CN215155585U - High integration first aid rescue unmanned aerial vehicle - Google Patents
High integration first aid rescue unmanned aerial vehicle Download PDFInfo
- Publication number
- CN215155585U CN215155585U CN202121254731.0U CN202121254731U CN215155585U CN 215155585 U CN215155585 U CN 215155585U CN 202121254731 U CN202121254731 U CN 202121254731U CN 215155585 U CN215155585 U CN 215155585U
- Authority
- CN
- China
- Prior art keywords
- battery
- rotating block
- aerial vehicle
- unmanned aerial
- control platform
- 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.)
- Active
Links
- 230000010354 integration Effects 0.000 title claims abstract description 10
- 238000010030 laminating Methods 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 4
- 230000008569 process Effects 0.000 abstract description 4
- 230000009467 reduction Effects 0.000 abstract description 3
- 238000005452 bending Methods 0.000 abstract 1
- 210000002414 leg Anatomy 0.000 description 5
- 238000001125 extrusion Methods 0.000 description 4
- 238000009434 installation Methods 0.000 description 4
- 230000007246 mechanism Effects 0.000 description 3
- 241000883990 Flabellum Species 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000011324 bead Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
Images
Landscapes
- Toys (AREA)
Abstract
The utility model provides a high integration emergency rescue unmanned aerial vehicle, include: the fuselage body, the fuselage body is the fretwork form, just the downward bending of fuselage body forms the rhombus, bottom surface is fixed with control platform under the fuselage body, the control platform lower extreme is provided with two battery casees, battery box card is inserted bottom surface under the control platform, two be provided with rotatable spacing portion in the middle of the battery case, wherein rotate spacing portion to with two when the battery case is perpendicular to each other, spacing portion can the chucking fix two the battery case. This practicality is through two set up spacing portion that can rotate in the middle of the battery case, rotate rotation portion to with two battery cases perpendicular after can the chucking fix two battery cases, great reduction the process that needs when changing the battery case, practiced thrift the time of changing the battery, promoted rescue efficiency.
Description
Technical Field
The utility model relates to a rescue unmanned aerial vehicle technical field, concretely relates to high integration rescue unmanned aerial vehicle.
Background
Application No.: CN201721758845.2, publication No.: CN207765493U, an adjustable battery compartment device of unmanned aerial vehicle, the utility model discloses an adjustable battery compartment device of unmanned aerial vehicle, which relates to the mechanical field, and comprises a battery compartment body with an opening at the upper end, 3 battery fixing mechanisms are arranged on the side wall of at least 3 battery compartment bodies, the battery fixing mechanism comprises a movable plate and an extrusion plate, the extrusion plate is fixed on the side wall of the other battery compartment body, at least two extrusion plates are also provided with a longitudinal positioning mechanism, and the two extrusion plates are symmetrically arranged with each other, the utility model has a simple and reasonable structure, and realizes the convenient installation of batteries; the retractable structure can adapt to batteries of various types and sizes on the market, and an independent battery bin does not need to be designed for each battery.
Among the prior art, because battery compartment upper end trompil, the protection battery that can not be fine, simultaneously through the bolt fastening battery, it is more troublesome that the battery is changed in the dismouting, and rescue unmanned aerial vehicle mostly needs longer continuation of the journey to guarantee the scope of search and rescue, in order to guarantee the promptness of rescue, the change backup battery that needs to be swift, and among the prior art, unmanned aerial vehicle's battery case installation is comparatively complicated, has influenced the rescue time, consequently need research and development a high integration rescue unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model is: in the prior art, the battery installation and replacement process is complex and takes too long. The utility model provides a high integration first aid unmanned aerial vehicle solves above-mentioned problem.
The utility model provides a technical scheme that its technical problem adopted is: a high integration first aid rescue unmanned aerial vehicle includes: the fuselage body, the fuselage body is the fretwork form, just the fuselage body bends downwards and forms the rhombus, bottom surface is fixed with control platform under the fuselage body, the control platform lower extreme is provided with two battery casees, battery box card is inserted bottom surface under the control platform, two be provided with rotatable spacing portion in the middle of the battery case, wherein
When the limiting part is rotated to be perpendicular to the two battery boxes, the limiting part can clamp and fix the two battery boxes.
