CN214138990U - Fire rescue detection aircraft - Google Patents
Fire rescue detection aircraft Download PDFInfo
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- CN214138990U CN214138990U CN202023321908.2U CN202023321908U CN214138990U CN 214138990 U CN214138990 U CN 214138990U CN 202023321908 U CN202023321908 U CN 202023321908U CN 214138990 U CN214138990 U CN 214138990U
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Abstract
The utility model discloses a fire rescue detection aircraft, including casing, apron, rotor device, rotor protection frame, safety frame, fuselage, camera, warning public address device, casing upper surface center is equipped with the warning public address device, casing lower surface center is equipped with the fuselage, the casing side is equipped with the camera, the casing is installed all around the rotor protection frame, rotor protection frame with apron lateral surface fixed connection, the apron top is equipped with the rotor device, safety frame installs perpendicularly at the casing lower surface, adopts fire-retardant material and refractory material, can adapt to adverse circumstances; the aerial shouting or forwarding instruction is realized by utilizing the aircraft, so that the shouting or instruction can be more effective than the ground; the bottom flame sensor detects flame and can transmit signals to the control panel in real time; the influence of vibration on machine body parts is reduced; the aircraft is equipped with rotor protection frame all around, can the anticollision.
Description
Technical Field
The utility model relates to a fire rescue detection aircraft field, concretely relates to fire rescue detection aircraft.
Background
Compared with conventional fire-fighting equipment, the fire-fighting unmanned aerial vehicle is an aircraft capable of realizing aerial operation, and can replace people to go deep into the field, so that manpower is effectively saved, and casualty rate is reduced. However, the function is comprehensive in the existing market, and the performance is good, but can advance the fire control unmanned aerial vehicle of scene of a fire executive task very fewly, and current many rotor type unmanned aerial vehicle is because technical limitation, the function singleness, and adverse circumstances can not use, and the unable fine command scheduling problem of giving down of ground operating personnel has restricted unmanned aerial vehicle in the application of fire control field.
Disclosure of Invention
In view of the above-described deficiencies or inadequacies in the prior art, it would be desirable to provide a fire rescue detection aircraft.
According to the technical scheme that this application embodiment provided, aircraft is surveyed in fire rescue, including casing, apron, rotor device, rotor protection frame, safety frame, fuselage, camera, warning public address set, casing upper surface center is equipped with warning public address set, casing lower surface center is equipped with the fuselage, the casing side is equipped with the camera, the casing is installed all around rotor protection frame, rotor protection frame with apron lateral surface fixed connection, the apron top is equipped with the rotor device, safety frame installs perpendicularly the casing lower surface.
The utility model discloses in, the casing is X shape structure, casing four corners side is equipped with the locating hole, be equipped with on the apron with the supporting mounting hole of locating hole, the apron pass through the bolt the mounting hole the locating hole with the casing is connected.
The utility model discloses in, the rotor protection frame with apron structure as an organic whole, the rotor protection frame is fan-shaped frame construction of class.
The utility model discloses in, the rotor device includes wing, screw cap, motor, wing quantity has 2, the wing with screw cap structure as an organic whole, the screw cap is installed through internal thread in the motor shaft, the motor is installed casing upper surface is all around, the motor is connected to through the cable the fuselage.
The utility model discloses in, safety frame quantity has 2, for U type structure, locates respectively the fuselage both sides.
The utility model discloses in, be equipped with flame sensor and control panel in the fuselage, the rotor device the warning public address set flame sensor is connected to through the cable respectively the control panel.
The utility model discloses in, be equipped with megaphone and alarm in the warning public address set, the megaphone with the alarm is connected to through the cable respectively the fuselage.
The utility model discloses in, fire rescue surveys the aircraft and is fire-retardant material, and the surface coating has corrosion-resistant and high temperature resistance coating.
