CN209739347U - Fire control is with broken window unmanned aerial vehicle - Google Patents
Fire control is with broken window unmanned aerial vehicle Download PDFInfo
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- CN209739347U CN209739347U CN201920216220.6U CN201920216220U CN209739347U CN 209739347 U CN209739347 U CN 209739347U CN 201920216220 U CN201920216220 U CN 201920216220U CN 209739347 U CN209739347 U CN 209739347U
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Abstract
The utility model discloses a fire control is with broken window unmanned aerial vehicle, including unmanned aerial vehicle main part and a plurality of rotor, each the rotor install in the unmanned aerial vehicle main part, the fixed arm is installed to the below of unmanned aerial vehicle main part, broken window saw is installed to the one end of fixed arm, and broken window hammer is installed to the other end. The utility model discloses a fire control is with broken window unmanned aerial vehicle has simple structure, fixes a position advantages such as accurate, broken window is effectual.
Description
Technical Field
The utility model mainly relates to the technical field of unmanned aerial vehicles, refer in particular to a broken window unmanned aerial vehicle for fire control.
Background
Along with the development of the society, commercial and residential buildings are higher and denser, while the development of fire-fighting equipment for high-rise buildings is not more and more consistent with the increase of the height of the buildings, once a fire occurs in the high-rise buildings, the existing fire-fighting aerial ladder cannot reach the fire-firing floor, fire fighters cannot carry out fire-fighting rescue work, and if the fire behavior cannot be controlled within the fastest time, the fire-fighting aerial ladder brings great loss to the lives and properties of people.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model lies in: to the technical problem that prior art exists, the utility model provides a simple structure's broken window unmanned aerial vehicle is used in fire control.
In order to solve the technical problem, the utility model provides a technical scheme does:
The utility model provides a fire control is with broken window unmanned aerial vehicle, includes unmanned aerial vehicle main part and a plurality of rotor, each the rotor install in the unmanned aerial vehicle main part, the fixed arm that the level was arranged is installed to the below of unmanned aerial vehicle main part, broken window saw is installed to the one end of fixed arm, and broken window hammer is installed to the other end.
As a further improvement of the above technical solution:
The window breaking hammer comprises a box body, wherein a partition plate is arranged in the middle of the box body and is used for dividing the box body into two cavities, namely a front cavity and a rear cavity; a first shaft hole is formed in the front cover plate, opposite to the partition plate, on one side of the front cavity, a second shaft hole is formed in the partition plate, and the first shaft hole and the second shaft hole are coaxially arranged and are provided with shaft sleeves; a shaft lever is arranged in the front cavity, two ends of the shaft lever are respectively installed in shaft sleeves on a first shaft hole and a second shaft hole, an impact head is installed at the end part, extending out of the first shaft hole, of the shaft lever, a baffle is sleeved on the shaft lever, the baffle is close to the first shaft hole, a limiting part used for limiting the baffle to move towards the direction of the first shaft hole is arranged on the shaft lever, and a compression spring is sleeved on the shaft lever between the baffle and the baffle; an electromagnet is arranged in the rear cavity.
the electromagnet is fastened to the inner side of the rear cover plate, opposite to the partition plate, on one side of the rear cavity through a fastener.
The rear cover plate is provided with a mounting hole, the fastener is a bolt, and the bolt penetrates through the mounting hole and is in threaded connection with a threaded hole in the electromagnet.
The limiting piece comprises a pin, and the pin is pressed into a pin hole of the shaft rod to limit the baffle in a single direction.
And an end plate is arranged at one end of the shaft lever extending into the rear cavity.
The fixed arm is followed the both sides direction of unmanned aerial vehicle main part is arranged, and is longer than at the projection length of horizontal direction unmanned aerial vehicle main part at the projection length of horizontal direction.
The unmanned aerial vehicle main body is connected with the rotor wings through connecting arms; the connecting arm comprises a front arm, a rear arm and a locking assembly; the one end of forearm is installed in the unmanned aerial vehicle main part, the one end and the rotor of postbrachium are fixed continuous, it is articulated and lock through locking Assembly between the other end of forearm and the other end of postbrachium.
The front arm is connected with a landing gear.
The quantity of rotor is 4 ~ 8, follows the circumference direction of unmanned aerial vehicle main part distributes.
