CN207258001U - A kind of fast assembly and disassembly mechanism of photoelectric nacelle and carrier aircraft - Google Patents
A kind of fast assembly and disassembly mechanism of photoelectric nacelle and carrier aircraft Download PDFInfo
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- CN207258001U CN207258001U CN201721109597.9U CN201721109597U CN207258001U CN 207258001 U CN207258001 U CN 207258001U CN 201721109597 U CN201721109597 U CN 201721109597U CN 207258001 U CN207258001 U CN 207258001U
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- China
- Prior art keywords
- guide post
- carrier aircraft
- photoelectric nacelle
- location hole
- disassembly mechanism
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Abstract
The utility model embodiment discloses a kind of photoelectric nacelle and the fast assembly and disassembly mechanism of carrier aircraft, including：It is provided with the dismounting bottom plate, elastic sleeve-board, the fixed plate for being provided with location hole and guide chute of guide post；Ring groove is set on guide post one end of the dismounting bottom plate；The elasticity sleeve-board is socketed on the guide post；The location hole is arranged on one end of the guide chute；The diameter of the location hole and the outside diameter of the guide post match；The width of the guide chute and the internal diameter of the guide post match.The utility model provides a kind of time saving and energy saving, simple and fast mechanism for assembling-disassembling, so that when effectively solving the problems, such as dismounting mode short life and installation fee of the photoelectric nacelle in the practical work process of outfield, can substantially reduce the difficulty of outfield work.
Description
Technical field
It the utility model is related to airborne photoelectric field, more particularly to a kind of photoelectric nacelle and the fast assembly and disassembly mechanism of carrier aircraft.
Background technology
With the fast development of photoelectric technology, the photoelectric nacelle under airborne circumstance is in frontier defense warning, rescue and forest fire protection
In application it is more and more, especially unmanned plane use or the airborne circumstance of dirigible etc. under the photoelectric nacelle that uses, its volume compared with
It is small, light-weight, more using the single photoelectric nacelle such as visible ray, infrared, laser.This airborne photoelectric gondola is not pacified generally for a long time
In carrier aircraft, simply just installed before aerial mission is performed, after aerial mission, just from necessary during aircraft accumulating
Dismantled from carrier aircraft, particularly the multiple flight of multitask load when, this dismounting number is especially frequent.
The connection to photoelectric nacelle and carrier aircraft is substantially by the way of screw fastening, but use the screw Connection Time at present
It is long, and be easy to cause screw and lose so that must not be without supplement.
Utility model content
In view of this, the utility model embodiment discloses a kind of photoelectric nacelle and the fast assembly and disassembly mechanism of carrier aircraft, can have
Technological deficiency when the screw connecting mode short life and installation fee of effect solution photoelectric nacelle and carrier aircraft.
The utility model embodiment provides a kind of photoelectric nacelle and the fast assembly and disassembly mechanism of carrier aircraft, including：
It is provided with the dismounting bottom plate, elastic sleeve-board, the fixed plate for being provided with location hole and guide chute of guide post；
Ring groove is set on guide post one end of the dismounting bottom plate；
The elasticity sleeve-board is socketed on the guide post；
The location hole is arranged on one end of the guide chute, and the location hole is communicated with the guide chute；
The diameter of the location hole and the outside diameter of the guide post match；
The width of the guide chute and the internal diameter of the guide post match.
Wherein, the guide post sets a diameter of internal diameter of one end of ring groove, the non-ring-like groove ends of the guide post
A diameter of outside diameter.
Wherein, the depth of the ring groove on guide post is cave in distance of the guide post periphery from guide post central axis direction, therefore,
The depth that the outside diameter of guide post subtracts ring groove is the internal diameter of guide post.
, wherein it is desired to which explanation is that guide chute position does not limit, guide chute is arranged on solid for modes such as straight line, circles
Fixed board bottom.
Preferably, the fast assembly and disassembly mechanism further includes photoelectric nacelle；The dismounting bottom plate is fixed on the photoelectricity and hangs
On cabin.
Preferably, the fast assembly and disassembly mechanism further includes carrier aircraft；The fixed plate is fixed in the carrier aircraft.
Preferably, the upper surface of the elasticity sleeve-board exceedes the bottom surface preset distance of the ring groove of the guide post.
