CN205738049U - Multi-functional unmanned plane rack kit - Google Patents
Multi-functional unmanned plane rack kit Download PDFInfo
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- CN205738049U CN205738049U CN201620680620.9U CN201620680620U CN205738049U CN 205738049 U CN205738049 U CN 205738049U CN 201620680620 U CN201620680620 U CN 201620680620U CN 205738049 U CN205738049 U CN 205738049U
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Abstract
Multi-functional unmanned plane rack kit, it is characterized in that, including the first frame, the second frame and connecting rod, described first frame includes the first fuselage, the first horn being connected to described first fuselage and is connected to the first undercarriage of described first fuselage, and described first fuselage is provided with first connecting rod connecting portion；Described second frame includes the second fuselage and is connected to the second horn of described second fuselage, and described second fuselage is provided with second connecting rod connecting portion；It is mounted on propeller on described first horn end and described second horn end；Described first frame includes that the first horn described at least two, described second frame include the second horn described at least two；First connection end of described connecting rod is fixedly installed in described first connecting rod connecting portion, second connection end of described connecting rod is fixedly installed in described second connecting rod connecting portion, described first frame and described second frame and is relatively fixed by described connecting rod and is combined into combined rack.
Description
Technical field
This utility model relates to mechanical field, particularly to a kind of multi-functional unmanned plane rack kit.
Background technology
At present, unmanned plane is usually integrated fixed structure, the most first determines target load weight, target load body
Long-pending, make after designing the parameters such as unmanned plane type, the number of axle and bar length.After the unmanned plane frame molding of prior art,
Bay form can not arbitrarily be changed, and accordingly, applicable load weight scope, applicable load volume range are also can not
Expanding, three rotors, four rotors are applicable to the work that load is little, and the little flying power of power consumption is strong, and six rotors, eight rotors are applicable to
The work that load is big, power consumption is big and flying power is not strong, and function is the most single；It addition, can the big unmanned plane of negative load weight
The generally number of axle is many, drives motor to support more propeller works during unmanned plane work, and such unmanned plane is used for load capacity
Less load operation efficiency is low.
Summary of the invention
In view of this, it is necessary to provide a kind of multi-functional unmanned plane rack kit, i.e. a tractor serves several purposes frame, according to different
Job task requires to use and assembles different frames.
This utility model embodiment provide a kind of multi-functional unmanned plane rack kit, including the first frame, the second frame and
Connecting rod, described first frame includes the first fuselage, the first horn being connected to described first fuselage and is connected to described first
First undercarriage of fuselage, described first fuselage is provided with first connecting rod connecting portion；Described second frame includes the second fuselage
Be connected to the second horn of described second fuselage, described second fuselage is provided with second connecting rod connecting portion；Described first machine
It is mounted on motor cabinet on arm end and described second horn end, described motor cabinet is provided with motor, described motor is pacified
Equipped with propeller；Described first frame includes that the first horn described at least two, described second frame include described at least two
Second horn；First connection end of described connecting rod is fixedly installed in described first connecting rod connecting portion, the second connection of described connecting rod
End is fixedly installed in described second connecting rod connecting portion, described first frame and described second frame and is relatively fixed by described connecting rod
And it is combined into combined rack.
It is also preferred that the left described first fuselage includes the first cover plate and the first fixed plate being relatively fixed setting up and down, described
One fixed plate includes the first connecting portion stationary plane towards described first cover plate and the first undercarriage back to described first cover plate
Stationary plane, described first connecting rod connecting portion is arranged at described first connecting portion stationary plane, on described first connecting portion stationary plane also
Being provided with the first pipe box, the first expansion position c-type button, the first folding position c-type button, described first horn is installed on described first pipe box
In, described first pipe box is movably connected on described first fixed plate and decided at the higher level but not officially announced in a planar range together with described first horn
Point rotates, and when described first horn moves to the expansion position of described first horn, described first horn enters described first to launch
The position opening of c-type button is also fixed on described first and launches in the c-type button of position, and described first horn moves to the folding of described first horn
During folded position, described first horn enters the opening of described first folding position c-type button and is fixed on described first folding position c-type button
In, the opening of described first expansion position c-type button is relative with the opening of described first folding position c-type button；Described first cover plate and institute
Stating and connect by the first support column is fixing between the first fixed plate, described first undercarriage is fixedly installed in described first undercarriage
Stationary plane；
Described second fuselage includes the second cover plate and the second fixed plate being relatively fixed setting up and down, described second fixed plate
Including the second connecting portion stationary plane towards described second cover plate, described second connecting rod connecting portion is arranged at described second connecting portion
On stationary plane, described second connecting portion stationary plane is additionally provided with the second pipe box, the second expansion position c-type button, the second folding position c-type
Button, described second horn is installed in described second pipe box, described second pipe box be movably connected on described second fixed plate and with
Described second horn Fixed-point Motion of A in two planar range, when described second horn moves to the expansion position of described second horn,
Described second horn enters the described second opening launching position c-type button and is fixed on described second and launches in the c-type button of position, and described the
When two horns move to the folding position of described second horn, described second horn enters the opening of described second folding position c-type button
And be fixed in described second folding position c-type button, described second launches the opening of position c-type button and described second folding position c-type button
Opening relative；It is connected by the second support column is fixing between described second cover plate with described second fixed plate.
