CN206231611U - Off-loadable unmanned aerial vehicle body structure - Google Patents
Off-loadable unmanned aerial vehicle body structure Download PDFInfo
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- CN206231611U CN206231611U CN201621328942.3U CN201621328942U CN206231611U CN 206231611 U CN206231611 U CN 206231611U CN 201621328942 U CN201621328942 U CN 201621328942U CN 206231611 U CN206231611 U CN 206231611U
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- connection framework
- loadable
- vehicle body
- aerial vehicle
- unmanned aerial
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Abstract
A kind of off-loadable unmanned aerial vehicle body structure that the utility model is provided, is that whole fuselage is provided a supporting role by the effect of support bar in the utility model；The support bar can be unloaded from fuselage；By by the first connection framework it is corresponding with the bottom of the second connection framework engagement, by the first position limiting structure, the second position limiting structure, and fixation is connected by screw in the screw of connecting portion, pin is inserted into cotter slot, you can realize being fixedly connected for unmanned aerial vehicle body.In further by the way that banking stop is inserted into the stopper slot of the first position limiting structure and the second position limiting structure respectively by the spacing slotted eye of base, it is ensured that fuselage stabilization in the process of running.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, more particularly to a kind of off-loadable unmanned aerial vehicle body structure.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without driving cabin on machine, but the equipment such as automatic pilot, presetting apparatus, information collecting device are installed.
On ground, naval vessels or machine tool remote control station personnel are by the equipment such as radar, it is tracked, is positioned, remote control, remote measurement and numeral are passed
It is defeated.Can take off or be launched with booster rocket as conventional airplane under wireless remotecontrol, can also be taken in the air by machine tool
Deliver flight.
For unmanned plane, unmanned aerial vehicle body of the prior art is formed using integrally formed structure fabrication.So
And, making is designed using fuselage as an entirety, cause and repair extremely inconvenient, and when damaging occurs in a certain position of fuselage
When wound cannot be repaired, have to change the whole fuselage of unmanned plane, significantly increase maintenance cost.
Utility model content
The utility model provides a kind of off-loadable unmanned aerial vehicle body structure, solves or part solves to know clearly in the prior art
Hand throws the fuselage maintenance cost technological deficiency high of unmanned plane.
The utility model provides a kind of off-loadable unmanned aerial vehicle body structure, including the first side section, tow side section, the first company
Connect framework, the second connection framework, supporting part, it is characterised in that first connection framework is connected with one end of the first side section, institute
State the second connection framework to be connected with one end of tow side section, first connection framework is connected with the second connection framework, institute
Stating supporting part includes being symmetrically distributed in four support bars of fuselage interior, and the support bar is through first side section, the second side
Section, the first connection framework and the second connection framework.
The off-loadable one end for being connected to the first side section of first connection framework；Second connection framework is detachable
The one end for being connected to the tow side section for carrying.
First connection framework is the double-deck tetragonal structure for including bottom and surface layer, by positioned at corner between two-layer
The cotter slot of hollow cylindrical be fixedly connected, fabric is located at the symmetrically arranged location hole in bottom two ends, is set inside bottom
It is equipped with cross framework, the connecting portion of circle, the connecting portion is provided with positioned at the cross junction
Center is provided with screw.
The bottom two ends of first connection framework are provided with the first stopper slot and the second stopper slot, in first stopper slot
It is respectively symmetrically inside portion and the second stopper slot and is provided with the spacing hole that cross section is rectangle.
Second connection framework is consistent with the structure of first connection framework.
Described off-loadable unmanned aerial vehicle body structure, also including the first position limiting structure and the second position limiting structure, described first
Position limiting structure includes base, and the symmetrically arranged clamping piece extended from base, and the clamping piece is internally provided with two
Stopper slot, the base is symmetrically arranged with two spacing slotted eyes, and the stopper slot is connected with spacing slotted eye；The second spacing knot
Structure includes base, and the clamping piece extended from base, and the clamping piece is internally provided with stopper slot, and the base is provided with
Spacing slotted eye, the stopper slot is connected with spacing slotted eye.First is inserted respectively by the spacing slotted eye of base by by banking stop
In the stopper slot of position limiting structure and the second position limiting structure, it is ensured that fuselage stabilization in the process of running.
