CN210852921U - Formula fast assembly unmanned aerial vehicle is inhaled to magnetism - Google Patents
Formula fast assembly unmanned aerial vehicle is inhaled to magnetism Download PDFInfo
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- CN210852921U CN210852921U CN201921969457.8U CN201921969457U CN210852921U CN 210852921 U CN210852921 U CN 210852921U CN 201921969457 U CN201921969457 U CN 201921969457U CN 210852921 U CN210852921 U CN 210852921U
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Abstract
The utility model relates to an unmanned air vehicle technique field discloses a formula fast assembly unmanned aerial vehicle is inhaled to magnetism. The utility model provides a formula fast assembly unmanned aerial vehicle is inhaled to magnetism, includes unmanned aerial vehicle, first powerful magnetite and the powerful magnetite of second, unmanned aerial vehicle comprises fuselage, horn and spiral, the one end connection of horn is fixed on the fuselage, the horn is equipped with a plurality ofly, and is a plurality of the horn sets up all around the fuselage, all is equipped with a spiral on every horn, is equipped with first powerful magnetite with the contact position department of spiral on the horn, and spiral and the contact position department of horn are equipped with the powerful magnetite of second, the horn is equipped with the connector with the contact position department of spiral, the spiral with the junction of horn is equipped with the connecting piece, the connecting piece cartridge is in the connector. The utility model discloses unmanned aerial vehicle makes spiral piece and horn interconnect through first powerful magnetite and the powerful magnetite of second to suction through the magnetite provides the electric energy with the connecting piece cartridge for the spiral piece in the connector, makes it carry out the dismouting fast.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to formula fast assembly unmanned aerial vehicle is inhaled to magnetism.
Background
The unmanned plane is called unmanned plane for short, and is called UAV in English for short, and is an unmanned plane operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, and the unmanned plane is divided into civil use and military use, and is really just needed by the unmanned plane in civil use and applied in the unmanned plane + industry; 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 industrial application and develop unmanned aerial vehicle technology.
Common civilian unmanned aerial vehicle is many rotor crafts, drive unmanned aerial vehicle through a plurality of augments and fly, generally in order to improve unmanned aerial vehicle's duration and flight performance, need alleviate unmanned aerial vehicle's whole weight, helical blade's length promotes unmanned aerial vehicle's flight performance in the increase augments, consequently, lead to the blade in the augments bulky and easily receive the damage, portable, unmanned aerial vehicle often dismantles the augments in unmanned aerial vehicle in the transportation and gets off and deposit alone and transport, in order to prevent that the augments from receiving the extrusion in the transportation and causing the damage, but the dismouting process of the augments among the prior art is loaded down with trivial details, need demolish a large amount of small-size screw, be not convenient for accomodate and lose easily.
The information disclosed in this background section is only for enhancement of understanding of the general background of the invention and should not be taken as an acknowledgement or any form of suggestion that this information constitutes prior art already known to a person skilled in the art.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a formula fast assembly unmanned aerial vehicle is inhaled to the spiral piece among the unmanned aerial vehicle among the solution prior art is not convenient for the technical problem of dismouting.
The utility model provides a formula fast assembly unmanned aerial vehicle is inhaled to magnetism, includes unmanned aerial vehicle, first powerful magnetite and the powerful magnetite of second, unmanned aerial vehicle comprises fuselage, horn and spiral piece, the one end of horn is connected to be fixed on the fuselage, the horn is equipped with a plurality ofly, and is a plurality of the horn sets up around the fuselage, every all be equipped with a spiral piece on the horn, be equipped with first powerful magnetite with the contact position department of spiral piece on the horn, the spiral piece is equipped with the powerful magnetite of second with the contact position department of horn, the horn is equipped with the connector with the contact position department of spiral piece, the spiral piece with the junction of horn is equipped with the connecting piece, the connecting piece cartridge is in the connector.
Furthermore, a limiting sleeve is arranged on the spiral part, the second powerful magnet and the connecting piece are arranged in the limiting sleeve, and the machine arm is inserted in the limiting sleeve.
Further, the spiral part is provided with a safety locking part, the horn is provided with a safety lock catch, and the safety locking part is clamped on the safety lock catch.
Furthermore, a first positioning mark is arranged on the spiral piece, a second positioning mark is arranged on the machine arm, and the first positioning mark and the second positioning mark correspond to each other.
Furthermore, a protective guard is arranged on the spiral piece.