It is also preferred that the left be provided with in described first fixed plate, the first pi/2 launches position c-type button installing hole, position C is launched in the one 2 π/3
Installing hole buckled by type, the one 5 π/6 are launched position c-type and buckled installing hole；
Described first launches position c-type button is installed on described first pi/2 when launching position c-type button installing hole, is fixed on described the
One angle launched between described first horn and the described connecting rod that position c-type is smashed is pi/2；
Described first launches position c-type button is installed on described one 2 π/3 when launching position c-type button installing hole, is fixed on described the
One angle launched between described first horn and the described connecting rod that position c-type is smashed is 2 π/3；
Described first launches position c-type button is installed on described one 5 π/6 when launching position c-type button installing hole, is fixed on described the
One angle launched between described first horn and the described connecting rod that position c-type is smashed is 5 π/6；
It is provided with the second pi/2 in described second fixed plate and launches position c-type button installing hole, the 2nd 2 expansion position, π/3 c-type button peace
Position c-type button installing hole is launched in dress hole, the 2nd 5 π/6；
Described second launches position c-type button is installed on described second pi/2 when launching position c-type button installing hole, is fixed on described the
Two angles launched between described second horn and the described connecting rod that position c-type is smashed are pi/2；
Described second launches position c-type button is installed on described 2nd 2 π/3 when launching position c-type button installing hole, is fixed on described the
Two angles launched between described second horn and the described connecting rod that position c-type is smashed are 2 π/3；
Described second launches position c-type button is installed on described 2nd 5 π/6 when launching position c-type button installing hole, is fixed on described the
Two angles launched between described second horn and the described connecting rod that position c-type is smashed are 5 π/6.
It is also preferred that the left described first frame includes that two described first horns, two described first horns are both secured to each
Described first launch position c-type and smash and symmetrical relative to described connecting rod place straight line；Described second frame includes described in two
Second horn, two described second horns are both secured to respective described second expansion position c-type and smash and relative to described connecting rod
Place straight line is symmetrical；The folder between angle and described second horn and described connecting rod between described first horn and described connecting rod
Angle is identical；Described first frame and described second frame in combination become one or four axle combined racks；
One described motor is installed on the described motor cabinet on described first horn；Or, on described first horn
Be provided with on described motor cabinet about a pair back to arrange described motor, each described motor is mounted on a described spiral shell
Rotation oar；It is provided with on described second horn and the described first equal number of described motor of horn and described propeller.
It is also preferred that the left two described first horns all move to respective described first folding position c-type and smash, two described
Two horns all move to respective described second folding position c-type and smash, and relative to described connecting rod, described first horn is positioned at described
Inside second horn.
It is also preferred that the left described second frame also includes the second undercarriage being connected to described second fuselage, described second fixes
Plate also includes the second undercarriage stationary plane being oppositely arranged with described second connecting portion stationary plane, the fixing peace of described second undercarriage
It is loaded on described second undercarriage stationary plane.
It is also preferred that the left described multi-functional unmanned plane rack kit also includes that the 3rd frame, described 3rd frame include the 3rd machine
Body, be connected to the 3rd horn of described 3rd fuselage, the 3rd cover plate that described 3rd fuselage includes being relatively fixed setting up and down and
3rd fixed plate, described 3rd fixed plate is provided with third connecting rod fixed part, described connecting rod is positioned at described first and connects end
And described second the position connected between end be fixedly mounted on described third connecting rod fixed part；The end of described 3rd horn is installed
There is described propeller；Described 3rd frame includes that two described 3rd horns, two described 3rd horns are connected to the described 3rd
Fixed plate, two described 3rd horns are symmetrical arranged and are perpendicular to described connecting rod relative to described connecting rod, two described 3rd machines
Arm is respectively positioned in described first horn free cheek.
It is also preferred that the left described first frame includes two described first horns and two described second horns, two described
One horn is symmetrical relative to described connecting rod place straight line and is both secured to respective described first and launches position c-type and smash, and described the
One launches position c-type button is installed on described one 2 π/3 and launches in the c-type button installing hole of position, make described first horn and described connecting rod it
Between angle be 2 π/3；Two described second horns relative to described connecting rod place straight line symmetry and are both secured to respective institute
Stating the second expansion position c-type to smash, described second launches position c-type button is installed in described 2nd 2 expansion position, π/3 c-type button installing hole,
Making the angle between described second horn and described connecting rod is 2 π/3；With said two the 3rd horn place straight line and described connecting rod
Centered by the intersection point of place straight line, in described first frame, described second frame, described 3rd frame each described propeller with
Described center is equidistant, and described first frame, described second frame, described 3rd frame in combination become six axle combined racks；Described
One described motor is installed on the described motor cabinet on the first horn；Or, on the described motor cabinet on described first horn
Be provided with about a pair back to arrange described motor, each described motor is mounted on a described propeller；Described
It is provided with on two horns, described 3rd horn and the described first equal number of described motor of horn and described propeller.
It is also preferred that the left described first frame includes two described first horns, two described first horns are relative to described company
Bar place straight line is symmetrical and is both secured to respective described first and launches position c-type and smash；Described multi-functional unmanned plane rack kit
Also including foot piece, remove described connecting rod, described foot piece is fixedly installed to the described first connecting rod connecting portion of described first frame, institute
State and described motor cabinet is installed on the end of foot piece, described motor cabinet is provided with described motor, described motor is installed
State propeller, equidistant between each described propeller in described first frame and described foot piece, described first frame and described
Foot piece is combined into three axle combined racks；
Described first launches position c-type button is installed in described first pi/2 expansion position c-type button installing hole, makes described first machine
Angle between arm and described connecting rod is pi/2；Or,
Described first launches position c-type button is installed in described one 2 expansion position, π/3 c-type button installing hole, makes described first machine
Angle between arm and described connecting rod is 2 π/3；Or,
Described first launches position c-type button is installed in described one 5 expansion position, π/6 c-type button installing hole, makes described first machine
Angle between arm and described connecting rod is 5 π/6；
One described motor is installed on the described motor cabinet on described foot piece, described first horn is provided with described
The equal number of described motor of foot piece and described propeller；Or,
About a pair it is provided with back to the described motor arranged, each described motor on described motor cabinet on described foot piece
On be mounted on a described propeller, described first horn is provided with described motor equal number of with described foot piece and institute
State propeller；Or,
About a pair it is provided with back to the described motor arranged, each described motor on described motor cabinet on described foot piece
On be mounted on a described propeller, described first horn is provided with a described motor.
