CN208007272U - A kind of unmanned drive end unit fast assembling disassembling structure of fixed-wing - Google Patents
A kind of unmanned drive end unit fast assembling disassembling structure of fixed-wing Download PDFInfo
- Publication number
- CN208007272U CN208007272U CN201820409209.7U CN201820409209U CN208007272U CN 208007272 U CN208007272 U CN 208007272U CN 201820409209 U CN201820409209 U CN 201820409209U CN 208007272 U CN208007272 U CN 208007272U
- Authority
- CN
- China
- Prior art keywords
- quick release
- mounting rod
- male connector
- fixed
- wing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- Quick-Acting Or Multi-Walled Pipe Joints (AREA)
Abstract
A kind of unmanned drive end unit fast assembling disassembling structure of fixed-wing, including empennage mounting rod, fuselage mounting rod, Quick Release male connector and Quick Release female；One end of the empennage mounting rod configures the Quick Release male connector or Quick Release female, the corresponding Quick Release female of one end configuration or Quick Release male connector of the fuselage mounting rod；The body of rod of the empennage mounting rod is for configuring the unmanned drive end unit of fixed-wing；The unmanned drive end unit fast assembling disassembling structure of fixed-wing of the utility model overcomes the big problem of transport occupied space of existing fixed-wing unmanned plane, unmanned aerial vehicle body and tail are designed to two-part detachable structure, and tear open devise Quick Release male connector and Quick Release female at conjunction quickly tear conjunction structure open, object is locked without other tools or screw etc., lock directly is devised in junction, pressing is directly locked；It can be put into smaller container after dismantling, to solve the problems, such as that free space is big.
Description
Technical field
The utility model is related to a kind of unmanned drive end unit fast assembling disassembling structures of fixed-wing.
Background technology
In existing fixed-wing unmanned plane, the length of empennage has key effect, empennage to get over the pitching stability of aircraft
Long stability is better, but since the long transport that can make fixed-wing unmanned plane of fuselage becomes difficult, the long unmanned plane of fuselage
Need the space of bigger to be transported, thus on the market mainly with short fuselage, stub fin fixed-wing based on.
Utility model content
In order to overcome the deficiencies of the prior art, the utility model provides a kind of unmanned drive end unit fast assembling disassembling structure of fixed-wing.
Technical solution provided by the utility model is：
A kind of unmanned drive end unit fast assembling disassembling structure of fixed-wing, including empennage mounting rod, fuselage mounting rod, Quick Release male connector and
Quick Release female；
One end of the empennage mounting rod configures the Quick Release male connector or Quick Release female, one end of the fuselage mounting rod are matched
Set the corresponding Quick Release female or Quick Release male connector；The body of rod of the empennage mounting rod is for configuring the unmanned drive end unit of fixed-wing；
The Quick Release male connector includes fixed seat and extension block, and the fixed seat is sheet, and middle part protrudes from institute for configuring
The extension block of fixed seat is stated, the side of the extension block includes the arc-shaped slot portion of recess, and the empennage mounting rod passes through described
The middle part of fixed seat and extension block；The Quick Release female includes containing cavities and lock, is used to configure described prolong in the containing cavities
Stretch block, the arc-shaped slot portion of the extension block exposes from the side of the containing cavities, and the lock be configured at by shaft and
On the corresponding containing cavities in arc-shaped slot portion；The lock includes handle and tapered end, and the tapered end is configured at described
One end of handle, it is long side that the side of the tapered end, which is the short side other side, and the tapered end is corresponding with the arc-shaped slot portion, institute
State the Quick Release male connector and the locking of Quick Release female, the tapered end when part of the tapered end configuration in the arc-shaped slot portion is long side
The Quick Release male connector and the locking of Quick Release female when the part in the arc-shaped slot portion is short side is configured to disconnect.
Preferably, in the fixed seat of the Quick Release male connector include accommodating groove for configuring the handle.
Preferably, the side of the fixed seat and containing cavities includes threading hole.
Preferably, the empennage mounting rod stretches out the Quick Release male connector or Quick Release female.
Preferably, the empennage mounting rod stretches out the outer diameter of the part of the Quick Release male connector less than the fuselage mounting rod
Internal diameter, the fuselage mounting rod be it is hollow, the part that the empennage mounting rod bar stretches out the Quick Release male connector is configured in institute
It states in fuselage mounting rod.
