CN207759024U - A kind of multi-rotor unmanned aerial vehicle horn folding device - Google Patents

A kind of multi-rotor unmanned aerial vehicle horn folding device Download PDF

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Publication number
CN207759024U
CN207759024U CN201721849489.5U CN201721849489U CN207759024U CN 207759024 U CN207759024 U CN 207759024U CN 201721849489 U CN201721849489 U CN 201721849489U CN 207759024 U CN207759024 U CN 207759024U
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CN
China
Prior art keywords
connector
horn
square hole
aerial vehicle
unmanned aerial
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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.)
Expired - Fee Related
Application number
CN201721849489.5U
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Chinese (zh)
Inventor
雷乾勇
朱国民
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shenzhen Gkxn Technology Co Ltd
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Shenzhen Gkxn Technology Co Ltd
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Filing date
Publication date
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Priority to CN201721849489.5U priority Critical patent/CN207759024U/en
Application granted granted Critical
Publication of CN207759024U publication Critical patent/CN207759024U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model is related to a kind of multi-rotor unmanned aerial vehicle horn folding devices, include the fold mechanism of the first horn, the second horn and connection first horn and the second horn;The fold mechanism includes the first connector, the second connector, screw thread shell and central balancing bar, and first connector is fixed on first horn, and second connector is fixed on second horn;The central balancing bar is rotatablely connected with first connector and the second connector.By the way that connector is respectively set on two horns, so that horn is folded and expansion by central balancing bar and connector rotation connection, be fixed after deployment by screw thread shell, provide screen resilience by the spring set in connector when folding.Entire folding devices fold and expansion easy switching, it is simple in structure, it is reliable and stable, it is easy to use.

