CN208715484U - A kind of lifesaving aircraft - Google Patents
A kind of lifesaving aircraft Download PDFInfo
- Publication number
- CN208715484U CN208715484U CN201821330646.6U CN201821330646U CN208715484U CN 208715484 U CN208715484 U CN 208715484U CN 201821330646 U CN201821330646 U CN 201821330646U CN 208715484 U CN208715484 U CN 208715484U
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- CN
- China
- Prior art keywords
- master station
- lifesaving
- connect
- striker
- transmission module
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Abstract
The utility model discloses a kind of lifesaving aircraft, including aircraft, aircraft includes master station, flight computer interconnected is respectively arranged with inside master station, remote control receiver unit and supplying cell, it further include multiple rotor racks that master control lateral wall is set, master station lateral wall is also respectively provided with wireless image transmission mould, camera and infrared distance sensor, figure transmission module is connected with camera, figure transmission module and infrared distance sensor are connect with flight computer respectively, master station bottom surface is respectively arranged with electromagnet apparatus and lifesaving appliance, the lifesaving appliance is mounted in master station bottom surface by electromagnet apparatus, it further include the remote controler being connect with remote control receiver unit, the monitoring computer being connect with wireless image transmission module;This waters deliverance apparatus can find quickly the position of drowning people in high-altitude, and the movement velocity of this deliverance apparatus is fast, not need rescuer and enter water to sue and labour, and rescue efficiency is high.
Description
Technical field
The utility model belongs to lifesaving appliance technical field, and in particular to a kind of lifesaving aircraft.
Background technique
Nowadays, the careless overboard event of being drowned that man-made lake waters occurs is commonplace, and as country advocates people and oneself
Right harmonious coexistence Development strategy, man-made lake waters are increasingly paid attention to by country, many regional Development control area man-made lake waters energetically,
But potential security risk is not considered while development & construction.Relatively reliable man-made lake waters rescue system is not built
System, if personnel are accidentally overboard, none rescue method rapidly and efficiently is generated.Therefore, a kind of reliable, quick man-made lake
Waters early warning, the construction of rescue system can solve existing man-made lake waters security risk.
Utility model content
The purpose of the utility model is to provide a kind of lifesaving aircraft, provide a kind of reliable, quick waters rescue dress
It sets.
The utility model is respectively arranged with interconnection inside master station the technical scheme adopted is that including master station
Flight computer, remote control receiver unit and supplying cell, further include multiple rotor racks that master control lateral wall is set, master control
Platform lateral wall is also respectively provided with wireless image transmission mould, camera and infrared distance sensor, and figure transmission module is connected with camera, figure
Transmission module and infrared distance sensor are connect with flight computer respectively, the bottom surface of master station be respectively arranged with electromagnet apparatus and
Lifesaving appliance, the lifesaving appliance are mounted in master station bottom surface by electromagnet apparatus, further include connecting with remote control receiver unit
Remote controler, the monitoring computer connecting with wireless image transmission module, electromagnet apparatus includes iron core, the coil that is wrapped on iron core,
It further include DC power supply and switch, DC power supply is connect with coil, and switch is connect with flight computer, and iron core is fixed on master station
Bottom surface.
The utility model is also characterized by:
Each rotor rack includes the horn that master station lateral wall is arranged in, the other end of horn set gradually upwards whether there is or not
The main shaft of brush motor and propeller, brushless motor is connect with propeller, and brushless motor is also connect with flight computer.
Lifesaving appliance includes type inflatable life buoy and self-filler, and the side of type inflatable life buoy is provided with iron plate),
Type inflatable life buoy is connect by iron plate with electromagnet apparatus, and self-filler includes small gas cylinder, the opening of small gas cylinder
Place is provided with hollow bottle stopper, and gas outlet is provided on the side wall of bottle stopper, and gas outlet is connected by check-valves and type inflatable life buoy
It connects, bottle stopper is internally provided with the first striker, another end face of bottle stopper is additionally provided with water-soluble priming device, water-soluble priming device packet
The shell connecting with the end face of bottle stopper is included, the enclosure interior of shell is respectively arranged with sequentially connected water-soluble tablet, the second striker
And spring, water-soluble tablet is located among the first striker and the second striker and the first striker, water-soluble tablet, the second striker and spring position
In on same straight line, spring is fixed on the inner sidewall of shell.