Compared with the prior art, the utility model has the advantages of:
The utility model discloses a fire control is with broken window unmanned aerial vehicle installs the fixed arm on the unmanned aerial vehicle main part, installs broken window saw and broken window hammer respectively at the both ends of fixed arm, simple structure, easy dismounting; through unmanned aerial vehicle flying height and the accurate advantage of location, destroy the window of high-rise building, be convenient for to the prevention and the control of conflagration.
The utility model discloses a fire control is with broken window unmanned aerial vehicle, broken window hammer when carrying out work, switches on for the electro-magnet, after the electro-magnet switches on, produces magnetic force and attracts the axostylus axostyle to the motion of rear chamber direction, through the effect of baffle at this moment, makes compression spring compression energy storage, after the electro-magnet outage, the electro-magnet loses magnetic force, the axostylus axostyle is the high-speed impact forward under compression spring's elasticity effect, the superhard impact head (being coniform) of axostylus axostyle front end high-speed impact to window glass, smash glass, thereby; the whole structure is simple, and the operation is simple and convenient; the power supply of the electromagnet can be remotely controlled, so that the window breaking operation of remote control is realized, and the working safety is improved; in addition, the window breaking operation can be continuously carried out for many times, and the window breaking device is used for operating in areas where personnel cannot reach, such as high altitude, toxicity, high temperature and the like, and has the characteristics of high reliability, environmental protection, easiness in operation and the like.
Drawings
Fig. 1 is a schematic perspective view of the present invention.
Fig. 2 is a schematic view of the structure of the present invention.
Fig. 3 is an explosion structure diagram of the window breaking hammer of the present invention.
Fig. 4 is the assembly structure diagram of the window breaking hammer of the present invention.
The reference numbers in the figures denote: 1. an unmanned aerial vehicle main body; 2. a rotor; 3. a connecting arm; 301. a forearm; 302. a rear arm; 303. a landing gear; 4. a fixed arm; 5. breaking the window saw; 6. breaking the window hammer; 61. a box body; 6101. a front cover plate; 61011. a first shaft hole; 6102. a rear cover plate; 6103. a top plate; 6104. a base plate; 61041. mounting an ear seat; 6105. a front cavity; 6106. a rear cavity; 62. a partition plate; 6201. a second shaft hole; 63. a shaft sleeve; 64. a shaft lever; 65. a baffle plate; 66. an end plate; 67. a compression spring; 68. a limiting member; 69. an impact head; 610. an electromagnet; 611. a fastener.
Detailed Description
The invention is further described with reference to the drawings and the specific embodiments.
As shown in fig. 1 and 2, the fire control of this embodiment is with broken window unmanned aerial vehicle, including unmanned aerial vehicle main part 1 and a plurality of rotor 2, each rotor 2 is installed on unmanned aerial vehicle main part 1, and fixed arm 4 is installed through the installing support below the web of unmanned aerial vehicle main part 1, and broken window saw 5 is installed to the one end of fixed arm 4, and broken window hammer 6 is installed to the other end. Specifically, fixed arm 4 is arranged along the both sides direction (left and right direction) of unmanned aerial vehicle main part 1, and is longer than the projection length of unmanned aerial vehicle main part 1 in the horizontal direction at the horizontal direction's of horizontal direction to be convenient for carry out broken window operation. Of course, in other embodiments, the unmanned aerial vehicle main body 1 may be arranged in the front-rear direction or other directions. The utility model discloses a fire control is with broken window unmanned aerial vehicle installs fixed arm 4 on unmanned aerial vehicle main part 1, installs broken window saw 5 and broken window hammer 6 respectively at the both ends of fixed arm 4, simple structure, easy dismounting; through the high, the strong and accurate advantage of location of unmanned aerial vehicle flying height, destroy the window of high-rise building, be convenient for to the prevention and the control of conflagration.