To sum up, the beneficial effect of this application: the body is high temperature resistant and can adapt to severe environment by adopting flame-retardant materials and refractory materials; the top of the aircraft is provided with the loudspeaker and the alarm, the aircraft is used for realizing air shouting or forwarding instructions, the ground shouting or instructions can be more effective, and the aircraft is suitable for rescuing in high-altitude and high-rise fire-fighting projects; the bottom flame sensor detects flame and can transmit signals to the control panel in real time; the safety frame is arranged at the bottom of the aircraft, so that the aircraft can land safely, and the influence of vibration on the machine body parts is reduced; the aircraft is equipped with rotor protection frame all around, can the anticollision, the protection rotor to effectively avoid the aircraft flight in-process to cause the harm to object on every side.
Drawings
Other features, objects and advantages of the present application will become more apparent upon reading of the following detailed description of non-limiting embodiments thereof, made with reference to the accompanying drawings in which:
FIG. 1 is a perspective view of the present invention;
fig. 2 is a top view of the present invention;
fig. 3 is a structure view of the rotor device of the present invention.
Reference numbers in the figures: a case-1; a cover plate-2; a rotor device-3; a rotor wing protection frame-4; a safety frame-5; a fuselage-6; a camera-7; alarm amplification device-8; wing-3.1; 3.2 of a screw cap; motor-3.3.
Detailed Description
The present application will be described in further detail with reference to the following drawings and examples. It is to be understood that the specific embodiments described herein are merely illustrative of the relevant invention and not restrictive of the invention. It should be noted that, for convenience of description, only the portions related to the present invention are shown in the drawings.
It should be noted that the embodiments and features of the embodiments in the present application may be combined with each other without conflict. The present application will be described in detail below with reference to the embodiments with reference to the attached drawings.
As shown in fig. 1-3, fire rescue detection aircraft, including casing 1, apron 2, rotor device 3, rotor protection frame 4, safety frame 5, fuselage 6, camera 7, warning public address set 8, 1 upper surface center of casing is equipped with warning public address set 8, 1 lower surface center of casing is equipped with fuselage 6, 1 side of casing is equipped with camera 7, install all around casing 1 rotor protection frame 4, rotor protection frame 4 with 2 lateral surfaces fixed connection of apron, 2 tops of apron are equipped with rotor device 3, safety frame 5 is installed perpendicularly the 1 lower surface of casing. The casing 1 is of an X-shaped structure, positioning holes are formed in the side faces of four corners of the casing 1, mounting holes matched with the positioning holes are formed in the cover plate 2, and the cover plate 2 is connected with the casing 1 through bolts, the mounting holes and the positioning holes. Rotor protection frame 4 with apron 2 structure as an organic whole, rotor protection frame 4 is fan-shaped frame structure of class. Rotor device 3 includes wing 3.1, spiral shell 3.2, motor 3.3, wing 3.1 quantity has 2, wing 3.1 with spiral shell 3.2 structure as an organic whole, spiral shell 3.2 is installed through internal thread in the motor 3.3 pivot, motor 3.3 is installed around 1 upper surface of casing, motor 3.3 is connected to through the cable fuselage 6. The number of the safety racks 5 is 2, the safety racks are of U-shaped structures and are respectively arranged on two sides of the machine body 6. Be equipped with flame sensor and control panel in the fuselage 6, rotor device 3 alarm public address set 8 the flame sensor is connected to through the cable respectively the control panel. A loudspeaker and an alarm are arranged in the alarm sound amplification device 8, and the loudspeaker and the alarm are connected to the machine body 6 through cables respectively. The fire rescue detection aircraft is made of flame-retardant materials, and the outer surface of the fire rescue detection aircraft is coated with a corrosion-resistant and high-temperature-resistant coating.