Compared with the prior art, the beneficial effects of the utility model are that:
(1) in the utility model, the body and the arm of the unmanned aerial vehicle are fixed into a whole, the spiral part is designed into an independent individual body, the machine arm is provided with a first strong magnet, the spiral piece is provided with a second strong magnet, the spiral piece is quickly connected with the machine arm by utilizing the principle that the magnets attract each other in opposite polarities, the first strong magnet and the second strong magnet can be provided with a plurality of magnets which are mutually matched, thereby increasing the connection strength between the machine arm and the spiral piece, and the machine arm is provided with a connector which is connected to an electric control unit in the machine body through a line, the spiral piece is provided with a connecting piece, when the first powerful magnet and the second powerful magnet are mutually adsorbed, the connecting piece is inserted into the connecting head under the action of magnetic force, thereby let the automatically controlled unit can provide the electric energy for the spiral and ten make it can carry out work to this technical problem that the spiral among the prior art in the unmanned aerial vehicle is not convenient for the dismouting effectively solved.
(2) The utility model provides a spiral is solitary individuality, can make unmanned aerial vehicle can continue to carry out normal use through changing the spiral when having the unable normal work of spiral of independent direction among the unmanned aerial vehicle, has improved unmanned aerial vehicle's life.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic view of the split structure of the present invention;
FIG. 3 is an enlarged view of the structure at A in FIG. 2;
FIG. 4 is an enlarged view of the structure at B in FIG. 2;
FIG. 5 is an enlarged view of the structure at C in FIG. 2;
description of the main reference numerals:
1-unmanned aerial vehicle; 11-a fuselage; 2-a first strong magnet; 3-a second strong magnet; 4-a machine arm; 41-a connector; 42-safety lock catch; 43-a second locator; 5-a screw element; 51-a connector; 52-a stop collar; 53-safety lock; 54-first location flag; 55-protective fence.
Detailed Description
The following detailed description of the present invention is provided in conjunction with the accompanying drawings, but it should be understood that the scope of the present invention is not limited by the following detailed description.
Throughout the specification and claims, unless explicitly stated otherwise, the word "comprise", or variations such as "comprises" or "comprising", will be understood to imply the inclusion of a stated element or component but not the exclusion of any other element or component.
Referring to fig. 1-5, a formula fast assembly unmanned aerial vehicle is inhaled to magnetism, including unmanned aerial vehicle 1, first powerful magnetite 2 and second powerful magnetite 3, unmanned aerial vehicle 1 comprises fuselage 11, horn 4 and spiral 5, the one end of horn 4 is connected to be fixed on the fuselage 11, horn 4 is equipped with a plurality ofly, and is a plurality of horn 4 sets up fuselage 11 is all around, every all be equipped with a spiral 5 on the horn 4, be equipped with first powerful magnetite 2 with the contact position department of spiral 5 on the horn 4, spiral 5 is equipped with second powerful magnetite 3 with the contact position department of horn 4, be equipped with connector 41 with the contact position department of spiral 5 on the horn 4, spiral 5 go up with the junction of horn 4 is equipped with connecting piece 51, connecting piece 51 cartridge is in connector 41.
In the utility model, the body 11 and the arm 4 of the unmanned aerial vehicle 1 are fixed into a whole, the spiral part 5 is designed into a single individual body, the first strong magnet 2 is arranged on the machine arm 4, the second strong magnet 3 is arranged on the screw part 5, the screw part 5 and the machine arm 4 are quickly connected by utilizing the principle that the magnets are attracted in opposite directions, the first strong magnet 2 and the second strong magnet 3 can be arranged in a plurality of interaction matching, thereby increasing the connection strength of the horn 4 and the screw 5, and the connecting head 41 is provided on the horn 4, the connector 41 is connected to an electric control unit in the body 11 through a line, the screw 5 is provided with a connector 51, when the first powerful magnet 2 and the second powerful magnet 3 are attracted to each other, the connecting piece 51 is inserted into the connecting head 41 under the action of magnetic force, so that the electronic control unit can provide electric energy for the screw 5 to enable the screw to work.
Preferably, a limiting sleeve 52 is arranged on the spiral part 5, the second powerful magnet 3 and the connecting piece 51 are arranged in the limiting sleeve 52, the horn 4 is inserted into the limiting sleeve 52, when the spiral part 5 and the horn 4 need to be connected with each other, the limiting sleeve 52 on the spiral part 5 is aligned to the horn 4, the adsorption position of the first powerful magnet 2 and the second powerful magnet 3 is limited, so that the position of the first powerful magnet 2 and the position of the second powerful magnet 3 in the mutual adsorption process are prevented from being deviated, the connecting head 41 cannot be accurately inserted into the connecting piece 51, the spiral part 5 cannot normally work, even the connecting head 41 can be damaged, meanwhile, when the unmanned aerial vehicle 1 flies, a certain supporting force can be provided for the horn 4 through the limiting sleeve 52 on the spiral part 5, and the connecting strength between the spiral part 5 and the horn 4 is increased, prevent that screw 5 and horn 4 disconnection from leading to unmanned aerial vehicle 1 unable normal flight at operation in-process spiral 1.
Preferably, be equipped with insurance latch fitting 53 on spiral 5, be equipped with insurance hasp 42 on the horn 4, insurance latch fitting 53 blocks admittedly on insurance hasp 42, after spiral 5 and horn 4 interconnect are fixed, block insurance latch fitting 53 admittedly on insurance hasp 42, mutually support through insurance latch fitting 53 and insurance hasp 42 and make being connected between spiral 5 and the horn 4 more stable, increased spiral 5 and horn 4's joint strength, prevent that unmanned aerial vehicle 1 leads to the unable normal flight of unmanned aerial vehicle 1 at operation in-process spiral 5 and horn 4 disconnection.
Preferably, be equipped with first locating mark 54 on spiral piece 5, be equipped with second locating mark 43 on the horn 4, first locating mark 54 corresponds each other with second locating mark 43, when the manual work docks spiral piece 5 and horn 4 each other, looks for first locating mark 54 and second locating mark 43 on spiral piece 5 and the horn 4 through observing to dock spiral piece 5 and horn 4 after aligning first locating mark 54 and second locating mark 43 each other, to prevent that the angle of spiral piece 5 and horn 4 butt joint process from appearing the deviation and leading to causing the damage to connector 41 in the butt joint process.
Preferably, a protective guard 55 is arranged on the screw 5, and objects which may be touched by the unmanned aerial vehicle 1 during operation are blocked by the protective guard 55, so that the screw 5 is prevented from being damaged due to contact with hard objects.
The foregoing descriptions of specific exemplary embodiments of the present invention have been presented for purposes of illustration and description. It is not intended to limit the invention to the precise form disclosed, and obviously many modifications and variations are possible in light of the above teaching. The exemplary embodiments were chosen and described in order to explain certain principles of the invention and its practical application to enable one skilled in the art to make and use various exemplary embodiments of the invention and various alternatives and modifications as are suited to the particular use contemplated. It is intended that the scope of the invention be defined by the claims and their equivalents.
Claims (5)
1. The utility model provides a formula fast assembly unmanned aerial vehicle is inhaled to magnetism, its characterized in that, includes unmanned aerial vehicle (1), first powerful magnetite (2) and second powerful magnetite (3), unmanned aerial vehicle (1) comprises fuselage (11), horn (4) and spiral (5), the one end of horn (4) is connected to be fixed on fuselage (11), horn (4) are equipped with a plurality ofly, and is a plurality of horn (4) set up around fuselage (11), every be equipped with a spiral (5) on horn (4), be equipped with first powerful magnetite (2) with the contact position department of spiral (5) on horn (4), spiral (5) are equipped with second powerful magnetite (3) with the contact position department of horn (4), horn (4) and the contact position department of spiral (5) are equipped with connector (41), spiral (5) with the junction of horn (4) is equipped with connecting piece (51), the connecting piece (51) is inserted in the connecting head (41).
2. The unmanned aerial vehicle is assembled to formula of inhaling fast of claim 1, characterized in that, be equipped with stop collar (52) on spiral spare (5), second powerful magnetite (3) and connecting piece (51) set up in stop collar (52), horn (4) cartridge is in stop collar (52).
3. The unmanned aerial vehicle is assembled to formula fast of inhaling of claim 1, characterized in that, be equipped with insurance latch fitting (53) on spiral (5), be equipped with insurance hasp (42) on horn (4), insurance latch fitting (53) card is fixed on insurance hasp (42).
4. Magnetic-type rapid-assembly unmanned aerial vehicle according to claim 1, wherein the screw (5) is provided with a first positioning mark (54), the arm (4) is provided with a second positioning mark (43), and the first positioning mark (54) and the second positioning mark (43) correspond to each other.
5. Magnetic-type rapid assembly drone according to claim 1, characterized in that said screws (5) are provided with protective guards (55).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921969457.8U CN210852921U (en) | 2019-11-14 | 2019-11-14 | Formula fast assembly unmanned aerial vehicle is inhaled to magnetism |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921969457.8U CN210852921U (en) | 2019-11-14 | 2019-11-14 | Formula fast assembly unmanned aerial vehicle is inhaled to magnetism |
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| CN210852921U true CN210852921U (en) | 2020-06-26 |
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| CN201921969457.8U Active CN210852921U (en) | 2019-11-14 | 2019-11-14 | Formula fast assembly unmanned aerial vehicle is inhaled to magnetism |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20200207469A1 (en) * | 2017-05-19 | 2020-07-02 | The Texas A&M University System | Multi-modal vehicle |
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2019
- 2019-11-14 CN CN201921969457.8U patent/CN210852921U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20200207469A1 (en) * | 2017-05-19 | 2020-07-02 | The Texas A&M University System | Multi-modal vehicle |
| US11673663B2 (en) * | 2017-05-19 | 2023-06-13 | The Texas A&M University System | Multi-modal vehicle |
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