Preferably, the stopper portion includes: the middle of the rotating block is hollow, the rotating block is rotatably arranged on the lower bottom surface of the control platform, and the cross section of the rotating block is rectangular; the rotating block is slidably connected with a limiting plate, wherein
And when the limiting plate is pulled downwards to exceed the lower bottom surface of the battery box, the limiting plate is rotated to support and pull the battery box.
Preferably, the stopper further includes: the connecting rod, the upper end of connecting rod is fixed with first locating plate, first locating plate slidable sets up inside the turning block, the lower extreme vertical fixation of connecting rod is in on the limiting plate, encircle the connecting rod cover is equipped with tension spring, tension spring's both ends respectively with the limiting plate with turning block fixed connection, wherein
When the limiting plate is parallel to the long edge of the battery box, the tension spring can pull the first positioning plate to be attached to the control platform.
Preferably, a second positioning plate is fixed at the lower end of the rotating block, a through hole suitable for the connecting rod to pass through is formed in the middle of the second positioning plate, a second positioning groove is formed in the upper end of the second positioning plate, and the second positioning groove is formed in the upper end of the second positioning plate
After the first positioning plate is clamped into the second positioning groove, the limiting plate is rotated to drive the rotating block to rotate synchronously.
Preferably, the two side edges of the lower bottom surface of the control platform respectively protrude downwards to form fixed blocks, and the fixed blocks are provided with fixed grooves; the outer side wall of the battery box protrudes outwards to form a clamping block matched with the fixing groove, the inner side wall of the battery box is provided with spring balls, and the two long side walls of the rotating block are provided with first positioning grooves respectively, wherein the first positioning grooves are formed in the two long side walls of the rotating block
After the rotating block is rotated, the spring ball card is inserted into the first positioning groove.
Preferably, the machine body is further fixed with four driving propellers, and the four driving propellers are respectively and rotatably connected to the lower side of the machine body.
Preferably, the aircraft body is further fixedly provided with four supporting feet, each supporting foot is correspondingly arranged on the outer side of one driving propeller, and the distance from each supporting foot to the lower bottom surface of the aircraft body is greater than the distance from each driving propeller blade to the aircraft body.
The utility model has the advantages that: a high integration first aid rescue unmanned aerial vehicle includes: the portable electronic device comprises a machine body, a power supply and a control circuit, wherein the machine body is hollowed and is bent downwards to form a diamond shape, a control platform is fixed on the lower bottom surface of the machine body, two battery boxes are arranged at the lower end of the control platform, the battery boxes are clamped on the lower bottom surface of the control platform, and a rotatable limiting part is arranged between the two battery boxes; the utility model discloses the simple operation, through two set up rotatable spacing portion between the battery case, rotate spacing portion to with when the battery case is perpendicular, two battery cases can be fixed to spacing portion, and the mode of spacing portion is rotated to the battery case through the card, great reduction the process that the battery case was changed, practiced thrift the time of changing the battery case, great promotion the efficiency of rescue.
Drawings
The present invention will be further explained with reference to the drawings and examples.
Fig. 1 is a schematic view of a high-integration integrated rescue unmanned aerial vehicle in a bottom view;
fig. 2 is a perspective view of the control platform of the present invention;
fig. 3 is a longitudinal sectional view of the control platform of the present invention;
FIG. 4 is a partial enlarged view of A in FIG. 3
Fig. 5 is a top perspective view of the present invention.
In the figure:
the device comprises a machine body 1, a driving propeller 11, supporting legs 12, a control platform 2, a fixing block 21, a fixing groove 211, a battery box 3, a clamping block 31, a spring ball 32, a limiting part 4, a rotating block 41, a first positioning groove 410, a second positioning plate 411, a second positioning groove 412, a limiting plate 42, a connecting rod 43, a first positioning plate 431 and a tension spring 44.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present invention, and should not be construed as limiting the present invention. On the contrary, the embodiments of the invention include all changes, modifications and equivalents coming within the spirit and terms of the claims appended hereto.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "axial", "radial", "circumferential", and the like, indicate orientations and positional relationships based on the orientations and positional relationships shown in the drawings, and are used only for convenience in describing and simplifying the present invention, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
Furthermore, the terms "first," "second," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance. In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "connected" and "connected" are to be interpreted broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; may be directly connected or indirectly connected through an intermediate. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art. In addition, in the description of the present invention, "a plurality" means two or more unless otherwise specified.
