CN204956925U - Urgent medicine transports system based on fuselage formula of verting rotor unmanned aerial vehicle - Google Patents
Urgent medicine transports system based on fuselage formula of verting rotor unmanned aerial vehicle Download PDFInfo
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- CN204956925U CN204956925U CN201520508552.3U CN201520508552U CN204956925U CN 204956925 U CN204956925 U CN 204956925U CN 201520508552 U CN201520508552 U CN 201520508552U CN 204956925 U CN204956925 U CN 204956925U
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Abstract
The utility model provides an urgent medicine transports system based on fuselage formula of verting rotor unmanned aerial vehicle, the system is including verting fuselage formula rotor unmanned aerial vehicle and embedded load cabin, wherein: the fuselage formula of verting rotor unmanned aerial vehicle is equipped with the fixed wing, is provided with embedded load cabin on the fixed wing, and embedded load cabin is used for placing the medicine box. The system can accessiblely send urgent medicine to patient at one's side in traffic jams, area with a varied topography fast, saves life, the specification of common tens kinds of urgent medicines has been considered to the capacity of medicine box, can be competent at transporting of general urgent medicine.
Description
Technical field
The utility model relates to emergency drug delivery system, concrete, relate to and be embedded in medicine box in the fuselage load cabin of the fuselage formula rotor wing unmanned aerial vehicle that verts, cover covering fastening, do not destroy the aerodynamic configuration of unmanned plane, when keeping original aerodynamic force and airworthiness, by unmanned plane, emergency drug is transported to destination.
Background technology
When patient is in peril of one's life, use first aid medicine to patient timely, treatment rate can be increased, even can remove life danger.Due to ground communications inconvenience, consuming time long between patient and hospital of traditional emergency vehicle, not only can not reach the effect of first aid, even can delay life because of wait emergency vehicle blindly.
Traditional medical rescue rotor craft is not owing to having wing, and the aerodynamic lift that wing can not be leaned on to produce overcomes gravity, and therefore energy consumption is high, and flying speed is slow, voyage is near, cruise duration is short, maneuvering range is little.
As the Chinese utility model that Patent publication No is CN103792947A, this utility model provides a kind of small medical to succour rotor flying robot, comprises body, also comprises autopilot system and medical rescue system.This autopilot system comprises sensor subsystem, flight-control computer and servo and to be used as power system; Flight-control computer connecting sensor subsystem, the data that processes sensor subsystem obtains; Flight-control computer connects servo and to be used as power system, controls servo and to be used as power the work of system, adjustment flying speed and flight attitude; This utility model small medical relief rotor flying robot, have low cost, fast, the advantage of accurate positioning.
Although above prior art can reach the object of delivering drugs, because it adopts rotor flying robot, the lift of wing can not be leaned on to overcome gravity, overall process relies on the dynamic lift of rotor overcome gravity and provide the thrust of advance, therefore cruising speed is low, and energy consumption is high, and flight range is little.
Utility model content
For real-life problem, the purpose of this utility model is to provide a kind of restriction that can not be subject to ground communications, promptly medicine will can be delivered to patient's fuselage formula rotor wing unmanned aerial vehicle system of verting at one's side without barrier fast.
For achieving the above object, the utility model provides a kind of emergency drug delivery system based on the fuselage formula rotor wing unmanned aerial vehicle that verts, described system comprises vert fuselage formula rotor wing unmanned aerial vehicle and embedded load cabin, wherein: described in the fuselage formula rotor wing unmanned aerial vehicle that verts be provided with fixed wing, fixed wing is provided with embedded load cabin, and embedded load cabin is for placing medicine box.
Preferably, the described fuselage formula rotor wing unmanned aerial vehicle that verts comprises airborne equipment and carries out with record equipment the surface control station that communication is connected, surface control station verts according to place where the accident occurred spot control the course line of fuselage formula rotor wing unmanned aerial vehicle, and the fuselage formula rotor wing unmanned aerial vehicle that verts being loaded with medicine box to fly place where the accident occurred point automatically according to this course line.
