CN205819577U - For carry-on fast assembling and disassembling device and aircraft - Google Patents
For carry-on fast assembling and disassembling device and aircraft Download PDFInfo
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- CN205819577U CN205819577U CN201620501332.2U CN201620501332U CN205819577U CN 205819577 U CN205819577 U CN 205819577U CN 201620501332 U CN201620501332 U CN 201620501332U CN 205819577 U CN205819577 U CN 205819577U
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- fast assembling
- disassembling device
- carry
- aircraft
- locating part
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Abstract
This utility model provides one for carry-on fast assembling and disassembling device and aircraft, and wherein fast assembling and disassembling device includes: installing plate；Deck, is fixed on described installing plate, and described deck has the first inserted area, and described first inserted area is for the plug connector grafting with described aircraft；Locating part, is located in described deck, and when described plug connector is plugged in described first inserted area, described locating part is for being fixed on described plug connector by described deck.Fast assembling and disassembling device of the present utility model can be loaded and unloaded on aircraft conveniently and efficiently, without this loaded down with trivial details mode of operation of screw locking, thus can be by some special applications modules, it is fixed on fast assembling and disassembling device, it is achieved that some application modules of carry on board the aircraft on the premise of not destroying aircraft existing structure.Therefore, aircraft of the present utility model can carry various for module, there is the application of more function, thus widened the application of aircraft.
Description
Technical field
This utility model relates to a kind of for carry-on fast assembling and disassembling device and aircraft.
Background technology
Aircraft has high using value, often a lot of application scenarios in many fields, needs to install
Some special application modules, module of such as jettisoninging and talk through aircraft loudspeaker module.In prior art, if flying
Application module is installed on row device, general by this loaded down with trivial details mode of operation of screw locking, need in flight
Hole on device, the most also because of the structural particularity of application module, need the existing structure of change of flight device.
Utility model content
The technical problems to be solved in the utility model is the defect in order to overcome prior art, it is provided that Yi Zhongke
Make application module be loaded and unloaded on conveniently and efficiently carry-on for carry-on fast assembling and disassembling device and
Aircraft.
This utility model is to solve above-mentioned technical problem by following technical proposals:
A kind of for carry-on fast assembling and disassembling device, its feature is, described fast assembling and disassembling device bag
Include:
Installing plate；
Deck, is fixed on described installing plate, and described deck has the first inserted area, described first grafting
District is for the plug connector grafting with described aircraft；
Locating part, is located in described deck, when described plug connector is plugged in described first inserted area,
Described locating part is for being fixed on described plug connector by described deck.
Removably grafting it is plugged to described in it is preferred that.
It is preferred that described installing plate is provided with some adapters, each adapter is for connecting an application
Module.
It is preferred that described deck includes a receiving district, described locating part is located in described receiving district；
Described locating part includes that spacing base and limited block, described limited block are located on described spacing base,
And described limited block be positioned at described receiving district with in the intersection region of described first inserted area；
Described fast assembling and disassembling device also includes telescopic component, is used for driving described locating part in described receiving district
Middle movement, makes described limited block remove from described intersection region.
It is preferred that described telescopic component includes connecting rod, handle, elastic component；
Described installing plate is provided with the first through hole, and described connecting rod runs through described first through hole, described spacing
The bottom of part is provided with groove, and the upper end of described connecting rod is arranged in described groove, lower end and described handle
Connect；
Described elastic component, for described locating part is applied elastic force, makes described limited block move to described intersection
In region.
It is preferred that described elastic component is spring, described spring housing is located in described connecting rod, described spring
One end support and be located at the upper surface of described installing plate, the other end is arranged in described groove；
The external diameter of described spring is more than the diameter of described first through hole.
It is preferred that described installing plate is provided with two described first through holes, each first through hole is provided with one
Group telescopic component.
It is preferred that described handle is W type handle, and/or, described connecting rod is female thread bar.
It is preferred that described plug connector to include that the first plugboard, described first plugboard are used for being plugged in described
In first inserted area, described first plugboard has the second through hole；
Described locating part is used for being arranged in described second through hole.