Several water inlets are provided on the outside of shell.
Gyroplane erection is equipped with 4, and electromagnet apparatus and lifesaving appliance are respectively arranged with 4, each lifesaving appliance with
Corresponding electromagnet apparatus connection.
The bottom surface of master station is additionally provided with support frame.
The beneficial effects of the utility model are: a kind of lifesaving aircraft of the utility model, aircraft can be quickly in high-altitude
The position for finding drowning people, and flying speed is fast, can shorten rescue time to reach drowning people overhead in the short time;It rescues
Small gas cylinder gas rate of release in generating apparatus is fast, i.e. inflatable in type inflatable life buoy several seconds to finish, and saves in time overboard
Personnel, the deliverance apparatus of the utility model do not need personnel and enter water to sue and labour, and eliminate the risk that rescuer drowns, while this reality
With novel device using when be swift in response, shorten man overboard's rescue time, improve rescue efficiency.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of lifesaving aircraft of the utility model;
Fig. 2 is a kind of lifesaving aircraft principle modules structural schematic diagram schematic diagram of the utility model;
Fig. 3 is bottom view in a kind of lifesaving aircraft of the utility model;
Fig. 4 is electromagnet apparatus structural schematic diagram in a kind of lifesaving aircraft of the utility model;
Fig. 5 is schematic diagram when lifesaving appliance is unfolded in a kind of lifesaving aircraft of the utility model;
Fig. 6 is the structural schematic diagram of self-filler in a kind of lifesaving aircraft of the utility model.
In figure, 1. master stations, 2. flight computers, 3. remote control receiver units, 4. supplying cells, 5. wireless image transmission modules,
6. electromagnet apparatus, 6-1. DC power supply, 6-2. switch, 6-3. coil, 6-4. iron core, 7. lifesaving appliances, 8. automatic inflatings dress
It sets, the gas outlet 8-1., 8-2. small gas cylinder, 8-3. check-valves, 8-4. bottle stopper, the first striker of 8-5., the water-soluble tablet of 8-6., 8-7.
Second striker, 8-8. spring, 8-9. iron plate, 8-10. shell, 9. rotor racks, 9-1. horn, 9-2. brushless motor, 9-3. spiral shell
Revolve paddle, 10. type inflatable life buoys, 11. infrared distance sensors, 12. cameras, 13. support frames.
Specific embodiment
The utility model is described in detail with reference to the accompanying drawings and detailed description.
A kind of lifesaving aircraft of the utility model is set inside master station 1 respectively as shown in Figure 1 and Figure 2, including master station 1
It is equipped with flight computer 2, remote control receiver unit 3 and supplying cell 4 interconnected, further includes being uniformly arranged on outside master station 1
Multiple rotor racks 9 of side wall, each rotor rack 9 include the horn 9-1 that 1 lateral wall of master station is arranged in, and horn 9-1's is another
One end is disposed with brushless motor 9-2 and propeller 9-3 upwards, and the main shaft of brushless motor 9-2 is connect with propeller 9-3, nothing
Brush motor 9-2 is also connect with flight computer 2;As shown in figure 3, be also respectively provided on the outside of master station 1 wireless image transmission module 5,
Camera 12 and infrared distance sensor 11, wireless image transmission module 5 and camera 12 connect, wireless image transmission module 5 and infrared survey
It is connect respectively with flight computer 2 away from sensor 11, the bottom surface of master station 1 is respectively arranged with electromagnet apparatus 6 and lifesaving appliance
7, lifesaving appliance 7 is mounted in 1 bottom surface of master station by electromagnet apparatus 6, as shown in figure 4, electromagnet apparatus 6 includes iron core 6-4, twines
The coil 6-3 being wound on iron core 6-4, further includes DC power supply 6-1 and switch 6-2, and DC power supply 6-1 connect with coil 6-3, opens
It closes 6-2 to connect with flight computer 2, iron core 6-4 is fixed on the bottom surface of master station 1;As shown in figure 5, lifesaving appliance 7 includes inflation
Formula lifebuoy 10 and self-filler 8, as shown in fig. 6, the side of type inflatable life buoy 10 is provided with iron plate 8-9, inflatable
