CN206318011U - Extension type unmanned plane - Google Patents
Extension type unmanned plane Download PDFInfo
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- CN206318011U CN206318011U CN201621321953.9U CN201621321953U CN206318011U CN 206318011 U CN206318011 U CN 206318011U CN 201621321953 U CN201621321953 U CN 201621321953U CN 206318011 U CN206318011 U CN 206318011U
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- Prior art keywords
- slide rail
- sliding track
- motor
- track mechanism
- main cabin
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- 238000003466 welding Methods 0.000 description 5
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- FGRBYDKOBBBPOI-UHFFFAOYSA-N 10,10-dioxo-2-[4-(N-phenylanilino)phenyl]thioxanthen-9-one Chemical compound O=C1c2ccccc2S(=O)(=O)c2ccc(cc12)-c1ccc(cc1)N(c1ccccc1)c1ccccc1 FGRBYDKOBBBPOI-UHFFFAOYSA-N 0.000 description 1
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Abstract
The utility model provides a kind of extension type unmanned plane, including main cabin, the left and right side in the main cabin is respectively arranged with shield, the first sliding track mechanism in each shield respectively by concertina type slidably connects motor paddle mechanism, each motor paddle mechanism is slidably connected by the second sliding track mechanism of concertina type with main cabin, the motor paddle mechanism is contained in when the first sliding track mechanism and the second sliding track mechanism are in contraction state in the space that shield is constituted with main cabin, and the main cabin is in two shields.The utility model extension type unmanned plane can realize the disposition for reducing volume and blade during unmanned plane inoperative to greatest extent, in order to store and transport and provide higher security.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, and in particular to a kind of extension type unmanned plane.
Background technology
Unmanned plane is the unmanned vehicle manipulated using radio robot and self-contained program's control device, at present
It is used in combination mostly with capture apparatus, applied to patrolling and take photo by plane.Existing unmanned air vehicle technique is constantly improving, using also more and more wider
It is general, but because its horn and blade need to stretch to individual direction, to cause it to take up space excessive, is not easy to store and transports.In order to solve
The problem, current solution is the volume reduced by folding under unmanned plane off working state, but so again can not be real
The omnibearing protection of existing blade, therefore there is potential safety hazard.
Utility model content
The purpose of this utility model is to provide a kind of extension type unmanned plane, and it can realize maximum during unmanned plane inoperative
The diminution volume and the disposition of blade of limit, in order to store and transport and provide higher security.
In order to solve the above-mentioned technical problem, the utility model provides a kind of extension type unmanned plane, including main cabin, institute
The left and right side for stating main cabin is respectively arranged with shield, each shield respectively by the first sliding track mechanism slip company of concertina type
Motor paddle mechanism is connected to, each motor paddle mechanism is slidably connected by the second sliding track mechanism of concertina type with main cabin, institute
State motor paddle mechanism and be contained in what shield was constituted with main cabin when the first sliding track mechanism and the second sliding track mechanism are in contraction state
In space, and the main volume of compartment is placed in two shields.
Preferably, first sliding track mechanism includes the first slide rail for being arranged at shroud interior side wall, the motor paddle
Position corresponding with the first sled position is provided with the second slide rail in mechanism, and second slide rail is slided on the first slide rail, institute
Stating between shield and motor paddle mechanism together be slidably connected with the second slide rail by the first slide rail.
Preferably, second sliding track mechanism includes second slide rail and corresponding with the second sled position is arranged at master
3rd slide rail of cabin side wall, second slide rail is slided on the 3rd slide rail, is led between the motor paddle mechanism and main cabin
Cross together with the second slide rail is slidably connected with the 3rd slide rail.
Preferably, the motor paddle mechanism includes two motor paddle components and two bases, two motor slurries
Leaf component is installed on two bases in front and rear portions.
Preferably, also including motor connection lever, two bases are arranged at the front and rear portions of motor connection lever.
Preferably, motor slide rail mechanism, the motor are also slidably connected between the main cabin and each motor paddle component
Sliding track mechanism includes the 4th slide rail being arranged on the motor paddle mechanism and the motor slide rail for being arranged at main cabin side wall, each institute
Stating between motor paddle mechanism and main cabin together be slidably connected with motor slide rail by the 4th slide rail.
Preferably, also including auxiliary sliding track mechanism, the auxiliary sliding track mechanism includes being arranged on front side of main cabin and/or rear side
The first auxiliary slide rail and be arranged on front side of shroud interior and/or rear side the second auxiliary slide rail, between the main cabin and shield
Aided in by the first auxiliary slide rail with second together with slide rail is slidably connected.
Preferably, first sliding track mechanism, the second sliding track mechanism are the channel-section steel structure or groove coupling that can be slided relatively
Structure or socket join structure.
Preferably, the motor slide rail mechanism and auxiliary sliding track mechanism are the groove coupling structure that can be slided relatively or socket
Structure.
Preferably, the shield has the guard of multiple mesh for surface layout, the shield towards the side in main cabin be spacious
Mouthful.
Preferably, first sliding track mechanism is provided with the first stop bit in steady status in its expansion or contraction state
Mechanism, second sliding track mechanism is provided with the second stop mechanism in steady status in its expansion or contraction state.
Preferably, first stop mechanism includes being connected to the hollow installation set of motor connection lever side, the installation set
Screens latch is inside installed, the top of the screens latch is provided with the first spring, and the bottom of the screens latch is multi-diameter shaft,
It is provided with to be provided with to second close to the side of the first slide rail on the first limited block, first limited block in the middle part of the screens latch and slides
First inclined-plane of rail inclined downward, the forward and backward upper lateral part of first limited block is close to the direction of the first slide rail provided with two the
The to the second slide rail inclined downward is respectively equipped with close to the side of the first slide rail on two limited blocks, two second limited blocks
Two inclined-planes, when first sliding track mechanism and the second sliding track mechanism are in deployed condition, the multi-diameter shaft is set in the first slide rail
On the second slide rail, when first sliding track mechanism and the second sliding track mechanism are in contraction state, the multi-diameter shaft is set in the
On one slide rail, the second slide rail and the 3rd slide rail.
Preferably, the top cross sectional dimensions of the multi-diameter shaft is more than remote on lower cross section size, first slide rail
Leaned on from the second slide rail and close to being respectively arranged at two ends with the first connecting hole and the second connecting hole, second slide rail for the second slide rail
One end of nearly first slide rail is provided with the 3rd connecting hole, the 3rd slide rail close to one end of the second slide rail provided with the 4th connection
Hole, when first sliding track mechanism and the second sliding track mechanism are in deployed condition, the top of the multi-diameter shaft is set in the second company
Connect on hole and the 3rd connecting hole, when first sliding track mechanism and the second sliding track mechanism are in contraction state, the multi-diameter shaft
Top is set on the first connecting hole and the 3rd connecting hole, and the bottom of the multi-diameter shaft is set on the 4th connecting hole.
Preferably, second stop mechanism is arranged at the position in 90 degree of angles, described second with the first stop mechanism
Stop mechanism includes second spring and bearing pin, and the second spring is installed on bearing pin one end, and the bearing pin other end is close to first
The side of slide rail is provided with the 3rd inclined-plane, second slide rail and slided on one end of the 3rd slide rail and the 3rd slide rail close to second
One end of rail is respectively equipped with the 5th connecting hole and the 6th connecting hole, and when second sliding track mechanism deploys, the bearing pin is passed through
5th connecting hole and the 6th connecting hole, when first sliding track mechanism and the contraction of the second sliding track mechanism, the first slide rail edge
Second slide rail surface is slided and is against on the 3rd inclined-plane, makes the slip relative with the 3rd slide rail of the second slide rail.
Preferably, also include：Unlocking mechanism：It is installed on the first slide rail, for the first sliding track mechanism to be deployed into shape
Its steady status is released when state or contraction state.