It is also preferred that the left described first horn, a length of 24cm of described second horn, the size of described propeller is 9 cun；Or
Person, described first horn, a length of 34cm of described second horn, the size of described propeller is 13 cun；Or, described first
Horn, a length of 41cm of described second horn, the size of described propeller is 16 cun.
The multi-functional unmanned plane rack kit that this utility model embodiment provides independent assortment can go out the nothing that the number of axle is different
Man-machine frame, can be adjusted flexibly be suitable for load weight scope, applicable load volume range, has various unmanned plane type concurrently
Advantage, easy to use, folding portable portable.
Accompanying drawing explanation
In order to be illustrated more clearly that the technical scheme of this utility model embodiment, will use required in embodiment below
Accompanying drawing be briefly described, it should be apparent that, the accompanying drawing in describing below is some embodiments of this utility model embodiment,
For those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to obtain according to these accompanying drawings
Other accompanying drawing.
Accompanying drawing 1 is four axle combined rack the first structural representations of the multi-functional unmanned plane rack kit of a better embodiment
Figure.
Accompanying drawing 2 is four axle combined rack the second structural representations of the multi-functional unmanned plane rack kit of a better embodiment
Figure.
Accompanying drawing 3 is four axle combined rack the 3rd structural representations of the multi-functional unmanned plane rack kit of a better embodiment
Figure.
Accompanying drawing 4 is four axle combined rack the 4th structural representations of the multi-functional unmanned plane rack kit of a better embodiment
Figure.
Accompanying drawing 5 is four axle combined rack the 5th structural representations of the multi-functional unmanned plane rack kit of a better embodiment
Figure.
Accompanying drawing 6 is the first fixed plate schematic diagram of the multi-functional unmanned plane rack kit of a better embodiment.
Accompanying drawing 7 is six axle combined rack the first structural representations of the multi-functional unmanned plane rack kit of a better embodiment
Figure.
Accompanying drawing 8 is six axle combined rack the second structural representations of the multi-functional unmanned plane rack kit of a better embodiment
Figure.
Accompanying drawing 9 is six axle combined rack the 3rd structural representations of the multi-functional unmanned plane rack kit of a better embodiment
Figure.
Accompanying drawing 10 is that six axle combined rack the 4th structures of the multi-functional unmanned plane rack kit of a better embodiment are shown
It is intended to.
Accompanying drawing 11 is that three axle combined rack the first structures of the multi-functional unmanned plane rack kit of a better embodiment are shown
It is intended to.
Accompanying drawing 12 is that three axle combined rack the second structures of the multi-functional unmanned plane rack kit of a better embodiment are shown
It is intended to.
Accompanying drawing 13 is that three axle combined rack the 3rd structures of the multi-functional unmanned plane rack kit of a better embodiment are shown
It is intended to.
Accompanying drawing 14 is that four axle combined racks of the multi-functional unmanned plane rack kit of a better embodiment fold schematic diagram.
Accompanying drawing 15 is that three axle combined racks the first foldings of the multi-functional unmanned plane rack kit of a better embodiment are shown
It is intended to.
Accompanying drawing 16 is that three axle combined racks the second foldings of the multi-functional unmanned plane rack kit of a better embodiment are shown
It is intended to.
In figure: first frame the 1, second frame 2, connecting rod 3, propeller the 4, the 3rd frame the 5, first fuselage the 11, first horn
12, the first undercarriage 13, first connecting rod connecting portion the 14, first pipe box 15, first launch c-type button the 16, first folding position, position c-type button
17, first cover plate the 111, first fixed plate the 112, second fuselage the 21, second horn the 22, second undercarriage 23, second connecting rod connect
Portion's the 24, second pipe box 25, second launches c-type button the 26, second folding position, position c-type button the 27, second cover plate the 211, second fixed plate
212, the first connection end 31 of connecting rod 3, connecting rod 3 the second connection end the 32, the 3rd fuselage the 51, the 3rd horn 52, third connecting rod solid
Determine portion the 53, the 3rd cover plate the 511, the 3rd fixed plate 512, foot piece 6, motor cabinet the 7, first support column the 8, first pi/2 launch position c-type and buckle
Installing hole the 91, the 1st π/3 are launched c-type button installing hole the 92, the 1st π/6, position and are launched position c-type button installing hole 93.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is a part of embodiment of this utility model rather than whole enforcement
Example.Based on the embodiment in this utility model, those of ordinary skill in the art are obtained under not making creative work premise
The every other embodiment obtained, broadly falls into the scope of this utility model protection.
This utility model embodiment is intended to provide the unmanned plane frame of a kind of combined use, by multi-functional unmanned plane machine
Frame external member, it is convenient to be combined into the unmanned plane frame of the different number of axle.
