CN206456562U - A kind of unmanned plane - Google Patents

A kind of unmanned plane Download PDF

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Publication number
CN206456562U
CN206456562U CN201621423972.2U CN201621423972U CN206456562U CN 206456562 U CN206456562 U CN 206456562U CN 201621423972 U CN201621423972 U CN 201621423972U CN 206456562 U CN206456562 U CN 206456562U
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CN
China
Prior art keywords
rotor
main body
unmanned plane
fuselage main
magnet
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Withdrawn - After Issue
Application number
CN201621423972.2U
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Chinese (zh)
Inventor
何健豪
陳之信
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.)
Goertek Techology Co Ltd
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Goertek Techology Co Ltd
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Publication date
Application filed by Goertek Techology Co Ltd filed Critical Goertek Techology Co Ltd
Priority to CN201621423972.2U priority Critical patent/CN206456562U/en
Application granted granted Critical
Publication of CN206456562U publication Critical patent/CN206456562U/en
Withdrawn - After Issue legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of unmanned plane, including fuselage main body, fuselage main body side is connected with rotor support, and rotor support is to be provided with rotor on folding linkage structure, rotor support;In use, rotor support-folding, deploys rotor, aerial mission is performed, during storage, rotor support stretches to form rhabodoid, draws rotor in, is accommodated in rhabodoid.Folding linkage structure rotor support is connected in fuselage main body side, in use, passing through folding rotor support, deploy the rotor on rotor support, aerial mission is performed, during storage, rotor support is stretched, it is morphed into rhabodoid, rotor thereon is drawn in, and is accommodated in rhabodoid, it is achieved thereby that by way of folding and stretching, reduce unmanned plane volume, make unmanned plane be easy to store the effect carried.