Wherein, the preset distance be less than ring groove width, the width of the ring groove as shown in the c of Fig. 2,
The elastic plate set upper surface is higher by the ring groove bottom certain distance of the guide post, when photoelectric nacelle and carrier aircraft are installed,
Outer force compresses cause bottom surface of the elastic plate set upper bottom surface completely with the ring groove of the guide post to flatten so that guide post can be in institute
The guide chute for stating fixed plate slides, bottom of the elastic plate set upper bottom surface higher than the ring groove of the guide post when external force disappears
Face, so as to be firmly secured to guide chute non-locating hole one end of the fixed plate；Separated in photoelectric nacelle with carrier aircraft dismounting
When, the guide post is fixed on guide chute non-locating hole one end of the fixed plate, and external force make it that elastic plate set upper bottom surface is complete
Flattened with the bottom surface of the ring groove of the guide post so that guide post can be slided in the guide chute of the fixed plate, when described
When guide post slides into the location hole of the guide chute of the fixed plate, elastic sleeve-board discharges thrust so that guide post is from fixed plate
Location hole pop-up.
Preferably, the elasticity sleeve-board is sponge rubber sleeve-board.
Preferably, the guide post is integrally formed with the dismounting bottom plate.
Wherein, it is described to be integrally molded so as not doing and splitting when the guide post is prepared with the dismounting bottom plate, directly manufacture completion.
Preferably, the guide post is 3.
Preferably, the location hole is 3；The guide chute is 3.
Preferably, 3 guide chutes are circumferentially arranged in the fixed plate.
Wherein, the quantity of the guide post, location hole and guide chute is not specifically limited, if can realize photoelectric nacelle with
Fast assembling-disassembling function between carrier aircraft.
The utility model embodiment provides a kind of photoelectric nacelle and the fast assembly and disassembly mechanism of carrier aircraft, including：It is provided with and leads
The dismounting bottom plate of column, elastic sleeve-board, the fixed plate for being provided with location hole and guide chute；Set on described guide post one end ring-like recessed
Groove；The elasticity sleeve-board is socketed on the guide post；The location hole be arranged on the guide chute one end, the location hole with
The guide chute communicates；The diameter of the location hole and the outside diameter of the guide post match；The width of the guide chute with
The internal diameter of the guide post matches.
The operation of the photoelectric nacelle and the fast assembly and disassembly mechanism of carrier aircraft is specially：
It is fastenedly connected soon between quick-detach bottom plate and photoelectric nacelle；Between the fixed plate and carrier aircraft of the fast assembly and disassembly mechanism
It is fastenedly connected.When photoelectric nacelle and carrier aircraft are installed, the location hole of the guide post insertion fixed plate of the fast quick-detach bottom plate；External force
So that bottom surface of the elastic plate set upper bottom surface completely with the ring groove of the guide post flattens so that guide post can be in the fixed plate
Guide chute slide, when external force disappears elastic plate set upper bottom surface higher than the ring groove of the guide post bottom surface, it is elastic
Sleeve-board causes the guide chute non-locating hole one end for being connected to the fixed plate of the guide post tightly；In photoelectric nacelle and carrier aircraft
During dismounting separation, the guide post is fixed on guide chute non-locating hole one end of the fixed plate, and external force causes elastic plate to put on
Bottom surface is flattened with the bottom surface of the ring groove of the guide post completely so that guide post can be slided in the guide chute of the fixed plate
Dynamic, when the guide post slides into the location hole of the guide chute of the fixed plate, elastic sleeve-board discharges thrust so that guide post
Ejected from the location hole of fixed plate.
In conclusion on the premise of photoelectric nacelle internal structure is not changed, the utility model provide it is a kind of it is time saving and energy saving,
The dismounting connection mode of simple and fast, so that effectively solve the problems, such as dismounting of the photoelectric nacelle in the practical work process of outfield,
Reduce outfield work difficulty.
Brief description of the drawings
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, drawings in the following description are only
It is some embodiments of the utility model, for those of ordinary skill in the art, before not making the creative labor property
Put, other attached drawings can also be obtained according to these attached drawings.
Fig. 1 shows the shape of a kind of photoelectric nacelle provided in the utility model embodiment and the fast assembly and disassembly mechanism of carrier aircraft
Figure；
Fig. 2 shows the partial cutaway of a kind of photoelectric nacelle provided in the utility model embodiment and the fast assembly and disassembly mechanism of carrier aircraft
View；
Fig. 3 shows the connecting pin of a kind of photoelectric nacelle provided in the utility model embodiment and the fast assembly and disassembly mechanism of carrier aircraft
Schematic diagram；
After Fig. 4 shows the connection of a kind of photoelectric nacelle provided in the utility model embodiment and the fast assembly and disassembly mechanism of carrier aircraft
Partial sectional view；
Wherein, reference numeral：Photoelectric nacelle 1, dismounting bottom plate 2, elastic sleeve-board 3, guide post 4, location hole 5, fixed plate 6, lead
To sliding slot 7, carrier aircraft 8, ring groove 9, a is the outside diameter of guide post, and b is the internal diameter of guide post, and c is ring groove width.
Embodiment
The utility model embodiment discloses a kind of photoelectric nacelle and the fast assembly and disassembly mechanism of carrier aircraft, which can effectively solve
The certainly technological deficiency when screw connecting mode short life and installation fee of photoelectric nacelle and carrier aircraft.
Please refer to Fig.1 to Fig.4, the embodiment 1 provided in the utility model embodiment includes：It is provided with the dismounting bottom of guide post
Plate 2, elastic sleeve-board 3, the fixed plate 6 for being provided with location hole 5 and guide chute 7；Ring groove 9 is set on described 4 one end of guide post；
The elasticity sleeve-board 3 is socketed on the guide post 4；The location hole 5 is arranged on one end of the guide chute 7, the location hole 5
Communicated with the guide chute 7；The diameter of the location hole 5 matches with the outside diameter a of the guide post；The guide chute 7
The internal diameter b of width and the guide post matches.
Please refer to Fig.1 to Fig.4, the embodiment 2 provided in the utility model embodiment includes：It is provided with the dismounting bottom of guide post
Plate 2, elastic sleeve-board 3, the fixed plate 6 for being provided with location hole 5 and guide chute 7；The dismounting bottom plate 2 is fixed on photoelectric nacelle 1
On；The fixed plate 6 is fixed in carrier aircraft 8；Ring groove 9 is set on described 4 one end of guide post；The elasticity sleeve-board 3 is socketed in
On the guide post 4；The upper surface of the elasticity sleeve-board 3 exceedes the bottom surface preset distance of the ring groove 7 of the guide post 4；It is described
Location hole 5 is arranged on one end of the guide chute 7, and the location hole 5 is communicated with the guide chute 7；The location hole 5
The outside diameter a of diameter and the guide post matches；The width of the guide chute 7 matches with the internal diameter b of the guide post.
Further, elastic sleeve-board 3 is specially sponge rubber sleeve-board.
Further, the guide post 4 is integrally formed with the dismounting bottom plate 2；It is described to be integrally molded so as the guide post 4 and institute
State not do when prepared by dismounting bottom plate 2 and split, directly manufacture is completed.
Please refer to Fig.1 to Fig.4, the embodiment 3 provided in the utility model embodiment includes：It is provided with the dismounting bottom of guide post
Plate 2, elastic sleeve-board 3, the fixed plate 6 for being provided with location hole 5 and guide chute 7；The quantity of elastic sleeve-board 3 is 3, location hole 5
Quantity be that the quantity of 3 and guide chute 7 is 3；3 guide chutes are circumferentially arranged in the fixed plate 6；Institute
Dismounting bottom plate 2 is stated to be fixed on photoelectric nacelle 1；The fixed plate 6 is fixed in carrier aircraft 8；Set on described 4 one end of guide post ring-like
Groove 9；The elasticity sleeve-board 3 is socketed on the guide post 4；The upper surface of the elasticity sleeve-board 3 exceedes the ring-like of the guide post 4
The bottom surface preset distance of groove 7；The location hole 5 is arranged on one end of the guide chute 7, the location hole 5 and the guiding
Sliding slot 7 communicates；The diameter of the location hole 5 matches with the outside diameter a of the guide post；The width of the guide chute 7 with it is described
The internal diameter b of guide post matches.