As shown in fig. 1 to 5, the utility model provides a high integration first aid rescue unmanned aerial vehicle, include: fuselage body 1, fuselage body 1 is the fretwork form, just fuselage body 1 downwarping forms the rhombus, the bottom surface is fixed with control platform 2 under the fuselage body 1, 2 lower extremes of control platform are provided with two battery casees 3, battery case 3 card is inserted bottom surface, two under the control platform 2 be provided with rotatable spacing portion 4 in the middle of the battery case 3, wherein rotate spacing portion 4 to with two when battery case 3 is mutually perpendicular, spacing portion 4 can the chucking two battery case 3. Insert two battery case 3 cards extremely back under control platform 2, rotate spacing portion 4 extremely with two battery case 3 is perpendicular mutually, spacing portion 4 can hold and fix two battery case 3, battery case 3 can fix battery case 3 through the card mode of inserting and rotating spacing portion 4 the lower bottom surface of control platform 2 compares other fixed mode, the utility model operation is convenient, great reduction the installation of battery case 3, practiced thrift the time of changing battery case 3, great promotion the efficiency of rescue.
Optionally, the limiting part 4 includes: the middle of the rotating block 41 is hollow, the rotating block 41 is rotatably arranged on the lower bottom surface of the control platform 2, and the cross section of the rotating block 41 is rectangular; the rotating block 41 is slidably connected with a limiting plate 42, the limiting plate 42 is perpendicular to the rotating block 41, when the limiting plate 42 is pulled downwards to exceed the lower bottom surface of the battery box 3, the limiting plate 42 is rotated to synchronously drive the rotating block 41 to rotate, when the limiting plate 42 is rotated to be perpendicular to the two battery boxes 3, the limiting plate 42 is combined with the rotating block 41 to upwards support and pull the battery box 3, so that the two battery boxes 3 are clamped and fixed on the control platform 2.
Optionally, the limiting portion 4 further includes: a connecting rod 43, wherein a first positioning plate 431 is fixed at the upper end of the connecting rod 43, the first positioning plate 431 is square, and the side length of the first positioning plate 431 is smaller than the diameter of the hollow part of the rotating block 41; the first positioning plate 431 is slidably arranged inside the rotating block 41, the lower end of the connecting rod 43 is vertically fixed on the limiting plate 42, a tension spring 44 is sleeved around the connecting rod 43, two ends of the tension spring 44 are respectively and fixedly connected with the limiting plate 42 and the rotating block 41, and the length of the connecting rod 43 is greater than that of the rotating block 41, so that when the tension spring 44 pulls the limiting plate 42 upwards until the first positioning plate 431 is attached to the lower bottom surface of the control platform 2, the tension spring 44 still has a certain upward pulling force on the limiting plate 42; when the limiting plate 42 is parallel to the long side of the battery box 3, the limiting plate 42 is located in the gap between two adjacent battery boxes 3, the tension spring 44 can pull the first positioning plate 431 to be attached to the control platform 2, and at the moment, the battery can be detached by pulling the battery box 3 downwards.
Preferably, a second positioning plate 411 is fixed at the lower end of the rotating block 41, the second positioning plate 411 is fixed at the lower opening of the rotating block 41, a through hole suitable for the connecting rod 43 to pass through is formed in the middle of the second positioning plate 411, the connecting rod 43 can slide in the rotating block 41 in a sliding manner, and the second positioning plate 411 and the first positioning plate 431 are matched with each other to prevent the connecting rod 43 from sliding down from the rotating block 41; the second positioning groove 412 is formed at the upper end of the second positioning plate 411, the second positioning groove 412 is square, the side length of the second positioning groove 412 is larger than that of the first positioning plate 431, and after the first positioning plate 431 is clamped in the second positioning groove 412, the limiting plate 42 is rotated to drive the rotating block 41 to rotate synchronously.