Preferably, the unlocking mechanism includes being provided with elongated hole, first slide rail on base plate, the base plate and is provided with
Projection, the base plate is installed on projection by what elongated hole can be moved left and right, on the base plate close to the second slide rail side before,
Rear portion, which is arranged with the base plate between two push rods, two push rods, is provided with two the first pushing blocks, two described first
On pushing block the 4th inclined-plane corresponding with the first incline position, angle is provided with close to the side of the second slide rail, two push rods
Suspension end is respectively equipped with the second sliding block, two second sliding blocks and is provided with and two the second inclined-planes close to the side of the second slide rail
Position, corresponding 5th inclined-plane of angle.
Preferably, first stop mechanism is the buckle structure being arranged on the first slide rail and the second slide rail.
Preferably, the auxiliary sliding track mechanism is provided with the first sliding track mechanism, the expansion or contraction-like of the second sliding track mechanism
In the stop mechanism of steady status during state.
After such scheme, the utility model extension type unmanned plane has the advantages that：
1st, by being set in main cabin left and right side in shield, each shield by the sliding track mechanism of concertina type first connection motor slurry
Leaf mechanism, each motor paddle mechanism is connected by the sliding track mechanism of concertina type second with main cabin, makes motor paddle mechanism first and second
Sliding track mechanism is contained in the space that shield is constituted with main cabin when being in contraction state, and main cabin is also placed in two shields, so
Design it is simple and compact for structure, easy to operate, the complete of overall volume and motor blade can be reduced to greatest extent in inoperative
Orientation is protected, in order to store and transport and provide higher security；
2nd, by setting motor slide rail mechanism between main cabin and motor paddle mechanism, setting auxiliary between main cabin and shield
Sliding track mechanism is helped, so design is further ensured that the slip stationarity between main cabin, motor paddle mechanism and shield, and be more convenient for behaviour
Make and storage, the security of transport；
3rd, by setting the first stop mechanism and the second stop bit machine respectively on the first sliding track mechanism and the second sliding track mechanism
Structure, the steady status of main cabin, motor paddle mechanism and shield three in deployed condition can be ensured by so setting, and make each part
Do not slide；
4th, by setting unlocking mechanism, it can facilitate the first sliding track mechanism, the second sliding track mechanism from the firm shape of expansion
State, which becomes, turns to sliding mode, and convenient to carry out shrinkage operation, its is simple in construction, easy to operate.
Brief description of the drawings
Fig. 1 is the dimensional decomposition structure diagram of the utility model extension type unmanned aerial vehicle example one；
Fig. 2 is the deployed condition structural representation of the utility model extension type unmanned aerial vehicle example one；
Fig. 3 is the dimensional decomposition structure diagram of the utility model extension type unmanned aerial vehicle example two；
Fig. 4 is the deployed condition structural representation of the utility model extension type unmanned aerial vehicle example two；
Fig. 5 is the dimensional decomposition structure diagram of the utility model extension type unmanned aerial vehicle example three；
Fig. 6 is the screens latch dimensional structure diagram of the utility model extension type unmanned aerial vehicle example three；
Fig. 7 is first stop mechanism connection knot of the utility model extension type unmanned aerial vehicle example three in deployed condition
Structure schematic diagram；
Fig. 8 is first stop mechanism connection knot of the utility model extension type unmanned aerial vehicle example three in contraction state
Structure schematic diagram；
Fig. 9 is the vertical view of second stop mechanism of the utility model extension type unmanned aerial vehicle example three in deployed condition
Attachment structure schematic diagram；
Figure 10 is the dimensional decomposition structure diagram of the utility model extension type unmanned aerial vehicle example four；
Figure 11 is the unlocking mechanism dimensional structure diagram of the utility model extension type unmanned aerial vehicle example four；
Figure 12 is first stop mechanism and solution of the utility model extension type unmanned aerial vehicle example four in deployed condition
The attachment structure schematic diagram of latch mechanism；
Figure 13 is first stop mechanism and solution of the utility model extension type unmanned aerial vehicle example four in contraction state
The attachment structure schematic diagram of latch mechanism；
Figure 14 is structure change of the utility model extension type unmanned aerial vehicle example four from deployed condition to contraction state
Schematic diagram；
Figure 15 is the dimensional decomposition structure diagram of the utility model extension type unmanned aerial vehicle example five；
Figure 16 is the contraction state structural representation of the utility model extension type unmanned aerial vehicle example five；
Figure 17 is the motor paddle mechanism dimensional structure diagram of the utility model extension type unmanned aerial vehicle example five；
Figure 18 is the dimensional decomposition structure diagram of the utility model extension type unmanned aerial vehicle example six；
Figure 19 is the deployed condition structural representation of the utility model extension type unmanned aerial vehicle example six；
Figure 20 is the contraction state structural representation of the utility model extension type unmanned aerial vehicle example six.
Embodiment
The utility model is illustrated below according to accompanying drawing illustrated embodiment.This time disclosed embodiment can consider in institute
There is aspect to be illustration, it is without limitation.Scope of the present utility model is not limited by the explanation of implementation below, only by right
Shown in the scope of claim, and including having all changes in the same meaning and right with right
Shape.
The dimensional decomposition structure diagram of embodiment one of the utility model extension type unmanned plane as shown in Figure 1, including nothing
People owner cabin 1, all round closure in main cabin 1, the left and right side positioned at main cabin 1 is respectively arranged with shield 2, and shield 2 is provided with for surface
The guard of multiple mesh 3, shield 2 towards main cabin 1 side be open design.Pass through the first of concertina type respectively in each shield 2
Sliding track mechanism 4 slidably connects motor paddle mechanism, motor paddle mechanism includes before being located on motor connection lever 5, motor connection lever 5,
Rear portion, which is respectively arranged with base 6, two bases 6, is separately installed with motor paddle component 7, and motor paddle component 7 is existing production
Product, including motor and motor paddle, this embodiment motor paddle component 7 are bolted on base 6, can also be by it
Its connected mode, such as the mode such as welding is the novel protected scope of this reality.
First sliding track mechanism 4 includes the first slide rail 8 for being arranged at the intracavity sidewall of shield 2, and first slide rail 8 is that cross section is
The projection of inverted L-shaped is made.Position corresponding with the position of the first slide rail 8 is provided with the second slide rail 9, second on the side of motor connection lever 5
The top of slide rail 9 is provided with the first rail groove 10 that cross section is inverted L-shaped, and its underpart is provided with the second rail groove that cross section is L-shaped
11, the first rail groove 10 of the second slide rail 9 is slided on the first slide rail 8, the motor connection lever 5 of shield 2 and motor paddle mechanism
Between be slidably connected with the first rail groove 10 of the second slide rail 9 by the first slide rail 8 together with, first sliding track mechanism 4 also may be used
Think socket join structure.
Two motor paddle mechanisms are slidably connected at by the second sliding track mechanism 12 and the side in main cabin 1 of concertina type respectively
Together, the second sliding track mechanism 12 includes the second rail groove 11 of the second slide rail 9 and setting corresponding with the position of the second rail groove 11
In the 3rd slide rail 13 of the main side wall of cabin 1, the 3rd slide rail 13 is made up of cross section of the projection of L-shaped.Second rail of the second slide rail 9
Road groove 11 is slided on the 3rd slide rail 13, and the motor connection lever 5 of motor paddle mechanism passes through the second of the second slide rail 9 with main cabin 1
Together with rail groove 11 is slidably connected with the 3rd slide rail 13, second sliding track mechanism 12 can also be socket join structure.