Positional symmetry of the two ends of first side intersegmental part in four corners is provided with 4 locating rings.
Positional symmetry of the two ends of second side intersegmental part in four corners is provided with 4 locating rings.
In the utility model, by the effect of support bar, the first side section, the locating ring of tow side section and the are each passed through
One connection framework, the whole fuselage that act as of the connection member of the second connection framework are provided a supporting role；The support bar can be from
Fuselage is unloaded；By by the engagement corresponding with the bottom of the second connection framework of the first connection framework, by the first position limiting structure, second
Position limiting structure, and fixation is connected by screw in the screw of connecting portion, pin is inserted into cotter slot, you can real
Show being fixedly connected for unmanned aerial vehicle body.Further spacing by the way that banking stop is inserted into first respectively by the spacing slotted eye of base
In the stopper slot of structure and the second position limiting structure, it is ensured that fuselage stabilization in the process of running.
The beneficial effects of the utility model：
A kind of off-loadable unmanned aerial vehicle body structure that the utility model is provided, the first side is divided into by by the fuselage of unmanned plane
Section and tow side section, are attached with reference to the connected mode of the first connection framework and the second connection framework detachable connection, with
This constitutes a dismountable fuselage of structure, so that when local damage occurs in the fuselage of unmanned plane, corresponding can tear open
It is simple, convenient except the position for occurring damaging is repaired.And when the part of fuselage is when occurring to be repaired damaging,
Can also the position that cannot repair of corresponding dismounting, i.e., the position that cannot be repaired is substituted, overcome prior art
It is middle because fuselage is using integrated global design, and when causing that fuselage local damage occur cannot repair, it has to more hand-off throwing nothing
The technological deficiency of man-machine whole fuselage, significantly reduces maintenance cost.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is structural representation of the present utility model；
Fig. 3 is structural representation of the present utility model.
Specific embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment for being obtained, belongs to the scope of the utility model protection.
The utility model provides a kind of off-loadable unmanned aerial vehicle body structure, including the first side section 1, tow side section 2, first
Connection framework 3, the second connection framework 4, supporting part 5, it is characterised in that one end of the side of first connection framework 3 and first section 1
Connection, second connection framework 4 is connected with one end of tow side section 2, the connection framework 4 of first connection framework 3 and second
It is connected, the supporting part includes being symmetrically distributed in four support bars of fuselage interior, the support bar runs through described first
Side section 1, tow side section 2, the first connection framework 3 and the second connection framework 4.
The off-loadable one end for being connected to the first side section 1 of first connection framework 3；Second connection framework 4
Off-loadable one end for being connected to the tow side section 2.
First connection framework 3 is the double-deck tetragonal structure for including bottom and surface layer, by positioned at four between two-layer
The cotter slot 31 of the hollow cylindrical at angle is fixedly connected, and fabric is located at the symmetrically arranged location hole 32 in bottom two ends, bottom
It is internally provided with cross framework 33, the connecting portion 34 of circle is provided with positioned at the cross junction, it is described
Connecting portion center is provided with screw 35.
The bottom two ends of first connection framework 3 are provided with the first stopper slot 36 and the second stopper slot 37, first limit
It is respectively symmetrically inside position groove inside and the second stopper slot and is provided with the spacing hole that cross section is rectangle.
The first connection framework lower section is symmetrically arranged with Access Division 8, and the support bar fixes clamping with the Access Division.
Second connection framework 4 is consistent with the structure of first connection framework 3.
Described off-loadable unmanned aerial vehicle body structure, also including the first position limiting structure 6 and the second position limiting structure 7, described
One position limiting structure includes base 61, and the symmetrically arranged clamping piece 62 extended from base, and the clamping piece inside is set
There are two stopper slots, the base is symmetrically arranged with two spacing slotted eyes, and the stopper slot is connected with spacing slotted eye；Described second
Position limiting structure includes base 71, and the clamping piece 72 extended from base, and the clamping piece is internally provided with stopper slot, described
Base is provided with spacing slotted eye, and the stopper slot is connected with spacing slotted eye.
The positional symmetry of two ends inside first side section 1 in four corners is provided with 4 locating rings（Do not mark）.