Preferably, on described wing, the embedded size in load cabin is mated with the size compatibility of medicine box, can put into some urgent tablet and injections in medicine box.
Preferably, after described medicine box is positioned over described embedded load cabin, to be covered by covering and fastening, thus the aerodynamic configuration of the fuselage formula rotor wing unmanned aerial vehicle that makes to vert is not destroyed, and still keeps original aeroperformance and airworthiness.
Principle of work of the present utility model is: when receiving transport first aid medicine task or wanting to buy medicine information, first aid medicine is put into medicine box, and medicine box is carried out filling process, to avoid concussion.Medicine box is embedded into unmanned plane load cabin.Determine place where the accident occurred point by surface control station, planning course line, fuselage formula of verting rotor wing unmanned aerial vehicle automatically flies to place where the accident occurred according to course line and is sent to by medicine box.
Compared with prior art, the utility model has following beneficial effect:
1, the utility model is that one both can vertical takeoff and landing and hovering, the unmanned plane cruised when the aerodynamic lift that wing can be utilized again to produce carries out low energy consumption, long boat, can solve that conventional many rotor wing unmanned aerial vehicles cruise duration is short, load is little, and the landing of fixed-wing unmanned plane needs the difficult problem providing a series of technical requirements harshness such as runway or feedway specially.Make model machine at present, and complete a series of flight, platform property is good.
2, after this unmanned plane arranges medicine box load cabin, centre-of-gravity displacement is normal, does not affect original airworthiness.
3, because medicine box can embed in the load cabin of this unmanned plane a pair wing body respectively, reality can double carrying amount.
4, medicine box is behind embedding unmanned plane load cabin, does not destroy the aerodynamic configuration of wing body; Because this unmanned plane adopts fixed wing, aerodynamic force can be relied on to carry out horizontal flight, and compared with common cyclogyro, cruising speed is high, and handling is good, good economy performance.
Accompanying drawing explanation
By reading the detailed description done non-limiting example with reference to the following drawings, other features, objects and advantages of the present utility model will become more obvious:
Fig. 1 is the structural representation being embedded in medicine box in fuselage formula rotor wing unmanned aerial vehicle load cabin of verting of the utility model one embodiment;
In figure: fuselage formula of verting rotor wing unmanned aerial vehicle 1, embed the load cabin 2 of medicine box, medicine box 3, covering 4.
Detailed description of the invention
Below in conjunction with specific embodiment, the utility model is described in detail.Following examples will contribute to those skilled in the art and understand the utility model further, but not limit the utility model in any form.It should be pointed out that to those skilled in the art, without departing from the concept of the premise utility, some distortion and improvement can also be made.These all belong to protection domain of the present utility model.
As shown in Figure 1, the present embodiment provides a kind of emergency drug delivery system based on the fuselage formula rotor wing unmanned aerial vehicle that verts, described system comprises the fuselage formula rotor wing unmanned aerial vehicle 1 that verts, and embedded load cabin 2, the described fuselage formula rotor wing unmanned aerial vehicle 1 that verts is provided with fixed wing, fixed wing is provided with embedded load cabin 2, and embedded load cabin is for placing medicine box 3.
The described fuselage formula rotor wing unmanned aerial vehicle 1 that verts comprises airborne equipment and carries out with record equipment the surface control station that communication is connected, surface control station verts according to place where the accident occurred spot control the course line of fuselage formula rotor wing unmanned aerial vehicle, and the fuselage formula rotor wing unmanned aerial vehicle that verts being loaded with medicine box to fly place where the accident occurred point automatically according to this course line.
The described fuselage verting fuselage formula rotor wing unmanned aerial vehicle 1 comprises two fixed wings of Parallel Symmetric placement and the bracing frame of centre, two fixed wings is provided with altogether four cover rotors.Described fixed wing is each on the position of middle part symmetry installs two cover motors, and screw propeller installed by motor; The hand of rotation of adjacent described screw propeller is contrary.On described fixed wing except the rotating shaft of screw propeller and motor can normally rotate, there is no other parts that are rotatable or movement.As shown in Figure 1.
