CN210761297U - Multifunctional emergency rescue unmanned aerial vehicle - Google Patents
Multifunctional emergency rescue unmanned aerial vehicle Download PDFInfo
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- CN210761297U CN210761297U CN201921869874.5U CN201921869874U CN210761297U CN 210761297 U CN210761297 U CN 210761297U CN 201921869874 U CN201921869874 U CN 201921869874U CN 210761297 U CN210761297 U CN 210761297U
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Abstract
The utility model provides a multi-functional emergency rescue unmanned aerial vehicle relates to unmanned air vehicle technical field, which comprises an outer shell, surface one side fixedly connected with steering mechanism of shell, bottom one side fixedly connected with bracing piece of shell, the one end fixedly connected with flight ring of bracing piece, the internal surface one side fixedly connected with connecting rod of flight ring, there is the screw one side of connecting rod, the fixedly connected with lithium cell between the internal surface both sides of shell, the bottom that just is located the lithium cell between the internal surface both sides of shell is provided with rescue device, the bottom that just is located rescue device between the internal surface both sides of shell is provided with the radio signal receiver. The unmanned aerial vehicle solves the problems that most of the existing unmanned aerial vehicles are used for simple shooting and convenient application such as air monitoring, and people who are in danger of drowning cannot be provided with remote and timely help, and long-term development of the unmanned aerial vehicle is not facilitated.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field especially relates to a multi-functional emergency rescue unmanned aerial vehicle.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand the industrial application and develop the unmanned aerial vehicle technology.
The current unmanned aerial vehicle mostly carries out some simple shootings and carries out convenient applications such as air monitering, still can not give the crowd that receives drowned danger and carry out long-range timely help, is unfavorable for unmanned aerial vehicle's long-term development.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Not enough to prior art, the utility model provides a multi-functional emergency rescue unmanned aerial vehicle possesses the advantage that can carry out timely rescue to drowned people, has solved current unmanned aerial vehicle and has not carried out the problem of the application in the aspect of rescuing to drowned crowd.
(II) technical scheme
In order to realize the above-mentioned purpose that can carry out timely succour to drowned people, the utility model provides a following technical scheme: the utility model provides a multi-functional emergency rescue unmanned aerial vehicle, includes the shell, surface one side fixedly connected with steering mechanism of shell, bottom one side fixedly connected with bracing piece of shell, the one end fixedly connected with flight ring of bracing piece, the internal surface one side fixedly connected with connecting rod of flight ring, there is the screw one side of connecting rod, fixedly connected with lithium cell between the internal surface both sides of shell, the bottom that just is located the lithium cell between the internal surface both sides of shell is provided with the rescue device, just the bottom that is located the rescue device between the internal surface both sides of shell is provided with the radio signal receiver.
Preferably, the rescue device includes the framework, be fixed connection between the surface both sides of framework and the internal surface both sides of shell, top one side of framework is provided with the air inlet net, the bottom of framework is provided with the bottom plate, be provided with the joint tape between one side of bottom plate and the bottom opposite side of framework, the bottom of framework is provided with the life buoy, fixedly connected with diaphragm between the internal surface both sides of framework, the top of diaphragm is provided with the air pump, the end of giving vent to anger of air pump is provided with the gas tube, the top of diaphragm and the one side that is located the air pump are provided with wireless control mechanism.
Preferably, the material of the air inlet net is non-woven fabrics, and one side of the bottom plate is rotatably connected with one side of the bottom of the frame body.
Preferably, the material of the connecting adhesive tape is transparent adhesive tape, and the other side of the bottom plate is in contact with the other side of the bottom of the frame body.
Preferably, one end of the inflation tube is communicated with the air outlet end of the air pump, and the other end of the inflation tube is communicated with the inflation port of the life buoy.
Preferably, the number of the flight rings is four, and a driving motor is arranged at the axis of the propeller.
(III) advantageous effects
Compared with the prior art, the utility model provides a multi-functional emergency rescue unmanned aerial vehicle possesses following beneficial effect:
the utility model discloses in, the rescue device of adoption, the realization can carry out timely rescue to drowned people, when needs use, start driving motor earlier, it rotates to drive the screw, make unmanned aerial vehicle can take off, then control flight position through radio signal receiver and steering mechanism, make it remove the top that needs the rescue personnel, then through wireless control mechanism, start the air pump, make the air pump pass through the gas tube and aerify the life buoy, make the increase of volume of life buoy, then ejecting bottom plate when increasing to the certain degree, make the sticky tape tear, make the bottom plate open downwards, then the life buoy falls near drowned personnel under the effect of gravity, give drowned personnel's help, be convenient for carry out the rescue that comes off.