The body is high temperature resistant and can adapt to severe environment by adopting flame-retardant materials and refractory materials; the top of the aircraft is provided with the loudspeaker and the alarm, the aircraft is used for realizing air shouting or forwarding instructions, the ground shouting or instructions can be more effective, and the aircraft is suitable for rescuing in high-altitude and high-rise fire-fighting projects; the flame sensor is arranged below the aircraft and used for detecting whether flames exist in the flying process, and if the flames are sensed, signals can be transmitted to the control panel in real time; the safety frame is arranged at the bottom of the aircraft, so that the aircraft can land safely, and the influence of vibration on the machine body parts is reduced; the aircraft is equipped with rotor protection frame all around, can the anticollision, the protection rotor to effectively avoid the aircraft flight in-process to cause the harm to object on every side.
The foregoing description is only exemplary of the preferred embodiments of the application and is provided for the purpose of illustrating the general principles of the technology and the like. Meanwhile, the scope of the invention according to the present application is not limited to the technical solutions in which the above-described technical features are combined in a specific manner, and also covers other technical solutions in which the above-described technical features or their equivalent are combined arbitrarily without departing from the inventive concept described above. For example, the above features may be replaced with (but not limited to) features having similar functions disclosed in the present application.
Claims (8)
1. Aircraft is surveyed in fire rescue, including casing (1), apron (2), rotor device (3), rotor protection frame (4), safety frame (5), fuselage (6), camera (7), warning public address set (8), characterized by: casing (1) upper surface center is equipped with warning public address set (8), casing (1) lower surface center is equipped with fuselage (6), casing (1) side is equipped with camera (7), install all around casing (1) rotor protection frame (4), rotor protection frame (4) with apron (2) lateral surface fixed connection, apron (2) top is equipped with rotor device (3), safety shelf (5) are installed perpendicularly casing (1) lower surface.
2. A fire rescue detection aircraft as claimed in claim 1, wherein: the casing (1) is of an X-shaped structure, positioning holes are formed in the side faces of four corners of the casing (1), mounting holes matched with the positioning holes are formed in the cover plate (2), and the cover plate (2) is connected with the casing (1) through bolts, the mounting holes and the positioning holes.
3. A fire rescue detection aircraft as claimed in claim 1, wherein: rotor protection frame (4) with apron (2) structure as an organic whole, rotor protection frame (4) are fan-shaped frame structure of class.
4. A fire rescue detection aircraft as claimed in claim 1, wherein: rotor device (3) are including wing (3.1), spiral shell cap (3.2), motor (3.3), wing (3.1) quantity has 2, wing (3.1) with spiral shell cap (3.2) structure as an organic whole, install through internal thread spiral shell cap (3.2) in motor (3.3) pivot, install motor (3.3) casing (1) upper surface is all around, motor (3.3) are connected to through the cable fuselage (6).
5. A fire rescue detection aircraft as claimed in claim 1, wherein: the number of the safety racks (5) is 2, the safety racks are of U-shaped structures and are respectively arranged on two sides of the machine body (6).
6. A fire rescue detection aircraft as claimed in claim 1, wherein: be equipped with flame sensor and control panel in fuselage (6), rotor device (3) warning public address set (8) flame sensor is connected to through the cable respectively the control panel.
7. A fire rescue detection aircraft as claimed in claim 1, wherein: a loudspeaker and an alarm are arranged in the alarm sound amplification device (8), and the loudspeaker and the alarm are connected to the machine body (6) through cables respectively.
8. A fire rescue detection aircraft as claimed in claim 1, wherein: the fire rescue detection aircraft is made of flame-retardant materials, and the outer surface of the fire rescue detection aircraft is coated with a corrosion-resistant and high-temperature-resistant coating.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023321908.2U CN214138990U (en) | 2020-12-31 | 2020-12-31 | Fire rescue detection aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023321908.2U CN214138990U (en) | 2020-12-31 | 2020-12-31 | Fire rescue detection aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214138990U true CN214138990U (en) | 2021-09-07 |
Family
ID=77545260
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023321908.2U Active CN214138990U (en) | 2020-12-31 | 2020-12-31 | Fire rescue detection aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214138990U (en) |
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2020
- 2020-12-31 CN CN202023321908.2U patent/CN214138990U/en active Active
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