In the embodiment, the number of the rotor wings 2 is six, and the rotor wings are distributed along the circumferential direction of the main body 1 of the unmanned aerial vehicle (for example, symmetrically distributed along two sides of the main body or uniformly distributed along the circumferential direction of the main body), so that the hovering reliability of the unmanned aerial vehicle is ensured, and the number of the rotor wings 2 is not limited herein and can be selected according to actual conditions; the unmanned aerial vehicle main body 1 is connected with each rotor wing 2 through a connecting arm 3; wherein the connecting arm 3 comprises a front arm 301, a rear arm 302 and a locking component; the one end of forearm 301 is installed on unmanned aerial vehicle main part 1, and the one end and the rotor 2 of postbrachium 302 are fixed continuous, and articulated and lock through locking Assembly (like the hasp) between the other end of forearm 301 and the other end of postbrachium 302. When not in use, the front arm 301 and the rear arm 302 can be folded mutually, so that the occupied volume is saved; in use, the front arm 301 and the rear arm 302 are opened from each other and locked by a latch. In addition, a landing gear 303 is removably attached (e.g., snapped) to the forearm 301. The unmanned aerial vehicle main body 1 is driven in an oil-electricity hybrid mode and has the advantages of long endurance, sufficient power and the like; in addition, a camera and the like are installed on the unmanned aerial vehicle main body 1, so that the window breaking operation can be observed accurately. Wherein broken window saw 5 is the electric saw selectable, and its power is provided by the power of unmanned aerial vehicle main part 1 to the break-make that can the remote control power.
as shown in fig. 3 and 4, in the present embodiment, the window breaking hammer 6 includes a box 61, a partition plate 62 is disposed in the middle of the box 61, and is used to divide the box 61 into two cavities, which are a front cavity 6105 and a rear cavity 6106, respectively, where a front cover plate 6101 is disposed on one side of the front cavity 6105 opposite to the partition plate 62, and a rear cover plate 6102 is disposed on one side of the rear cavity 6106 opposite to the partition plate 62; a first shaft hole 61011 is formed in the front cover plate 6101, a second shaft hole 6201 is formed in the partition plate 62, the first shaft hole 61011 and the second shaft hole 6201 are coaxially arranged and are provided with shaft sleeves 63; a shaft lever 64 is arranged in the front cavity 6105, two ends of the shaft lever 64 are respectively arranged in the shaft sleeves 63 on the first shaft hole 61011 and the second shaft hole 6201, and an impact head 69 is arranged at the end part of the shaft lever 64 extending out of the first shaft hole 61011; the shaft lever 64 is sleeved with a baffle plate 65, the baffle plate 65 is close to the first shaft hole 61011, the shaft lever 64 is provided with a limiting member 68 for limiting the baffle plate 65 to move towards the first shaft hole 61011, the limiting member 68 specifically comprises a pin pressed into a pin hole of the shaft lever 64, and the shaft lever 64 between the baffle plate 65 and the partition plate 62 is sleeved with a compression spring 67; an electromagnet 610 is mounted in the rear cavity 6106. When the window breaking device works, the electromagnet 610 is electrified, magnetic force is generated after the electromagnet 610 is electrified to attract the shaft lever 64 to move towards the direction of the rear cavity 6106, at the moment, the compression spring 67 is compressed to store energy through the action of the baffle 65, after the electromagnet 610 is powered off, the electromagnet 610 loses magnetic force, the shaft lever 64 is impacted forwards at high speed under the action of the elastic force of the compression spring 67, the superhard impact head 69 (in a conical shape) at the front end of the shaft lever 64 is impacted towards the window glass at high speed to break the glass, and therefore the window breaking work is completed; the whole structure is simple, and the operation is simple and convenient; the power supply of the electromagnet 610 can be remotely controlled, so that the window breaking operation of remote control is realized, and the working safety is improved; in addition, the window breaking operation can be continuously carried out for many times, and the window breaking device is used for operating in areas where personnel cannot reach, such as high altitude, toxicity, high temperature and the like, and has the characteristics of high reliability, environmental protection, easiness in operation and the like.
In this embodiment, an end plate 66 is disposed at an end of the shaft 64 extending into the back cavity 6106, so as to increase the magnetic force of the electromagnet 610 acting on the shaft 64. The back cover plate 6102 is a detachable back cover plate, and the electromagnet 610 is fastened to the inner side of the back cover plate 6102 through a fastening piece 611; specifically, the back cover plate 6102 is provided with mounting holes, the fastening members 611 are bolts, and the bolts penetrate through the mounting holes and are then screwed into the threaded holes of the electromagnet 610, so that the electromagnet 610 is fastened to the inside of the back cover plate 6102. In addition, the top plate 6103 of the box body 61 is a detachable top plate, and is fastened and connected with other side plates in a bolt manner; the bottom plate 6104 of the box 61 is provided with a mounting lug 61041, and the mounting lug 61041 is provided with a mounting hole, so that the window breaking hammer 6 can be conveniently and integrally mounted on other equipment.