Drawings
Fig. 1 is a schematic view of the overall structure of a multifunctional emergency rescue unmanned aerial vehicle provided by the utility model;
fig. 2 is a schematic view of the internal structure of the housing of the multifunctional emergency rescue unmanned aerial vehicle provided by the utility model;
fig. 3 is the utility model provides a rescue device's among multi-functional emergency rescue unmanned aerial vehicle structure schematic diagram.
Illustration of the drawings:
1. a housing; 2. a steering mechanism; 3. a support bar; 4. a flying ring; 5. a connecting rod; 6. a propeller; 7. a lithium battery; 8. a rescue device; 81. a frame body; 82. an air inlet net; 83. a base plate; 84. connecting an adhesive tape; 85. a life buoy; 86. a transverse plate; 87. an air pump; 88. an inflation tube; 89. a wireless control mechanism; 9. a wireless signal receiver.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand and understand, the present invention is further described below with reference to the following embodiments.
Referring to fig. 1-3, a multi-functional emergency rescue unmanned aerial vehicle, including shell 1, surface one side fixedly connected with steering mechanism 2 of shell 1, bottom one side fixedly connected with bracing piece 3 of shell 1, the one end fixedly connected with flight ring 4 of bracing piece 3, internal surface one side fixedly connected with connecting rod 5 of flight ring 4, there is screw 6 one side of connecting rod 5, fixedly connected with lithium cell 7 between the internal surface both sides of shell 1, the bottom that just is located lithium cell 7 between the internal surface both sides of shell 1 is provided with rescue device 8, the bottom that just is located rescue device 8 between the internal surface both sides of shell 1 is provided with wireless signal receiver 9.
Further, the rescue device 8 includes a frame 81, two sides of the outer surface of the frame 81 are fixedly connected to two sides of the inner surface of the housing 1, an air inlet net 82 is disposed on one side of the top of the frame 81, a bottom plate 83 is disposed on the bottom of the frame 81, a connecting adhesive tape 84 is disposed between one side of the bottom plate 83 and the other side of the bottom of the frame 81, a life ring 85 is disposed on the bottom of the frame 81, a transverse plate 86 is fixedly connected between two sides of the inner surface of the frame 81, an air pump 87 is disposed on the top of the transverse plate 86, a power line of the air pump 87 is electrically connected to the lithium battery 7, the air pump 87 is in a type of VAY8828, an air outlet end of the air pump 87 is provided with an air charging pipe 88, a wireless control mechanism 89 is disposed on one side of the.
Furthermore, the air inlet net 82 is made of non-woven fabric, and one side of the bottom plate 83 is rotatably connected with one side of the bottom of the frame 81, so that the air inlet net is not blocked when being inflated.
Further, the connecting tape 84 is made of a transparent tape, and the other side of the bottom plate 83 is in contact with the other side of the bottom of the frame 81, so that the bottom plate 83 can be opened conveniently.
Further, one end of the inflation tube 88 is communicated with the air outlet end of the air pump 87, and the other end of the inflation tube 88 is communicated with the inflation port of the life buoy 85, so that the inflation speed is higher.
Further, the number of flight ring 4 is four groups, and the axle center department of screw 6 is provided with driving motor for unmanned aerial vehicle is more stable when flying.
The utility model discloses a theory of operation and use flow: rescue device 8 through setting up, the realization can carry out timely rescue to drowned people, when needs use, start driving motor earlier, drive screw 6 and rotate, make unmanned aerial vehicle can take off, then control flight position through radio signal receiver 9 and steering mechanism 2, make it remove the top that needs the succour, then through radio control mechanism 89, start air pump 87, make air pump 87 aerify life buoy 85 through gas tube 88, make life buoy 85's volume increase, then ejecting bottom plate 83 when increasing to the certain degree, make connecting adhesive tape 84 tear, make bottom plate 83 open downwards, then life buoy 85 falls near drowned personnel under the effect of gravity, give drowned personnel's help, be convenient for carry out rescue next.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a multi-functional emergency rescue unmanned aerial vehicle, includes shell (1), its characterized in that: the utility model discloses a rescue device, including shell (1), outer surface one side fixedly connected with steering mechanism (2) of shell (1), bottom one side fixedly connected with bracing piece (3) of shell (1), the one end fixedly connected with flight ring (4) of bracing piece (3), internal surface one side fixedly connected with connecting rod (5) of flight ring (4), there is screw (6) one side of connecting rod (5), fixedly connected with lithium cell (7) between the internal surface both sides of shell (1), the bottom that just is located lithium cell (7) between the internal surface both sides of shell (1) is provided with rescue device (8), the bottom that just is located rescue device (8) between the internal surface both sides of shell (1) is provided with wireless signal receiver (9).
2. The multifunctional unmanned emergency rescue vehicle of claim 1, wherein: rescue device (8) include framework (81), be fixed connection between the surface both sides of framework (81) and the internal surface both sides of shell (1), top one side of framework (81) is provided with air-supply net (82), the bottom of framework (81) is provided with bottom plate (83), be provided with between one side of bottom plate (83) and the bottom opposite side of framework (81) and connect sticky tape (84), the bottom of framework (81) is provided with life buoy (85), fixedly connected with diaphragm (86) between the internal surface both sides of framework (81), the top of diaphragm (86) is provided with air pump (87), the end of giving vent to anger of air pump (87) is provided with gas tube (88), the top of diaphragm (86) and the one side that is located air pump (87) are provided with wireless control mechanism (89).
3. The multifunctional unmanned emergency rescue vehicle of claim 2, wherein: the air inlet net (82) is made of non-woven fabric, and one side of the bottom plate (83) is rotatably connected with one side of the bottom of the frame body (81).
4. The multifunctional unmanned emergency rescue vehicle of claim 2, wherein: the connecting adhesive tape (84) is made of transparent adhesive tape, and the other side of the bottom plate (83) is in contact with the other side of the bottom of the frame body (81).
5. The multifunctional unmanned emergency rescue vehicle of claim 2, wherein: one end of the inflation tube (88) is communicated with the air outlet end of the air pump (87), and the other end of the inflation tube (88) is communicated with the inflation port of the life buoy (85).
6. The multifunctional unmanned emergency rescue vehicle of claim 1, wherein: the number of the flying rings (4) is four, and a driving motor is arranged at the axis of the propeller (6).
Priority Applications (1)
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CN201921869874.5U CN210761297U (en) | 2019-11-01 | 2019-11-01 | Multifunctional emergency rescue unmanned aerial vehicle |
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CN201921869874.5U CN210761297U (en) | 2019-11-01 | 2019-11-01 | Multifunctional emergency rescue unmanned aerial vehicle |
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CN201921869874.5U Expired - Fee Related CN210761297U (en) | 2019-11-01 | 2019-11-01 | Multifunctional emergency rescue unmanned aerial vehicle |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112009647A (en) * | 2020-09-10 | 2020-12-01 | 张愉 | Fire-fighting robot |
CN112173116A (en) * | 2020-11-12 | 2021-01-05 | 重庆凯创荣智能科技有限公司 | Unmanned aerial vehicle for urban rescue and using method thereof |
CN113602453A (en) * | 2021-09-10 | 2021-11-05 | 陕西蓝悦无人机技术有限公司 | Multifunctional water search and rescue unmanned aerial vehicle |
CN113636040A (en) * | 2021-09-10 | 2021-11-12 | 陕西蓝悦无人机技术有限公司 | Method for searching and rescuing unmanned aerial vehicle on water and method for amphibious emergency forced landing |
-
2019
- 2019-11-01 CN CN201921869874.5U patent/CN210761297U/en not_active Expired - Fee Related
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112009647A (en) * | 2020-09-10 | 2020-12-01 | 张愉 | Fire-fighting robot |
CN112173116A (en) * | 2020-11-12 | 2021-01-05 | 重庆凯创荣智能科技有限公司 | Unmanned aerial vehicle for urban rescue and using method thereof |
CN113602453A (en) * | 2021-09-10 | 2021-11-05 | 陕西蓝悦无人机技术有限公司 | Multifunctional water search and rescue unmanned aerial vehicle |
CN113636040A (en) * | 2021-09-10 | 2021-11-12 | 陕西蓝悦无人机技术有限公司 | Method for searching and rescuing unmanned aerial vehicle on water and method for amphibious emergency forced landing |
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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: 20200616 Termination date: 20201101 |