Description

A kind of multi-rotor unmanned aerial vehicle horn folding device
Technical field
The utility model is related to air vehicle technique fields, are folded more specifically to a kind of multi-rotor unmanned aerial vehicle horn Device.
Background technology
Multi-rotor unmanned aerial vehicle is a kind of tool there are three and the above rotor shaft special pilotless helicopter.It passes through Motor rotation on each axis, drives rotor, to generate a liter thrust.Rotor always away from fixation, rather than general helicopter It is variable like that.By changing the relative rotation speed between different rotors, thus it is possible to vary the size of uniaxial propulsive force, to control flight The running orbit of device.
The horn of multi-rotor unmanned aerial vehicle is longer, and the storage and transport to body bring inconvenience, existing unmanned plane machine Arm foldable structure mostly uses bolt plug-in type bindiny mechanism and is folded, and dismounting is inconvenient, and process is cumbersome, some also need to special tool Tool so that working efficiency is relatively low, and structure safety and reliability reduce.
Utility model content
The technical problems to be solved in the utility model is:A kind of multi-rotor unmanned aerial vehicle horn folding device is provided, overcome on The deficiency stated, achievees the effect that folding convenient and stability is good.
The technical solution of the utility model is:The utility model provides a kind of multi-rotor unmanned aerial vehicle horn folding dress It sets, includes the fold mechanism of the first horn, the second horn and connection first horn and the second horn;The fold mechanism Including the first connector, the second connector, screw thread shell and central balancing bar, first connector is fixed on first machine On arm, second connector is fixed on second horn;The central balancing bar and first connector and second Connector is rotatablely connected.
Further, first connector and the second connector are equipped with external screw thread, and the screw thread shell is equipped with interior spiral shell Line;First connector and the second connector are connect with the screw thread outer casing screw.
Further, offer the first square hole in the middle part of first connector, first square hole it is upper Portion and lower part are equipped with the first guide groove, and the right side level fluting of first square hole extends to the outer surface of the first connector Form the first supporting table;The second square hole, the top of second square hole are offered in the middle part of second connector It is equipped with the second guide groove with lower part, the left side level fluting of second square hole extends to the outer surface shape of the second connector At the second supporting table.
Further, the central balancing bar includes the body of rod, and the both ends of the body of rod are respectively equipped with first rotating shaft and second Shaft;The body of rod is the cuboid that middle part offers through-hole;The first rotating shaft is sheathed in first guide groove, and described Two shafts are sheathed in second guide groove.
Further, it is fixed with the first adjustable spring in first square hole, is fixed in second square hole There is the second adjustable spring;The free end of first adjustable spring is fixed in the first rotating shaft, second adjustable spring Free end be fixed in second shaft.
Further, the width of first guide groove and the second guide groove is more than the straight of the first rotating shaft and the second shaft Diameter.
Further, the width of first square hole and the second square hole is more than the width of the central balancing bar Degree;The sum of length of first square hole and the second square hole is more than the length of the central balancing bar.
Further, the width of first supporting table and the second supporting table is equal to the width of the central balancing bar.
The multi-rotor unmanned aerial vehicle horn folding device for implementing the utility model, has the advantages that:By at two Connector is respectively set on horn, so that horn is folded and is unfolded by central balancing bar and connector rotation connection, after deployment It is fixed by screw thread shell, provides screen resilience by the spring set in connector when folding.Entire folding devices fold and Easy switching is unfolded, it is simple in structure, it is reliable and stable, it is easy to use.
Description of the drawings
Below in conjunction with accompanying drawings and embodiments, the utility model is described in further detail, in attached drawing:
Fig. 1 is the structural schematic diagram of the utility model multi-rotor unmanned aerial vehicle horn folding device;
Fig. 2 is the sectional view of the utility model multi-rotor unmanned aerial vehicle horn folding device;
Fig. 3 is the schematic diagram of folding device before horn expansion;
Fig. 4 is the schematic diagram that horn is fully deployed rear folding device;
Fig. 5 is the sectional view of folding device before horn expansion;
Fig. 6 is the sectional view that horn is fully deployed rear folding device;
Fig. 7 is the structural schematic diagram of the first connector of the utility model multi-rotor unmanned aerial vehicle horn folding device;
Fig. 8 is the sectional view of the first connector of the utility model multi-rotor unmanned aerial vehicle horn folding device;
Fig. 9 is the structural schematic diagram of the second connector of the utility model multi-rotor unmanned aerial vehicle horn folding device;
Figure 10 is the sectional view of the second connector of the utility model multi-rotor unmanned aerial vehicle horn folding device;
Figure 11 is the structural schematic diagram of the central balancing bar of the utility model multi-rotor unmanned aerial vehicle horn folding device;
Figure 12 is the structural schematic diagram of the screw thread shell of the utility model multi-rotor unmanned aerial vehicle horn folding device.
Specific implementation mode
Fig. 1 to Figure 12 shows a preferred embodiment of the utility model multi-rotor unmanned aerial vehicle horn folding device, packet Include the first horn 1, the second horn 2 and the fold mechanism 3 for connecting the first horn 1 and the second horn 2;Fold mechanism 3 includes the A connection piece 31, the second connector 32, screw thread shell 33 and central balancing bar 34, the first connector 31 are fixed on the first horn 1 On, the second connector 32 is fixed on the second horn 2;Central balancing bar 34 and the first connector 31 and the second connector 32 rotate Connection.First connector 31 and the second connector 32 are respectively used to connect with the first horn 1 and the second horn 2, to keep connection steady Surely it is reliably connected mode to select to be bolted, the outer diameter of 32 connecting pin of the first connector 31 and the second connector is less than the first horn 1 and second horn 2 internal diameter, the first connector 31 and the second connector 32 are respectively sleeved at the first horn 1 and the second horn 2 Interior, interconnecting piece presets bolt hole, is bolted.First connector 31 and the second connector 32 are equipped with external screw thread, screw thread Shell 33 is equipped with internal thread;First connector 31 and the second connector 32 are threadedly coupled with screw thread shell 33.When horn folds, spiral shell In the rotation to the first horn 1 or the second horn 2 of line shell 33, two horns is enable to fold;When horn is unfolded, screw thread shell 33 turn to 32 middle part of the first connector 31 and the second connector, for fixing the first connector 31 and the second connector 32.In Entreat balancing pole 34 for connecting the first connector 31 and the second connector 32, to which the first horn 1 and the second horn 2 to be connected as One.
