CN106828866A - A kind of unmanned plane - Google Patents
A kind of unmanned plane Download PDFInfo
- Publication number
- CN106828866A CN106828866A CN201611226966.2A CN201611226966A CN106828866A CN 106828866 A CN106828866 A CN 106828866A CN 201611226966 A CN201611226966 A CN 201611226966A CN 106828866 A CN106828866 A CN 106828866A
- Authority
- CN
- China
- Prior art keywords
- main body
- fuselage main
- rotor support
- rotor
- unmanned plane
- Prior art date
- 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
- B64C1/063—Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Catching Or Destruction (AREA)
Abstract
The invention discloses a kind of unmanned plane, including fuselage main body, some slide rails are provided with fuselage main body, some rotor supports are connected with by slide rail, rotor is provided with rotor support, rotor support can reciprocatingly slide along slide rail, be extend out to outside fuselage main body together with rotor thereon, or in storage to fuselage main body.By the present invention in that connecting unmanned plane rotor support with slide rail so that after flight terminates, rotor bracket slide can be received into fuselage main body, so as to reduce unmanned plane volume, beneficial to the storage and carrying of unmanned plane.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly to a kind of unmanned plane for being easy to receive.
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, such as military surveillance, movie and television play shooting, public affairs
The scenes such as peace, fire-fighting, agricultural plant protection, power-line patrolling and aerial delivery, and development along with unmanned air vehicle technique and perfect, it is existing
Unmanned plane cost have obvious reduction, price is more human-oriented, and operation difficulty is also more and more lower, practicality enhancing, thus
Receive more and more extensive favor so that the utilization field of unmanned plane is popularized for ordinary consumer gradually from specialty shooting.
Portable volume is the principal element of the acceptant unmanned plane of consumer, and the usual volume of existing unmanned plane
Larger not easily contained carrying, accordingly, it would be desirable to design a kind of portable unmanned plane storage mode, puts forth effort on to reduce the body of unmanned plane
Product.
The content of the invention
In view of prior art unmanned plane volume increases the problem of inconvenience storage, it is proposed that a kind of unmanned plane of the invention, with
Just overcome above mentioned problem or solve the above problems at least in part.
To achieve these goals, present invention employs following technical scheme：
A kind of unmanned plane, including fuselage main body, are provided with some slide rails in the fuselage main body, connected by the slide rail
Some rotor supports are connected to, rotor is provided with the rotor support, the rotor support can reciprocatingly slide along the slide rail, even
It is extend out to outside the fuselage main body with rotor thereon, or in storage to the fuselage main body.
Alternatively, the rotor support includes two travelling arms be arrangeding in parallel, described in every travelling arm and one
Slide rail is slidably connected, and is connected with fixed arm between two travelling arms, the fixed arm respectively with the travelling arm towards institute
State the one end on the outside of fuselage main body to be connected, the rotor is provided with the fixed arm.
Alternatively, slide rail in the fuselage main body is parallel to be alternately arranged on same level position, connects the slide rail
The rotor support for connecing is located at same level position, and the rotor support that the fuselage main body both sides are oppositely arranged is received to the machine
When in body main body, travelling arm thereon is staggered along the slide rail respectively.
Alternatively, in the rotor support that the fuselage main body both sides are oppositely arranged, the fixed arm of the rotor support is set
For one is long and the other is short, the rotor support is set to receive during to the fuselage main body, one of rotor support can be enclosed within another
Outside rotor support.
Alternatively, the rotor support is the round rectangle of openings at one side, and its one group of relative opposite side is the travelling arm,
The corresponding one side of its open side is fixed arm, and two rotors are provided with the fixed arm, and the fuselage main body both sides are relative to be set
In the rotor support put, the relatively described fuselage main body of rotor on the fixed arm is symmetrical arranged.
Alternatively, the rotor includes two panels blade, and the two panels blade can be rotated against, two panels blade when using
To offside distribution, the two panels blade is rotated to homonymy distribution during storage for rotation.
Alternatively, the slide rail for being set in the fuselage main body is enclosed slide rail.
Alternatively, release button is provided with the fuselage main body, is set between the rotor support and the fuselage main body
Elastomeric element is equipped with, the rotor support is received during to the fuselage main body, the release button and the rotor bracket clamp
Connect, press the release button, the release button departs from clamping with the rotor support, and the rotor support is in the elasticity
Outside lower ejection to the fuselage main body of part effect.
Alternatively, projection is provided with the release button, draw-in groove, the rotor support is provided with the rotor support
When in storage to the fuselage main body, the raised draw-in groove for snapping in the rotor support positioned at the fuselage main body both sides simultaneously
In, make rotor support clamping of the release button simultaneously with the fuselage main body both sides, the release button is pressed, it is described to release
Put button and depart from clamping with the rotor support of the fuselage main body both sides simultaneously.
