeaker connecting wire 501 and the signal receiving wire 502 can be connected to the inside of the aircraft main body 4, then the threaded connecting piece 503 is installed at the upper end of the aircraft main body 4, when in fire rescue, the fire rescue personnel can control the loudspeaker to play audio through the signal transmitting equipment, can also shout in real time, call and remind trapped personnel, is beneficial to the use of fire rescue, the water surface takeoff base 1 is arranged, when in need of taking off on the water surface, can install aircraft support 3 lower extreme with convenient installation 104 frame, rethread rotatory installation knob 101 is fixed, cystosepiment 103 can improve six rotor craft's whole buoyancy, make it float and take off and descend at the surface of water, reduce six rotor craft's use limitation, blotter 102 can also cushion the impact force when descending, be favorable to six rotor craft's use, the multi-functional fire rescue mechanism 2 of its setting, when the fire rescue at night, can install installation pole 8 outer walls through mount 204 with connecting shell 203, group battery 201 provides electric power for LED banks 202 and lasts the illumination to the fire rescue region, wire rod fixing hook 205 can also make things convenient for the rescue personnel to promote the eminence with electric power electric wire netting wire rod, carry out electric power electric wire netting and salvage, be favorable to improving fire rescue efficiency, and is relatively practical.
The foregoing shows and describes the general principles and broad features of the present invention and advantages thereof. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the invention as claimed. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (8)
1. The utility model provides an overhead power grid six rotor crafts of fire control, includes aircraft main part (4), its characterized in that: the aircraft is characterized in that a fire-fighting calling mechanism (5) is arranged on the outer surface of the upper end of the aircraft body (4), an aircraft support (3) is arranged on the outer surface of the lower end of the aircraft body (4), an installation rod (8) is arranged in the middle of the aircraft support (3), a multifunctional fire rescue mechanism (2) is arranged on the outer surface of the lower end of the installation rod (8), and a water surface take-off base (1) is arranged on the outer surface of the lower end of the aircraft support (3).
2. An overhead power grid fire-fighting six-rotor aircraft according to claim 1, characterized in that: the outer wall of aircraft main part (4) is provided with connecting rod (6), one side surface of connecting rod (6) is provided with promotes screw (7), connecting rod (6) are six groups with the quantity that promotes screw (7).
3. An overhead power grid fire-fighting six-rotor aircraft according to claim 1, characterized in that: fire control calling mechanism (5) are including megaphone wiring (501), signal reception line (502), threaded connection spare (503), fixed shell (504), signal transmission antenna (505) and megaphone (506), the inner wall of fixed shell (504) is provided with megaphone (506), the upper end surface of fixed shell (504) is provided with signal transmission antenna (505), the lower extreme surface of fixed shell (504) is provided with threaded connection spare (503), the lower extreme surface of threaded connection spare (503) is provided with megaphone wiring (501) and signal reception line (502), megaphone wiring (501) are located one side of signal reception line (502).
4. An overhead power grid fire-fighting six-rotor aircraft according to claim 1, characterized in that: the water surface takeoff base (1) comprises an installation knob (101), a cushion pad (102), a foam board (103), a convenient installation frame (104), an illumination groove (105) and a handle groove (106), wherein the foam board (103) is arranged on the outer surface of the upper end of the cushion pad (102), the convenient installation frame (104) is arranged on the two sides of the upper end of the foam board (103), the installation knob (101) is arranged in the middle of the convenient installation frame (104), the illumination groove (105) and the handle groove (106) are formed in the outer walls of the foam board (103) and the cushion pad (102), and the handle groove (106) is located on one side of the illumination groove (105).
5. An overhead power grid fire-fighting six-rotor aircraft according to claim 1, characterized in that: multifunctional fire rescue mechanism (2) are including group battery (201), LED banks (202), connect shell (203), mount (204) and wire rod fixed hook (205), the both sides surface of connecting shell (203) all is provided with wire rod fixed hook (205), the inner wall of connecting shell (203) is provided with group battery (201), the lower extreme surface of connecting shell (203) is provided with LED banks (202), the upper end surface of connecting shell (203) is provided with mount (204).
6. An overhead power grid fire-fighting six-rotor aircraft according to claim 3, characterized in that: the inner wall of fixed shell (504) and the outer wall fixed connection of megaphone (506), the upper end surface of fixed shell (504) and the lower extreme surface fixed connection of signal transmission antenna (505), the lower extreme surface of fixed shell (504) and the upper end surface fixed connection of threaded connection spare (503), the upper end surface of megaphone wiring (501) runs through the inner wall of threaded connection spare (503) and fixed shell (504) and the inner wall electric connection of megaphone (506), the upper end surface of signal reception line (502) runs through the inner wall of fixed shell (504) and the inner wall electric connection of signal transmission antenna (505), the lower extreme surface of fire call mechanism (5) passes through threaded connection spare (503) and can dismantle with the upper end surface of aircraft main part (4) and be connected.
7. An overhead power grid fire-fighting six-rotor aircraft according to claim 4, characterized in that: the utility model discloses a take-off device, including bumper pad (102), foam board (103), the upper end surface of bumper pad (102) and the lower extreme surface fixed connection of foam board (103), the upper end both sides of foam board (103) all are connected with the lower extreme surface fixed connection of convenient mounting bracket (104), the middle part of convenient mounting bracket (104) can be dismantled with the outer wall of installation knob (101) and be connected, the quantity of handle groove (106) is two sets of, the upper end surface of water take-off base (1) can be dismantled through convenient mounting bracket (104) and installation knob (101) and be connected with the lower extreme surface of aircraft support (3).
8. An overhead power grid fire-fighting six-rotor aircraft according to claim 5, characterized in that: the utility model discloses a multifunctional fire rescue mechanism, including connection shell (203), the both sides surface of connection shell (203) all is connected with one side surface fixed connection of wire rod fixed hook (205), the inner wall of connection shell (203) and the outer wall fixed connection of group battery (201), the lower extreme surface of connection shell (203) can be dismantled with the upper end surface of LED banks (202) and be connected, the upper end surface of connection shell (203) can be dismantled with the lower extreme surface of mount (204) and be connected, be provided with the power cord between group battery (201) and LED banks (202), the middle part electric connection of one side surface of group battery (201) through power cord and LED banks (202), the upper end surface of multi-functional fire rescue mechanism (2) passes through mount (204) and can be dismantled with the outer wall of installation pole (8) and be connected.
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| CN202110975076.6A CN113460305B (en) | 2021-08-24 | 2021-08-24 | Six rotor crafts of aerial power grid fire control |
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| CN202110975076.6A CN113460305B (en) | 2021-08-24 | 2021-08-24 | Six rotor crafts of aerial power grid fire control |
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| Title |
|---|
| 段治良: "无人机在消防应急通信保障中的应用和发展探讨", 《中国管理信息化》 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN113460305B (en) | 2023-05-12 |
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