As shown in Figures 1 to 5, this utility model embodiment provides a kind of multi-functional unmanned plane rack kit, it may include the
One frame the 1, second frame 2 and connecting rod 3, wherein, the first frame 1 can be as the mainframe of multi-functional unmanned plane rack kit, its
Using separately as a unmanned plane frame after can installing a foot piece, the second frame 2 can be as multi-functional unmanned plane frame set
The slave frame of part, is used for expanding the number of axle of mainframe, changing rack construction, by the interconnection function of connecting rod 3, by two kinds of frame groups
It is combined together and becomes a kind of new bay form.
In this utility model embodiment, the first frame 1 can include the first fuselage 11, be connected to the first machine of the first fuselage 11
Arm 12 and be connected to the first undercarriage 13 of the first fuselage 11, and, the first fuselage 11 is provided with first connecting rod connecting portion
14, the first horn 12 end is provided with motor cabinet 7, and motor cabinet 7 is provided with the motor for driving propeller, and this motor is pacified
Equipped with propeller 4；Second frame 2 includes the second fuselage 21 and is connected to the second horn 22 of the second fuselage 21, and, the second machine
Being provided with second connecting rod connecting portion 24 on body 21, the second horn 22 end is provided with motor cabinet 7, motor cabinet 7 is provided with for
Drive the motor of propeller, this motor is provided with propeller 4；First connection end 31 of connecting rod 3 is fixedly installed in first connecting rod
Connecting portion 14, the second connection end 32 of connecting rod 3 is fixedly installed in second connecting rod connecting portion 24, and the first frame 1 and the second frame 2 are led to
Cross connecting rod 3 be relatively fixed and be combined into combined rack.Wherein, the first frame 1 can go up and can be provided with at least two the first horn
12, the second frame 2 can be provided with at least two the second horn 22, by combinations thereof mode, the first frame 1 can be carried out shape
Shape improves.
Concrete, as shown in Figures 2 and 3, the first fuselage 11 can include the first cover plate 111 He being relatively fixed setting up and down
First fixed plate 112, wherein, the first fixed plate 112 includes towards the first connecting portion stationary plane of the first cover plate 111 with back to
First undercarriage stationary plane of one cover plate 111, first connecting rod connecting portion 14 is arranged on the first connecting portion stationary plane, and first connects
It is additionally provided with the first pipe box 15, first on portion's stationary plane and launches position c-type button 16 and the first folding position c-type button 17, the first horn 12
Being installed in the first pipe box 15, the first pipe box 15 is movably connected on the first fixed plate 112 and flat together with the first horn 12
Fixed-point Motion of A in the range of face, when the first horn 12 moves to the expansion position of the first horn 12, the first horn 12 enters the first expansion
The position opening of c-type button 16 is also fixed in the first expansion position c-type button 16, and the first horn 12 moves to the folding position of the first horn 12
Time, the first horn 12 enters the opening of the first folding position c-type button 17 and is fixed in the first folding position c-type button 17, and first launches
The opening of position c-type button 16 and the opening of the first folding position c-type button 17 are relative；Lead between first cover plate 111 and the first fixed plate 112
Crossing the first fixing connection of support column 8, the first undercarriage 13 is fixedly installed in the first undercarriage stationary plane.
When being positioned at expansion position due to the first horn 12, it is to carry out working flight for unmanned plane, therefore first launches position c-type button
16 can use double C to detain, to be fastened by the first horn 12；When first horn 12 is positioned at folding position, unmanned plane is in inoperative
State, therefore the first folding position c-type button 17 can use single C to detain, and plays general fixation.
As shown in Figures 2 and 3, the second fuselage 21 can include that the second cover plate 211 and second being relatively fixed setting up and down is solid
Determining plate 212, wherein, the second fixed plate 212 includes the second connecting portion stationary plane towards the second cover plate 211, and second connecting rod connects
Portion 24 is arranged on the second connecting portion stationary plane, the second connecting portion stationary plane is additionally provided with the second pipe box 25, second and launches position C
Type buckle 26 and second folding position c-type buckle 27, the second horn 22 is installed in the second pipe box 25, and the second pipe box 25 is movably connected on
Two fixed plates 212 and together with the second horn 22 in a planar range Fixed-point Motion of A, the second horn 22 moves to the second horn
22 expansion position time, the second horn 22 enters the opening of the second expansion position c-type button 26 and is fixed on the second expansion position c-type button 26
In, when the second horn 22 moves to the folding position of the second horn 22, the second horn 22 enters the opening of the second folding position c-type button 17
And be fixed in the second folding position c-type button 27, second launches opening and the opening of the second folding position c-type button 27 of position c-type button 26
Relatively；It is connected by the second support column is fixing between second cover plate 211 with the second fixed plate 212, the second fixing peace of undercarriage 23
It is loaded on the second undercarriage stationary plane.
When being positioned at expansion position due to the second horn 12, it is to carry out working flight for unmanned plane, therefore second launches position c-type button
16 can use double C to detain, to be fastened by the second horn 12；When second horn 12 is positioned at folding position, unmanned plane is in inoperative
State, therefore the second folding position c-type button 17 can use single C to detain, and plays general fixation.
As arranging at least two the first horn 12 in the first frame 1 of mainframe, and correspondingly, the first connecting portion
The first spacing active connection part of horn 15 with the first horn 12 equal number it is provided with on stationary plane.When setting in the first frame 1
When being equipped with two the first horns 12, by the multi-functional unmanned plane rack kit of this utility model embodiment, two can be combined into
Axle frame, three axle frames etc., when being provided with three the first horns 12 in the first frame 1, can be combined into three axle frames, four
Axle frame etc., determines horn spacing according to horn number, and adaptively adjusts the angle of each horn.