In this embodiment, when the window breaking hammer 6 is assembled, the rear cover plate 6102 is firstly disassembled, the shaft lever 64 is horizontally inserted into the shaft sleeve 63 of the second shaft hole 6201, the compression spring 67 and the baffle 65 are sequentially inserted into the shaft lever 64, the shaft lever 64 is then passed out from the shaft sleeve 63 on the first shaft hole 61011, the pin is then pressed into the pin hole of the shaft lever 64, and finally the ultra-hard head 69 is installed in the hole at the front end of the shaft lever 64; then the electromagnet 610 is placed inside the back cover plate 6102, a screw hole (not shown in the figure) at the back of the electromagnet 610 is coaxial with the round hole at the center of the back cover plate 6102, then a fastener 611 composed of a bolt, an elastic gasket and a flat gasket is installed in the hole, the back cover plate 6102 and the electromagnet 610 are fixed together, wherein the power line of the electromagnet 610 extends out through the line hole of the top plate 6103; finally, the top plate 6103, the back cover 6102, and the casing 61 are assembled together.
When high-altitude window breaking is carried out, under the control of ground control personnel, the unmanned aerial vehicle provided with the remote visual system reaches a fire floor, and according to the fire behavior of a fire scene and the structure and the size of a window, a mode of cutting a window frame is determined in advance, or a scheme of directly breaking window glass is carried out for rescue; if the cutting of window is carried out earlier, then the frame lower part that the personnel of controlling control broken window saw 5 of unmanned aerial vehicle's one end is close the window cuts the operation, moves unmanned aerial vehicle to window upper portion again after the cutting finishes and cuts the operation, then aims at window glass with broken window hammer 6 one side of unmanned aerial vehicle and destroys the glass operation, until accomplishing whole broken window operation, opens up sufficient space for subsequent putting out a fire and rescue. And after the operation is finished, returning according to a set route.
Although the present invention has been described with reference to the preferred embodiments, it is not intended to limit the present invention. The technical solution of the present invention can be used by anyone skilled in the art to make many possible variations and modifications, or to modify equivalent embodiments, without departing from the scope of the technical solution of the present invention, using the technical content disclosed above. Therefore, any simple modification, equivalent change and modification made to the above embodiments by the technical entity of the present invention should fall within the protection scope of the technical solution of the present invention.
Claims (10)
1. The utility model provides a fire control is with broken window unmanned aerial vehicle, includes unmanned aerial vehicle main part (1) and a plurality of rotor (2), each rotor (2) install in on the unmanned aerial vehicle main part (1), its characterized in that, fixed arm (4) that the level was arranged are installed to the below of unmanned aerial vehicle main part (1), broken window saw (5) are installed to the one end of fixed arm (4), and broken window hammer (6) are installed to the other end.
2. a fire fighting window breaking unmanned aerial vehicle according to claim 1, wherein the window breaking hammer (6) comprises a box body (61), and a partition plate (62) is arranged in the middle of the box body (61) and is used for dividing the box body (61) into two cavities, namely a front cavity (6105) and a rear cavity (6106); a first shaft hole (61011) is formed in a front cover plate (6101) on one side of the front cavity (6105) opposite to the partition plate (62), a second shaft hole (6201) is formed in the partition plate (62), and shaft sleeves (63) are respectively installed in the first shaft hole (61011) and the second shaft hole (6201) which are coaxially arranged; a shaft lever (64) is arranged in the front cavity (6105), two ends of the shaft lever (64) are respectively arranged in shaft sleeves (63) on the first shaft hole (61011) and the second shaft hole (6201), and an impact head (69) is arranged at the end part of the shaft lever (64) extending out of the first shaft hole (61011); a baffle plate (65) is sleeved on the shaft lever (64), the baffle plate (65) is close to the first shaft hole (61011), a limiting piece (68) used for limiting the baffle plate (65) to move towards the first shaft hole (61011) is arranged on the shaft lever (64), and a compression spring (67) is sleeved on the shaft lever (64) between the baffle plate (65) and the partition plate (62); an electromagnet (610) is arranged in the rear cavity (6106).
3. A fire fighting window breaking unmanned aerial vehicle according to claim 2, wherein the electromagnet (610) is fastened to an inner side of the back cover plate (6102) opposite to the partition plate (62) at one side of the back cavity (6106) by a fastener (611).
