CN218806657U - First-aid unmanned aerial vehicle device - Google Patents
First-aid unmanned aerial vehicle device Download PDFInfo
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- CN218806657U CN218806657U CN202220959156.2U CN202220959156U CN218806657U CN 218806657 U CN218806657 U CN 218806657U CN 202220959156 U CN202220959156 U CN 202220959156U CN 218806657 U CN218806657 U CN 218806657U
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
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Abstract
The utility model discloses a first aid unmanned aerial vehicle device, including the unmanned aerial vehicle body, the fuselage shell of unmanned aerial vehicle body is provided with control circuit, first holding chamber and second holding chamber, control circuit sets up first holding intracavity, the top of fuselage shell be provided with the last opening that second holding chamber is linked together, the bottom of fuselage shell be provided with the lower opening that second holding chamber is linked together, the upper shed department is provided with the flip structure, the medial surface orientation of flip structure second holding chamber, the medial surface of flip structure is provided with accomodates the structure. The utility model discloses technical scheme can transport the scene by the required first aid equipment of treatment personnel fast effectively to do benefit to and implement first aid work fast.
Description
Technical Field
The utility model relates to the technical field of medical equipment, in particular to first aid unmanned aerial vehicle device.
Background
At present, the two most basic types of first-aid equipment needed in the first-aid process are the cardiopulmonary resuscitator, also called a cardiopulmonary resuscitator, and the cardiopulmonary resuscitator is a type of equipment which uses machinery to replace manpower to implement basic life support operations such as artificial respiration and chest compression, and the portable and movable cardiopulmonary resuscitator can be used in pre-hospital first-aid, and even in the process of transporting patients, the work of the portable and movable cardiopulmonary resuscitator cannot be obviously influenced. The other is an automatic External Defibrillator (hereinafter referred to as AED), which is a medical instrument for rescuing patients with specific arrhythmia, and can quickly diagnose specific arrhythmia and help patients recover normal heartbeat by defibrillation by electric shock. The automatic external defibrillator is provided with defibrillation electrode plates communicated through a lead, and is adhered to a specific part of a human body in a self-suction mode during working.
At present, the transportation for hospital indoor and outdoor emergency loading equipment is mainly a hand-push four-wheel nurse car, and is motor vehicles outside the hospital. The device has the characteristics of large volume, heavy weight and inconvenience in carrying, transporting and moving related treatment equipment, and the transportation of the related treatment equipment needed by rescuing patients is often delayed.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a first aid unmanned aerial vehicle device can transport the scene by the required first aid equipment of treatment personnel fast effectively to do benefit to and implement first aid work fast.
In order to realize the above-mentioned purpose, the utility model provides an emergency unmanned aerial vehicle device, including the unmanned aerial vehicle body, the fuselage shell of unmanned aerial vehicle body is provided with control circuit, first holding chamber and second holding chamber, control circuit sets up first holding intracavity, the top of fuselage shell be provided with the last opening that second holding chamber is linked together, the bottom of fuselage shell be provided with the lower opening that second holding chamber is linked together, the upper shed department is provided with the flip structure, the medial surface orientation of flip structure second holding chamber, the medial surface of flip structure is provided with accomodates the structure.
Optionally, the unmanned aerial vehicle device still includes automatic external defibrillator body, automatic external defibrillator body sets up the second holding intracavity, automatic external defibrillator body is provided with the electrode piece of defibrillating, the electrode piece of defibrillating pass through the wire with automatic external defibrillator body electric connection, the electrode piece of defibrillating sets up in accomodating the structure.
Optionally, a winding post is disposed on an inner side of the flip structure, and the wire is wound and received on the winding post.
Optionally, the unmanned aerial vehicle device further comprises a cardiopulmonary resuscitation machine body, the cardiopulmonary resuscitation machine body is arranged in the second accommodating cavity, the cardiopulmonary resuscitation machine body comprises a pressing mechanism and a binding belt, and the pressing mechanism and the binding belt are arranged at the bottom of the body shell in a protruding mode.
Optionally, a display screen is arranged in the second accommodating cavity, and the automatic external defibrillator body and the cardiopulmonary resuscitation machine body are respectively electrically connected with the display screen.
Optionally, the receiving structure is a receiving bag.