Preferably, the empennage mounting rod and fuselage mounting rod are hollow rectangular carbon pipe.
The beneficial effects of the utility model：
The unmanned drive end unit fast assembling disassembling structure of fixed-wing of the utility model overcomes the transport of existing fixed-wing unmanned plane
Unmanned aerial vehicle body and tail are designed to two-part detachable structure, and are devised at conjunction soon tearing open by the big problem of occupied space
It tears male connector open and the quick of Quick Release female tears conjunction structure open, lock object without other tools or screw etc., directly set in junction
Lock is counted, pressing is directly locked；It can be put into smaller container after dismantling, to solve the problems, such as that free space is big.
Description of the drawings
Fig. 1 is the structural schematic diagram of the unmanned drive end unit fast assembling disassembling structure of fixed-wing of the utility model；
Fig. 2 is the assembling schematic diagram of the unmanned drive end unit fast assembling disassembling structure of fixed-wing of the utility model；
Fig. 3 is the dress of the Quick Release male connector and Quick Release female of the unmanned drive end unit fast assembling disassembling structure of fixed-wing of the utility model
With schematic diagram；
Fig. 4 is the dress of the Quick Release male connector and Quick Release female of the unmanned drive end unit fast assembling disassembling structure of fixed-wing of the utility model
With constructed profile.
Specific implementation mode
The utility model is described in further detail below in conjunction with the accompanying drawings, as shown in Figure 1, a kind of unmanned drive end unit of fixed-wing is fast
Fast disassembly and assembly structure, including empennage mounting rod 1, fuselage mounting rod 2, Quick Release male connector 3 and Quick Release female 4；
One end configuration Quick Release male connector 3 or Quick Release female 4 of the empennage mounting rod 1, the one of the fuselage mounting rod 2
The corresponding Quick Release female 4 of end configuration or Quick Release male connector 3, so realize the function of fastening；The body of rod of the empennage mounting rod 1
For configuring the unmanned drive end unit 5 of fixed-wing, the fuselage mounting rod 2 is used to configure the fuselage 6 of fixed-wing unmanned plane；
As shown in Figure 2, Figure 3 and Figure 4, the Quick Release male connector 3 includes fixed seat 7 and extension block 8, and the fixed seat 7 is piece
Shape, middle part include the arc-shaped slot of recess for configuring the extension block 8 for protruding from the fixed seat 7, the side of the extension block 8
Portion 9, the empennage mounting rod 1 pass through the middle part of the fixed seat 7 and extension block 8 to be fixed in the Quick Release male connector 3；It is described fast
It includes containing cavities 10 and lock to tear female 4 open, is used to configure the extension block 8, the arc of the extension block 8 in the containing cavities 10
Card slot portion 9 exposes from the side of the containing cavities 10, and the lock is configured at the arc-shaped slot portion 9 relatively by shaft
On the containing cavities answered；The lock includes handle 11 and tapered end, and the tapered end is configured at one end of the handle 11, described
The side of tapered end is that 12 other side of short side is long side 13, and the tapered end is corresponding with the arc-shaped slot portion 9, the tapered end configuration
Part in the arc-shaped slot portion 9 the Quick Release male connector 3 and the locking of Quick Release female 4 when being long side 13, the tapered end configuration
Part in the arc-shaped slot portion 9 the Quick Release male connector 3 and the locking disconnection of Quick Release female 4 when being short side 12；That is unmanned plane
Fuselage and tail are designed to two-part detachable structure, part design lock are closed tearing open, by the combination of the fixed tail portion of lock, lock
It being designed with lever construction, pressing is convenient, is not necessarily to other installation tools, irregular ellipsoidal structure is utilized at the top of lock,
It latches for oval short side distance as short side when opening, 9 space of arc-shaped slot portion is sufficient, is oval long side pressing after lock locking
Arc-shaped slot portion 9, position is compacted, and so realizes fast quick-detach.
Meanwhile including accommodating groove 14 for configuring the handle 11 in the fixed seat of the Quick Release male connector 3, so pass through
The handle 11 is disposed completely in Quick Release male connector 3 and Quick Release female 4 by the accommodating groove 14.
The side of the fixed seat 7 and containing cavities 10 includes threading hole 15.
The empennage mounting rod 1 stretches out the Quick Release male connector 3 or Quick Release female 4, optimal, the empennage mounting rod 1
The outer diameter for stretching out the part 16 of the Quick Release male connector 3 is less than the internal diameter of the fuselage mounting rod 2, during the fuselage mounting rod 2 is
Sky, the part 16 that the empennage mounting rod bar stretches out the Quick Release male connector are configured in the fuselage mounting rod 2.
The empennage mounting rod 1 and fuselage mounting rod 2 use the hollow rectangular carbon pipe of lightweight.
When in use, the part 16 that empennage mounting rod bar is stretched out to the Quick Release male connector is inserted into fuselage mounting rod 2, and
To Quick Release male connector 3 and Quick Release female 4 to be aligned, extension block 8 stretches into the containing cavities 10 at this time, and the short side 12 of tapered end is located at arc
In card slot portion 9, the two is movable at this time, then moves handle 11, the long side 13 of tapered end is made to withstand arc-shaped slot portion 9, so real
Now quickly it is fixedly connected.
Claims (6)
1. a kind of unmanned drive end unit fast assembling disassembling structure of fixed-wing, it is characterised in that：
Including empennage mounting rod, fuselage mounting rod, Quick Release male connector and Quick Release female；
One end of the empennage mounting rod configures the Quick Release male connector or Quick Release female, and one end of the fuselage mounting rod configures phase
The Quick Release female or Quick Release male connector answered；The body of rod of the empennage mounting rod is for configuring the unmanned drive end unit of fixed-wing；
The Quick Release male connector includes fixed seat and extension block, and the fixed seat is sheet, and middle part protrudes from described solid for configuration
The extension block of reservation, the side of the extension block include the arc-shaped slot portion of recess, and the empennage mounting rod passes through the fixation
The middle part of seat and extension block；The Quick Release female includes containing cavities and lock, is used to configure the extension block in the containing cavities,
The arc-shaped slot portion of the extension block exposes from the side of the containing cavities, and the lock is configured at and the arc by shaft
On the corresponding containing cavities in shape card slot portion；The lock includes handle and tapered end, and the tapered end is configured at the handle
One end, it is long side that the side of the tapered end, which is the short side other side, and the tapered end is corresponding with the arc-shaped slot portion, the tapered end
The Quick Release male connector and the locking of Quick Release female, the tapered end configuration when part in the arc-shaped slot portion is long side is configured to exist
Part in the arc-shaped slot portion Quick Release male connector and the locking disconnection of Quick Release female when being short side.
2. the unmanned drive end unit fast assembling disassembling structure of fixed-wing according to claim 1, it is characterised in that：
It include the accommodating groove for configuring the handle in the fixed seat of the Quick Release male connector.
3. the unmanned drive end unit fast assembling disassembling structure of fixed-wing according to claim 1, it is characterised in that：
The side of the fixed seat and containing cavities includes threading hole.
4. the unmanned drive end unit fast assembling disassembling structure of fixed-wing according to claim 1, it is characterised in that：
The empennage mounting rod stretches out the Quick Release male connector or Quick Release female.
5. the unmanned drive end unit fast assembling disassembling structure of fixed-wing according to claim 4, it is characterised in that：
The empennage mounting rod stretches out internal diameter of the outer diameter less than the fuselage mounting rod of the part of the Quick Release male connector, the machine
Body mounting rod is hollow, and the part that the empennage mounting rod bar stretches out the Quick Release male connector is configured in the fuselage mounting rod
It is interior.
6. the unmanned drive end unit fast assembling disassembling structure of fixed-wing as claimed in any of claims 1 to 5, feature exist
In：
The empennage mounting rod and fuselage mounting rod are hollow rectangular carbon pipe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820409209.7U CN208007272U (en) | 2018-03-26 | 2018-03-26 | A kind of unmanned drive end unit fast assembling disassembling structure of fixed-wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820409209.7U CN208007272U (en) | 2018-03-26 | 2018-03-26 | A kind of unmanned drive end unit fast assembling disassembling structure of fixed-wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208007272U true CN208007272U (en) | 2018-10-26 |
Family
ID=63890365
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820409209.7U Expired - Fee Related CN208007272U (en) | 2018-03-26 | 2018-03-26 | A kind of unmanned drive end unit fast assembling disassembling structure of fixed-wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208007272U (en) |
-
2018
- 2018-03-26 CN CN201820409209.7U patent/CN208007272U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181026 Termination date: 20210326 |