Lifebuoy 10 is connect by iron plate 8-9 with electromagnet apparatus 6, and self-filler 8 includes small gas cylinder 8-2, small gas cylinder 8-2
Opening be provided with hollow bottle stopper 8-4, gas outlet 8-1 is provided on the side wall of bottle stopper 8-4, gas outlet 8-1 passes through non-return
Valve 8-3 is connect with type inflatable life buoy 10, and bottle stopper 8-4 is internally provided with the first striker 8-5, and another end face of bottle stopper 8-4 is also
It is provided with water-soluble priming device, water-soluble priming device includes the shell 8-10 connecting with the end face of bottle stopper 8-4, the shell of shell 8-10
Internal body portion is not provided with sequentially connected water-soluble tablet 8-6, the second striker 8-7 and spring 8-8, and water-soluble tablet 8-6 is located at the
Among one striker 8-5 and the second striker 8-7 and the first striker 8-5, water-soluble tablet 8-6, the second striker 8-7 and spring 8-8 are located at
On same straight line, spring 8-8 is fixed on the inner sidewall of shell 8-10, and several water inlets are provided on the outside of shell 8-10;
It further include the remote controler being connect with remote control receiver unit 3, the monitoring computer being connect with wireless image transmission module 5;The bottom of master station 1
Face is additionally provided with support frame 13, and support frame 13 parks support on ground convenient for aircraft.
Rotor rack 9 is provided with 4, and electromagnet apparatus 6 and lifesaving appliance 7 are respectively arranged with 4, each lifesaving appliance
7 connect with corresponding electromagnet apparatus 6.
A kind of one quadrotor of lifesaving aircraft of the utility model is platform, carries wireless image transmission mould on board the aircraft
Block 5, camera 12 and infrared distance sensor 11, camera 12 will acquire surface condition and the novel acquisition of flight path
Video information be transmitted to wireless image transmission module 5, the information that wireless image transmission module 5 acquires respectively issues flight computer 2 and monitoring
Computer, the flying height information for the aircraft that infrared distance sensor 11 will test are transmitted to flight computer 2, and monitoring calculates
Machine examination measure someone person it is drowned after, staff is by controlling remote remote control aircraft, and then flight computer 2 is to flying
The flight path of row device is controlled, and control aircraft flies to above drowning person, while control switch 6-2 is disconnected, and is completed to filling
The dispensing of gas formula lifesaving appliance 7, after lifesaving appliance 7 is overboard, water enters water-soluble priming device from the water inlet on shell 8-10, makes
Water-soluble tablet 8-6 is obtained quickly to dissolve, under the pressure effect of spring 8-8, direction bullet of the second striker 8-7 to separate spring 8-8
Out, it hits the first striker 8-5, the first striker 8-5 and wears out bottle stopper 8-4, the carbon dioxide gas inside small gas cylinder 8-2 enters bottle
Plug 8-4 simultaneously enters type inflatable life buoy 10 by check-valves 8-3, and drowning man catches inflatable life preserver later, completes to overboard
The rescue work of personnel;The waters flight deliverance apparatus of the utility model, electromagnet power supply are adopted with flight instruments supplying cell
With independently-powered, electromagnet is by switch control, and be powered absorption, power-off release, has 4 lifesaving appliances, aircraft on aircraft
Equipped with 4 lifesaving appliances 7, thereon by electromagnet absorption, lifesaving appliance 7 is equipped on aircraft in advance, once occur
Dangerous situation can be used directly, electromagnet small power consumption, heat up low, power off without remanent magnetism.
By the above-mentioned means, this waters deliverance apparatus can find quickly the position of drowning people in high-altitude, this deliverance apparatus
Movement velocity is fast, and drowning people overhead can be reached in the short time, shortens rescue time, while lifesaving appliance is inflated also rapidly,
Release, inflation movement can be completed within several seconds, carry out rescue work, the present apparatus can solve multiple drowning peoples, and be not required to
It wants rescuer to enter water rescue, eliminates the drowned risk of rescuer.
Claims (6)
1. a kind of lifesaving aircraft, which is characterized in that including master station (1), be respectively arranged with inside the master station (1) mutually
Flight computer (2), remote control receiver unit (3) and the supplying cell (4) of connection, further include setting the master station (1) outside
Multiple rotor racks (9) of side wall, master station (1) lateral wall are also respectively provided with wireless image transmission module (5), camera
(12) with infrared distance sensor (11), the figure transmission module (5) and camera (12) connection, the figure transmission module (5) and red
Outer distance measuring sensor (11) connect with the flight computer (2) respectively, and the bottom surface of the master station (1) is respectively arranged with electromagnetism
Iron device (6) and lifesaving appliance (7), the lifesaving appliance (7) are mounted in the master station (1) by the electromagnet apparatus (6)
Bottom surface further includes the remote controler connecting with the remote control receiver unit (3), the monitoring connecting with the wireless image transmission module (5)
Computer, the electromagnet apparatus (6) include iron core (6-4), the coil (6-3) being wrapped on the iron core (6-4), further include
DC power supply (6-1) and switch (6-2), the DC power supply (6-1) connect with the coil (6-3), the switch (6-2) and
Flight computer (2) connection, the iron core (6-4) are fixed on the bottom surface of the master station (1).
2. a kind of lifesaving aircraft according to claim 1, which is characterized in that each rotor rack (9) includes setting
The horn (9-1) in master station (1) lateral wall is set, the other end of the horn (9-1) is disposed with brushless motor (9- upwards
2) it is connect with propeller (9-3), the main shaft of the brushless motor (9-2) with the propeller (9-3), the brushless motor (9-
2) it is also connect with the flight computer (2).
3. a kind of lifesaving aircraft according to claim 1, which is characterized in that the lifesaving appliance (7) includes inflatable
The side of lifebuoy (10) and self-filler (8), the type inflatable life buoy (10) is provided with iron plate (8-9), described to fill
Gas formula lifebuoy (10) is connect by the iron plate (8-9) with the electromagnet apparatus (6), self-filler (8) packet
It includes small gas cylinder (8-2), the opening of the small gas cylinder (8-2) is provided with hollow bottle stopper (8-4), the bottle stopper (8-4)
Side wall on be provided with gas outlet (8-1), the gas outlet (8-1) passes through check-valves (8-3) and the type inflatable life buoy
(10) it connects, the bottle stopper (8-4) is internally provided with the first striker (8-5), another end face of the bottle stopper (8-4) is also set up
There is water-soluble priming device, the water-soluble priming device includes the shell (8-10) connecting with the end face of the bottle stopper (8-4), described
The enclosure interior of shell (8-10) is respectively arranged with sequentially connected water-soluble tablet (8-6), the second striker (8-7) and spring (8-
8), the water-soluble tablet (8-6) is located at first striker (8-5) and the second striker (8-7) centre and the first striker (8-
5), water-soluble tablet (8-6), the second striker (8-7) and spring (8-8) are located along the same line, and the spring (8-8) is fixed on institute
On the inner sidewall for stating shell (8-10).
4. a kind of lifesaving aircraft according to claim 3, which is characterized in that the lateral wall of the shell (8-10) is arranged
There are several water inlets.
5. a kind of lifesaving aircraft according to claim 1, which is characterized in that the rotor rack (9) is provided with 4,
The electromagnet apparatus (6) and lifesaving appliance (7) are respectively arranged with 4, each lifesaving appliance (7) and corresponding electromagnetism
Iron device (6) connection.
6. a kind of lifesaving aircraft according to claim 1, which is characterized in that the bottom surface of the master station (1) is also set up
There are support frame (13).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201821330646.6U CN208715484U (en) | 2018-08-17 | 2018-08-17 | A kind of lifesaving aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201821330646.6U CN208715484U (en) | 2018-08-17 | 2018-08-17 | A kind of lifesaving aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
CN208715484U true CN208715484U (en) | 2019-04-09 |
Family
ID=65978105
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201821330646.6U Expired - Fee Related CN208715484U (en) | 2018-08-17 | 2018-08-17 | A kind of lifesaving aircraft |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN208715484U (en) |
-
2018
- 2018-08-17 CN CN201821330646.6U patent/CN208715484U/en not_active Expired - Fee Related
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190409 Termination date: 20190817 |