The size in described embedded load cabin 2 and the size of medicine box 3 can be compatible and mate, after described medicine box 3 is positioned over described embedded load cabin 2, to be covered by covering 4 and fastening, ensure that the aerodynamic configuration of unmanned plane as before, not destroyed, maintain original aerodynamic force and airworthiness.
Further, two fixed wings of the described fuselage formula rotor wing unmanned aerial vehicle 1 that verts are respectively equipped with embedded load cabin, two embedded load cabin positional symmetry, thus medicine carrying amount reality can be made to double.
Principle of work of the present utility model is: when receiving transport first aid medicine task or wanting to buy medicine information, first aid medicine is put into medicine box 3, and medicine box 3 is carried out filling process, to avoid concussion.Medicine box 3 is embedded into unmanned plane load cabin 2.Determine place where the accident occurred point by surface control station, planning course line, fuselage formula of verting rotor wing unmanned aerial vehicle 1 automatically flies to place where the accident occurred according to course line and is sent to by medicine box 3.
Above specific embodiment of the utility model is described.It is to be appreciated that the utility model is not limited to above-mentioned particular implementation, those skilled in the art can make various distortion or amendment within the scope of the claims, and this does not affect flesh and blood of the present utility model.
Claims (5)
1. the emergency drug delivery system based on the fuselage formula rotor wing unmanned aerial vehicle that verts, it is characterized in that, described system comprises vert fuselage formula rotor wing unmanned aerial vehicle and embedded load cabin, wherein: described in the fuselage formula rotor wing unmanned aerial vehicle that verts be provided with fixed wing, fixed wing is provided with embedded load cabin, and embedded load cabin is for placing medicine box.
2. a kind of emergency drug delivery system based on the fuselage formula rotor wing unmanned aerial vehicle that verts according to claim 1, it is characterized in that, the described fuselage formula rotor wing unmanned aerial vehicle that verts comprises airborne equipment and carries out with record equipment the surface control station that communication is connected, surface control station verts according to place where the accident occurred spot control the course line of fuselage formula rotor wing unmanned aerial vehicle, and the fuselage formula rotor wing unmanned aerial vehicle that verts being loaded with medicine box to fly place where the accident occurred point automatically according to this course line.
3. a kind of emergency drug delivery system based on the fuselage formula rotor wing unmanned aerial vehicle that verts according to claim 1, is characterized in that, on described wing, the embedded size in load cabin is mated with the size compatibility of medicine box.
4. a kind of emergency drug delivery system based on the fuselage formula rotor wing unmanned aerial vehicle that verts according to any one of claim 1-3, is characterized in that, after described medicine box is positioned over described embedded load cabin, to be covered and fastening by covering.
5. a kind of emergency drug delivery system based on the fuselage formula rotor wing unmanned aerial vehicle that verts according to any one of claim 1-3, it is characterized in that, the described fuselage formula rotor wing unmanned aerial vehicle that verts is provided with two fixed wings, two fixed wings are respectively equipped with embedded load cabin, two embedded load cabin positional symmetry.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520508552.3U CN204956925U (en) | 2015-07-14 | 2015-07-14 | Urgent medicine transports system based on fuselage formula of verting rotor unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520508552.3U CN204956925U (en) | 2015-07-14 | 2015-07-14 | Urgent medicine transports system based on fuselage formula of verting rotor unmanned aerial vehicle |
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| CN204956925U true CN204956925U (en) | 2016-01-13 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113043281A (en) * | 2021-04-21 | 2021-06-29 | 北京小乔机器人科技发展有限公司 | Application of intelligent robot in outdoor logistics medicine delivery |
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2015
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113043281A (en) * | 2021-04-21 | 2021-06-29 | 北京小乔机器人科技发展有限公司 | Application of intelligent robot in outdoor logistics medicine delivery |
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