4. The fire-fighting window breaking unmanned aerial vehicle of claim 3, wherein a mounting hole is formed in the rear cover plate (6102), the fastener (611) is a bolt, and the bolt penetrates through the mounting hole and is in threaded connection with a threaded hole in the electromagnet (610).
5. Fire fighting window breaking drone according to claim 2 or 3 or 4, characterized in that the limit (68) comprises a pin pressed into a pin hole of the shaft (64) to limit the baffle (65) unidirectionally.
6. Fire fighting window breaking unmanned aerial vehicle according to claim 2, 3 or 4, wherein an end plate (66) is provided at an end of the shaft lever (64) extending into the rear cavity (6106).
7. A fire fighting window breaking unmanned aerial vehicle according to any one of claims 1 to 4, wherein the fixing arm (4) is arranged along both side directions of the unmanned aerial vehicle main body (1), and the projection length in the horizontal direction is longer than the projection length of the unmanned aerial vehicle main body (1) in the horizontal direction.
8. A fire fighting window breaking unmanned aerial vehicle according to any one of claims 1 to 4, wherein the unmanned aerial vehicle main body (1) is connected to each rotor (2) through a connecting arm (3); the connecting arm (3) comprises a front arm (301), a rear arm (302) and a locking assembly; the one end of forearm (301) is installed on unmanned aerial vehicle main part (1), the one end and the rotor (2) of postbrachium (302) are fixed continuous, articulate and lock through locking Assembly between the other end of forearm (301) and the other end of postbrachium (302).
9. A fire fighting window breaking unmanned aerial vehicle according to claim 8, wherein a landing gear (303) is connected to the front arm (301).
10. Fire control is with broken window unmanned aerial vehicle of claim 8, characterized in that, the quantity of rotor (2) is 4 ~ 8, distributes along the circumferential direction of unmanned aerial vehicle main part (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920216220.6U CN209739347U (en) | 2019-02-20 | 2019-02-20 | Fire control is with broken window unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920216220.6U CN209739347U (en) | 2019-02-20 | 2019-02-20 | Fire control is with broken window unmanned aerial vehicle |
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| CN209739347U true CN209739347U (en) | 2019-12-06 |
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| CN201920216220.6U Active CN209739347U (en) | 2019-02-20 | 2019-02-20 | Fire control is with broken window unmanned aerial vehicle |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111870827A (en) * | 2020-07-30 | 2020-11-03 | 郑州妙灿智能科技有限公司 | Unmanned aerial vehicle for emergency rescue of high-rise fire |
| CN112439141A (en) * | 2020-12-07 | 2021-03-05 | 江苏东迈重工机械有限公司 | Buffer device in high-altitude operation protection robot |
| US20220288757A1 (en) * | 2021-03-09 | 2022-09-15 | Blake RESNICK | Drone glass breaker |
| KR20220140911A (en) * | 2021-04-09 | 2022-10-19 | 한국과학기술원 | A drone for emergency and a controlling method of the same |
| CN117504188A (en) * | 2024-01-05 | 2024-02-06 | 中影智能技术发展（福建）有限公司 | Fire extinguishing type unmanned helicopter for high-rise fire control |
-
2019
- 2019-02-20 CN CN201920216220.6U patent/CN209739347U/en active Active
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111870827A (en) * | 2020-07-30 | 2020-11-03 | 郑州妙灿智能科技有限公司 | Unmanned aerial vehicle for emergency rescue of high-rise fire |
| CN111870827B (en) * | 2020-07-30 | 2021-06-15 | 山东龙翼航空科技有限公司 | Unmanned aerial vehicle for emergency rescue of high-rise fire |
| CN112439141A (en) * | 2020-12-07 | 2021-03-05 | 江苏东迈重工机械有限公司 | Buffer device in high-altitude operation protection robot |
| US20220288757A1 (en) * | 2021-03-09 | 2022-09-15 | Blake RESNICK | Drone glass breaker |
| KR20220140911A (en) * | 2021-04-09 | 2022-10-19 | 한국과학기술원 | A drone for emergency and a controlling method of the same |
| KR102571270B1 (en) | 2021-04-09 | 2023-08-30 | 한국과학기술원 | A drone for emergency and a controlling method of the same |
| CN117504188A (en) * | 2024-01-05 | 2024-02-06 | 中影智能技术发展（福建）有限公司 | Fire extinguishing type unmanned helicopter for high-rise fire control |
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