Motor slide rail mechanism is also slidably connected between main cabin 1 and motor paddle mechanism respectively, motor slide rail mechanism includes
It is arranged at two the 4th slide rails 14 of the front and rear portions of motor connection lever 5 and is arranged at two motor slide rails 15 of the main side wall of cabin 1, this reality
It is two groups of groove coupling structures that can be slided relatively, i.e. the 4th slide rail 14 to apply two the 4th slide rails 14 of example and two motor slide rails 15
For a groove structure, motor slide rail 15 is a projection cube structure that can be slidably inserted into the 4th slide rail 14.Each motor paddle component 7 and master
Together with being slidably connected between cabin 1 with motor slide rail 15 by the 4th slide rail 14, the 4th slide rail 14 can also with motor slide rail 15
For socket join structure.
The present embodiment preferably also includes auxiliary sliding track mechanism, auxiliary sliding track mechanism include being arranged at the front side of main cabin 1 and/or
In first auxiliary slide rail 16 of rear side and the second auxiliary slide rail 17 for being arranged at the inner chamber of shield 2 front side and/or rear side, the present embodiment
First auxiliary slide rail 16 is arranged at the main rear side of cabin 1, and the second auxiliary slide rail 17 is arranged on rear side of the inner chamber of shield 2, main cabin 1 and shield
Aided between 2 by the first auxiliary slide rail 16 with second together with slide rail 17 is slidably connected.First auxiliary slide rail in this embodiment
16 and second auxiliary slide rail 17 be the groove coupling structure that relative can be slidably connected.
Motor paddle mechanism is contained in two shields when the first sliding track mechanism 4 and the second sliding track mechanism 12 are in contraction state
In space between 2 and main cabin 1, and main cabin 1 is all placed in the inner chamber of two shields 2.
With reference to shown in Fig. 2, when unmanned plane works, the first sliding track mechanism 4 and the second sliding track mechanism 12 are deployed, make two
Relative to the two motor paddle mechanisms of shield 2 deploy respectively, two motor paddle mechanisms is distinguished relative to the main left and right side of cabin 1
Expansion, now, the first slide rail 8 slide outwardly into the two maximum for keeping connection relative to the first rail groove 10 of the second slide rail 9
Limit position, while second rail groove 11 of the second slide rail 9 is slide outwardly into the two relative to the 3rd slide rail 13 keeps connection
Greatest limit position, the 4th slide rail 14 can slide outwardly into greatest limit position, the second auxiliary cunning by motor slide rail 15 relatively during being somebody's turn to do
Rail 17 slide outwardlys into greatest limit position relative to the first auxiliary slide rail 16, unmanned plane is normally patrolled
With work of taking photo by plane；And when unmanned plane does not work, the first sliding track mechanism 4 and the second sliding track mechanism 12 are shunk, make two motors
Paddle mechanism is placed in two shields 2, while the main cabin 1 of unmanned plane is placed in two shields 2 completely, two such shield
Cover is 2-in-1 and main cabin 1 and two motor paddle mechanisms cover completely get up, two motor paddle mechanisms be respectively contained in main cabin 1 with
In accommodation space between two shields 2, its is simple and compact for structure, easy to operate, can be reduced to greatest extent in inoperative
The disposition of overall volume and motor blade, in order to store and transport and provide higher security.
As shown in Figure 3 and Figure 4 the dimensional decomposition structure diagram of embodiment two of the utility model extension type unmanned plane and
The structural representation of deployed condition, includes the main cabin 1 of unmanned plane, and all round closure in main cabin 1, the left and right side positioned at main cabin 1 is distinguished
Shield 2 is provided with, shield 2 is provided with the multiple formation of mesh 3 hub-likes in the guard of multiple mesh 3, this embodiment for surface.Shield
Cover 2 is open design towards the side and upper end in main cabin 1.The first sliding track mechanism 4 in each shield 2 respectively by concertina type is slided
Dynamic to be connected with motor paddle mechanism, motor paddle mechanism includes setting respectively positioned at front and rear portions on motor connection lever 5, motor connection lever 5
Have and motor paddle component 7 be separately installed with base 6, two bases 6, motor paddle component 7 be existing product, including motor and
Motor paddle, this embodiment motor paddle component 7 is bolted on base 6, can also by other connected modes, than
Such as welding mode is the novel protected scope of this reality.
First sliding track mechanism 4 includes being arranged at the ＇ of the first slide rail 8 in the middle part of the intracavity sidewall of shield 2, and first slide rail 8 ＇ is by C
Type groove steel is made.Position corresponding with the ＇ positions of the first slide rail 8 is provided with the ＇ of the second slide rail 9, the second slide rail on the side of motor connection lever 5
9 ＇ are also to be made up of C-shaped channel steel, and its cross sectional dimensions is slightly less than the ＇ of the first slide rail 8 size, and the ＇ of the second slide rail 9, which is slided, is located at first
On the ＇ of slide rail 8, it is slidably connected between the motor connection lever 5 of shield 2 and motor paddle mechanism by the ＇ of the first slide rail 8 with the ＇ of the second slide rail 9
Together.
Two motor paddle mechanisms are slidably connected at by the second sliding track mechanism 12 and the side in main cabin 1 of concertina type respectively
Together, the second sliding track mechanism 12 includes the ＇ of the second slide rail 9 and corresponding with the ＇ positions of the second slide rail 9 is arranged at the of the main side wall of cabin 1
The ＇ of three slide rail 13, the ＇ of the 3rd slide rail 13 is also to be made up of C-shaped channel steel.The ＇ of second slide rail 9 cross sectional dimensions is slightly larger than the 3rd slide rail
13 ＇ transverse cutting machine size.The ＇ of second slide rail 9 is slided on the ＇ of the 3rd slide rail 13, and motor connection lever 5 passes through the second slide rail with main cabin 1
Together with 9 ＇ are slidably connected with the ＇ of the 3rd slide rail 13.
Motor slide rail mechanism is also slidably connected between main cabin 1 and motor paddle mechanism respectively, motor slide rail mechanism includes
It is arranged at two the 4th slide rails 14 of the front and rear portions of motor paddle component 7 and is arranged at two motor slide rails 15 of the main side wall of cabin 1,
Two the 4th slide rails 14 and two motor slide rails 15 are the two groups of groove coupling structures that can be slided relatively, i.e., the 4th in this embodiment
Slide rail 14 is a groove structure, and motor slide rail 15 is a projection cube structure that can be slidably inserted into the 4th slide rail 14.Each motor paddle group
Together with being slidably connected between part 7 and main cabin 1 with motor slide rail 15 by the 4th slide rail 14, the 4th slide rail 14 and motor slide rail 15
It can also be socket join structure.
The present embodiment preferably also includes auxiliary sliding track mechanism, auxiliary sliding track mechanism include being arranged at the front side of main cabin 1 and/or
The first auxiliary ＇ of slide rail 16 of rear side and the second auxiliary ＇ of slide rail 17 for being arranged at the inner chamber of shield 2 front side and/or rear side, the present embodiment
In the first auxiliary ＇ of slide rail 16 be arranged at the front side of main cabin 1, the second auxiliary ＇ of slide rail 17 is arranged on front side of the inner chamber of shield 2, main cabin 1 with
Aided between shield 2 by the first auxiliary ＇ of slide rail 16 with second together with the ＇ of slide rail 17 is slidably connected.First is auxiliary in this embodiment
The C-shaped channel steel construction for helping the ＇ of slide rail 16 and second to aid in the ＇ of slide rail 17 relative to be slidably connected.
Motor paddle mechanism is contained in two shields when the first sliding track mechanism 4 and the second sliding track mechanism 12 are in contraction state
In space between 2 and main cabin 1, and main cabin 1 is all placed in the inner chamber of two shields 2.
The occupation mode and process of the present embodiment and the occupation mode and process of above-described embodiment one are essentially identical, herein not
Repeat again, its same design it is simple and compact for structure, easy to operate, can be reduced to greatest extent in inoperative overall volume and
The disposition of motor blade, in order to store and transport and provide higher security.
The dimensional decomposition structure diagram of embodiment three of the utility model extension type unmanned plane as shown in Figure 5, its big portion
Separation structure is identical with the structure of embodiment two described in above-mentioned Fig. 3, includes the main cabin 1 of unmanned plane, and all round closure in main cabin 1 is located at
The left and right side in main cabin 1 is respectively arranged with shield 2, and shield 2 is provided with multiple in the guard of multiple mesh 3, this embodiment for surface
The formation hub-like of mesh 3.Shield 2 is open design towards the side and upper end in main cabin 1.Respectively by flexible in each shield 2
First sliding track mechanism 4 of type slidably connects motor paddle mechanism, and motor paddle mechanism is included on motor connection lever 5, motor connection lever 5
It is respectively arranged with positioned at front and rear portions on base 6, two bases 6 and is separately installed with motor paddle component 7, motor paddle component 7 is
Existing product, including motor and motor paddle, this embodiment motor paddle component 7 are bolted on base 6, can also
By other connected modes, such as the mode such as welding is the novel protected scope of this reality.
First sliding track mechanism 4 includes being arranged at the ＇ of the first slide rail 8 in the middle part of the intracavity sidewall of shield 2, and first slide rail 8 ＇ is by C
Type groove steel is made.Position corresponding with the ＇ positions of the first slide rail 8 is provided with the ＇ of the second slide rail 9, the second slide rail on the side of motor connection lever 5
9 ＇ are also to be made up of C-shaped channel steel, and its cross sectional dimensions is slightly less than the ＇ of the first slide rail 8 size, and the ＇ of the second slide rail 9, which is slided, is located at first
On the ＇ of slide rail 8, it is slidably connected between the motor connection lever 5 of shield 2 and motor paddle mechanism by the ＇ of the first slide rail 8 with the ＇ of the second slide rail 9
Together.
Two motor paddle mechanisms are slidably connected at by the second sliding track mechanism 12 and the side in main cabin 1 of concertina type respectively
Together, the second sliding track mechanism 12 includes the ＇ of the second slide rail 9 and corresponding with the ＇ positions of the second slide rail 9 is arranged at the of the main side wall of cabin 1
The ＇ of three slide rail 13, the ＇ of the 3rd slide rail 13 is also to be made up of C-shaped channel steel.The ＇ of second slide rail 9 cross sectional dimensions is slightly larger than the 3rd slide rail
13 ＇ transverse cutting machine size.The ＇ of second slide rail 9 is slided on the ＇ of the 3rd slide rail 13, and motor connection lever 5 passes through the second slide rail with main cabin 1
Together with 9 ＇ are slidably connected with the ＇ of the 3rd slide rail 13.
Motor slide rail mechanism is also slidably connected between main cabin 1 and motor paddle mechanism respectively, motor slide rail mechanism includes
It is arranged at two the 4th slide rails 14 of the front and rear portions of motor paddle component 7 and is arranged at two motor slide rails 15 of the main side wall of cabin 1,
Two the 4th slide rails 14 and two motor slide rails 15 are two groups of groove coupling structures that can be slided relatively, i.e., the 4th in this embodiment
Slide rail 14 is a groove structure, and motor slide rail 15 is a projection cube structure that can be slidably inserted into the 4th slide rail 14.Each motor paddle group
Together with being slidably connected between part 7 and main cabin 1 with motor slide rail 15 by the 4th slide rail 14, the 4th slide rail 14 and motor slide rail 15
It can also be socket join structure.
The present embodiment preferably also includes auxiliary sliding track mechanism, auxiliary sliding track mechanism include being arranged at the front side of main cabin 1 and/or
The first auxiliary ＇ of slide rail 16 of rear side and the second auxiliary slide rail for being arranged at the inner chamber of shield 2 front side and/or rear side（Do not show in figure
Go out）, the first auxiliary ＇ of slide rail 16 is arranged at the main front side of cabin 1 in the present embodiment, and the second auxiliary slide rail is arranged at before the inner chamber of shield 2
Side, main cabin 1 by the first auxiliary ＇ of slide rail 16 between shield 2 with second with being aided in together with slide rail is slidably connected.In this embodiment
The C-shaped channel steel construction that the first auxiliary ＇ of slide rail 16 and second aids in slide rail relative to be slidably connected.
In the present embodiment, the first sliding track mechanism 4 is provided with to be stopped in its expansion or contraction state in the first of steady status
Position mechanism, the second sliding track mechanism 12 is provided with the second stop mechanism in steady status in its expansion or contraction state.
First stop mechanism, which includes being connected in the hollow installation set 18 of the side of motor connection lever 5, installation set 18, is provided with card
Position latch 19, with reference to shown in Fig. 6, the top of screens latch 19 is that the first spring 21 is installed on circular shaft 20, the circular shaft 20, and screens is inserted
The bottom of pin 19 is multi-diameter shaft 22, and the top cross sectional dimensions of multi-diameter shaft 22 is more than lower cross section size.Screens latch 19
Middle part is provided with the first limited block 23, and the cross sectional dimensions of first limited block 23 is more than the cross section chi of circular shaft 20 and multi-diameter shaft 22
It is very little.It is provided with first limited block 23 close to the ＇ of the first slide rail 8 side to the first inclined-plane 24 of the ＇ inclined downwards of the second slide rail 9, the
The forward and backward upper lateral part of one limited block 23 is close to the ＇ of the first slide rail 8 direction provided with two the second limited blocks 25, and two second spacing
The close ＇ of first slide rail 8 side is respectively equipped with the second inclined-plane 26 to the ＇ inclined downwards of the second slide rail 9 on block 25.
With reference to shown in Fig. 7 and Fig. 8, away from the ＇ of the second slide rail 9 and close to the ＇ of the second slide rail 9 two ends difference on the ＇ of the first slide rail 8
Provided with the first connecting hole 27 and the second connecting hole 28, the 3rd connecting hole is provided with close to the ＇ of the first slide rail 8 one end on the ＇ of the second slide rail 9
The 4th connecting hole 30 is provided with close to the ＇ of the second slide rail 9 one end on 29, the ＇ of the 3rd slide rail 13, when the first sliding track mechanism 4 and second is slided
When rail mechanism 12 is in deployed condition, multi-diameter shaft 22 is set on the second connecting hole 28 and the 3rd connecting hole 29, when the first slide rail machine
When the sliding track mechanism 12 of structure 4 and second is in contraction state, the top of multi-diameter shaft 22 is set in the first connecting hole 27 and the 3rd connecting hole
On 29, the bottom of multi-diameter shaft 22 is set on the 4th connecting hole 30.
The set location of second stop mechanism and the angle that the first stop mechanism is in 90 degree, with reference to shown in Fig. 9, the second stop bit
Mechanism includes second spring 31 and bearing pin 32, and second spring 31 is installed on one end of bearing pin 32, and the other end of bearing pin 32 is close to the
The ＇ of one slide rail 8 side is provided with the 3rd inclined-plane 33, the ＇ of the second slide rail 9 on the ＇ of the 3rd slide rail 13 one end and the ＇ of the 3rd slide rail 13
One end close to the ＇ of the second slide rail 9 is respectively equipped with the 5th connecting hole 34 and the 6th connecting hole 35, when the second sliding track mechanism 12 deploys
When, bearing pin 32 passes through the 5th connecting hole 34 and the 6th connecting hole 35, when the first sliding track mechanism 4 shrinks with the second sliding track mechanism 12
When, the ＇ of the first slide rail 8 along the ＇ surfaces of the second slide rail 9 slide be against on the 3rd inclined-plane 33, bearing pin 32 push up back, make the ＇ of the second slide rail 9 and
The ＇ of 3rd slide rail 13 is relative to be slided.
When unmanned plane works, the first sliding track mechanism 4 and the second sliding track mechanism 12 are deployed, make two shields 2 relative to
Two motor paddle mechanisms deploy respectively, two motor paddle mechanisms is deployed respectively relative to the main left and right side of cabin 1, when first
The ＇ of slide rail 8 slide outwardlys into as shown in Figure 7 relative to the ＇ of the second slide rail 9, i.e., the second connecting hole 28 and the 3rd connecting hole are about 29
At corresponding position, being inserted by the multi-diameter shaft 22 of the first stop mechanism in the second connecting hole 28 and the 3rd connecting hole 29 makes first
The ＇ of the slide rail 8 and ＇ of the second slide rail 9 deploys and in steady status, while the ＇ of the second slide rail 9 is slid in and out relative to the ＇ of the 3rd slide rail 13
To as shown in Figure 9, i.e., the ＇ of the 3rd slide rail 13 the 6th connecting hole 35 and the 5th connecting hole on the ＇ of the second slide rail 9 are corresponding about 34
Position at, being inserted by the bearing pin 32 of the second stop mechanism in the 5th connecting hole 34 and the 6th connecting hole 35 makes the ＇ of the second slide rail 9
With the ＇ of the 3rd slide rail 13 expansion and can be with normal work in steady status, the i.e. unmanned plane；And when unmanned plane does not work, pass through
External force makes the multi-diameter shaft 22 of the first stop mechanism depart from the 3rd connecting hole 29, promotes the ＇ of the first slide rail 8, makes the ＇ of the first slide rail 8 relative
Slided in the ＇ of the second slide rail 9, and the ＇ of the first slide rail 8 is at sliding process to the position of bearing pin 32, can be against bearing pin 32 the 3rd is oblique
On face 33, bearing pin 32 is set to depart from the 5th connecting hole 34 so that the ＇ of the second slide rail 9 is slided with respect to the ＇ of the 3rd slide rail 13, by the first slide rail
8 ＇, the ＇ of the second slide rail 9 are together slided on the ＇ of the 3rd slide rail 13, when the first connecting hole 27, the 3rd connecting hole 29 and the 4th connecting hole 30
The multi-diameter shaft 22 of the first stop mechanism is connected through the first connecting hole 27, the 3rd connecting hole 29 and the 4th when above and below position to correspondence
First sliding track mechanism 4, the full retraction of the second sliding track mechanism 12, motor paddle mechanism are contained in two shields 2 and main cabin 1 by hole 30
Between space in, and main cabin 1 is all placed in two shields 2.
The example IV dimensional decomposition structure diagram of the utility model extension type unmanned plane as shown in Figure 10, it includes
All structures of above-described embodiment three, repeat no more with the identical structure of embodiment three, are a difference in that：The embodiment is also wrapped
Include：Unlocking mechanism 36：It is installed on the ＇ of the first slide rail 8, for the first sliding track mechanism 4 to be solved in deployed condition or contraction state
Except its steady status.
With reference to shown in Figure 11, the unlocking mechanism 36 includes being provided with elongated hole 38 on base plate 37, base plate 37, the ＇'s of the first slide rail 8
The position that upper surface is located between the side wall of shield 2 and the first connecting hole 27 is provided with projection 39, and base plate 37 can be left by elongated hole 38
What is moved right is installed on projection 39, and the side front and rear portions on base plate 37 close to the ＇ of the second slide rail 9 are arranged with two push rods 40,
It is provided with base plate 37 between two push rods 40 on two the first pushing blocks 41, two the first pushing blocks 41 close to the ＇'s of the second slide rail 9
Side is provided with the 4th inclined-plane 42 corresponding with the position of the first inclined-plane 24, angle, and the suspension end of two push rods 40 is respectively equipped with second
Close to the ＇ of the second slide rail 9 side provided with corresponding with two the second inclined-planes 26 position, angle on sliding block 43, two the second sliding blocks 43
The 5th inclined-plane 44.
With reference to shown in Figure 14, when unmanned plane works, the first sliding track mechanism 4 and the second sliding track mechanism 12 are in deployed condition,
When it does not work, unlocking mechanism 36 is moved along along elongated hole 38, with reference to shown in Figure 12, by the second sliding block 43 of unlocking mechanism 36
The 5th inclined-plane 44 fitted with the second inclined-plane 26 on the second limited block 25 of screens latch 19, afterwards promote unlocking mechanism 36,
The 3rd connecting hole 29 for making screens latch 19 depart from the second slide rail 9 ＇, promotes the ＇ of the first slide rail 8, makes the ＇ of the first slide rail 8 relative to the
The ＇ surfaces of two slide rail 9 are slided, when three inclined-plane 33 on the bearing pin 32 that the ＇ of the first slide rail 8 touches the second stop mechanism, bearing pin
32 lower end departs from the ＇ of the second slide rail 9 the 5th connecting hole 34, and the ＇ of the first slide rail 8 and the ＇ of the second slide rail 9 are together along the ＇ of the 3rd slide rail 13
Surface slide, when the first connecting hole 27, the 3rd connecting hole 29 and the 4th connecting hole are corresponded to and when communicating about 30, screens latch
The multi-diameter shaft 22 of 19 bottoms is set on the first connecting hole 27, the 3rd connecting hole 29 and the 4th connecting hole 30, thus makes the 3rd
The ＇ of slide rail 13 is on the ＇ of the second slide rail 9, and the ＇ of the 3rd slide rail 13, the ＇ of the second slide rail 9 make three sections of slide rails on the ＇ of the first slide rail 8
Length shortens the ＇ of the first slide rail 8 length into, and motor paddle mechanism is contained in the space between two shields 2 and main cabin 1, and main
Cabin 1 is all placed in two shields 2；And when unmanned plane works, with reference to shown in Figure 13, slided by the first of unlocking mechanism 36
The 4th inclined-plane 42 on block 41 is fitted with the first inclined-plane 24 on the first limited block 23 of screens latch 19, and solution lock machine is promoted afterwards
Structure 36, makes the 4th connecting hole 30 on the lower end of multi-diameter shaft 22 disengaging the 3rd slide rail 13 ＇ of screens latch 19, so that the first slide rail
8 ＇, the ＇ of the second slide rail 9 are slided with respect to the ＇ of the 3rd slide rail 13 and outwards deployed, until the insertion of bearing pin 32 the 5th of the second stop mechanism connects
Connect and make in the connecting hole 35 of hole 34 and the 6th ＇ of the second slide rail 9 and ＇ of the 3rd slide rail 13 expansion and in steady status, and the ＇ of the first slide rail 8
Deploy with the ＇ of the second slide rail 9 by the way that the unblock of unlocking mechanism is same, the multi-diameter shaft 22 of the first stop mechanism is inserted the second connecting hole
28 and the 3rd make in connecting hole 29 ＇ of the first slide rail 8 and ＇ of the second slide rail 9 deploy and can be normal in steady status, the i.e. unmanned plane
Work.
As shown in Figure 15, Figure 16 the dimensional decomposition structure diagram of embodiment five of the utility model extension type unmanned plane and
Contraction state structural representation, includes the main cabin 1 of unmanned plane, and all round closure in main cabin 1, the left and right side in main cabin 1 is connected to
The open outer cover 45 of outboard end, outer cover 45 is the cover body of work grid shape, and shield 2 is respectively arranged with the left and right side of outer cover 45,
Shield 2 which is provided with multiple mesh 3 to there is work grid shape guard.Shield 2 towards main cabin 1 side be open design.Each shield
Motor paddle mechanism is slidably connected by the first sliding track mechanism 4 of concertina type respectively in cover 2, motor paddle mechanism includes motor
It is respectively arranged with connecting rod 5, motor connection lever 5 positioned at front and rear portions on base 6, two bases 6 and is separately installed with motor paddle component
7, motor paddle component 7 is existing product, including motor and motor paddle, this embodiment motor paddle component 7 are connected by bolt
It is connected on base 6, the novel protected scope of this reality can also be by other connected modes, such as the mode such as welding.
First sliding track mechanism 4 includes the first slide rail 8 for being arranged at the intracavity sidewall of shield 2 ", first slide rail 8 is " by cross section
It is made up of the projection of inverted T-shaped.With the first slide rail 8 " position corresponding position be provided with the second slide rail 9 " on the side of motor connection lever 5,
Second slide rail 9 " is connected and composed by superposed T-shaped upper rail block 46 and the lower rail block 47 positioned at bottom, and upper rail block 46 is provided with
Cross section be inverted T-shaped the first chute 48, upper rail block 46 located at the upper surface of lower rail block 47 close to the first slide rail 8 " end, lower rail
The lower surface of block 47 is provided with the second chute 49 that cross section is T-shaped.First slide rail 8 " is slided in the first chute 48.Shield 2
Pass through the first chute 48 of the upper rail block 46 of the first slide rail 8 " with second slide rail 9 " between the motor connection lever 5 of motor paddle mechanism
It is slidably connected together.
Two motor paddle mechanisms are slidably connected at by the second sliding track mechanism 12 and the side in main cabin 1 of concertina type respectively
Together, the second sliding track mechanism 12 includes the second slide rail 9 " lower rail block 47 and with the second slide rail 9 " position is corresponding to be arranged at main cabin
1 side wall the 3rd slide rail 13 ", the 3rd slide rail 13 " is made up of cross section of the projection of T-shaped.The lower rail block 47 of second slide rail 9 "
The second chute 49 slide and be located at the 3rd slide rail 13 " on, motor connection lever 5 and main cabin 1 pass through the second slide rail 9 " with the 3rd slide rail 13 "
It is slidably connected together.
Motor slide rail mechanism, with reference to shown in Figure 17, motor are also slidably connected respectively between main cabin 1 and motor paddle mechanism
Sliding track mechanism includes being arranged at two the 4th slide rails 14 of the front and rear portions of motor connection lever 5 and is arranged at the main side wall front and rear portions of cabin 1
Two the 4th slide rails 14 and two motor slide rails 15 are two groups of grooves that can be slided relatively in two motor slide rails 15, this embodiment
Projection cube structure, i.e. the 4th slide rail 14 are that a cross section is T-slot structure, and motor slide rail 15 can be slidably inserted into the 4th slide rail 14 for one
T-shaped projection cube structure.It is slidably connected between each motor paddle component 7 and main cabin 1 by the 4th slide rail 14 and motor slide rail 15
Together.
Also include auxiliary sliding track mechanism, auxiliary sliding track mechanism includes the first auxiliary slide rail 16 for being arranged at the forward and backward side in main cabin 1
And be arranged at the forward and backward side in the inner chamber of shield 2 second auxiliary slide rail 17, between main cabin 1 and shield 2 by first auxiliary slide rail 16 with
Second auxiliary slide rail 17 is slidably connected together.In this embodiment first auxiliary slide rail 16 with second auxiliary slide rail 17 be can be relative
The groove coupling structure being slidably connected.
In the present embodiment, the first sliding track mechanism 4 is provided with to be stopped in its expansion or contraction state in the first of steady status
Position mechanism, the second sliding track mechanism 12 is provided with the second stop mechanism in steady status in its expansion or contraction state.
First stop mechanism includes being arranged at a pair of first slide rail 8 " forward and backward side upper end is close to the second slide rail 9 " end the
One stop block 50 and " a pair of second stop blocks 51 of end that are arranged at the forward and backward side in the upper surface of upper rail block 46 close to the first slide rail 8.
Second stop mechanism includes being arranged at the forward and backward side of the lower surface of lower rail block 47 close to the 3rd " a pair of end of slide rail 13
3rd stop block 52 and it is arranged at a pair fourth stop blocks 53 of the forward and backward side lower surface of the 3rd slide rail close to the second extreme.
Motor paddle mechanism is contained in two shields when the first sliding track mechanism 4 and the second sliding track mechanism 12 are in contraction state
In space between 2 and main cabin 1, and main cabin 1 is all placed in the inner chamber of two shields 2.
When unmanned plane works, the first sliding track mechanism 4 and the second sliding track mechanism 12 are deployed, make two shields 2 relative to
Two motor paddle mechanisms deploy respectively, two motor paddle mechanisms is deployed respectively relative to the main left and right side of cabin 1, now, the
First chute 48 of the upper rail block 46 of one slide rail 8 " relative to the second slide rail 9 " slide outwardlys into the maximum pole that the two keeps connection
Spacing, i.e. a pair of first stop blocks 50 and a pair of second stop blocks 51 of the first stop mechanism mutually block holding stable state, simultaneously
Second slide rail 9 " the second chute 49 relative to the 3rd slide rail 13 " is slide outwardly into the two greatest limit position for keeping connection,
That is a pair of the 3rd stop blocks 52 of the second stop mechanism and a pair of the 4th stop blocks 53 mutually block holding stable state.Should during the
Four slide rails 14 can slide outwardly into greatest limit position by motor slide rail 15 relatively, and the second auxiliary slide rail 17 is relative to the first auxiliary slide rail
16 slide outwardly into greatest limit position, unmanned plane is normally patrolled and taken photo by plane work；And work as unmanned plane
When not working, the first sliding track mechanism 4 is shunk with the second sliding track mechanism 12, i.e., first release the first stop mechanism a pair first stop
Clamping lock state between position block 50 and a pair of second stop blocks 51, and release a pair of the 3rd stop blocks 52 of the second stop mechanism with
Clamping lock state between a pair of the 4th stop blocks 53, makes the first of the upper rail block 46 of the first slide rail 8 " relative to the second slide rail 9 " to slide
Groove 48 is slided in shrinking, while the second slide rail 9 " the second chute 49 relative to the 3rd slide rail 13 " is slided in shrinking, makes two
Motor paddle mechanism is placed in two shields 2, while the main cabin 1 of unmanned plane is placed in two shields 2 completely, such two
Individual shield is 2-in-1 and main cabin 1 and two motor paddle mechanisms cover completely are got up, and two motor paddle mechanisms are respectively contained in main cabin
In accommodation space between 1 and two shields 2, its is simple and compact for structure, easy to operate, can be contracted to greatest extent in inoperative
The disposition of small overall volume and motor blade, in order to store and transport and provide higher security.
The dimensional decomposition structure of the embodiment six of the utility model extension type unmanned plane as shown in Figure 18, Figure 19 and Figure 20
Schematic diagram, deployed condition and contraction state structural representation, include the main cabin 1 of unmanned plane, all round closure in main cabin 1, main cabin 1
Left and right side is connected to the open outer cover 45 of outboard end, and outer cover 45 is the cover body of work grid shape, in the left and right of outer cover 45
Side is respectively arranged with shield 2, and shield 2 which is provided with multiple mesh 3 to there is work grid shape guard.Shield 2 is towards main cabin 1
Side is open design.The first sliding track mechanism 4 in each shield 2 respectively by concertina type slidably connects motor paddle mechanism,
Motor paddle mechanism includes being separately installed with motor paddle component 7 on two bases 6, two bases 6, and motor paddle component 7 is
Existing product, including motor and motor paddle, this embodiment motor paddle component 7 are bolted on base 6, can also
By other connected modes, such as the mode such as welding is the novel protected scope of this reality.
First sliding track mechanism 4 includes the first slide rail 8 ' for being arranged at the inner chamber upper side wall of shield 2 ' ', first slide rail 8 ' ' ' be
It is arranged at the long chute that the inner chamber upper side wall of shield 2 can be moved left and right.The upper surface of base 6 is provided with the second slide rail 9 ' ' ', second slides
Rail 9 ' ' ' include the track 55 that is fixed on the lower slide pin 54 of the upper surface of base 6 and is fixed on base 6, lower slide pin 54 is located at track
55 side and the position of close shield 2, the upper end of lower slide pin 54 are provided with the upper sliding pin 56 that cross section is T-shaped.Upper sliding pin 56
Slide and be located at the first slide rail 8 ' ' ' on.By the first slide rail 8 ' between shield 2 and motor paddle mechanism ' ' and the second slide rail 9 ' ' '
Upper sliding pin 56 be slidably connected together.
Two motor paddle mechanisms are slidably connected at by the second sliding track mechanism 12 and the side in main cabin 1 of concertina type respectively
Together, the second sliding track mechanism 12 includes the second slide rail 9 ' ' ' track 55 and with the second slide rail 9 ' ' ' position is corresponding is arranged at master
3rd slide rail 13 ' of the upper side wall of cabin 1 ' '.Second slide rail 9 ' ' in ' track 55 slide be located at the 3rd slide rail 13 ' ' ', the 3rd slide rail
13 ' ' ' there is groove corresponding with the shape of cross section of track 55, motor paddle mechanism and main cabin 1 pass through the second slide rail 9 ' ' ' rail
Road 55 and the 3rd slide rail 13 ' ' ' be slidably connected together with.
Also include auxiliary sliding track mechanism, auxiliary sliding track mechanism includes the first auxiliary slide rail 16 for being arranged at the forward and backward side in main cabin 1
And be arranged at the forward and backward side in the inner chamber of shield 2 second auxiliary slide rail 17, between main cabin 1 and shield 2 by first auxiliary slide rail 16 with
Second auxiliary slide rail 17 is slidably connected together.In this embodiment first auxiliary slide rail 16 with second auxiliary slide rail 17 be can be relative
The groove coupling structure being slidably connected.
In the present embodiment, auxiliary sliding track mechanism, which is provided with, to deploy or shrinks in the first sliding track mechanism 4, the second sliding track mechanism 12
In the stop mechanism of steady status during state.Stop mechanism includes being arranged at the lateral surface of the first auxiliary slide rail 16 close to the second auxiliary
A pair of the 3rd stop blocks 57 of the end of slide rail 17 and the lateral surface of the second auxiliary slide rail 17 is arranged at close to the first auxiliary slide rail 16 end
A pair of position-arresting grooves 58 in portion, the 3rd stop block 57 forms concavo-convex fastener matching structure with position-arresting groove 58.
Motor paddle mechanism is contained in two shields when the first sliding track mechanism 4 and the second sliding track mechanism 12 are in contraction state
In space between 2 and main cabin 1, and main cabin 1 is all placed in the inner chamber of two shields 2.
When unmanned plane works, the first sliding track mechanism 4 and the second sliding track mechanism 12 are deployed, make two shields 2 relative to
Two motor paddle mechanisms deploy respectively, and the first auxiliary auxiliary slide rail 17 of slide rail 16 and second is relative to deploy, motor paddle mechanism
Left and right side relative to main cabin 1 deploys respectively.Now the first auxiliary slide rail 16 keeps what is be connected with second auxiliary both slide rails 17
Holding stable state is mutually blocked in greatest limit position, i.e. the 3rd stop block 57 with position-arresting groove 58.Meanwhile, the first slide rail 8 ' ' ' and the second cunning
Rail 9 ' ' ' upper sliding pin 56 both keep connection greatest limit position, can thus make unmanned plane carry out normally patrol and navigate
Clap work；And when unmanned plane does not work, the first sliding track mechanism 4 and the second sliding track mechanism 12 are shunk, release the 3rd stop block
Clamping lock state between 57 and position-arresting groove 58, makes sliding pin 56 relative to the first slide rail 8 ' ' ' in shrink slide, while second
Slided on slide rail 9 ' ' ' track 55 relative to the 3rd slide rail 13 ' ' ' in shrinking.And the first auxiliary slide rail 16 and second is aided in
Slide rail 17 makes two motor paddle mechanisms be placed in two shields 2, while the main cabin 1 of unmanned plane is complete in slip is shunk
It is placed in two shields 2, two such shield is 2-in-1 and main cabin 1 and two motor paddle mechanisms cover completely are got up, two electricity
Machine paddle mechanism is respectively contained in the accommodation space between main cabin 1 and two shields 2, and its is simple and compact for structure, easy to operate,
The disposition of overall volume and motor blade can be reduced to greatest extent in inoperative, in order to store and transport and carry
For higher security.
Above-mentioned six embodiments are summarized and had the advantage that：
1st, electricity is connected by the first sliding track mechanism of concertina type 4 by being set in the main left and right side of cabin 1 in shield 2, each shield 2
Machine paddle mechanism, each motor paddle mechanism is connected by the second sliding track mechanism of concertina type 12 with main cabin 1, motor paddle mechanism is existed
First sliding track mechanism 4, the second sliding track mechanism 12 are contained in the space that shield 2 is constituted with main cabin 1, and main cabin 1 when being in contraction state
Also the inner chamber of two shields 2 is placed in completely, that so designs simple and compact for structure, easy to operate, the maximum limit in inoperative
Degree can reduce the disposition of overall volume and motor blade, in order to storing and transport and provide higher security；
2nd, by setting motor slide rail mechanism between main cabin 1 and motor paddle mechanism, being set between main cabin 1 and shield 2
Auxiliary sliding track mechanism is put, so design is further ensured that the slip stationarity between main cabin 1, motor paddle and shield 2, is more convenient for
Operation and storage, the security of transport；
3rd, by setting the first stop mechanism and the second stop bit respectively on the first sliding track mechanism 4 and the second sliding track mechanism 12
Mechanism, main cabin 1, the steady status of motor paddle mechanism and the three of shield 2 in deployed condition can be ensured by so setting, and be made each
Part is not slided；
4th, by setting unlocking mechanism, it can facilitate and consolidate the first sliding track mechanism 4, the second sliding track mechanism 12 from expansion
State change is sliding mode, and convenient to carry out shrinkage operation, its is simple in construction, easy to operate.
Those skilled in the art will readily occur to this practicality after considering specification and putting into practice utility model disclosed herein
New other embodiments.The application is intended to any modification of the present utility model, purposes or adaptations, these
Modification, purposes or adaptations follow general principle of the present utility model and including it is undocumented in the art
Common knowledge or conventional techniques.Description and embodiments be considered only as it is exemplary, true scope of the present utility model and
Spirit is pointed out by following claim.
It should be appreciated that the accurate knot that the utility model is not limited to be described above and is shown in the drawings
Structure, and various modifications and changes can be being carried out without departing from the scope.Scope of the present utility model only will by appended right
Ask to limit.
Claims (17)
1. a kind of extension type unmanned plane, it is characterised in that including main cabin, the left and right side in the main cabin is respectively arranged with shield,
Motor paddle mechanism, each motor paddle are slidably connected by the first sliding track mechanism of concertina type respectively in each shield
Mechanism is slidably connected by the second sliding track mechanism of concertina type with main cabin, and the motor paddle mechanism is in the first sliding track mechanism and
Two sliding track mechanisms are contained in when being in contraction state in the space that shield is constituted with main cabin, and the main volume of compartment is placed in two shields
It is interior.
2. extension type unmanned plane according to claim 1, it is characterised in that first sliding track mechanism includes being arranged at
Position corresponding with the first sled position is slided provided with second on first slide rail of shroud interior side wall, the motor paddle mechanism
Rail, second slide rail is slided on the first slide rail, passes through the first slide rail and the between shield and the motor paddle mechanism
Two slide rails are slidably connected together.
3. extension type unmanned plane according to claim 2, it is characterised in that second sliding track mechanism includes described the
Two slide rails and the 3rd slide rail for being arranged at main cabin side wall corresponding with the second sled position, second slide rail, which is slided, is located at the 3rd
On slide rail, the motor paddle mechanism between main cabin with the 3rd slide rail together with being slidably connected by the second slide rail.
4. extension type unmanned plane according to claim 3, it is characterised in that the motor paddle mechanism includes two electricity
Machine paddle component and two bases, two motor paddle components are installed on two bases in front and rear portions.