Alternatively, the release button is also equipped with elastomeric element, and in the presence of the elastomeric element, the release is pressed
Button and the rotor support clamping, press the release button, and the elastomeric element is deformed upon, the release button with it is described
Rotor support departs from clamping.
The beneficial effects of the invention are as follows：
Unmanned plane rotor support is connected by using slide rail so that after flight terminates, rotor bracket slide can be received
Receive in fuselage main body, so as to reduce unmanned plane volume, beneficial to the storage and carrying of unmanned plane.
Brief description of the drawings
Fig. 1 is deployed into the signal outside fuselage main body for a kind of unmanned plane rotor support that one embodiment of the invention is provided
Figure；
A kind of schematic diagram of unmanned plane rotor blade rotation receiving state that Fig. 2 is provided for one embodiment of the invention；
Fig. 3 receives the signal to fuselage main body for a kind of unmanned plane rotor support that one embodiment of the invention is provided
Figure；
A kind of unmanned plane side schematic view that Fig. 4 is provided for one embodiment of the invention；
Line A-A profile in Fig. 4 when Fig. 5 is unmanned plane rotor support of the present invention expansion；
Line A-A profile in Fig. 4 when Fig. 6 is unmanned plane rotor support of the present invention storage；
A kind of unmanned plane release button schematic diagram that Fig. 7 is provided for one embodiment of the invention；
Signal during a kind of unmanned plane rotor release button clamping rotor support that Fig. 8 is provided for one embodiment of the invention
Figure；
Signal during a kind of unmanned plane rotor release button release rotor support that Fig. 9 is provided for one embodiment of the invention
Figure；
In figure, 1, fuselage main body；2nd, rotor；3rd, rotor support；31st, travelling arm；32nd, fixed arm；4th, slide rail；5th, release is pressed
Button；6th, spring.
Specific embodiment
Core concept of the invention is：Rotor bracket slide is connected to the fuselage main body of unmanned plane by using slide rail
On, after unmanned plane has performed aerial mission, slide rotor support and be accommodated into fuselage main body, so as to realize reducing nothing
Man-machine volume, the storage beneficial to unmanned plane is carried.
To make the object, technical solutions and advantages of the present invention clearer, below in conjunction with accompanying drawing to embodiment party of the present invention
Formula is described in further detail.
Fig. 1-Fig. 9 shows one embodiment of unmanned plane of the invention, as shown in Fig. 1-Fig. 9, a kind of unmanned plane, including
Some slide rails 4 are provided with fuselage main body 1, fuselage main body 1, some rotor supports 3, rotor support 3 are connected with by slide rail 4
On be provided with rotor 2.In the present embodiment, four slide rails 4 are had in fuselage main body 1, the two of the both sides of fuselage main body 1 is corresponded to respectively
Individual rotor support 3 (referring to shown in Fig. 5 and 6), rotor support 3 can reciprocatingly slide along slide rail 4, be extend out to together with rotor 2 thereon
Outside fuselage main body 1, or in storage to fuselage main body 1, it stretches out deployed condition as shown in figure 1, its receiving state is as shown in Figure 3.
Rotor support 3 is slided in storage to fuselage main body 1 by slide rail 4, realizes efficient and convenient storage, and effectively subtract
The small volume of unmanned plane, the storage beneficial to unmanned plane is carried.
Preferably, as shown in Fig. 1,5 and 6, rotor support 3 includes two travelling arms 31 be arrangeding in parallel, every travelling arm
31 are slidably connected with a slide rail 4, are connected with fixed arm 32 between two travelling arms 31, fixed arm 32 respectively with the court of travelling arm 31
One end to the outside of fuselage main body 1 is connected, and rotor 2 is provided with fixed arm 32, and two travelling arms 31 are connected by fixed arm 32
It is connected together, two rotors 2 for being located at homonymy can be made to be fixed together, synchronous slide stretches out and receives, is conducive to simplification to make
Stability during with operation and maintenance unmanned plane during flying.
Preferably, with reference to Fig. 4-6, slide rail 4 in fuselage main body 1 is parallel to be alternately arranged on same level position, makes cunning
The rotor support 3 of the connection of rail 4 is located at same level position, and the rotor support 3 that the both sides of fuselage main body 1 are oppositely arranged is received to machine
When in body main body 1, travelling arm 31 thereon is staggered along slide rail 4 respectively, by the parallel slide rail 4, Ke Yi being staggered
Same level position, the rotor support 3 of both sides is overlapped simultaneously and is accommodated in fuselage main body 1, can effective utilization space, design
Go out width and the close rotor support 3 of fuselage main body 1, so that providing enough distances installs rotor 2.
It is highly preferred that in the rotor support 3 that is oppositely arranged of the both sides of fuselage main body 1, the fixed arm 32 of rotor support 3 is set to
One is long and the other is short, rotor support 3 is received during to fuselage main body 1, and one of rotor support 3 can be enclosed within another rotor support
Outside 3, rotor 2 is symmetrical arranged beneficial in the both sides of fuselage main body 1, wherein, rotor support 3 can be fine using quality small intensity carbon high
Dimension makes.
Preferably, rotor support 3 is the round rectangle of openings at one side, i.e., overall is in " Qian " font, and both sides fillet is conducive to
Play a protective role, prevent accident occur during flight, cause to thrust into and hurt sb.'s feelings, its one group of relative opposite side is travelling arm 31, and it is opened
The corresponding one side in mouth side is fixed arm 32, and two rotors 2, the rotation that the both sides of fuselage main body 1 are oppositely arranged are provided with fixed arm 32
In wing support 3, the rotor 2 on fixed arm 32 is symmetrical arranged with respect to fuselage main body 1, and in the present embodiment, rotor support 3 is integrated
The structure of shaping, overall structure more stable and stronger.
Preferably, rotor 2 includes two panels blade, and two panels blade can be rotated against, and two panels blade is rotated to offside when using
Distribution, as shown in figure 1, storage when two panels blade rotate to homonymy distribution, convenient for collecting, as shown in Figure 2.
Preferably, the slide rail 4 for being set in fuselage main body 1 is enclosed slide rail 4, and such as T-shaped slide rail can prevent rotor support
3 from interior disengaging.
Preferably, release button 5 is provided with fuselage main body 1, as shown in fig. 7, between rotor support 3 and fuselage main body 1
Elastomeric element is provided with, in the present embodiment, the elastomeric element is spring 6, and rotor support 3 is received during to fuselage main body 1, released
Button 5 and the clamping of rotor support 3 are put, release button 5 is pressed, release button 5 departs from clamping with rotor support 3, and rotor support 3 exists
Outside lower ejection to the fuselage main body 1 of elastomeric element effect, so as to realize the automatic spring of rotor support 3, grasp the expansion of unmanned plane
Make more quick and convenient.
Fig. 8-Fig. 9 schematically shows the release principle of release button 5 in the present embodiment, wherein, set in release button 5
Projection is equipped with, draw-in groove is provided with rotor support 3, rotor support 3 is received during to fuselage main body 1, raised snapping in simultaneously is located at
In the draw-in groove of the rotor support 3 of the both sides of fuselage main body 1, make release button 5 while blocking with the rotor support 3 of the both sides of fuselage main body 1
Connect, press release button 5, release button 5 departs from clamping with the rotor support 3 of the both sides of fuselage main body 1 simultaneously, so as to complete simultaneously
The expansion of the rotor support 3 of both sides.
Preferably, release button 5 is also equipped with elastomeric element, in the presence of elastomeric element, release button 5 and rotor branch
The clamping of frame 3, presses release button 5, and elastomeric element is deformed upon, and release button 5 departs from clamping with rotor support 3, for example, release
Button 5 divides into spring, and the projection in release button 5 is horizontally disposed with, and is extended laterally in fuselage main body 1 and is connected to rotor support 3
Draw-in groove in, pressing release button 5 when, spring-compressed, make release button 5 projection from draw-in groove deviate from, while discharge both sides
Rotor support 3.
The above, specific embodiment only of the invention, under above-mentioned teaching of the invention, those skilled in the art
Other improvement or deformation can be carried out on the basis of above-described embodiment.It will be understood by those skilled in the art that above-mentioned tool
The purpose of the present invention is simply preferably explained in body description, and protection scope of the present invention should be defined by scope of the claims.
Claims (10)
1. a kind of unmanned plane, including fuselage main body, it is characterised in that some slide rails are provided with the fuselage main body, are passed through
The slide rail is connected with some rotor supports, and rotor is provided with the rotor support, and the rotor support can be along the slide rail
Reciprocatingly slide, extend out to outside the fuselage main body together with rotor thereon, or in storage to the fuselage main body.
2. unmanned plane as claimed in claim 1, it is characterised in that the rotor support includes two slips be arrangeding in parallel
Arm, every travelling arm is slidably connected with a slide rail, and fixed arm is connected between two travelling arms, described solid
Determine arm to be connected towards the one end on the outside of the fuselage main body with the travelling arm respectively, the rotation is provided with the fixed arm
The wing.
3. unmanned plane as claimed in claim 2, it is characterised in that slide rail in the fuselage main body is parallel to be alternately arranged on
Same level position, makes the rotor support of the slide rail connection be located at same level position, and the fuselage main body both sides are relative
The rotor support of setting is received during to the fuselage main body, and travelling arm thereon is staggered along the slide rail respectively.
4. unmanned plane as claimed in claim 3, it is characterised in that the rotor support that the fuselage main body both sides are oppositely arranged
In, the fixed arm of the rotor support is set to that one is long and the other is short, the rotor support is received during to the fuselage main body, its
In a rotor support can be enclosed within outside another rotor support.
5. unmanned plane as claimed in claim 2, it is characterised in that the rotor support is the round rectangle of openings at one side, its
One group of relative opposite side is the travelling arm, and the corresponding one side of its open side is fixed arm, and two are provided with the fixed arm
Rotor, in the rotor support that the fuselage main body both sides are oppositely arranged, the relatively described fuselage main body of rotor on the fixed arm
It is symmetrical arranged.
6. unmanned plane as claimed in claim 1, it is characterised in that the rotor includes two panels blade, and the two panels blade can
Rotate against, the two panels blade is rotated to offside distribution when using, the two panels blade is rotated to homonymy distribution during storage.
7. unmanned plane as claimed in claim 1, it is characterised in that the slide rail set in the fuselage main body is enclosed slide rail.
8. unmanned plane as claimed in claim 1, it is characterised in that release button, the rotation are provided with the fuselage main body
Elastomeric element is provided between wing support and the fuselage main body, the rotor support is received during to the fuselage main body, institute
Release button and the rotor support clamping are stated, the release button is pressed, the release button departs from the rotor support
Clamping, the rotor support is ejected to outside the fuselage main body under elastomeric element effect.
9. unmanned plane as claimed in claim 8, it is characterised in that projection, the rotor branch are provided with the release button
Draw-in groove is provided with frame, the rotor support is received during to the fuselage main body, it is described raised while snapping in positioned at the machine
In the draw-in groove of the rotor support of body main body both sides, make rotor bracket clamp of the release button simultaneously with the fuselage main body both sides
Connect, press the release button, the release button departs from clamping with the rotor support of the fuselage main body both sides simultaneously.
10. unmanned plane as claimed in claim 8, it is characterised in that the release button is also equipped with elastomeric element, described
In the presence of elastomeric element, the release button and the rotor support clamping press the release button, the elastomeric element
Deform upon, the release button departs from clamping with the rotor support.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611226966.2A CN106828866A (en) | 2016-12-27 | 2016-12-27 | A kind of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611226966.2A CN106828866A (en) | 2016-12-27 | 2016-12-27 | A kind of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106828866A true CN106828866A (en) | 2017-06-13 |
Family
ID=59136650
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611226966.2A Pending CN106828866A (en) | 2016-12-27 | 2016-12-27 | A kind of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106828866A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112793761A (en) * | 2017-08-29 | 2021-05-14 | 深圳市大疆创新科技有限公司 | Frame and unmanned aerial vehicle |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204998767U (en) * | 2015-08-24 | 2016-01-27 | 深圳市诺亚星辰科技开发有限公司 | Double -deck rotor unmanned aerial vehicle of modified |
| CN205707325U (en) * | 2016-04-26 | 2016-11-23 | 普宙飞行器科技（深圳）有限公司 | Telescopic blade driving means and unmanned plane |
| CN106184729A (en) * | 2016-07-18 | 2016-12-07 | 山东龙翼航空科技有限公司 | A kind of many rotor wing unmanned aerial vehicles |
| CN206456543U (en) * | 2016-12-27 | 2017-09-01 | 歌尔科技有限公司 | A kind of unmanned plane |
-
2016
- 2016-12-27 CN CN201611226966.2A patent/CN106828866A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204998767U (en) * | 2015-08-24 | 2016-01-27 | 深圳市诺亚星辰科技开发有限公司 | Double -deck rotor unmanned aerial vehicle of modified |
| CN205707325U (en) * | 2016-04-26 | 2016-11-23 | 普宙飞行器科技（深圳）有限公司 | Telescopic blade driving means and unmanned plane |
| CN106184729A (en) * | 2016-07-18 | 2016-12-07 | 山东龙翼航空科技有限公司 | A kind of many rotor wing unmanned aerial vehicles |
| CN206456543U (en) * | 2016-12-27 | 2017-09-01 | 歌尔科技有限公司 | A kind of unmanned plane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112793761A (en) * | 2017-08-29 | 2021-05-14 | 深圳市大疆创新科技有限公司 | Frame and unmanned aerial vehicle |
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