Above example, when being installed between photoelectric nacelle 1 and carrier aircraft 8, is first inserted into fixation by the guide post 4 dismantled on bottom plate 2
In the location hole 5 of plate 6, then firmly compress elastic sleeve-board 3 so that 3 upper bottom surface of elastic sleeve-board completely with 4 ring groove 9 of guide post
Bottom surface flattens, and then rotation dismounting bottom plate 2 is so that guide post 4 is slided in the guide chute 7 of fixed plate 6 until guide post 4 moves to
During the end of guide chute 7, external force is not applied to elastic sleeve-board 3, installation process terminates, and it is non-fixed that guide post 4 snaps fit onto guide chute 7
Position 5 one end of hole.When being dismantled between photoelectric nacelle 1 and carrier aircraft 8, rotation dismounting bottom plate 2 is so that lead after first compressing elastic sleeve-board 3
Column 4 is slided in the guide chute 7 of fixed plate 6 until when guide post 4 is moved in the location hole 5 of fixed plate 6, discharges compression
Elastic sleeve-board 3 can discharge thrust, and guide post 4 is ejected from the location hole 5 of fixed plate 6, and disassembly process terminates, guide post 4 to
In 7 location hole 5 of guide chute out.
Detailed Jie has been carried out to the fast assembly and disassembly mechanism of a kind of photoelectric nacelle provided by the utility model and carrier aircraft above
Continue, for those of ordinary skill in the art, based on the idea of the embodiment of the present invention, in embodiment and using model
There will be changes are placed, in conclusion this specification content should not be construed as the limitation to the utility model.
Claims (10)
- A kind of 1. fast assembly and disassembly mechanism of photoelectric nacelle and carrier aircraft, it is characterised in that including：It is provided with the dismounting bottom plate, elastic sleeve-board, the fixed plate for being provided with location hole and guide chute of guide post；Ring groove is set on described guide post one end；The elasticity sleeve-board is socketed on the guide post；The location hole is arranged on one end of the guide chute, and the location hole is communicated with the guide chute；The diameter of the location hole and the outside diameter of the guide post match；The width of the guide chute and the internal diameter of the guide post match.
- 2. the fast assembly and disassembly mechanism of photoelectric nacelle according to claim 1 and carrier aircraft, it is characterised in that the dismounting bottom plate It is fixed on photoelectric nacelle.
- 3. the fast assembly and disassembly mechanism of photoelectric nacelle according to claim 2 and carrier aircraft, it is characterised in that the fixed plate is consolidated It is scheduled in carrier aircraft.
- 4. the fast assembly and disassembly mechanism of photoelectric nacelle according to claim 1 and carrier aircraft, it is characterised in that the elasticity sleeve-board Upper surface exceed the guide post ring groove bottom surface preset distance.
- 5. the fast assembly and disassembly mechanism of photoelectric nacelle according to claim 4 and carrier aircraft, it is characterised in that the elasticity sleeve-board Lower surface be fixed on it is described dismounting bottom plate upper surface on.
- 6. the fast assembly and disassembly mechanism of photoelectric nacelle according to claim 5 and carrier aircraft, it is characterised in that the elasticity sleeve-board For sponge rubber sleeve-board.
- 7. the fast assembly and disassembly mechanism of photoelectric nacelle according to claim 1 and carrier aircraft, it is characterised in that the guide post and institute Dismounting bottom plate is stated to be integrally formed.
- 8. the fast assembly and disassembly mechanism of photoelectric nacelle according to claim 1 and carrier aircraft, it is characterised in that the guide post is 3 It is a.
- 9. the fast assembly and disassembly mechanism of photoelectric nacelle according to claim 8 and carrier aircraft, it is characterised in thatThe location hole is 3；The guide chute is 3.
- 10. the fast assembly and disassembly mechanism of photoelectric nacelle according to claim 9 and carrier aircraft, it is characterised in that 3 guiding Sliding slot is circumferentially arranged in the fixed plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721109597.9U CN207258001U (en) | 2017-08-31 | 2017-08-31 | A kind of fast assembly and disassembly mechanism of photoelectric nacelle and carrier aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721109597.9U CN207258001U (en) | 2017-08-31 | 2017-08-31 | A kind of fast assembly and disassembly mechanism of photoelectric nacelle and carrier aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207258001U true CN207258001U (en) | 2018-04-20 |
Family
ID=61923519
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721109597.9U Active CN207258001U (en) | 2017-08-31 | 2017-08-31 | A kind of fast assembly and disassembly mechanism of photoelectric nacelle and carrier aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207258001U (en) |
-
2017
- 2017-08-31 CN CN201721109597.9U patent/CN207258001U/en active Active
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