5. extension type unmanned plane according to claim 4, it is characterised in that also including motor connection lever, two bottoms
Seat is arranged at the front and rear portions of motor connection lever.
6. the extension type unmanned plane according to claim 4 or 5, it is characterised in that the main cabin and each motor paddle group
Motor slide rail mechanism is also slidably connected between part, the motor slide rail mechanism includes being arranged on the motor paddle mechanism
4th slide rail and the motor slide rail for being arranged at main cabin side wall, between each motor paddle mechanism and main cabin by the 4th slide rail with
Motor slide rail is slidably connected together.
7. extension type unmanned plane according to claim 6, it is characterised in that described auxiliary also including auxiliary sliding track mechanism
Help sliding track mechanism include being arranged on front side of main cabin and/or rear side the first auxiliary slide rail and be arranged on front side of shroud interior and/or
Second auxiliary slide rail of rear side, is slidably connected between the main cabin and shield by the first auxiliary slide rail with the second auxiliary slide rail
Together.
8. extension type unmanned plane according to claim 7, it is characterised in that first sliding track mechanism, the second slide rail
Mechanism is can the relative channel-section steel structure slided or groove coupling structure or socket join structure.
9. extension type unmanned plane according to claim 8, it is characterised in that the motor slide rail mechanism and auxiliary slide rail
Mechanism is can the relative groove coupling structure slided or socket join structure.
10. extension type unmanned plane according to claim 9, it is characterised in that the shield has multiple for surface layout
The guard of mesh, the shield is open towards the side in main cabin.
11. the extension type unmanned plane according to claim 4 or 5, it is characterised in that first sliding track mechanism is provided with
In its expansion or the first stop mechanism during contraction state in steady status, second sliding track mechanism be provided with its expansion or
In the second stop mechanism of steady status during contraction state.
12. extension type unmanned plane according to claim 11, it is characterised in that first stop mechanism includes connection
Screens latch is installed, the top of the screens latch is installed in the hollow installation set in motor connection lever side, the installation set
There is the first spring, the bottom of the screens latch is to be provided with the first limited block, described first in the middle part of multi-diameter shaft, the screens latch
It is provided with limited block close to the side of the first slide rail to the first inclined-plane of the second slide rail inclined downward, first limited block
Forward and backward upper lateral part is provided with two the second limited blocks, two second limited blocks close to first close to the direction of the first slide rail
The side of slide rail is respectively equipped with the second inclined-plane to the second slide rail inclined downward, when first sliding track mechanism and the second slide rail machine
When structure is in deployed condition, the multi-diameter shaft is set on the first slide rail and the second slide rail, when first sliding track mechanism and second
When sliding track mechanism is in contraction state, the multi-diameter shaft is set on the first slide rail, the second slide rail and the 3rd slide rail.
13. extension type unmanned plane according to claim 12, it is characterised in that the top cross section chi of the multi-diameter shaft
It is very little to be more than lower cross section size, the is respectively arranged at two ends with away from the second slide rail and close to the second slide rail on first slide rail
On one connecting hole and the second connecting hole, second slide rail the 3rd connecting hole, the described 3rd are provided with close to one end of the first slide rail
The 4th connecting hole is provided with close to one end of the second slide rail on slide rail, when first sliding track mechanism and the second sliding track mechanism are in deploying
During state, the top of the multi-diameter shaft is set on the second connecting hole and the 3rd connecting hole, when first sliding track mechanism and
When two sliding track mechanisms are in contraction state, the top of the multi-diameter shaft is set on the first connecting hole and the 3rd connecting hole, the rank
The bottom of terraced axle is set on the 4th connecting hole.
14. extension type unmanned plane according to claim 13, it is characterised in that second stop mechanism be arranged at
First stop mechanism is in the position of 90 degree of angles, and second stop mechanism includes second spring and bearing pin, the second spring
Bearing pin one end is installed on, the bearing pin other end is provided with the 3rd inclined-plane, second slide rail close to the side of the first slide rail and leaned on
One end on one end of nearly 3rd slide rail and the 3rd slide rail close to the second slide rail is respectively equipped with the 5th connecting hole and the 6th connecting hole,
When second sliding track mechanism deploys, the bearing pin passes through the 5th connecting hole and the 6th connecting hole, when the first slide rail machine
When structure and the contraction of the second sliding track mechanism, first slide rail is slided along the second slide rail surface and is against on the 3rd inclined-plane, makes the second cunning
Rail is relative with the 3rd slide rail to be slided.
15. extension type unmanned plane according to claim 14, it is characterised in that also include：Unlocking mechanism：It is installed on
On one slide rail, for the first sliding track mechanism to be released into its steady status in deployed condition or contraction state.
16. extension type unmanned plane according to claim 15, it is characterised in that the unlocking mechanism includes base plate, institute
State and elongated hole is provided with base plate, projection, the installation that the base plate can be moved left and right by elongated hole are provided with first slide rail
In on projection, the side front and rear portions on the base plate close to the second slide rail are arranged between two push rods, two push rods
Base plate on be provided with two the first pushing blocks, two first pushing blocks close to the second slide rail side be provided with and the first inclined-plane
Position, corresponding 4th inclined-plane of angle, the suspension end of two push rods are respectively equipped with the second sliding block, two second sliding blocks
The upper side close to the second slide rail is provided with the 5th inclined-plane corresponding with two the second incline positions, angle.
17. extension type unmanned plane according to claim 7, it is characterised in that the auxiliary sliding track mechanism is provided with
In the stop mechanism of steady status when the first sliding track mechanism, the expansion of the second sliding track mechanism or contraction state.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621321953.9U CN206318011U (en) | 2016-12-05 | 2016-12-05 | Extension type unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621321953.9U CN206318011U (en) | 2016-12-05 | 2016-12-05 | Extension type unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206318011U true CN206318011U (en) | 2017-07-11 |
Family
ID=59264815
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621321953.9U Withdrawn - After Issue CN206318011U (en) | 2016-12-05 | 2016-12-05 | Extension type unmanned plane |
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| Country | Link |
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| CN (1) | CN206318011U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106585987A (en) * | 2016-12-31 | 2017-04-26 | 歌尔科技有限公司 | Portable foldable unmanned aerial vehicle |
| CN107054622A (en) * | 2016-12-05 | 2017-08-18 | 普宙飞行器科技（深圳）有限公司 | Extension type unmanned plane |
-
2016
- 2016-12-05 CN CN201621321953.9U patent/CN206318011U/en not_active Withdrawn - After Issue
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107054622A (en) * | 2016-12-05 | 2017-08-18 | 普宙飞行器科技（深圳）有限公司 | Extension type unmanned plane |
| WO2018103641A1 (en) * | 2016-12-05 | 2018-06-14 | 普宙飞行器科技（深圳）有限公司 | Retractable drone |
| CN107054622B (en) * | 2016-12-05 | 2023-12-05 | 普宙科技有限公司 | Telescopic unmanned aerial vehicle |
| CN106585987A (en) * | 2016-12-31 | 2017-04-26 | 歌尔科技有限公司 | Portable foldable unmanned aerial vehicle |
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Address after: 430070 North of Floor 3, Building 2, No. 5, Huanglongshan South Road, Fozuling Street, Donghu New Technology Development Zone, Wuhan, Hubei Province (Wuhan Area of Free Trade Zone) Patentee after: Puzhou Technology Co.,Ltd. Address before: 518066 Room 201, building A, No. 1, Qian Wan Road, Qianhai Shenzhen Hong Kong cooperation zone, Shenzhen, Guangdong (Shenzhen Qianhai business secretary Co., Ltd.) Patentee before: Puzhou Technology (Shenzhen) Co.,Ltd. |
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Granted publication date: 20170711 Effective date of abandoning: 20231205 |
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Granted publication date: 20170711 Effective date of abandoning: 20231205 |