In first frame 1 of this utility model embodiment, launch position c-type button 16 by the first pipe box 15 and first, can be by
First horn 12 is fixed to different angles, as shown in Figure 6, the first fixed plate 112 can be provided with the first pi/2 and launch position c-type
Button installing hole the 91, the 1st π/3 are launched c-type button installing hole the 92, the 1st π/6, position and are launched position c-type button installing hole 93, wherein, such as Fig. 4
Shown in, when the first expansion position c-type button 16 is installed on the first pi/2 expansion position c-type button installing hole 91, it is fixed on the first expansion position c-type
The angle between the first horn 12 and connecting rod 3 in button 16 is pi/2；As shown in Figure 10, first launches position c-type button 16 and is installed on the
When position c-type button installing hole 92 is launched in one 2 π/3, it is fixed between the first horn 12 and the connecting rod 3 in the first expansion position c-type button 16
Angle be 2 π/3；When first expansion position c-type button 16 is installed on the one 5 π/6 expansion position c-type button installing hole 93, it is fixed on first
The angle launched between the first horn 12 and the connecting rod 3 in position c-type button 16 is 5 π/6.When being provided with at least two in the first frame 1
During individual first horn 12, correspondingly can be configured to install the first pi/2 of the first expansion position c-type button 16 for each first horn 12
Launch c-type button installing hole the 91, the 1st π/3, position and launch expansion position, c-type button installing hole the 92, the 1st π/6, position c-type button installing hole 93.
In second frame 2 of this utility model embodiment, launch position c-type button 26 by the second pipe box 25 and second, can be by
Second horn 22 is fixed to different angles, the second fixed plate is provided with the second pi/2 launch position c-type button installing hole, the 2nd 2 π/
3 launch position c-type button installing holes and the 2nd 5 π/6 launches position c-type button installing hole, and wherein, second launches position c-type button 26 is installed on the
When two pi/2s launch position c-type button installing hole, the folder being fixed between the second horn 22 and the connecting rod 3 in the second expansion position c-type button 26
Angle is pi/2；When second expansion position c-type button 26 is installed on the 2nd 2 π/3 expansion position c-type button installing hole, it is fixed on the second expansion position C
The angle that type is buckled between the second horn 22 and connecting rod 3 in 26 is 2 π/3；Second launches position c-type button 26 is installed on the 2nd 5 π/6 exhibition
During open position c-type button installing hole, the angle being fixed between the second horn 22 and the connecting rod 3 in the second expansion position c-type button 26 be 5 π/
6.When being provided with at least two the second horn 22 in the second frame 2, correspondingly peace can be configured to for each second horn 22
The second pi/2 filling the second expansion position c-type button 26 launches position c-type button installing hole, position c-type button installing hole and second is launched in the 2nd 2 π/3
Position c-type button installing hole is launched in 5 π/6.
As it is shown in figure 1, when the first frame 1 includes that two first horn the 12, second frames 2 include two the second horns 22
Time, the first frame 1 and the second frame 2 can be combined into four axle combined racks, wherein, two the first horn 12 phases by connecting rod 3
Symmetrical for connecting rod 3 place straight line, the second frame 2 includes two the second horns 22, and two the second horns 22 are relative to connecting rod 3 institute
Symmetrical at straight line, the angle between the first horn 12 and connecting rod 3 can be pi/2,2 π/3,5 π/6, the second horn 22 and connecting rod 3 it
Between angle equal to angle between the first horn 12 and connecting rod 3.It addition, the motor cabinet 7 of the first horn 12 can be provided with one
Motor or upper and lower a pair motor back to setting, each motor is mounted on a propeller 4, the second horn 22 can set
It is equipped with and equal number of motor and propeller 4 on the first horn 12.Can group please with reference to four axle frame institutes shown in form 1
The type (depending on wherein, type is according to motor number and the number of axle) become:
Form 1
Wherein, the type shown in Fig. 1 to Fig. 5 is H4 type, each type in form 1, first horn the 12, second horn
The length of 22, and the size of propeller 4 is all optional, such as, first horn the 12, second horn 22 selects 24cm length,
Propeller 4 selects 9 cun；Or, first horn the 12, second horn 22 selects 34cm length, propeller 4 to select 13 cun；Or, the
One horn the 12, second horn 22 selects 41cm length, propeller 4 to select 16 cun.
As it is shown in figure 5, in this utility model embodiment, the second frame 2 can also is that a kind of slave frame with undercarriage,
Such as, the second fixed plate 212 also includes the second undercarriage 23 stationary plane being oppositely arranged with the second connecting portion stationary plane, second
The frame 23 that falls is fixedly installed in the second undercarriage stationary plane.In second frame 2, nothing can preferably be supported by the second undercarriage 23 of configuration
Man-machine stably rise and fall.
Four axle combined racks are collapsible, particularly as follows: two the first horns 12 all move to respective first folding position c-type button
In 17, two the second horns 22 all move in respective second folding position c-type button 27, relative to connecting rod 3, the first horn 12
In the inner side of the second horn 22, the form after four axle combined racks foldings is as shown in figure 14.
As shown in Figure 7 to 10, the multi-functional unmanned plane rack kit of this utility model embodiment can also wrap further
Including the 3rd frame 5, the 3rd frame 5 is for a kind of that be installed between the first frame 1 and the second frame 2, for expanding unmanned plane machine
The middle framework of the frame number of axle, as it can be seen, wherein the 3rd frame 5 includes the 3rd fuselage 51, is connected to the 3rd of the 3rd fuselage 51
Horn 52, the 3rd fuselage 51 includes the 3rd cover plate 511 and the 3rd fixed plate 512 being relatively fixed setting up and down, the 3rd fixed plate
It is provided with third connecting rod fixed part 53 on 512, connecting rod 3 connects the position between end 31 and the second connection end 32 first solid
Dingan County is contained in third connecting rod fixed part 53；3rd horn 52 end is provided with propeller 4；3rd frame 5 includes two the 3rd machines
Arm 52, two the 3rd horns 52 are connected to the 3rd fixed plate 512, and two the 3rd horns 52 are symmetrical arranged relative to connecting rod 3 and hang down
Straight in connecting rod 3, two the 3rd horns 52 are respectively positioned in the first horn 12 free cheek.
By adding the 3rd frame 5 between the first frame 1 and the second frame 2, six axle combined racks be can be combined out, this
Time, two the first horns 12 are symmetrical relative to connecting rod 3 place straight line and be both secured to respective first and launch position c-type and buckle in 16,
First launches position c-type button 16 is installed in the one 2 expansion position, π/3 c-type button installing hole 92, makes between the first horn 12 and connecting rod 3
Angle be 2 π/3；Two the second horns 22 relative to connecting rod 3 place straight line symmetry and are both secured to respective second expansion position
In c-type button 26, second launches position c-type button 26 is installed in the 2nd 2 expansion position, π/3 c-type button installing hole, makes the second horn 22 and connects
Angle between bar 3 is 2 π/3；Centered by two the 3rd horn 52 place straight lines intersection point with connecting rod 3 place straight line, first
In frame the 1, second frame the 2, the 3rd frame 5, each propeller 4 is equidistant with center, so that it is determined that the length of the 3rd horn 52, with
Adapt to the requirement of six axle combined racks, finally, first frame the 1, second frame the 2, the 3rd frame 5 is combined into six axle unit mahines
Frame.Wherein, the motor cabinet 7 of the first horn 12 can be provided with one or about a pair motor back to setting, on each motor
It is mounted on a propeller 4；It is provided with and the first equal number of motor of horn 12 on second horn the 22, the 3rd horn 52
With propeller 4.
In six axle combined racks, the length of first horn the 12, second horn 22, and the size of propeller 4 is all optional
, such as, first horn the 12, second horn 22 selects 24cm length, propeller 4 to select 9 cun；Or, the first horn 12, second
Horn 22 selects 34cm length, propeller 4 to select 13 cun；Or, first horn the 12, second horn 22 selects 41cm length, spiral shell
Rotation oar 4 selects 16 cun.It addition, the length of the 3rd frame 5 should regard length and the horn interval of first horn the 12, second horn 22
Depending on angle.
As shown in Figure 11 to Figure 13, in this utility model embodiment, multi-functional unmanned plane rack kit also includes foot piece 6,
Motor cabinet 7 is installed on the end of foot piece 6, motor cabinet 7 is provided with the motor for driving propeller, this motor is provided with
Propeller 4, unloads lower link 3, and after foot piece 6 is arranged on the first connecting rod connecting portion 14 of the first frame 1, the first frame 1 can be independent
Becoming a unmanned plane frame, now, the first frame 1 includes two the first horns 12, and two the first horns 12 are relative to foot piece 6
Place straight line is symmetrical and is both secured in respective first expansion position c-type button 16, the angle between the first horn 12 and foot piece 6
Can be pi/2,2 π/3,5 π/6.It addition, one or about a pair can be provided with on motor cabinet 7 on foot piece 6 back to arranging
Motor, the motor cabinet 7 of two the first horns 12 also can be provided with a motor or about a pair motor back to setting.Please
The type (depending on wherein, type is according to motor number and the number of axle) that can form with reference to three axle frames shown in form 1 in the lump:
Form 2
Wherein, type shown in Figure 11, Figure 12 is Y3 type, and type shown in Figure 13 is Y4 type, each type in form 2
In, the length of the first horn 12, and the size of propeller 4 is all optional, such as, the first horn 12 selects 24cm length,
Propeller 4 selects 9 cun；Or, the first horn 12 selects 34cm length, propeller 4 to select 13 cun；Or, the first horn 12 selects
41cm length, propeller 4 is used to select 16 cun.It addition, the length of foot piece 6 should regard length and the horn angular interval of the first horn 12
Depending on degree.
Y3 type three axle combined rack shown in Figure 11 is the frame schematic diagram with three propellers, and it is collapsible, folds
After form as shown in figure 14；Three axle combined racks shown in Figure 13 are the frame schematic diagram with four propellers, and it can be rolled over
Folded, the form after folding is as shown in figure 16.
The multi-functional unmanned plane rack kit that this utility model embodiment provides independent assortment can go out the nothing that the number of axle is different
Man-machine frame, by being combined into three axle combination types, four axle combination types, is applicable to the work that load is little, and power consumption is little continuous
Boat ability is strong；By being combined into six axle combination types, it is adaptable to the work that load is big.This utility model embodiment can be adjusted flexibly
Applicable load weight scope, applicable load volume range, have feature easy to use, easy to carry.
Claims (10)
1. a multi-functional unmanned plane rack kit, it is characterised in that include the first frame, the second frame and connecting rod, described
One frame includes the first fuselage, the first horn being connected to described first fuselage and is connected to the first of described first fuselage
Undercarriage, described first fuselage is provided with first connecting rod connecting portion；Described second frame includes the second fuselage and is connected to institute
State the second horn of the second fuselage, described second fuselage is provided with second connecting rod connecting portion；Described first horn end and institute
State and be mounted on motor cabinet on the second horn end, described motor cabinet is provided with motor, described motor is provided with propeller；
Described first frame includes that the first horn described at least two, described second frame include the second horn described at least two；Institute
The the first connection end stating connecting rod is fixedly installed in described first connecting rod connecting portion, and the second connection end of described connecting rod is fixedly installed in
Described second connecting rod connecting portion, described first frame and described second frame are relatively fixed by described connecting rod and are combined into group
Close frame.
Multi-functional unmanned plane rack kit the most as claimed in claim 1, it is characterised in that
Described first fuselage includes the first cover plate and the first fixed plate being relatively fixed setting up and down, and described first fixed plate includes
The first connecting portion stationary plane towards described first cover plate and the first undercarriage stationary plane back to described first cover plate, described
One link joint feature is arranged at described first connecting portion stationary plane, and described first connecting portion stationary plane is additionally provided with the first pipe
Set, the first expansion position c-type button, the first folding position c-type button, described first horn is installed in described first pipe box, and described first
Pipe box be movably connected on described first fixed plate and together with described first horn in a planar range Fixed-point Motion of A, described
When first horn moves to the expansion position of described first horn, described first horn enters described first and launches opening of position c-type button
Mouth is also fixed in described first expansion position c-type button, when described first horn moves to the folding position of described first horn, described
First horn enters the opening of described first folding position c-type button and is fixed in described first folding position c-type button, described first exhibition
The opening of open position c-type button is relative with the opening of described first folding position c-type button；Described first cover plate and described first fixed plate it
Between connect by the first support column is fixing, described first undercarriage is fixedly installed in described first undercarriage stationary plane；
Described second fuselage includes the second cover plate and the second fixed plate being relatively fixed setting up and down, and described second fixed plate includes
Towards the second connecting portion stationary plane of described second cover plate, described second connecting rod connecting portion is arranged at described second connecting portion and fixes
On face, described second connecting portion stationary plane is additionally provided with the second pipe box, the second expansion position c-type button, the second folding position c-type button,
Described second horn is installed in described second pipe box, described second pipe box be movably connected on described second fixed plate and with institute
State the second horn Fixed-point Motion of A in two planar range, when described second horn moves to the expansion position of described second horn, institute
State the second horn enter the described second opening launching position c-type button and be fixed in described second expansion position c-type button, described second
When horn moves to the folding position of described second horn, described second horn enters the opening of described second folding position c-type button also
Being fixed in described second folding position c-type button, described second launches the opening of position c-type button and described second folding position c-type button
Opening is relative；It is connected by the second support column is fixing between described second cover plate with described second fixed plate.
Multi-functional unmanned plane rack kit the most as claimed in claim 2, it is characterised in that be provided with in described first fixed plate
First pi/2 launches position c-type button installing hole, position c-type button installing hole is launched in the one 2 π/3, position c-type button installing hole is launched in the one 5 π/6；
When described first expansion position c-type button is installed on described first pi/2 expansion position c-type button installing hole, it is fixed on described first exhibition
Angle between described first horn and described connecting rod that open position c-type is smashed is pi/2；
When described first expansion position c-type button is installed on described one 2 π/3 expansion position c-type button installing hole, it is fixed on described first exhibition
Angle between described first horn and described connecting rod that open position c-type is smashed is 2 π/3；
When described first expansion position c-type button is installed on described one 5 π/6 expansion position c-type button installing hole, it is fixed on described first exhibition
Angle between described first horn and described connecting rod that open position c-type is smashed is 5 π/6；
Be provided with in described second fixed plate that the second pi/2 launches position c-type button installing hole, position c-type button installing hole is launched in the 2nd 2 π/3,
Position c-type button installing hole is launched in 2nd 5 π/6；
When described second expansion position c-type button is installed on described second pi/2 expansion position c-type button installing hole, it is fixed on described second exhibition
Angle between described second horn and described connecting rod that open position c-type is smashed is pi/2；
When described second expansion position c-type button is installed on described 2nd 2 π/3 expansion position c-type button installing hole, it is fixed on described second exhibition
Angle between described second horn and described connecting rod that open position c-type is smashed is 2 π/3；
When described second expansion position c-type button is installed on described 2nd 5 π/6 expansion position c-type button installing hole, it is fixed on described second exhibition
Angle between described second horn and described connecting rod that open position c-type is smashed is 5 π/6.
Multi-functional unmanned plane rack kit the most as claimed in claim 2, it is characterised in that described first frame includes two institutes
Stating the first horn, two described first horns are both secured to respective described first expansion position c-type and smash and relative to described company
Bar place straight line is symmetrical；Described second frame includes that two described second horns, two described second horns are both secured to each
Described second launch position c-type and smash and symmetrical relative to described connecting rod place straight line；Described first horn and described connecting rod it
Between angle identical with the angle between described second horn and described connecting rod；Described first frame and described second frame in combination
Become one or four axle combined racks；
One described motor is installed on the described motor cabinet on described first horn；Or, described on described first horn
Be provided with on motor cabinet about a pair back to arrange described motor, each described motor is mounted on a described spiral
Oar；It is provided with on described second horn and the described first equal number of described motor of horn and described propeller.
Multi-functional unmanned plane rack kit the most as claimed in claim 4, it is characterised in that two described first horns all move
Smashing to respective described first folding position c-type, two described second horns all move to respective described second folding position c-type
Smashing, relative to described connecting rod, described first horn is positioned at inside described second horn.
Multi-functional unmanned plane rack kit the most as claimed in claim 2, it is characterised in that described second frame also includes connecting
In the second undercarriage of described second fuselage, described second fixed plate also includes being oppositely arranged with described second connecting portion stationary plane
The second undercarriage stationary plane, described second undercarriage is fixedly installed in described second undercarriage stationary plane.
Multi-functional unmanned plane rack kit the most as claimed in claim 3, it is characterised in that described multi-functional unmanned plane frame set
Part also includes that the 3rd frame, described 3rd frame include the 3rd fuselage, are connected to the 3rd horn of described 3rd fuselage, described
Three fuselages include the 3rd cover plate and the 3rd fixed plate being relatively fixed setting up and down, described 3rd fixed plate are provided with the 3rd even
Bar fixed part, described connecting rod is fixedly mounted on described at the described first position connected between end and described second connection end
Third connecting rod fixed part；The end of described 3rd horn is provided with described propeller；Described 3rd frame includes two described
Three horns, two described 3rd horns are connected to described 3rd fixed plate, and two described 3rd horns are relative to described connecting rod pair
Claiming arrange and be perpendicular to described connecting rod, two described 3rd horns are respectively positioned in described first horn free cheek.
Multi-functional unmanned plane rack kit the most as claimed in claim 7, it is characterised in that described first frame includes two institutes
Stating the first horn and two described second horns, two described first horns are symmetrical relative to described connecting rod place straight line and equal
Being fixed on respective described first expansion position c-type to smash, described first launches position c-type button is installed on described one 2 expansion position, π/3
In c-type button installing hole, making the angle between described first horn and described connecting rod is 2 π/3；Two described second horns relative to
Described connecting rod place straight line is symmetrical and is both secured to respective described second and launches position c-type and smash, and described second launches position c-type
Button is installed on described 2nd 2 π/3 to launch in the c-type button installing hole of position, and making the angle between described second horn and described connecting rod is 2
π/3；Centered by said two the 3rd horn place straight line intersection point with described connecting rod place straight line, described first frame, institute
State each described propeller in the second frame, described 3rd frame equidistant with described center, described first frame, described second machine
Frame, described 3rd frame in combination become six axle combined racks；One institute is installed on the described motor cabinet on described first horn
State motor；Or, the described motor cabinet on described first horn is provided with about a pair described motor back to setting, each
A described propeller it is mounted on described motor；It is provided with on described second horn, described 3rd horn and described
The one equal number of described motor of horn and described propeller.
Multi-functional unmanned plane rack kit the most as claimed in claim 3, it is characterised in that described first frame includes two institutes
Stating the first horn, two described first horns are symmetrical relative to described connecting rod place straight line and are both secured to respective described the
One launches position c-type smashs；Described multi-functional unmanned plane rack kit also includes foot piece, removes described connecting rod, and described foot piece is fixed
It is installed to the described first connecting rod connecting portion of described first frame, the end of described foot piece is provided with described motor cabinet, described
Described motor is installed on motor cabinet, described motor is provided with described propeller, each in described first frame and described foot piece
Equidistant between individual described propeller, described first frame and described foot piece are combined into three axle combined racks；
Described first launches position c-type button is installed on described first pi/2 and launches in the c-type button installing hole of position, make described first horn with
Angle between described connecting rod is pi/2；Or,
Described first launches position c-type button is installed on described one 2 π/3 and launches in the c-type button installing hole of position, make described first horn with
Angle between described connecting rod is 2 π/3；Or,
Described first launches position c-type button is installed on described one 5 π/6 and launches in the c-type button installing hole of position, make described first horn with
Angle between described connecting rod is 5 π/6；
One described motor is installed on the described motor cabinet on described foot piece, described first horn is provided with and described foot piece
Equal number of described motor and described propeller；Or,
About a pair described motor back to setting is installed, on the described motor cabinet on described foot piece on each described motor all
One described propeller is installed, described first horn is provided with described motor equal number of with described foot piece and described spiral shell
Rotation oar；Or,
About a pair described motor back to setting is installed, on the described motor cabinet on described foot piece on each described motor all
One described propeller is installed, described first horn is provided with a described motor.
Multi-functional unmanned plane rack kit the most as claimed in claim 1, it is characterised in that described first horn, described second
The a length of 24cm of horn, the size of described propeller is 9 cun；Or, described first horn, described second horn a length of
34cm, the size of described propeller is 13 cun；Or, described first horn, a length of 41cm of described second horn, described spiral shell
The size of rotation oar is 16 cun.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620680620.9U CN205738049U (en) | 2016-07-01 | 2016-07-01 | Multi-functional unmanned plane rack kit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620680620.9U CN205738049U (en) | 2016-07-01 | 2016-07-01 | Multi-functional unmanned plane rack kit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205738049U true CN205738049U (en) | 2016-11-30 |
Family
ID=57381254
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620680620.9U Withdrawn - After Issue CN205738049U (en) | 2016-07-01 | 2016-07-01 | Multi-functional unmanned plane rack kit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205738049U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005362A (en) * | 2016-07-01 | 2016-10-12 | 宁夏爱华芯科技有限公司 | Multifunctional unmanned aerial vehicle frame set |
| CN108313280A (en) * | 2018-03-05 | 2018-07-24 | 上海市第中学 | A kind of aircraft |
-
2016
- 2016-07-01 CN CN201620680620.9U patent/CN205738049U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005362A (en) * | 2016-07-01 | 2016-10-12 | 宁夏爱华芯科技有限公司 | Multifunctional unmanned aerial vehicle frame set |
| CN108313280A (en) * | 2018-03-05 | 2018-07-24 | 上海市第中学 | A kind of aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20161130 Effective date of abandoning: 20190125 |
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| AV01 | Patent right actively abandoned |