The positional symmetry of two ends inside the tow side section 2 in four corners is provided with 4 locating rings（Do not mark）.
Finally it should be noted that：Preferred embodiment of the present utility model is the foregoing is only, this is not limited to
Utility model, although being described in detail to the utility model with reference to the foregoing embodiments, for those skilled in the art
For, it can still modify to the technical scheme described in foregoing embodiments, or to which part technical characteristic
Equivalent is carried out, all within spirit of the present utility model and principle, any modification, equivalent substitution and improvements made etc.,
Should be included within protection domain of the present utility model.Originally it is all technical characteristics not described in detail in utility model,
Realized by any prior art.
Claims (8)
1. off-loadable unmanned aerial vehicle body structure, including the first side section, tow side section, the first connection framework, the second connection framework, branch
Support part, it is characterised in that first connection framework is connected with one end of the first side section, second connection framework and the second side
One end connection of section, first connection framework is connected with the second connection framework, and the supporting part includes being symmetrically distributed in
Four support bars of fuselage interior, the support bar runs through the first side section, tow side section, the first connection framework and second
Connection framework.
2. off-loadable unmanned aerial vehicle body structure according to claim 1, it is characterised in that first connection framework is detachable
What is carried is connected to one end of the first side section；Second connection framework it is off-loadable be connected to the tow side section one
End.
3. off-loadable unmanned aerial vehicle body structure according to claim 1, it is characterised in that first connection framework is bag
The double-deck tetragonal structure of bottom and surface layer is included, is fixed by the cotter slot of the hollow cylindrical positioned at corner between two-layer and connected
Connect, fabric is located at the symmetrically arranged location hole in bottom two ends, bottom is internally provided with cross framework, positioned at described
Cross junction is provided with the connecting portion of circle, and the connecting portion center is provided with screw.
4. off-loadable unmanned aerial vehicle body structure according to claim 3, it is characterised in that the bottom of first connection framework
Layer two ends are provided with the first stopper slot and the second stopper slot, are respectively symmetrically inside the first stopper slot inside and the second stopper slot and set
It is equipped with the spacing hole that cross section is rectangle.
5. off-loadable unmanned aerial vehicle body structure according to claim 1, it is characterised in that second connection framework and institute
The structure for stating the first connection framework is consistent.
6. off-loadable unmanned aerial vehicle body structure according to claim 1, it is characterised in that also including the first position limiting structure and
Second position limiting structure, first position limiting structure includes base, and the symmetrically arranged clamping piece extended from base, described
Clamping piece is internally provided with two stopper slots, and the base is symmetrically arranged with two spacing slotted eyes, the stopper slot and stopper slot
Hole connects；Second position limiting structure includes base, and the clamping piece extended from base, and the clamping piece is internally provided with
Stopper slot, the base is provided with spacing slotted eye, and the stopper slot is connected with spacing slotted eye.
7. off-loadable unmanned aerial vehicle body structure according to claim 1, it is characterised in that the two of first side intersegmental part
The positional symmetry in four corners is held to be provided with 4 locating rings.
8. off-loadable unmanned aerial vehicle body structure according to claim 1, it is characterised in that the two of second side intersegmental part
The positional symmetry in four corners is held to be provided with 4 locating rings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621328942.3U CN206231611U (en) | 2016-12-06 | 2016-12-06 | Off-loadable unmanned aerial vehicle body structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621328942.3U CN206231611U (en) | 2016-12-06 | 2016-12-06 | Off-loadable unmanned aerial vehicle body structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206231611U true CN206231611U (en) | 2017-06-09 |
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ID=58977879
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621328942.3U Active CN206231611U (en) | 2016-12-06 | 2016-12-06 | Off-loadable unmanned aerial vehicle body structure |
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| Country | Link |
|---|---|
| CN (1) | CN206231611U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108189999A (en) * | 2017-12-28 | 2018-06-22 | 宝鸡特种飞行器工程研究院有限公司 | A kind of split type unmanned plane |
-
2016
- 2016-12-06 CN CN201621328942.3U patent/CN206231611U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108189999A (en) * | 2017-12-28 | 2018-06-22 | 宝鸡特种飞行器工程研究院有限公司 | A kind of split type unmanned plane |
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