Optionally, two side edges of the lower bottom surface of the control platform 2 respectively protrude downward to form fixed blocks 21, and the fixed blocks 21 are provided with fixed grooves 211; the outer side wall of the battery case 3 is protruded outward to form a clamping block 31 fitted to the fixing groove 211, the inner side wall of the battery box 3 is provided with spring beads 32, the two long side walls of the rotating block 41 are respectively provided with a first positioning groove 410, when the battery box 3 is installed, the clamping block 31 at the outer side of the battery case 3 is inserted into the fixing groove 211, the battery is stably placed downward such that the spring ball 32 is adjacent to the rotating block 41, wherein after the rotating block 41 is rotated, the spring ball 32 is inserted into the first positioning slot 410, after the spring ball 32 is snapped into the first positioning groove 410, the battery case 3 achieves a primary fixing effect by the spring ball 32 and the clamping block 31, and the limiting plate 42 vertically arranged at the bottom of the battery box 3 can support the two battery boxes 3, so that the effect of fixing the battery boxes 3 is further improved.
Preferably, still be fixed with four drive screw 11 on the fuselage body 1, four drive screw 11 rotates respectively to be connected the downside of fuselage body 1 will drive screw 11 sets up 1 downside of fuselage body helps protecting drive screw 11, because unmanned aerial vehicle makes drive screw 11's flabellum receive the striking especially easily because be close to some buildings or woods at the non-open area in flight process especially, and will drive screw 11 and set up the fuselage body 1 downside at the dish-shaped, also be fuselage body 1 and receive the striking when bumping like this, has avoided drive screw 11's flabellum to receive the damage. Still be fixed with four supporting legss 12 on the fuselage body 1, every supporting legs 12 corresponds and sets up one the outside of drive screw 11, supporting legs 12 extremely the distance of bottom surface is greater than under the fuselage body 1 drive screw 11 blade extremely the distance of fuselage body 1, supporting legs 12 corresponds the setting and is in the outside of drive screw 11 helps protecting the screw to prevent to receive the impact loss.
In the description herein, references to the description of the term "one embodiment," "some embodiments," "an example," "a specific example," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, a schematic representation of the term does not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
In light of the foregoing, it will be apparent to those skilled in the art from this disclosure that various changes and modifications can be made without departing from the spirit and scope of the invention. The technical scope of the present invention is not limited to the content of the specification, and must be determined according to the scope of the claims.
Claims (7)
1. The utility model provides a high integration first aid rescue unmanned aerial vehicle which characterized in that includes:
fuselage body (1), fuselage body (1) is the fretwork form, just fuselage body (1) downwarping forms the rhombus, bottom surface is fixed with control platform (2) under fuselage body (1), control platform (2) lower extreme is provided with two battery casees (3), battery case (3) card is inserted bottom surface under control platform (2), two be provided with rotatable spacing portion (4) in the middle of battery case (3), wherein
When the limiting part (4) is rotated to be perpendicular to the two battery boxes (3), the limiting part (4) can clamp and fix the two battery boxes (3).
2. The high-integration integrated rescue unmanned aerial vehicle of claim 1,
the limiting part (4) comprises: the middle of the rotating block (41) is hollow, the rotating block (41) is rotatably arranged on the lower bottom surface of the control platform (2), and the cross section of the rotating block (41) is rectangular; a limit plate (42) is connected on the rotating block (41) in a sliding way, wherein
When the limiting plate (42) is pulled downwards to exceed the lower bottom surface of the battery box (3), the limiting plate (42) is rotated to support and pull the battery box (3).
3. The high-integration integrated rescue unmanned aerial vehicle of claim 2,
the limiting part (4) further comprises: connecting rod (43), the upper end of connecting rod (43) is fixed with first locating plate (431), first locating plate (431) slidable sets up inside turning block (41), the lower extreme vertical fixation of connecting rod (43) is in on limiting plate (42), encircle connecting rod (43) cover is equipped with tension spring (44), tension spring (44) both ends respectively with limiting plate (42) with turning block (41) fixed connection, wherein
When limiting plate (42) with battery case (3) long limit is parallel, tension spring (44) can stimulate first locating plate (431) laminating control platform (2).
4. The high-integration integrated rescue unmanned aerial vehicle of claim 3,
a second positioning plate (411) is fixed at the lower end part of the rotating block (41), a through hole suitable for the connecting rod (43) to pass through is formed in the middle of the second positioning plate (411), a second positioning groove (412) is formed in the upper end of the second positioning plate (411), and the connecting rod is fixed on the lower end part of the rotating block (41)
After the first positioning plate (431) is clamped into the second positioning groove (412), the limiting plate (42) is rotated to drive the rotating block (41) to rotate synchronously.