Optionally, a detachable structure is arranged on the flip structure, and the storage bag is arranged on the detachable structure.
Optionally, the fuselage shell is of an aluminum alloy construction.
Optionally, the outer contour of the fuselage shell is a cuboid structure.
Optionally, the body shell is provided with a ventilation structure communicated with the second accommodating cavity.
The technical scheme of the utility model among, can be fast effectively will be transported the scene by the required all kinds of first aid equipment of treatment personnel, for example automatic external defibrillator body and cardiopulmonary resuscitation machine body can be by the long-range delivery of unmanned aerial vehicle to do benefit to and implement first aid work fast. Further, the fuselage shell of unmanned aerial vehicle body has made structural improvement in order being applicable to installation automatic external defibrillator body and cardiopulmonary resuscitation machine body, specifically, the structural structure of accomodating of flip is used for accomodating the electrode piece of defibrillating specially, the bottom of fuselage shell is provided with the opening and is used for supplying the structure of pressing (pressing the clamp plate) and the outside that the bandage is exposed at the fuselage shell of cardiopulmonary resuscitation machine body bottom, among the practical application, the bandage is tied up fixedly on people's health, press the structure pressure and carry out pressing work in the front of people's chest, flip structure is turned over, take out to defibrillate the electrode piece and attach in human analysis and the work of defibrillating.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the structures shown in the drawings without creative efforts.
Fig. 1 is a schematic perspective view of an embodiment of the first-aid unmanned aerial vehicle device according to the present invention when opened;
fig. 2 is a top view of an embodiment of the emergency unmanned aerial vehicle apparatus of the present invention;
fig. 3 is a schematic view of a three-dimensional structure of the first-aid unmanned aerial vehicle device according to an embodiment of the present invention when the first-aid unmanned aerial vehicle device is turned over and opened;
fig. 4 is a front view of an embodiment of the emergency unmanned aerial vehicle device of the present invention;
fig. 5 is a schematic view of a three-dimensional structure of a pressing mechanism when a human body works according to an embodiment of the emergency unmanned aerial vehicle device of the present invention;
fig. 6 is a schematic view of the working principle of the defibrillation electrode plate in an embodiment of the emergency unmanned aerial vehicle of the present invention;
the reference numbers illustrate:
| name (R) | Reference numerals | Name (R) | Reference numerals |
| Unmanned |
1 | |
21 |
| |
11 | Conducting |
22 |
| |
12 | |
23 |
| |
121 | Cardiopulmonary |
3 |
| Wrapping |
122 | |
31 |
| Unlocking |
13 | |
32 |
| |
14 | |
4 |
| Automatic |
2 |
The objects, features and advantages of the present invention will be further described with reference to the accompanying drawings.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.
It should be noted that all the directional indicators (such as up, down, left, right, front, back \8230;) in the embodiments of the present invention are only used to explain the relative position relationship between the components, the motion situation, etc. in a specific posture (as shown in the attached drawings), and if the specific posture is changed, the directional indicator is changed accordingly.
In addition, the descriptions related to "first", "second", etc. in the present invention are for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicit ly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In addition, the technical solutions in the embodiments may be combined with each other, but it must be based on the realization of those skilled in the art, and when the technical solutions are contradictory to each other or cannot be realized, such a combination should not be considered to exist, and is not within the protection scope of the present invention.
The utility model provides a first aid unmanned aerial vehicle device, include: unmanned aerial vehicle body 1, fuselage shell 11 of unmanned aerial vehicle body 1 is provided with control circuit (not drawn in the figure), first holding chamber (not drawn in the figure) and second holding chamber (not marked in the figure), and control circuit (not drawn in the figure) sets up first holding intracavity, the top of fuselage shell 11 be provided with the last opening (not marked in the figure) that second holding chamber is linked together, the bottom of fuselage shell 11 be provided with the lower opening (not marked in the figure) that second holding chamber is linked together, the upper shed department is provided with flip 12, flip 12's medial surface orientation second holding chamber, flip 12's medial surface is provided with accomodates structure 121.
The technical scheme of the utility model, still include automatic external defibrillator body 2, automatic external defibrillator body 2 sets up second holding intracavity, automatic external defibrillator body 2 is provided with defibrillation electrode piece 21, defibrillation electrode piece 21 pass through wire 22 with automatic external defibrillator body 2 electric connection, defibrillation electrode piece 21 sets up in accomodate structure 121.
The technical scheme of the utility model in, still include cardiopulmonary resuscitation machine body 3, cardiopulmonary resuscitation machine body 3 sets up in the second holding intracavity, cardiopulmonary resuscitation machine body 3 is provided with pressing means 31 and bandage 32, pressing means 31 with bandage 32 is outstanding to be set up the bottom of fuselage shell 11. As shown in fig. 1-4.
In the technical scheme of the utility model, be provided with display screen 4 in the second holding intracavity, automatic external defibrillator body 2 with cardiopulmonary resuscitation machine body 3 respectively with 4 electric connection of display screen.
The technical scheme of the utility model among, as shown in fig. 1 to fig. 6, automatic external defibrillator body 2 and cardiopulmonary resuscitation machine body 3 can be by the long-range delivery of unmanned aerial vehicle, can transport the scene by the required first aid equipment of rescue personnel fast effectively to do benefit to and implement first aid work fast. This application technical scheme provides an unmanned aerial vehicle body 1, and make structural improvement in order to be applicable to installation automatic external defibrillator body 2 and cardiopulmonary resuscitation machine body 3 to the fuselage shell 11 of unmanned aerial vehicle body 1, specifically, accomodate structure 121 on flip 12 and be used for accomodating defibrillation electrode piece 21 specially, the bottom of fuselage shell 11 is provided with the opening and is used for supplying the external pressing mechanism 31 (electronic pressing plate subassembly) and the bandage 32 of cardiopulmonary resuscitation machine body 3 bottom to expose in the outside of fuselage shell 11, in the practical application, bandage 32 is tied up fixedly on the human body, pressing mechanism 31 presses and carries out pressing work before the people's chest, flip 12 is opened to the side, take out defibrillation electrode piece 21 and attach and carry out analysis and defibrillation work in the human body. After the defibrillation electrode pads 21 are connected with the patient, information such as the heart rhythm and the defibrillation frequency can be displayed on the display screen 4. Below the body shell 11 is a pressing mechanism 31 which can perform repeated pressing actions to achieve a cardiopulmonary resuscitation function. The display screen 4 can display information such as the pressing depth and the pressing frequency. Regarding the use method of the unmanned aerial vehicle body 1: unmanned aerial vehicle body 1 can be provided with remote control module, navigation module or the communication module who is connected with cell-phone APP remote communication etc. and the usable cell-phone APP of user calls unmanned aerial vehicle, and unmanned aerial vehicle receives distress notification after, can be according to the cell-phone location, automatic flight with land to the patient side. The rescuer puts the patient in a flat position, lays the patient on a hard board bed or the ground, places the unmanned aerial vehicle device (the cardio-pulmonary resuscitation pressing mechanism 31 at the bottom of the unmanned aerial vehicle body 1) above the chest of the patient, and fixes the device by the bandage 32. The upper cover of the machine body is opened, the electrolytic sheet is taken out and adhered to the corresponding part of the patient, then the AED mode is started for analyzing the heart rhythm, the electrocardio recognition algorithm contained in the defibrillation module (the defibrillation electrode sheet 21 and the control circuit thereof) can automatically judge whether the electrocardio waveform of the patient needs defibrillation treatment, when the defibrillation treatment is needed, the module can be automatically charged, and when the defibrillation button 23 is pressed, the current can be released for defibrillation treatment of the patient. When defibrillation is completed, the cardiopulmonary resuscitation button needs to be pressed down for external pressing, the pressing mode and the pressing depth are adjusted according to the prompt of the display screen 4, and continuous pressing and 2 can be selected: 15 (15 compressions, two ventilations), 2:30 (30 compressions and two ventilations) and the like. The utility model discloses can effectively treat because of the sudden cardiac arrest and the patient that need external pressing and defibrillate, external pressing and defibrillate can go on in step, shorten the treatment time, improve patient survival rate.
In the technical solution of the utility model, accomodate structure 121 for accomodating the bag.
This kind of structure setting accomodates the easy compression deformation of bag, is convenient for accomodate, saves unmanned aerial vehicle body inner space.
The technical scheme of the utility model in, flip is structural to be provided with detachable construction, it is in to accomodate the bag setting detachable construction. Further, the detachable structure may be a hook and loop fastener structure (not shown), and the storage bag is adhered to the hook and loop fastener structure. Of course, the detachable structure may also include a hook or a screw adhered to the lid 12.
In the technical scheme of the utility model, flip 12's medial surface is provided with wrapping post 122, wire 22 is convoluteed and is accomodate on the wrapping post 122.
In order to alleviate the pressure on the human body, in the technical scheme of the utility model, fuselage shell 11 is the aluminum alloy structure.
The technical scheme of the utility model, be provided with on the fuselage shell 11 and be used for the locking flip 12's hasp structure, be provided with on the fuselage shell 11 and be used for control the unblock button 13 of the switch of hasp structure. The unlocking button 13 of the locking structure and the switch for controlling the locking structure are both in the prior art, and the structure generated by combining the locking structure and the unlocking button is common in a pressing spring switch, and is not described in detail herein.
In the technical scheme of the utility model, fuselage shell 11's outline is the cuboid structure.
In order to cool down emergency equipment, the technical scheme of the utility model, fuselage shell 11 be provided with the ventilative structure that second holding chamber is linked together, ventilative structure can be bleeder vent 14, still can be ventilative grid etc..
The above only be the preferred embodiment of the utility model discloses a not consequently restriction the utility model discloses a patent range, all are in the utility model discloses a conceive, utilize the equivalent structure transform of what the content was done in the description and the attached drawing, or direct/indirect application all is included in other relevant technical field the utility model discloses a patent protection within range.
Claims (10)
1. The utility model provides a first aid unmanned aerial vehicle device, its characterized in that, includes the unmanned aerial vehicle body, the fuselage shell of unmanned aerial vehicle body is provided with control circuit, first holding chamber and second holding chamber, control circuit sets up first holding intracavity, the top of fuselage shell be provided with the last opening that second holding chamber is linked together, the bottom of fuselage shell be provided with the lower opening that second holding chamber is linked together, the upper shed department is provided with the flip structure, the medial surface orientation of flip structure second holding chamber, the medial surface of flip structure is provided with accomodates the structure.
2. The first aid unmanned aerial vehicle device of claim 1, further comprising an automated external defibrillator body disposed within the second receiving cavity, the automated external defibrillator body being provided with defibrillation electrode pads electrically connected to the automated external defibrillator body by wires, the defibrillation electrode pads being disposed within the receiving structure.
3. The first aid drone apparatus of claim 2, wherein the inner side of the flip structure is provided with a winding post on which the wire windings are received.
4. The first aid drone device of claim 2, further comprising a cardiopulmonary resuscitation machine body disposed within the second receiving cavity, the cardiopulmonary resuscitation machine body including a pressing mechanism and a strap, the pressing mechanism and the strap protrudingly disposed at a bottom of the body shell.
5. The rescue unmanned aerial vehicle device of claim 4, wherein a display screen is disposed in the second receiving cavity, and the external defibrillator body and the CPR body are electrically connected to the display screen respectively.
6. The first aid drone apparatus of claim 1, wherein the receiving structure is a receiving bag.
7. The first aid drone apparatus of claim 6, wherein the flip structure is provided with a detachable structure, the receiving pocket being provided on the detachable structure.
8. The first aid drone assembly of any one of claims 1 to 7, wherein the fuselage shell is of aluminum alloy construction.
9. The first aid drone device of any one of claims 1 to 7, characterised in that the outer profile of the fuselage housing is of cuboid configuration.
10. The first aid drone apparatus of any one of claims 1 to 7, wherein the fuselage housing is provided with a ventilation structure in communication with the second housing cavity.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220959156.2U CN218806657U (en) | 2022-04-21 | 2022-04-21 | First-aid unmanned aerial vehicle device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220959156.2U CN218806657U (en) | 2022-04-21 | 2022-04-21 | First-aid unmanned aerial vehicle device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218806657U true CN218806657U (en) | 2023-04-07 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220959156.2U Active CN218806657U (en) | 2022-04-21 | 2022-04-21 | First-aid unmanned aerial vehicle device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218806657U (en) |
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2022
- 2022-04-21 CN CN202220959156.2U patent/CN218806657U/en active Active
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