Description

A kind of unmanned plane
Technical field
The utility model is related to unmanned air vehicle technique field, more particularly to it is a kind of can stretcher strain, be easy to store nobody Machine.
Background technology
Unmanned plane is that one kind need not carry people to fly, and by the aircraft of controlled in wireless, is initially born in military use.OK Industry level UAS is unmanned flight's system of a kind of many carries, many application scenarios, has application in many industries at present, such as The scenes such as military surveillance, movie and television play shooting, public security, fire-fighting, agricultural plant protection, power-line patrolling and aerial delivery, because its purposes is wide It is general, distinct characteristics, thus obtained the positive research and development of every profession and trade.
And development along with unmanned air vehicle technique and perfect, existing unmanned plane cost has obvious reduction, and price is more It is human-oriented, and operation difficulty is also more and more lower, practicality enhancing, thus more and more extensive favor is received, more and more General public starts to buy and use unmanned plane, perform flight, take photo by plane, the recreation such as net cast, in choosing for unmanned plane During use, portable volume is the acceptable principal element of consumer.
However, common unmanned plane needs to rely on rotor flying at present, and the rotor deployed can cause unmanned plane volume compared with Greatly, it is not easy to store, is not suitable for carrying for a long time.
Utility model content
In view of the problem of larger inconvenience of prior art volume is stored and carried, it is proposed that it is of the present utility model it is a kind of nobody Machine, to overcome above mentioned problem or to solve the above problems at least in part.
To achieve these goals, the utility model employs following technical scheme:
A kind of unmanned plane, including fuselage main body, the fuselage main body side are connected with rotor support, and the rotor support is Rotor is provided with folding linkage structure, the rotor support;In use, the rotor support-folding, makes the rotor Expansion, performs aerial mission, during storage, the rotor support stretches to form rhabodoid, draws the rotor in, is accommodated in described In rhabodoid.
Alternatively, the rotor support includes being provided with a rotor on four bracket legs, every bracket legs, described Bracket legs are circumferentially uniformly distributed along the fuselage main body side, and its one end is connected in the fuselage main body, other end connection In same top fixed seat, during storage, four bracket legs are stretched, and surround a receiving space, the rotor is stored In the receiving space.
Alternatively, the bracket legs are disposed with rotor canned paragraph, vertical shield segment and horizontal protective section, the rotation Connected between wing canned paragraph, vertical shield segment and horizontal protective section by axis of rotation, the rotor canned paragraph and the fuselage Connected between main body and between horizontal protective section and the top fixed seat also by axis of rotation, the rotor is set On the inside of the rotor canned paragraph, in use, the vertical shield segment and horizontal protective section respectively from vertical direction with level side To around the rotor.
Alternatively, it is provided with the top fixed seat in top magnet, the fuselage main body and is correspondingly arranged on bottom magnet, is made Used time, the top magnet and the bottom magnet attract each other, by the top fixed seat together with fuselage main body attraction, Lock the collapsed shape of the rotor support.
Alternatively, the top magnet is arranged on the downside of the top fixed seat, during storage, the four walls difference of the top magnet Fitted with a part for the horizontal protective section of four bracket legs, be supported on the horizontal protective section lower section.
Alternatively, the interface arrangment of mutual cooperation is provided with the top fixed seat and the fuselage main body, in use, The top fixed seat and the fuselage main body are connected together by the interface arrangment, lock the folding of the rotor support Shape.
Alternatively, in the bracket legs, the magnetic attracted each other is provided with least one pair of bracket legs being oppositely arranged Iron, during storage, the bracket legs attract together, to lock the rotor support stretching shape by the magnetic effect of the magnet Into shaft-like shape.
Alternatively, the magnet on the bracket legs is arranged on the vertical shield segment of the bracket legs.
Alternatively, vertical shield segment described in the thickness ratio of the rotor canned paragraph and the thickness of horizontal protective section are big.
Alternatively, the fuselage main body cross section and the top fixed seat cross section be it is of the same size square, it is described The two ends of bracket legs are connected on the fuselage main body side corresponding with the top fixed seat.
The beneficial effects of the utility model are:
Folding linkage structure rotor support is connected in fuselage main body side, in use, by folding rotor support, making Rotor expansion on rotor support, performs aerial mission, during storage, stretches rotor support, is morphed into rhabodoid, will thereon Rotor draw in, and be accommodated in rhabodoid, it is achieved thereby that fold and stretching by way of, reduce unmanned plane volume, make Unmanned plane is easy to store the effect carried.
Brief description of the drawings
A kind of rotor support-folding use state signal for unmanned plane that Fig. 1 provides for the utility model one embodiment Figure;
State when a kind of rotor support for unmanned plane that Fig. 2 provides for the utility model one embodiment starts stretching is shown It is intended to;
A kind of rotor support for unmanned plane that Fig. 3 provides for the utility model one embodiment is in semi-folded semi-drawing shape State schematic diagram;
A kind of rotor support stretching receiving state signal for unmanned plane that Fig. 4 provides for the utility model one embodiment Figure;
In figure:1. fuselage main body;2. rotor canned paragraph;3. vertical shield segment;4. horizontal protective section;5. top fixed seat; 6. magnet;7. bottom magnet;8. push up magnet;9. rotor.
Embodiment
Core concept of the present utility model is:By connecting folding linkage structure rotor branch in fuselage main body side Frame, in use, folding rotor support, deploys the rotor on rotor support, performs aerial mission, during storage, stretches rotor branch Frame, is morphed into rhabodoid, and rotor thereon is drawn in, and is accommodated in rhabodoid, so as to reduce unmanned plane volume, reaches It is easy to store the effect carried.
It is new to this practicality below in conjunction with accompanying drawing to make the purpose of this utility model, technical scheme and advantage clearer Type embodiment is described in further detail.
Fig. 1-4 shows one embodiment of the utility model unmanned plane, as Figure 1-4, a kind of unmanned plane, including machine Body main body 1, the side of fuselage main body 1 is connected with rotor support, and rotor support is to be set on folding linkage structure, rotor support There is rotor 9;In use, rotor support-folding, deploys rotor 9, aerial mission is performed, as shown in figure 1, when storing, rotor branch Frame stretches to form rhabodoid, draws rotor 9 in, is accommodated in rhabodoid, as shown in Figure 4.
Preferably, rotor support includes being provided with a rotor 9 on four bracket legs, every bracket legs, support point Branch is circumferentially uniformly distributed along the side of fuselage main body 1, and its one end is connected in fuselage main body 1, and the other end is connected to same top and consolidated In reservation 5, during storage, four bracket legs are stretched, and surround a receiving space, and rotor 9 is accommodated in receiving space, specific to receive The process of receiving refers to Fig. 1-Fig. 4, pulls up top fixed seat 5, stretches four bracket legs, and final draw in merges, surround as Shaft-like shown in Fig. 4, four rotors 9 are accommodated in the shaft-like space.
Preferably, bracket legs are disposed with rotor canned paragraph 2, vertical shield segment 3 and horizontal protective section 4, specific ginseng Examine shown in Fig. 3, connected between rotor canned paragraph 2, vertical shield segment 3 and horizontal protective section 4 by axis of rotation, so as to side Just mutually rotate, rotor support is bent tensile deformation, between rotor canned paragraph 2 and fuselage main body 1 and level is anti- Connected between shield section 4 and top fixed seat 5 also by axis of rotation, rotor 9 is arranged on the inner side of rotor canned paragraph 2, in use, perpendicular Straight shield segment 3 and horizontal protective section 4 surrounds rotor 9 with horizontal direction from vertical direction respectively, from both vertically as well as horizontally constituting The protective cover of rotor 9.
Preferably due to rotor 9 will be fixedly mounted in rotor canned paragraph 2, thus during design, the thickness ratio of rotor canned paragraph 2 The thickness of vertical shield segment 3 and horizontal protective section 4 is big, to improve its intensity, increase rotor 9 and its downside motor and wire rod etc. portion The installing space of part.
Preferably, it is provided with top fixed seat 5 in top magnet 8, fuselage main body 1 and is correspondingly arranged on bottom magnet 7, is used When, top magnet 8 and bottom magnet 7 attract each other, top fixed seat 5 is attracted with fuselage main body 1 together with, locking rotor support Collapsed shape, as shown in figure 1, using the lock mode that magnet 8 and bottom magnet 7 attract each other is pushed up, it is simple to operate, it is easy to use.
It is highly preferred that top magnet 8 is arranged on the top downside of fixed seat 5, during storage, push up four walls of magnet 8 respectively with four The part laminating of the horizontal protective section 4 of bracket legs, is supported on the lower section of horizontal protective section 4, with reference to Fig. 3 and Fig. 4, pushes up magnet 8 Size it is consistent with the receiving space that bracket legs are surrounded, during storage, the top of top magnet 8 and horizontal protective section 4 have one section away from From laminating, being capable of the shaft-like receiving space that surrounds of Auxiliary support bracket legs, it is to avoid horizontal protective section 4 is squeezed, and is caused Shaft-like receiving space deformation, damages unmanned plane structure.
Preferably, the interface arrangment of mutual cooperation is provided with top fixed seat 5 and fuselage main body 1, in use, top is solid Reservation 5 and fuselage main body 1 are connected together by interface arrangment, lock the collapsed shape of rotor support, the fixation of interface arrangment Connection is more firm, specifically, can be realized using common interface arrangments such as the buckles and hole clipping cooperated, herein no longer Repeat.Certainly, interface arrangment and above-mentioned attraction structure can be used between top fixed seat 5 and fuselage main body 1 simultaneously, Gu When determining attended operation, the attraction of magnet can help interface arrangment to realize pre-determined bit, and attended operation can so more facilitated, The fastness of fixation can be improved again.
Preferably, in the various embodiments described above, it is provided with the bracket legs that at least one pair of in bracket legs is oppositely arranged The magnet 6 attracted each other, during storage, bracket legs are attracted together by the magnetic effect of magnet 6, the support stretching of locking rotor The shaft-like shape formed.
Preferably, with reference to Fig. 3 and Fig. 4, the magnet 6 on bracket legs is arranged on the vertical shield segment 3 of bracket legs, is led to The magnet 6 for crossing the opposed setting of vertical shield segment 3 is attracted each other, and rotor support is locked in into the shaft-like shape that stretching is formed, Meanwhile, attract magnet 6 together also can be as internal support, to provide filling support in the middle part of shaft-like receiving space, it is to avoid Rotor support is squeezed the structures such as the rotor 9 inside deformation, damage.
Preferably, the cross section of fuselage main body 1 and the cross section of top fixed seat 5 are of the same size square, support point The two ends of branch are connected in fuselage main body 1 and the corresponding side of top fixed seat 5, so that after stretching, rotor branch The staff-like shape of frame is consistent with the shape of fuselage main body 1 so that unmanned plane good appearance and be easy to store.
With reference to Fig. 1-4, the embodiment operating principle of the utility model unmanned plane is briefly explained:
Storage process as Fig. 1-4 successively shown in, wherein, Fig. 1 be rotor support-folding use state schematic diagram, in this state Under, top fixed seat 5 is pulled up, the top magnet 8 in the fixed seat 5 of top is separated with the bottom magnet 7 in fuselage main body 1, such as Shown in Fig. 2, under linkage effect, top fixed seat 5 gradually drives four bracket legs to stretch gathering merging, finally surrounds Fig. 4 Shown rod-like structure, completes to store, now, the magnet 6 for being arranged on vertical shield segment 3 attracts each other, it is fixed stretch back wall into Rod-like structure.
, will be wherein one to the vertical side draw of shield segment 3 of two panels so that attract magnet 6 together on the contrary, during expansion Separation, under linkage effect, each vertical shield segment 3 drives the rotor canned paragraph 2 that it is linked and horizontal protective section 4 together outward Stretching, while top fixed seat 5 is moved down, top fixed seat 5 moves down into bottom, top magnet 8 thereon and the bottom of fuselage main body 1 Magnet 7 is adsorbed, and completes the expansion of rotor support, as shown in Figure 1.
In summary, the storage expansion of the utility model unmanned plane is convenient, is conducive to the convenient storage of unmanned plane to carry.
It is described above, embodiment only of the present utility model, under above-mentioned teaching of the present utility model, this area Technical staff can carry out other improvement or deformation on the basis of above-described embodiment.It will be understood by those skilled in the art that Above-mentioned specific descriptions are more preferable explanation the purpose of this utility model, and protection domain of the present utility model should be with claim Protection domain be defined.

Claims (10)

1. a kind of unmanned plane, it is characterised in that including fuselage main body, the fuselage main body side is connected with rotor support, described Rotor support is to be provided with rotor on folding linkage structure, the rotor support;In use, the rotor support-folding, Deploy the rotor, perform aerial mission, during storage, the rotor support stretches to form rhabodoid, draw the rotor in, It is accommodated in the rhabodoid.
2. unmanned plane as claimed in claim 1, it is characterised in that the rotor support includes four bracket legs, every branch A rotor is provided with frame branch, the bracket legs are circumferentially uniformly distributed along the fuselage main body side, its one end connection In the fuselage main body, the other end is connected in same top fixed seat, during storage, and four bracket legs are stretched, and are enclosed Into a receiving space, the rotor is accommodated in the receiving space.
3. unmanned plane as claimed in claim 2, it is characterised in that the bracket legs are disposed with rotor canned paragraph, erected Straight shield segment and horizontal protective section, is connected between the rotor canned paragraph, vertical shield segment and horizontal protective section by axis of rotation Connect, also lead between the rotor canned paragraph and the fuselage main body and between horizontal protective section and the top fixed seat Axis of rotation connection is crossed, the rotor is arranged on the inside of the rotor canned paragraph, in use, the vertical shield segment and level are anti- Protect section and surround the rotor with horizontal direction from vertical direction respectively.
4. unmanned plane as claimed in claim 3, it is characterised in that top magnet, the machine are provided with the top fixed seat Bottom magnet is correspondingly arranged in body main body, in use, the top magnet and the bottom magnet attract each other, the top is fixed Together with seat attracts with the fuselage main body, the collapsed shape of the rotor support is locked.
5. unmanned plane as claimed in claim 4, it is characterised in that the top magnet is arranged on the downside of the top fixed seat, During storage, four walls of the top magnet are fitted with a part of of horizontal protective section of four bracket legs respectively, are supported on The horizontal protective section lower section.
6. unmanned plane as claimed in claim 3, it is characterised in that be provided with the top fixed seat and the fuselage main body The interface arrangment of mutual cooperation, in use, the top fixed seat and the fuselage main body are connected to by the interface arrangment Together, the collapsed shape of the rotor support is locked.
7. unmanned plane as claimed in claim 3, it is characterised in that in the bracket legs, at least one pair of branch being oppositely arranged The magnet attracted each other is provided with frame branch, during storage, the bracket legs are attracted by the magnetic effect of the magnet Together, lock the rotor support and stretch the shaft-like shape to be formed.
8. unmanned plane as claimed in claim 7, it is characterised in that the magnet on the bracket legs is arranged on the support point The vertical shield segment of branch.
9. unmanned plane as claimed in claim 3, it is characterised in that vertical shield segment described in the thickness ratio of the rotor canned paragraph Thickness with horizontal protective section is big.
10. unmanned plane as claimed in claim 2, it is characterised in that the fuselage main body cross section and the top fixed seat Cross section is of the same size square, and the two ends of the bracket legs are connected to the fuselage main body and the top is fixed On the corresponding side of seat.
CN201621423972.2U 2016-12-23 2016-12-23 A kind of unmanned plane Withdrawn - After Issue CN206456562U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201621423972.2U CN206456562U (en) 2016-12-23 2016-12-23 A kind of unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201621423972.2U CN206456562U (en) 2016-12-23 2016-12-23 A kind of unmanned plane

Publications (1)

Publication Number Publication Date
CN206456562U true CN206456562U (en) 2017-09-01

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CN201621423972.2U Withdrawn - After Issue CN206456562U (en) 2016-12-23 2016-12-23 A kind of unmanned plane

Country Status (1)

Country Link
CN (1) CN206456562U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106741943A (en) * 2016-12-23 2017-05-31 歌尔科技有限公司 A kind of unmanned plane

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106741943A (en) * 2016-12-23 2017-05-31 歌尔科技有限公司 A kind of unmanned plane
CN106741943B (en) * 2016-12-23 2023-10-20 歌尔科技有限公司 Unmanned aerial vehicle

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