5. The high-integration integrated rescue unmanned aerial vehicle of claim 4,
two side edges of the lower bottom surface of the control platform (2) respectively protrude downwards to form fixed blocks (21), and the fixed blocks (21) are provided with fixed grooves (211); the outer side wall of the battery box (3) protrudes outwards to form a clamping block (31) matched with the fixing groove (211), the inner side wall of the battery box (3) is provided with spring balls (32), two long side walls of the rotating block (41) are provided with first positioning grooves (410) respectively, and the two long side walls of the rotating block are provided with second positioning grooves (410) respectively
After the rotating block (41) is rotated, the spring ball (32) is inserted into the first positioning groove (410).
6. The high-integration integrated rescue unmanned aerial vehicle of claim 5,
the aircraft body is characterized in that four driving propellers (11) are further fixed on the aircraft body (1), and the four driving propellers (11) are respectively and rotatably connected to the lower side of the aircraft body (1).
7. The high-integration integrated rescue unmanned aerial vehicle of claim 6,
the aircraft is characterized in that four supporting legs (12) are further fixed on the aircraft body (1), each supporting leg (12) is correspondingly arranged on one outer side of the driving propeller (11), and the distance between each supporting leg (12) and the lower bottom surface of the aircraft body (1) is greater than the distance between the blades of the driving propeller (11) and the aircraft body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121254731.0U CN215155585U (en) | 2021-06-07 | 2021-06-07 | High integration first aid rescue unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121254731.0U CN215155585U (en) | 2021-06-07 | 2021-06-07 | High integration first aid rescue unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215155585U true CN215155585U (en) | 2021-12-14 |
Family
ID=79391164
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121254731.0U Active CN215155585U (en) | 2021-06-07 | 2021-06-07 | High integration first aid rescue unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215155585U (en) |
-
2021
- 2021-06-07 CN CN202121254731.0U patent/CN215155585U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104709460B (en) | Fixed-wing unmanned aerial vehicle capable of being quickly disassembled and assembled | |
| CN106379515B (en) | Scalable oar arm component and unmanned aerial vehicle | |
| CN215155585U (en) | High integration first aid rescue unmanned aerial vehicle | |
| CN112896497B (en) | Unmanned helicopter | |
| CN112429554B (en) | Pod rod folding and unfolding mechanism based on metal belt driving | |
| CN111409847B (en) | Middle-high speed fixed wing unmanned aerial vehicle launching cradle | |
| CN113212735B (en) | Air-jet unmanned aerial vehicle | |
| CN218949476U (en) | Unmanned aerial vehicle tail wing beta structure | |
| CN209993649U (en) | Quick assembly disassembly formula battery reaches unmanned aerial vehicle who contains it for unmanned aerial vehicle | |
| CN210503175U (en) | Collapsible unmanned aerial vehicle | |
| CN209208909U (en) | A kind of electric machine mounting device and portable type install equipment | |
| CN209852573U (en) | Commodity circulation unmanned aerial vehicle | |
| CN214451792U (en) | Side direction open-type unmanned aerial vehicle GPS antenna base | |
| CN113619774A (en) | Foldable air rudder | |
| CN217502062U (en) | Telescopic fan structure and fan | |
| CN109330218B (en) | Formula of book office supplies placer is blown in circulation distinguished and admirable | |
| CN217100482U (en) | Oil-electricity extended-range type six-rotor unmanned aerial vehicle | |
| CN211404722U (en) | Unmanned aerial vehicle-mounted antenna support | |
| CN221877841U (en) | Portable warning sign for road construction | |
| CN217864736U (en) | Dual-purpose unmanned aerial vehicle screw in plateau plain | |
| CN212861842U (en) | Unmanned aerial vehicle horn folding mechanism | |
| CN219380770U (en) | Diaphragm cutting device and diaphragm production device | |
| CN218054992U (en) | Vehicle-mounted take-off and landing device of vertical take-off and landing fixed wing aircraft | |
| CN220924541U (en) | Foldable light unmanned aerial vehicle wing | |
| CN210805979U (en) | Support frame of portable satellite station |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |