CN216943588U - Airborne unmanned wing plane - Google Patents
Airborne unmanned wing plane Download PDFInfo
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- CN216943588U CN216943588U CN202220204255.XU CN202220204255U CN216943588U CN 216943588 U CN216943588 U CN 216943588U CN 202220204255 U CN202220204255 U CN 202220204255U CN 216943588 U CN216943588 U CN 216943588U
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- 230000007246 mechanism Effects 0.000 claims abstract description 36
- 238000009434 installation Methods 0.000 claims abstract description 34
- 238000007789 sealing Methods 0.000 claims description 5
- 239000003973 paint Substances 0.000 claims description 4
- 210000002421 cell wall Anatomy 0.000 claims description 3
- 230000000694 effects Effects 0.000 claims description 3
- 230000003028 elevating effect Effects 0.000 claims description 3
- 230000000149 penetrating effect Effects 0.000 claims description 3
- 230000009471 action Effects 0.000 abstract description 5
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 230000008676 import Effects 0.000 abstract description 2
- 230000002349 favourable effect Effects 0.000 description 4
- 238000003780 insertion Methods 0.000 description 4
- 230000037431 insertion Effects 0.000 description 4
- 230000004075 alteration Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses an airborne unmanned wing plane, which comprises an unmanned plane, wherein the lower end of the unmanned plane is fixedly connected with an installation mechanism, the top end of the installation mechanism is fixedly connected with a lifting mechanism, and the lower end of the lifting mechanism is fixedly connected with a dismounting mechanism, and the airborne unmanned wing plane has the beneficial effects that: drive the lifter plate through setting up electric telescopic handle and slide in first spout is inside, thereby can drive the installation piece and pass to import and export and remove from the installation incasement portion, the pulling arm-tie this moment, the arm-tie stably drives the inserted bar under the elastic action of spring and removes from the mounting groove is inside, at this moment, conveniently install connecting block snap-on to the mounting groove through second spout and slider inside, then through loosening the arm-tie, the elastic action at the spring drives the inserted bar and resets and passes the jack and insert and establish inside the slot, be convenient for stabilize the dismantlement installation to the camera, it rises to drive the installation piece through electric telescopic handle this moment, protect.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an airborne unmanned bureaucratic plane.
Background
An unmanned plane is a manned plane operated by radio remote control equipment and a self-contained program control device, and is a general name of the unmanned plane, and a general airborne unmanned plane carries out escort and search monitoring through a camera when in use.
However, the cameras of the existing airborne unmanned wing aircraft are all fixedly mounted at the lower end of the unmanned wing aircraft, so that the existing airborne unmanned wing aircraft is very inconvenient to disassemble when being damaged during maintenance, is difficult to disassemble, is long in disassembling time, cannot be replaced quickly, and is inconvenient to use.
SUMMERY OF THE UTILITY MODEL
The present invention aims at providing airborne unmanned bureaucratic plane to solve the problems mentioned in the background art.
In order to achieve the purpose, the utility model provides the following technical scheme: an airborne unmanned wing plane comprises an unmanned aerial vehicle, wherein the lower end of the unmanned aerial vehicle is fixedly connected with an installation mechanism, the top end of the installation mechanism is fixedly connected with a lifting mechanism, the lower end of the lifting mechanism is fixedly connected with a dismounting mechanism, and the outside of the dismounting mechanism is fixedly connected with a limiting mechanism;
the mounting mechanism comprises a mounting box, the mounting box is fixedly connected to the lower end of the unmanned aerial vehicle, an inlet and an outlet are formed in the box wall of the lower end of the mounting box in a penetrating mode, and two first sliding grooves are formed in the box wall of the two sides of the mounting box;
elevating system includes an electric telescopic handle, electric telescopic handle fixed connection tank wall in the install bin top, just electric telescopic handle output end fixed connection has a lifter plate, lifter plate both sides sliding connection is in two first spouts, an installation piece of lifter plate lower extreme fixedly connected with, an installation groove has been seted up to installation piece lower extreme, two second spouts, two have been seted up to the cell wall in the installation groove both sides the second spout runs through installation piece surface, two the relative one side of second spout runs through and has seted up a jack.
Preferably, the dismounting mechanism comprises a connecting block, the connecting block is movably inserted into the mounting groove, two sliding blocks are fixedly connected to two sides of the connecting block, the two sliding blocks are slidably connected into the two second sliding grooves, the two sliding blocks and the two jacks are provided with a slot at corresponding positions, and the lower end of the connecting block is fixedly connected with a camera.
Preferably, stop gear includes two springs, two the spring is the symmetry and sets up fixed connection in the connecting block both sides, and two arm-tie of spring relative one side fixedly connected with, two the fixed loop of arm-tie has an inserted bar, two the inserted bar passes two springs and jack and inserts and establish in two slots.
Preferably, the two sides of the lower surface of the unmanned aerial vehicle are fixedly connected with four stand columns which are symmetrically arranged.
Preferably, the lower ends of the four upright posts are fixedly connected with a protection pad.
Preferably, the outer surfaces of the two springs are coated with a layer of sealing paint.
Compared with the prior art, the utility model has the beneficial effects that: drive the lifter plate through setting up electric telescopic handle and slide in first spout is inside, thereby can drive the installation piece and pass to import and export and remove from the installation incasement portion, the pulling arm-tie this moment, the arm-tie stably drives the inserted bar under the elastic action of spring and removes from the mounting groove is inside, at this moment, conveniently install connecting block snap-on to the mounting groove through second spout and slider inside, then through loosening the arm-tie, the elastic action at the spring drives the inserted bar and resets and passes the jack and insert and establish inside the slot, be convenient for stabilize the dismantlement installation to the camera, it rises to drive the installation piece through electric telescopic handle this moment, protect.
Drawings
FIG. 1 is a schematic external view of the present invention;
FIG. 2 is a schematic view of the internal structure of the mounting box of the present invention;
FIG. 3 is an enlarged view of portion A of FIG. 2;
FIG. 4 is a schematic bottom view of the mounting block of the present invention;
FIG. 5 is a schematic cross-sectional view taken along the line B-B in FIG. 2 according to the present invention.
In the figure: 1. an unmanned aerial vehicle;
2. an installation mechanism; 21. installing a box; 22. an inlet and an outlet; 23. a first chute;
3. a lifting mechanism; 31. an electric telescopic rod; 32. a lifting plate; 33. mounting blocks; 34. mounting grooves; 35. a second chute; 36. a jack;
4. a disassembly and assembly mechanism; 41. connecting blocks; 42. a slider; 43. a slot; 44. a camera;
5. a limiting mechanism; 51. a spring; 52. pulling a plate; 53. inserting a rod;
6. a column; 7. and (6) a protective pad.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-5, the present invention provides a technical solution: an airborne unmanned wing plane comprises an unmanned aerial vehicle 1, wherein the lower end of the unmanned aerial vehicle 1 is fixedly connected with an installation mechanism 2, the top end of the installation mechanism 2 is fixedly connected with a lifting mechanism 3, the lower end of the lifting mechanism 3 is fixedly connected with a dismounting mechanism 4, and the outside of the dismounting mechanism 4 is fixedly connected with a limiting mechanism 5;
the mounting mechanism 2 comprises a mounting box 21, the mounting box 21 is fixedly connected to the lower end of the unmanned aerial vehicle 1, an inlet and an outlet 22 are formed in the box wall of the lower end of the mounting box 21 in a penetrating mode, and two first sliding grooves 23 are formed in the inner box walls of two sides of the mounting box 21;
elevating system 3 includes an electric telescopic handle 31, electric telescopic handle 31 fixed connection is at the 21 top of install bin inner tank wall, and electric telescopic handle 31 output end fixedly connected with a lifter plate 32, lifter plate 32 both sides sliding connection is in two first spouts 23, an installation piece 33 of lifter plate 32 lower extreme fixedly connected with, an installation groove 34 has been seted up to installation piece 33 lower extreme, two second spouts 35 have been seted up to the cell wall in the 34 both sides of installation groove, two second spouts 35 run through the surface of installation piece 33, one side of two second spouts 35 is relative runs through and has been seted up a jack 36.
Dismouting mechanism 4 includes a connecting block 41, connecting block 41 activity is inserted and is established in mounting groove 34, two sliders 42 of connecting block 41 both sides fixedly connected with, two sliders 42 sliding connection are in two second spout 35, and a slot 43 has all been seted up to two sliders 42 and two corresponding positions of jack 36, camera 44 of connecting block 41 lower extreme fixedly connected with, be favorable to conveniently installing connecting block 41 fast in mounting groove 34 through slider 42 and second spout 35, be convenient for change camera 44.
Four stand 6 that are the symmetry and set up of 1 lower surface both sides fixedly connected with of unmanned aerial vehicle are favorable to supporting unmanned aerial vehicle 1 through four convenient stabilities of stand 6.
The equal fixedly connected with of four stand 6 lower extremes protects pad 7, is favorable to conveniently cushioning protection to stand 6 through protection pad 7.
The outer surfaces of the two springs 51 are coated with a layer of sealing paint, so that the sealing performance of the two springs 51 is improved through the sealing paint, and the springs are prevented from being rusted.
Specifically, when the present invention is used, the electric telescopic rod 31 drives the lifting plate 32 to descend, the lifting plate 32 can stably slide in the first sliding groove 23, the lifting plate 32 can drive the mounting block 33 to move to the lower end of the mounting box 21 through the entrance 22, then the two pulling plates 52 are pulled, the two pulling plates 52 drive the two inserting rods 53 to move from the mounting groove 34 to the inserting holes 36, at the moment, the two sliding blocks 42 are connected in the second sliding groove 35 in a sliding way through the connecting block 41, when the two slots 43 and the two insertion holes 36 are aligned, the two pulling plates 52 are loosened, the two insertion rods 53 are driven to reset through the elastic action of the two springs 51, at the moment, the two insertion rods 53 penetrate through the two insertion holes 36 and are inserted into the slots 43 to limit the connecting block 41, therefore, the camera 44 can be disassembled and assembled, and finally the electric telescopic rod 31 drives the installation block 33 to ascend to enter the installation box 21 for protection.
In the description of the present invention, it is to be understood that the terms "coaxial", "bottom", "one end", "top", "middle", "other end", "upper", "one side", "top", "inner", "front", "center", "both ends", and the like, indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the referenced device or element must have a particular orientation, be constructed and operated in a particular orientation, and thus, are not to be construed as limiting the present invention.
Furthermore, the terms "first", "second", "third", "fourth" are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated, whereby the features defined as "first", "second", "third", "fourth" may explicitly or implicitly include at least one such feature.
In the present invention, unless otherwise expressly specified or limited, the terms "mounted," "disposed," "connected," "secured," "screwed" and the like are to be construed broadly, e.g., as meaning fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; the terms may be directly connected or indirectly connected through an intermediate, and may be communication between two elements or interaction relationship between two elements, unless otherwise specifically limited, and the specific meaning of the terms in the present invention will be understood by those skilled in the art according to specific situations.
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 utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. An airborne unmanned wing plane, which is characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle (1), wherein the lower end of the unmanned aerial vehicle (1) is fixedly connected with an installation mechanism (2), the top end of the installation mechanism (2) is fixedly connected with a lifting mechanism (3), the lower end of the lifting mechanism (3) is fixedly connected with a dismounting mechanism (4), and the outside of the dismounting mechanism (4) is fixedly connected with a limiting mechanism (5);
the mounting mechanism (2) comprises a mounting box (21), the mounting box (21) is fixedly connected to the lower end of the unmanned aerial vehicle (1), an inlet and an outlet (22) are formed in the wall of the lower end of the mounting box (21) in a penetrating mode, and two first sliding grooves (23) are formed in the inner wall of the two sides of the mounting box (21);
elevating system (3) include an electric telescopic handle (31), electric telescopic handle (31) fixed connection is at the inner box wall of install bin (21) top, just electric telescopic handle (31) output end fixedly connected with lifter plate (32), lifter plate (32) both sides sliding connection is in two first spout (23), installation piece (33) of lifter plate (32) lower extreme fixedly connected with, an installation groove (34) has been seted up to installation piece (33) lower extreme, two second spout (35), two have been seted up to cell wall in installation groove (34) both sides second spout (35) run through installation piece (33) surface, two relative one side of second spout (35) is run through and has been seted up one jack (36).
2. An airborne unmanned wing-plane as defined in claim 1, wherein: dismouting mechanism (4) include a connecting block (41), connecting block (41) activity is inserted and is established in mounting groove (34), two slider (42), two of connecting block (41) both sides fixedly connected with slider (42) sliding connection is in two second spout (35), and two a slot (43) has all been seted up to slider (42) and two corresponding positions of jack (36), camera (44) of connecting block (41) lower extreme fixedly connected with.
3. An airborne unmanned wing-plane as defined in claim 1, wherein: stop gear (5) include two springs (51), two spring (51) are the symmetry and set up fixed connection in connecting block (41) both sides, and two spring (51) one side fixedly connected with two arm-tie (52) relatively, two arm-tie (52) are fixed to be cup jointed an inserted bar (53), two inserted bar (53) pass two springs (51) and jack (36) and insert and establish in two slots (43).
4. An airborne unmanned wing-plane as defined in claim 1, wherein: unmanned aerial vehicle (1) lower surface both sides fixedly connected with four stands (6) that are the symmetry and set up.
5. An airborne unmanned wing-plane as defined in claim 4, wherein: the lower ends of the four upright posts (6) are fixedly connected with a protection pad (7).
6. An airborne unmanned wing-plane according to claim 3, characterized in that: the outer surfaces of the two springs (51) are coated with a layer of sealing paint.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220204255.XU CN216943588U (en) | 2022-01-25 | 2022-01-25 | Airborne unmanned wing plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220204255.XU CN216943588U (en) | 2022-01-25 | 2022-01-25 | Airborne unmanned wing plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216943588U true CN216943588U (en) | 2022-07-12 |
Family
ID=82318764
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220204255.XU Active CN216943588U (en) | 2022-01-25 | 2022-01-25 | Airborne unmanned wing plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216943588U (en) |
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2022
- 2022-01-25 CN CN202220204255.XU patent/CN216943588U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 710089 No. 38, Hangkong 1st Road, National Aviation high tech industry base, Xi'an, Shaanxi Province Patentee after: Xi'an Yalong Aviation Electromechanical Co.,Ltd. Country or region after: China Address before: 710089 No. 38, Hangkong 1st Road, National Aviation high tech industry base, Xi'an, Shaanxi Province Patentee before: XI'AN YALONG AVIATION ELECTROMECHANICAL CO.,LTD. Country or region before: China |
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| CP03 | Change of name, title or address |