CN105035305B - Propeller folding device for unmanned plane - Google Patents

Propeller folding device for unmanned plane Download PDF

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Publication number
CN105035305B
CN105035305B CN201510550561.3A CN201510550561A CN105035305B CN 105035305 B CN105035305 B CN 105035305B CN 201510550561 A CN201510550561 A CN 201510550561A CN 105035305 B CN105035305 B CN 105035305B
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China
Prior art keywords
center ring
horn
bottom plate
unmanned plane
folding device
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CN201510550561.3A
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Chinese (zh)
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CN105035305A (en
Inventor
罗世彬
许良晓
王涛
吴雷
马波
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Hunan Airtops Intelligent Technology Co Ltd
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Hunan Airtops Intelligent Technology Co Ltd
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Priority to CN201510550561.3A priority Critical patent/CN105035305B/en
Publication of CN105035305A publication Critical patent/CN105035305A/en
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Abstract

The invention discloses a kind of propeller folding device for unmanned plane, including bottom plate, the horn of more than three, center ring, driving part and gear transmission part, the horn of more than three is circumferentially sequentially arranged on bottom plate, one end of horn is articulated with bottom plate by axle and can rotated around pin joint, and the other end of horn is used for installing unmanned plane propeller component;Center ring is located at the middle part of bottom plate, gear transmission part is installed on the week side of boss of center ring, the driving cog for coordinating with gear transmission part is provided with center ring, each that connecting rod is provided between horn and center ring, driving part is rotated center ring to push horn rotation completion opening or folding by connecting rod by gear transmission part.The present invention has the advantages that structure is simpler, it is easier to operate, can greatly improve portability.

Description

Propeller folding device for unmanned plane
Technical field
Present invention relates generally to unmanned plane field, a kind of propeller folding device suitable for Multi-axis aircraft is refered in particular to.
Background technology
At present, in unmanned plane field, Multi-axis aircraft(Multi-rotor unmanned aerial vehicle)Because its is simple in construction, low cost, manipulation Ability is preferable, can hover, and is adapted to the advantage of personal use, has attracted large quantities of airplane hobbyists and fan.And as people give birth to The diversity of mode living and rich, nowadays ordinary populace also generates keen interest to this kind of aircraft, therefore many rotors fly The row device market demand is huge, and especially consumer level is taken photo by plane unmanned plane.
Consumer level take photo by plane unmanned plane be mainly characterized by it is full-featured, compact portable, simple to operate, handling good etc..And Among these, portability is that consumer level is taken photo by plane unmanned plane one of outstanding feature the most.I.e. portability is better, and user group is bigger, The experience of user also will be better.For portability, several aspects are mainly reflected in:Overall volume and weight, inoperative shape Volume during state, whether it really is able to be easy to carry(Such as:Pocket).How unmanned plane is all from doing as far as possible in the prior art It is smaller on make an issue of, do not consider portability from multiple angles, thus can not be brought to user it is perfect just The impression taken.For example, in a non-operative state, the blade of existing unmanned plane can not all be drawn in together, carried or transported Just it is easy to that it is caused to damage during defeated, and exposed blade also can bring danger to personnel.
The content of the invention
The technical problem to be solved in the present invention is that:The technical problem existed for prior art, the present invention provides one Kind structure is simpler, operate the propeller folding device for unmanned plane that is easier, can greatly improving portability.
In order to solve the above technical problems, the present invention uses following technical scheme:
A kind of propeller folding device for unmanned plane, including bottom plate, the horn of more than three, center ring, drive division Part and gear transmission part, the horn of more than three are circumferentially sequentially arranged on bottom plate, and the one of the horn End is articulated with bottom plate by axle and can rotated around pin joint, and the other end of the horn is used for installing unmanned plane propeller group Part;The center ring is located at the middle part of bottom plate, and the gear transmission part is installed on the week side of boss of center ring, the center ring and set The driving cog for coordinating with gear transmission part is equipped with, connecting rod, the drive are each provided between the horn and center ring Dynamic component is rotated center ring to push horn rotation completion opening or folding by connecting rod by gear transmission part.
As a further improvement on the present invention:One end of the connecting rod is articulated with horn, the other end hinge of the connecting rod It is connected on center ring.
As a further improvement on the present invention:Several leads are provided with the center ring, the lead makes institute State the free degree that center ring is merely able to parallel rotation.
As a further improvement on the present invention:The center ring is the gear structure of an endless tooth, the gear drive Part is the travelling gear engaged with center ring.
As a further improvement on the present invention:The travelling gear is two, and the week side of boss of center ring is installed in symmetry shape, And be fixed on bottom plate.
As a further improvement on the present invention:Region on the bottom plate between center ring and bottom plate outward flange is provided with energy Enough accommodate the space of all horns.
As a further improvement on the present invention:Being shaped as of the bottom plate is equipped with receiving one at polygon, each edge The space of horn.
Compared with prior art, the advantage of the invention is that:
1st, the propeller folding device for unmanned plane of the invention, simple and compact for structure, small volume, gathering effect are good, The motion of all horns is so all in the region that each horn can turn to bottom plate completely when carrying out folding to rotate Horn will not be exposed, to ensure optimal portability.That is, the present invention will cause the consumer level unmanned plane of the type most Folding and unfolding is realized in limits, in the case where not sacrificing stability and basic function, real portability is realized.
2nd, the propeller folding device for unmanned plane of the invention, is driven, rotational angle can using motor mate gear To realize autonomous control by software, it can reach and preferably draw deployed condition in, so that the folding and unfolding of whole mechanism is realized, and Ensure stability.
3rd, the propeller folding device for unmanned plane of the invention, the design of center ring is in only two driving sources In the case of, it is ensured that the design of four power output synchronisms, this will cause four horn uniform forces and coordination is synchronous.
Brief description of the drawings
Fig. 1 is the structural representation when present invention is in open mode.
Fig. 2 is the structural representation when present invention is in rounding state.
Marginal data:
1st, horn;2nd, connecting rod;3rd, gear transmission part;4th, lead;5th, center ring;6th, bottom plate.
Embodiment
The present invention is described in further details below with reference to Figure of description and specific embodiment.
As depicted in figs. 1 and 2, the propeller folding device for unmanned plane of the invention, including bottom plate 6, more than three Horn 1, center ring 5, driving part(Do not show in figure)And gear transmission part 3, the horn 1 of more than three is circumferentially Be sequentially arranged on bottom plate 6, one end of horn 1 is articulated with bottom plate 6 by axle and can rotated around pin joint, horn 1 it is another End is used for installing unmanned plane propeller component.Center ring 5 is located at the middle part of bottom plate 6, and gear transmission part 3 is installed on center ring 5 The week side of boss, the driving cog for coordinating with gear transmission part 3 is provided with center ring 5, driving part passes through gear drive portion Part 3, which is rotated, rotates center ring 5.Region on bottom plate 6 between center ring 5 and the outward flange of bottom plate 6 is all provided with that can accommodate The space of horn 1.Connecting rod 2 is each provided between horn 1 and center ring 5, i.e. one end of connecting rod 2 is articulated with horn 1, connecting rod 2 other end is articulated with center ring 5.When center ring 5 is rotated, will drivening rod 2 move, so as to pass through connecting rod 2 Drive horn 1 to realize to be synchronized with the movement, reach the purpose that horn 1 is folded or opened.Because the motion of horn 1 is rotates, carrying out Each horn 1 can be turned in the region of bottom plate 6 completely during folding, and so all horns 1 will not be exposed, optimal to ensure Portability.
In the present embodiment, several leads 4 are provided with center ring 5(This example is 2), lead 4 include thrust Axle and central shaft, center ring 5 are clamped by several thrust shafts of periphery, center ring 5 is merely able to the free degree of parallel rotation.
In the present embodiment, center ring 5 is the gear structure of an endless tooth, and gear transmission part 3 is to be engaged with center ring 5 Travelling gear.Travelling gear is two in this example, and the week side of boss of center ring 5 is installed in symmetry shape, it is possible to which selection is installed In on bottom plate 6.During action, two travelling gears are synchronized with the movement, can with reference to travelling gear because motor accurately controls rotational angle With the advantage being accurately driven, the accurately lower opening folding and unfolding of control of horn 1 is realized.In addition after horn 1 is opened, it is possible to use motor It is locked, it is ensured that horn 1 open after can stablize use.
In the present embodiment, similar square bottom plate 6 has been used, and has employed four horns 1, so each horn 1 is uniform Put on the angle of square floor 6, the length of a horn 1 can be accommodated at each edge of the outer peripheral edge of square floor 6.So, It ensure that overall volume is small as far as possible.Similarly understand, bottom plate 6 can use triangle, pentagon or other polygons, To adapt to the needs of horn 1 of varying number, this also should be within the scope of the present invention.
It the above is only the preferred embodiment of the present invention, protection scope of the present invention is not limited merely to above-described embodiment, All technical schemes belonged under thinking of the present invention belong to protection scope of the present invention.It should be pointed out that for the art For those of ordinary skill, some improvements and modifications without departing from the principles of the present invention should be regarded as the protection of the present invention Scope.

Claims (7)

1. a kind of propeller folding device for unmanned plane, it is characterised in that including bottom plate(6), the horn of more than three (1), center ring(5), driving part and gear transmission part(3), the horn of more than three(1)Circumferentially successively It is arranged in bottom plate(6)On, the horn(1)One end bottom plate is articulated with by axle(6)Go up and can be rotated around pin joint, the machine Arm(1)The other end be used for unmanned plane propeller component is installed;The center ring(5)Positioned at bottom plate(6)Middle part, the gear Drive disk assembly(3)It is installed on center ring(5)The week side of boss, the center ring(5)On be provided with for gear transmission part(3)Match somebody with somebody The driving cog of conjunction, each horn(1)With center ring(5)Between be provided with connecting rod(2), the driving part passed by gear Dynamic component(3)Make center ring(5)Rotated with by connecting rod(2)Push horn(1)Rotate and complete to open or folding.
2. the propeller folding device according to claim 1 for unmanned plane, it is characterised in that the connecting rod(2)'s One end is articulated with horn(1)On, the connecting rod(2)The other end be articulated with center ring(5)On.
3. the propeller folding device according to claim 1 for unmanned plane, it is characterised in that the center ring(5) Place is provided with several leads(4), the lead(4)Make the center ring(5)It is merely able to the free degree of parallel rotation.
4. the propeller folding device for unmanned plane according to claim 1 or 2 or 3, it is characterised in that the center Ring(5)For the gear structure of an endless tooth, the gear transmission part(3)For with center ring(5)The travelling gear of engagement.
5. the propeller folding device according to claim 4 for unmanned plane, it is characterised in that the travelling gear is Two, center ring is installed in symmetry shape(5)The week side of boss.
6. the propeller folding device for unmanned plane according to claim 1 or 2 or 3, it is characterised in that at the bottom Plate(6)Upper center ring(5)With bottom plate(6)Region between outward flange, which is provided with, can accommodate all horns(1)Space.
7. the propeller folding device according to claim 6 for unmanned plane, it is characterised in that the bottom plate(6)'s It is shaped as being equipped with one horn of receiving at polygon, each edge(1)Space.
CN201510550561.3A 2015-09-01 2015-09-01 Propeller folding device for unmanned plane Active CN105035305B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510550561.3A CN105035305B (en) 2015-09-01 2015-09-01 Propeller folding device for unmanned plane

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Application Number Priority Date Filing Date Title
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CN105035305B true CN105035305B (en) 2017-09-15

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Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106114815B (en) * 2016-07-27 2024-02-27 上海未来伙伴机器人有限公司 Graded-adjustable aircraft horn and aircraft
CN106585971B (en) * 2016-12-31 2023-07-21 歌尔科技有限公司 Portable telescopic unmanned aerial vehicle
CN106828903B (en) * 2017-03-01 2020-06-09 曾雄文 Supporting structure and unmanned aerial vehicle

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Publication number Priority date Publication date Assignee Title
US7153100B2 (en) * 2004-12-23 2006-12-26 Fanimation, Inc. Ceiling fan with retractable fan blades
CN103625641B (en) * 2013-11-18 2016-01-20 北京中科飞鸿科技有限公司 Laterally folded formula quadrotor
MY170120A (en) * 2014-05-19 2019-07-05 Honn Shing Entpr Co Ltd Actuating device for stretching out fan blades of mechanical fan
CN104401484A (en) * 2014-10-16 2015-03-11 北京理工大学 Six-rotor aircraft rack capable of being folded and expanded automatically
CN205010478U (en) * 2015-09-01 2016-02-03 湖南云顶智能科技有限公司 A screw folding device for unmanned aerial vehicle

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