It is preferred that described fast assembling and disassembling device also includes hasp, it is located on described installing plate, described hasp
There is the second inserted area；
Described plug connector also includes that the second plugboard, described second plugboard are used for being plugged in described second and insert
Connect in district.
It is preferred that the quantity of described hasp is two, the two ends of described second plugboard are plugged in two respectively
In second inserted area of individual hasp.
It is preferred that described plug connector is The Cloud Terrace vibration damper plate.
This utility model also includes a kind of aircraft, and its feature is, described aircraft also includes as above institute
The fast assembling and disassembling device stated.
Positive progressive effect of the present utility model is: the installing plate in this utility model passes through deck and limit
Position part can be fixed on aircraft conveniently and efficiently, it is not necessary to this loaded down with trivial details mode of operation of screw locking, from
And can be by some special applications modules, module of such as jettisoninging and talk through aircraft loudspeaker module, it is fixed on installing plate,
Visible, the application extension of aircraft, height simple to operate is realized by fast assembling and disassembling device of the present utility model
Effect, easy to loading and unloading fast, safety is high, and will not destroy the existing structure of aircraft.This utility model
Aircraft can realize the expansion of various application module, the application of more function can be realized, thus widen
The application of aircraft.
Accompanying drawing explanation
Fig. 1 is the structural representation of the aircraft of this utility model one preferred embodiment.
Fig. 2 is the decomposition for carry-on fast assembling and disassembling device of this utility model one preferred embodiment
Structural representation.
Fig. 3 be in Fig. 2 after carry-on fast assembling and disassembling device is installed and with the knot of application module
Structure schematic diagram.
Fig. 4 is that the structure after carry-on fast assembling and disassembling device that plug connector is plugged in Fig. 3 is shown
It is intended to.
Detailed description of the invention
Name preferred embodiment, and combine accompanying drawing and become apparent from intactly illustrating this utility model.
As Figure 1-4, the aircraft of the present embodiment includes plug connector and fast assembling and disassembling device, fast quick-mounting
Handler can be arranged on aircraft by plug connector, thus can be by some application module carries in fast quick-mounting
On handler, such as the The Cloud Terrace module 4 in the present embodiment, make aircraft have the application of more function,
The application of aircraft can be widened.The shape device that flies of the present embodiment also includes the flying platform 5 of prior art
With foot rest 6 parts such as grade, here is omitted.
Concrete, as in Figure 2-4, the fast assembling and disassembling device of the present embodiment includes installing plate 2, deck
31 and locating part 32.Deck is fixed on installing plate 2, and deck 31 has the first inserted area (i.e. deck
The groove of side), the first inserted area for and plug connector grafting, inserting mode is removably grafting.
Wherein, plug connector can be The Cloud Terrace vibration damper plate 1, but is not limited to this.Locating part 32 is located in deck 31,
When plug connector is plugged in the first inserted area, locating part is used for deck is fixed on plug connector, thus
Avoid the shake of installing plate in the vertical direction and relative to plug connector movement in the horizontal direction.Tool
Body, if plug connector includes the first plugboard 11, then the first plugboard 11 is plugged in the first inserted area
In.First plugboard 11 has the second through hole 111 (for rectangular through-hole in the present embodiment, it is also possible to be it
His shape), when the first plugboard 11 is plugged in the first inserted area, locating part 32 is just arranged in
In second through hole 111, then locating part avoids the movement of horizontal direction of plug connector.Therefore, by this
Fast assembling and disassembling device in embodiment, only need to be plugged in the first plugboard in the first inserted area, it is not necessary to spiral shell
Installing plate can be fixed on aircraft by other fixtures such as bolt.Some inhomogeneities can be provided with on installing plate
The adapter (not shown) of type, each adapter can connect an application module, such as The Cloud Terrace mould
Block, module of jettisoninging and talk through aircraft loudspeaker module, thus application module can be with inserting, the most flexibly.
In the present embodiment, deck 31 includes accommodating district, and locating part 32 is located in receiving district.Locating part 32
Including spacing base and limited block, limited block is located on spacing base, and spacing base and limited block can be
Integrated.The fast assembling and disassembling device of the present embodiment also includes telescopic component.Generally, spacing
Block is positioned in the intersection region accommodating district and the first inserted area, and now plug connector cannot insert the first inserted area
In, limited block need to be removed intersection region, the present embodiment drives locating part 32 holding by telescopic component
Receiving and move in district, make limited block remove from intersection region, now plug connector could insert the first inserted area.
Concrete, the telescopic component of the present embodiment includes connecting rod 331, handle 332, elastic component, its
Middle handle can be W type handle, and connecting rod can be female thread bar.Installing plate 2 is provided with first and leads to
Hole 21, connecting rod 331 runs through the first through hole 21, and the bottom of locating part 32 is provided with groove and (also can cry blind
Hole), this groove can include the through hole being opened in spacing base and the part stretching in limited block,
The upper end of connecting rod 331 is arranged in groove, and lower end is connected with handle 332, as in figure 2 it is shown, now
Locating part 32 is positioned at the top of installing plate 2, and handle 332 is positioned at the lower section of installing plate 2.Elastic component is used
In locating part 32 is applied elastic force, limited block is made to move to intersection region.Wherein, elastic component is permissible
For spring 333, then spring 333 is sheathed in connecting rod 331, is installed on a mounting board by deck 3
After, the upper surface being located at installing plate 2 is supported in one end of spring 333, and the other end is arranged in groove, and bullet
The external diameter of spring 333 is more than the diameter of the first through hole.When applying a downward power to handle 332, connection
Bar 331 downwards and drives locating part 32 down so that limited block removes from intersection region, simultaneously bullet
Spring 333 compresses, and plug connector now can insert the first inserted area.The active force of handle is released, spring
Elastic force is applied to locating part 32, so that limited block is moved upward to during recovering naturalness
In intersection region, during now limited block is just arranged in the second through hole 111 of the first plugboard 11.For
Make to put on the elastic force stress balance of locating part, two the first through holes 21 can be provided with on a mounting board, often
Individual first through hole 21 is provided with one group of telescopic component.Certainly, can be stretched by a locating part and two
Assembly connects, it is possible to arrange a locating part on telescopic component often organizing.The number of locating part in the present embodiment
Amount is two, namely often group telescopic component on be respectively provided with a locating part.And the cross section of locating part is just
Square, the length of side is equal with the width of the second through hole 111.
In the present embodiment, fast assembling and disassembling device also includes hasp 7, is located on installing plate 2, and hasp 7 has
There is the second inserted area (i.e. the groove of hasp side).Plug connector also includes the second plugboard 12, and second inserts
Fishplate bar 12 is used for being plugged in the second inserted area.Wherein, hasp can arrange multiple, in the present embodiment
The quantity of hasp be two, the two ends of the second plugboard are plugged in the second inserted area of two hasps respectively
In.
Although the foregoing describing detailed description of the invention of the present utility model, but those skilled in the art should
Working as understanding, this is merely illustrative of, and protection domain of the present utility model is to be defined by the appended claims
's.Those skilled in the art, can be right on the premise of without departing substantially from principle of the present utility model and essence
These embodiments make various changes or modifications, but these changes and amendment each fall within of the present utility model
Protection domain.
Claims (13)
1. one kind is used for carry-on fast assembling and disassembling device, it is characterised in that described quick despatch fills
Put and include:
Installing plate；
Deck, is fixed on described installing plate, and described deck has the first inserted area, described first grafting
District is for the plug connector grafting with described aircraft；
Locating part, is located in described deck, when described plug connector is plugged in described first inserted area,
Described locating part is for being fixed on described plug connector by described deck.
2. as claimed in claim 1 for carry-on fast assembling and disassembling device, it is characterised in that
Described it is plugged to removably grafting.
3. as claimed in claim 1 for carry-on fast assembling and disassembling device, it is characterised in that
Described installing plate is provided with some adapters, and each adapter is for connecting an application module.
4. as claimed in claim 1 for carry-on fast assembling and disassembling device, it is characterised in that
Described deck includes a receiving district, and described locating part is located in described receiving district；
Described locating part includes that spacing base and limited block, described limited block are located on described spacing base,
And described limited block be positioned at described receiving district with in the intersection region of described first inserted area；
Described fast assembling and disassembling device also includes telescopic component, is used for driving described locating part in described receiving district
Middle movement, makes described limited block remove from described intersection region.