The middle part of the first connector 31 offers the first square hole 311 in the present embodiment, the first square hole 311 it is upper Portion and lower part are equipped with the first guide groove 10, and the right side level fluting of the first square hole 311 extends to the outer of the first connector 31 Surface forms the first supporting table 20;The middle part of second connector 32 offers the second square hole 321, the second square hole 321 Upper and lower part be equipped with the second guide groove 30, the left side level fluting of the second square hole 321 extends to the second connector 32 Outer surface formed the second supporting table 40.When horn folds or is unfolded, central balancing bar 34 is accommodated in the first connector 31 In the second connector 32, it is not take up additional space, keeps overall structure simple.When horn is unfolded, as shown in fig. 6, first connects Fitting 31 and the second connector 32 turn to the position of axle center coincidence, and central balancing bar 34 is accommodated in 311 He of the first square hole In second square hole 321, screw thread shell 33 turns to middle position, and horn is fixed.When horn folds, such as Fig. 1 institutes Show, horn 1 and horn 2 are in parallel position, and central balancing bar 34 is taken out from the first square hole 311 and the second square hole 321 Go out, is contained in the first supporting table 20 and the second supporting table 40.
Central balancing bar 34 includes the body of rod 341 in the present embodiment, and the both ends of the body of rod 341 are respectively equipped with 342 He of first rotating shaft Second shaft 343;The body of rod 341 is the cuboid that middle part offers through-hole;First rotating shaft 342 is sheathed in the first guide groove 10, the Two shafts 343 are sheathed in the second guide groove 30.To make central balancing bar 34 be fixed on the first connector 31 and the second connector 32 It is interior, it is provided with through-hole at the both ends of the body of rod 341, first rotating shaft 342 and the second shaft 343 are provided in through-hole, it is preferred that first turn Axis 342 and the second shaft 343 are screw rod, and the diameter of through-hole is slightly larger than the diameter of first rotating shaft 342 and the second shaft 343 so that First rotating shaft 342 and the second shaft 343 can rotate in through-hole.The end of first rotating shaft 342 and the second shaft 343 is blocked respectively It is slided in the first guide groove 10 and the second guide groove 30, the body of rod 341 is thus fixed on the first connector 31 and the second connector 32 Between, while the body of rod 341 can be made to rotate, to meet the needs of two horns fold and are unfolded.The body of rod 341 opens up for middle part It is rectangular-ambulatory-plane to have the cuboid of through-hole, cross-sectional shape, on the basis of proof strength, reduces the weight of central balancing bar 34, Horn is set to fold and be unfolded more convenient.
The first adjustable spring 100 is fixed in the present embodiment in first square hole 311, is consolidated in the second square hole 321 Surely there is the second adjustable spring 200;The free end of first adjustable spring 100 is fixed in first rotating shaft 342, the second adjustable spring 200 free end is fixed in the second shaft 343.It is for the ease of in specifically to make the folding of horn and being unfolded conveniently Centre balancing pole 34, which is converted to the state out of the first square hole 311 and the second square hole 321, is fixed on the first supporting table 20 and second supporting table 40 state.One end of first adjustable spring 100 and the second adjustable spring 200 is being individually fixed in first just The bottom of square hole 311 and the second square hole 321, it is preferred that fixed by the way of welding, the other end is separately fixed at the In one shaft 342 and the second shaft 343, thus by the first adjustable spring 100 and the second adjustable spring 200 and central balancing bar 34 Connection.When horn is unfolded, that is, central balancing bar 34 is in the first square hole 311 and the second square hole 321 When state, screw thread shell 33 fixes the first connector 31 and the second connector 32 in outside, the first adjustable spring 100 and second Adjustable spring 200 is in compressive state.When horn becomes folded state from unfolded state, screw thread shell 33 turns to the first company On fitting 31 or the second connector 32, the first adjustable spring 100 and the rebound of the second adjustable spring 200, central balancing bar 34 will be from Pop-up in first square hole 311 and the second square hole 321, then the first connector 31 and the second connector 32 are rotated 90 °, Central balancing bar 34 is fixed in the first supporting table 20 and the second supporting table 40, the first adjustable spring 100 and the second adjustable spring 200 are in tensional state.When being converted to unfolded state by folded state, the pulling force of spring pulls central balancing bar 34 to first Square hole 311 and the sliding of the second square hole 321, the conversion of horn two states have been utilized respectively the first adjustable spring 100 With the screen resilience and pulling force of the second adjustable spring 200, the consumption of power in expansion and folding process is reduced with this so that horn folds It is simple laborsaving with expansion switching, it is easy to use.
The width of the first guide groove 10 and the second guide groove 30 is more than first rotating shaft 342 and the second shaft 343 in the present embodiment Diameter, first rotating shaft 342 and the second shaft 343 are led in the first guide groove 10 and second respectively when being folded or be unfolded convenient for horn with this Slot 30 slides.
The width of the first square hole 311 and the second square hole 321 is more than the width of central balancing bar 34 in the present embodiment Degree;The sum of length of first square hole 311 and the second square hole 321 is more than the length of central balancing bar 34, is convenient for this The movement in the first square hole 311 and the second square hole 321 of central balancing bar 34, is in horn when horn transition status When unfolded state, central balancing bar 34 is completely accommodated in the first square hole 311 and the second square hole 321, makes horn Length will not be elongated because of folding device.
The width of the first supporting table 20 and the second supporting table 40 is equal to the width of central balancing bar 34 in the present embodiment, two When a horn is in folded state, central balancing bar 34 is fixed in the first supporting table 20 and the second supporting table 40, to make folding It is in stable condition reliable, therefore the width of the first supporting table 20 and the second supporting table 40 is made to be equal to or slightly less than central balancing bar 34 Width, can avoid central balancing bar 34 in this way and the connection of the first connector 31 and the second connector 32 loosens.
The multi-rotor unmanned aerial vehicle horn folding device of the utility model is during expansion, first the first connector and second Connector is rotated around central balancing bar, is rotated as the first connector and two axis axle center of the second connector on a horizontal line; Central balancing bar is connected to the first connector and second respectively under the pulling force effect of the first adjustable spring and the second adjustable spring Part internal slide finally fits together the end face of the first connector and the second connector, by rotating screw thread shell the A connection piece and the second connector are connected through a screw thread, and are played the role of fixed.The process of folding with the above process on the contrary, Screw thread shell turns on the first connector or the second connector, and the first adjustable spring and the rebound of the second adjustable spring, center are flat Weighing apparatus bar is popped up out of the first connector and the second connector, then the first connector and the second connector are rotated 90 °, central balancing Bar is fixed on the first connector and the second connector, that is, is completed horn and folded.
Using the multi-rotor unmanned aerial vehicle horn folding device of the utility model, by the way that connection is respectively set on two horns Part makes horn fold and be unfolded, is consolidated after deployment by screw thread shell by central balancing bar and connector rotation connection Calmly, when folding screen resilience is provided by the spring set in connector.Entire folding devices fold and expansion easy switching, structure letter It is single, it is reliable and stable, it is easy to use.
The above content is only the preferred embodiment of the utility model, for those of ordinary skill in the art, according to this reality It, in specific embodiments and applications can be with many changes may be made, as long as these variations are without departing from this with novel thought The design of utility model, belongs to the scope of protection of the utility model.

Claims (8)

1. a kind of multi-rotor unmanned aerial vehicle horn folding device, which is characterized in that including the first horn (1), the second horn (2) and Connect the fold mechanism (3) of first horn (1) and the second horn (2);
The fold mechanism (3) includes the first connector (31), the second connector (32), screw thread shell (33) and central balancing bar (34), first connector (31) is fixed on first horn (1), and second connector (32) is fixed on described On two horns (2);The central balancing bar (34) is rotatablely connected with first connector (31) and the second connector (32).
2. multi-rotor unmanned aerial vehicle horn folding device according to claim 1, which is characterized in that first connector (31) and the second connector (32) is equipped with external screw thread, and the screw thread shell (33) is equipped with internal thread;First connector (31) it is threadedly coupled with the screw thread shell (33) with the second connector (32).
3. multi-rotor unmanned aerial vehicle horn folding device according to claim 1, which is characterized in that first connector (31) the first square hole (311) is offered in the middle part of, the upper and lower part of first square hole (311) is equipped with first Guide groove (10), the outer surface that the right side level fluting of first square hole (311) extends to the first connector (31) are formed First supporting table (20);The second square hole (321), second square are offered in the middle part of second connector (32) The upper and lower part in hole (321) is equipped with the second guide groove (30), and the left side level fluting of second square hole (321) extends The second supporting table (40) is formed to the outer surface of the second connector (32).
4. multi-rotor unmanned aerial vehicle horn folding device according to claim 3, which is characterized in that the central balancing bar (34) include the body of rod (341), the both ends of the body of rod (341) are respectively equipped with first rotating shaft (342) and the second shaft (343);Institute It is the cuboid that middle part offers through-hole to state the body of rod (341);The first rotating shaft (342) is sheathed on first guide groove (10) In, second shaft (343) is sheathed in second guide groove (30).
5. multi-rotor unmanned aerial vehicle horn folding device according to claim 4, which is characterized in that first square hole (311) it is fixed with the first adjustable spring (100) in, the second adjustable spring is fixed in second square hole (321) (200);The free end of first adjustable spring (100) is fixed in the first rotating shaft (342), second adjustable spring (200) free end is fixed on second shaft (343).
6. multi-rotor unmanned aerial vehicle horn folding device according to claim 4, which is characterized in that first guide groove (10) It is more than the diameter of the first rotating shaft (342) and the second shaft (343) with the width of the second guide groove (30).
7. multi-rotor unmanned aerial vehicle horn folding device according to claim 3, which is characterized in that first square hole (311) and the width of the second square hole (321) be more than the central balancing bar (34) width;First square hole (311) and the sum of the length of the second square hole (321) is more than the length of the central balancing bar (34).
8. multi-rotor unmanned aerial vehicle horn folding device according to claim 3, which is characterized in that first supporting table (20) and the width of the second supporting table (40) be equal to the central balancing bar (34) width.
CN201721849489.5U 2017-12-26 2017-12-26 A kind of multi-rotor unmanned aerial vehicle horn folding device Expired - Fee Related CN207759024U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721849489.5U CN207759024U (en) 2017-12-26 2017-12-26 A kind of multi-rotor unmanned aerial vehicle horn folding device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721849489.5U CN207759024U (en) 2017-12-26 2017-12-26 A kind of multi-rotor unmanned aerial vehicle horn folding device

Publications (1)

Publication Number Publication Date
CN207759024U true CN207759024U (en) 2018-08-24

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ID=63184874

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721849489.5U Expired - Fee Related CN207759024U (en) 2017-12-26 2017-12-26 A kind of multi-rotor unmanned aerial vehicle horn folding device

Country Status (1)

Country Link
CN (1) CN207759024U (en)

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CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180824

Termination date: 20201226