5. as claimed in claim 4 for carry-on fast assembling and disassembling device, it is characterised in that
Described telescopic component includes connecting rod, handle, elastic component；
Described installing plate is provided with the first through hole, and described connecting rod runs through described first through hole, described spacing
The bottom of part is provided with groove, and the upper end of described connecting rod is arranged in described groove, lower end and described handle
Connect；
Described elastic component, for described locating part is applied elastic force, makes described limited block move to described intersection
In region.
6. as claimed in claim 5 for carry-on fast assembling and disassembling device, it is characterised in that
Described elastic component is spring, and described spring housing is located in described connecting rod, and one end of described spring is supported and is located at
The upper surface of described installing plate, the other end is arranged in described groove；
The external diameter of described spring is more than the diameter of described first through hole.
7. as claimed in claim 5 for carry-on fast assembling and disassembling device, it is characterised in that
Described installing plate is provided with two described first through holes, is provided with one group of telescopic component in each first through hole.
8. as claimed in claim 5 for carry-on fast assembling and disassembling device, it is characterised in that
Described handle is W type handle, and/or, described connecting rod is female thread bar.
9. as claimed in claim 1 for carry-on fast assembling and disassembling device, it is characterised in that
Described plug connector includes that the first plugboard, described first plugboard are used for being plugged in described first inserted area,
Described first plugboard has the second through hole；
Described locating part is used for being arranged in described second through hole.
10. as described in any one in claim 1-9 for carry-on fast assembling and disassembling device,
It is characterized in that, described fast assembling and disassembling device also includes hasp, is located on described installing plate, described hasp
There is the second inserted area；
Described plug connector also includes that the second plugboard, described second plugboard are used for being plugged in described second and insert
Connect in district.
11. as claimed in claim 10 for carry-on fast assembling and disassembling device, it is characterised in that
The quantity of described hasp is two, and the two ends of described second plugboard are plugged in the second of two hasps respectively
In inserted area.
12. as claimed in claim 10 for carry-on fast assembling and disassembling device, it is characterised in that
Described plug connector is The Cloud Terrace vibration damper plate.
13. 1 kinds of aircraft, it is characterised in that described aircraft also includes as in claim 1-12
Fast assembling and disassembling device described in any one.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620501332.2U CN205819577U (en) | 2016-05-27 | 2016-05-27 | For carry-on fast assembling and disassembling device and aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620501332.2U CN205819577U (en) | 2016-05-27 | 2016-05-27 | For carry-on fast assembling and disassembling device and aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205819577U true CN205819577U (en) | 2016-12-21 |
Family
ID=57557974
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620501332.2U Active CN205819577U (en) | 2016-05-27 | 2016-05-27 | For carry-on fast assembling and disassembling device and aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205819577U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106697311A (en) * | 2017-03-13 | 2017-05-24 | 广州鼎飞航空科技有限公司 | Unmanned aerial vehicle airborne multifunctional device and unmanned aerial vehicle |
| CN107719680A (en) * | 2017-10-13 | 2018-02-23 | 北京臻迪科技股份有限公司 | A kind of unmanned plane carry system |
| CN107757933A (en) * | 2017-10-13 | 2018-03-06 | 北京臻迪科技股份有限公司 | A kind of unmanned plane carry device |
-
2016
- 2016-05-27 CN CN201620501332.2U patent/CN205819577U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106697311A (en) * | 2017-03-13 | 2017-05-24 | 广州鼎飞航空科技有限公司 | Unmanned aerial vehicle airborne multifunctional device and unmanned aerial vehicle |
| CN107719680A (en) * | 2017-10-13 | 2018-02-23 | 北京臻迪科技股份有限公司 | A kind of unmanned plane carry system |
| CN107757933A (en) * | 2017-10-13 | 2018-03-06 | 北京臻迪科技股份有限公司 | A kind of unmanned plane carry device |
| CN107757933B (en) * | 2017-10-13 | 2019-11-29 | 北京臻迪科技股份有限公司 | A kind of unmanned plane carry device |
| CN107719680B (en) * | 2017-10-13 | 2019-12-13 | 北京臻迪科技股份有限公司 | Unmanned aerial vehicle mounting system |
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| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |