CN205854464U - Unmanned plane horizontal tail device for quickly disassembling - Google Patents
Unmanned plane horizontal tail device for quickly disassembling Download PDFInfo
- Publication number
- CN205854464U CN205854464U CN201620833628.4U CN201620833628U CN205854464U CN 205854464 U CN205854464 U CN 205854464U CN 201620833628 U CN201620833628 U CN 201620833628U CN 205854464 U CN205854464 U CN 205854464U
- Authority
- CN
- China
- Prior art keywords
- horizontal tail
- collision bead
- fuselage
- face
- intubate
- 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
Links
Abstract
This utility model relates to a kind of device for quickly disassembling, particularly to a kind of unmanned plane horizontal tail device for quickly disassembling.Its structure includes fuselage and horizontal tail, intubate before being provided with horizontal tail on fuselage and intubate after horizontal tail, intubate before described horizontal tail and intubate corresponding inserting respectively and be embedded in the sleeve pipe on described horizontal tail end face after horizontal tail, described horizontal tail end face and fuselage end face are additionally provided with the collision bead push-pull structure of mutual inlay card.A kind of unmanned plane horizontal tail device for quickly disassembling of the present utility model, it is on the basis of meeting horizontal tail and fuselage bonding strength, it is achieved the purpose of fast assembling-disassembling horizontal tail.
Description
Technical field
This utility model relates to a kind of device for quickly disassembling, particularly to a kind of unmanned plane horizontal tail device for quickly disassembling.
Background technology
China's unmanned plane field quickly grows in recent years, and the unmanned plane yield of China occupies first place in the world.Existing part is unmanned
The horizontal tail of machine is fixed with fuselage and is used the fixing mode being connected, and takies big quantity space during packing, transporting and collect, and
Being easily damaged, transport is got up very inconvenient.Some unmanned planes use plug-in type horizontal tail, i.e. horizontal tail to be installed to fuselage pluggablely
On, and be screwed, but the location comparison of screw is hidden, is not easy to dismounting.The unmanned plane horizontal tail also having and the company of fuselage
The mode of connecing adopt be screwed, these fixed form reliabilities of mode that rubber band is fixing the best, easy aged deterioration, dismount numerous
Trivial, part is many, thereby results in working performance outside relatively low.
Utility model content
In order to solve problem of the prior art, this utility model provides a kind of unmanned plane horizontal tail device for quickly disassembling, and it is full
On the basis of foot horizontal tail and fuselage bonding strength, it is achieved the purpose of fast assembling-disassembling horizontal tail.
The technical scheme that this utility model is used is as follows:
A kind of unmanned plane horizontal tail device for quickly disassembling, including fuselage and horizontal tail, intubate before fuselage is provided with horizontal tail with horizontal tail after
Intubate, intubate before described horizontal tail and intubate corresponding inserting respectively and be embedded in the sleeve pipe on described horizontal tail end face after horizontal tail, described
The collision bead push-pull structure of mutual inlay card it is additionally provided with on horizontal tail end face and fuselage end face.
Collision bead push-pull structure includes the horizontal tail base being fixed on described horizontal tail end face and the machine being fixed on fuselage end face
Body base, described horizontal tail base is provided with and meets and discusses, and described machine body base is provided with collision bead groove, in described collision bead groove
Being provided with collision bead, described collision bead is internally provided with spring, outside spacing by collision bead groove, described collision bead and the side met and discussed
Coordinate the mutual inlay card realizing collision bead push-pull structure.
The sidewall met and discussed is circular arc.
Lift and the moment of torsion of horizontal tail, as the force transmission mechanism of horizontal tail Yu fuselage, are passed to fuselage by the sleeve pipe in horizontal tail.
The effect of collision bead push-pull structure is to prevent horizontal tail transverse movement, is not involved in the transmission of power between horizontal tail and fuselage.
The technical scheme that this utility model provides has the benefit that
Unmanned plane horizontal tail device for quickly disassembling of the present utility model is by intubating and the sleeve pipe on fuselage and collision bead in horizontal tail
Push-pull structure with the use of, screw need not be used, just achieve being reliably connected of horizontal tail and fuselage, so achieve horizontal tail with
The fast assembling-disassembling of fuselage.
Accompanying drawing explanation
In order to be illustrated more clearly that the technical scheme in this utility model embodiment, required in embodiment being described below
Accompanying drawing to be used is briefly described, it should be apparent that, the accompanying drawing in describing below is only realities more of the present utility model
Execute example, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to according to these accompanying drawings
Obtain other accompanying drawing.
Fig. 1 is the overall structure schematic diagram of unmanned plane horizontal tail device for quickly disassembling of the present utility model；
Fig. 2 is the collision bead push-pull structure structural representation of unmanned plane horizontal tail device for quickly disassembling of the present utility model.
Detailed description of the invention
For making the purpose of this utility model, technical scheme and advantage clearer, new to this practicality below in conjunction with accompanying drawing
Type embodiment is described in further detail.
Embodiment one
As shown in Figure 1, a kind of unmanned plane horizontal tail device for quickly disassembling, including fuselage 1 and horizontal tail 2, fuselage 1 is provided with horizontal tail
Before intubate 3 and horizontal tail after intubate 4, intubate before described horizontal tail 3 and horizontal tail after intubate 4 respectively corresponding inserting be embedded in described horizontal tail 2 end
In sleeve pipe 5 on face, described horizontal tail end face and fuselage end face are additionally provided with the collision bead push-pull structure 6 of mutual inlay card.
As shown in Figure 2, collision bead push-pull structure 6 includes the horizontal tail base 61 being fixed on described horizontal tail 2 end face and fixes
Machine body base 62 on fuselage 1 end face, described horizontal tail base 61 is provided with and meets and discusses 63, described machine body base 62 sets
Being equipped with collision bead groove 64, be provided with collision bead 65 in described collision bead groove 64, described collision bead 65 is internally provided with spring, and outside is passed through
Collision bead groove 64 is spacing, described collision bead 65 with meet and discuss 63 side-fit realize the mutual inlay card of collision bead push-pull structure 6.
Meet and discuss 63 sidewall be circular arc.
Intubate before horizontal tail 3 and horizontal tail after intubate in the sleeve pipe 5 of 4 insertion fuselage 1 correspondences, then will meet and discuss and 63 snap in machine body base
In the collision bead groove 64 of 62 correspondences, just complete the fixing of horizontal tail 2 and fuselage 1.During dismounting horizontal tail 2, by plug auxiliary block firmly
Just horizontal tail 2 can be extracted.Horizontal tail anterior cannula 3 and horizontal tail rear sleeve 4 are as horizontal tail 2 and the force transmission mechanism of fuselage 1, by horizontal tail 2
Lift and moment of torsion pass to fuselage 1.The effect of collision bead push-pull structure 6 is to prevent horizontal tail 2 transverse movement, is not involved in horizontal tail 2 and machine
1 power of body and the transmission of moment of torsion.
The foregoing is only preferred embodiment of the present utility model, not in order to limit this utility model, all in this practicality
Within novel spirit and principle, any modification, equivalent substitution and improvement etc. made, should be included in guarantor of the present utility model
Within the scope of protecting.
Claims (3)
1. a unmanned plane horizontal tail device for quickly disassembling, including fuselage and horizontal tail, it is characterised in that be provided with horizontal tail on described fuselage
Before intubate and intubate after horizontal tail, intubate before described horizontal tail and intubate corresponding inserting respectively and be embedded on described horizontal tail end face after horizontal tail
In sleeve pipe, described horizontal tail end face and fuselage end face are additionally provided with the collision bead push-pull structure of mutual inlay card.
Unmanned plane horizontal tail device for quickly disassembling the most according to claim 1, it is characterised in that described collision bead push-pull structure includes
The horizontal tail base being fixed on described horizontal tail end face and the machine body base being fixed on fuselage end face, described horizontal tail base sets
It is equipped with and meets and discusses, described machine body base is provided with collision bead groove, is provided with collision bead in described collision bead groove, inside described collision bead
Being provided with spring, outside spacing by collision bead groove, described collision bead realizes the phase of collision bead push-pull structure with the side-fit met and discussed
Inlay card mutually.
Unmanned plane horizontal tail device for quickly disassembling the most according to claim 2, it is characterised in that the described sidewall met and discussed is circular arc
Shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620833628.4U CN205854464U (en) | 2016-08-03 | 2016-08-03 | Unmanned plane horizontal tail device for quickly disassembling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620833628.4U CN205854464U (en) | 2016-08-03 | 2016-08-03 | Unmanned plane horizontal tail device for quickly disassembling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205854464U true CN205854464U (en) | 2017-01-04 |
Family
ID=57654772
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620833628.4U Expired - Fee Related CN205854464U (en) | 2016-08-03 | 2016-08-03 | Unmanned plane horizontal tail device for quickly disassembling |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205854464U (en) |
-
2016
- 2016-08-03 CN CN201620833628.4U patent/CN205854464U/en not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107404028A (en) | A kind of novel deduster equipment | |
| CN106005370A (en) | Quick dismantling device for unmanned aerial vehicle wing | |
| CN106218855A (en) | Unmanned plane horizontal tail device for quickly disassembling | |
| CN205854464U (en) | Unmanned plane horizontal tail device for quickly disassembling | |
| CN202737946U (en) | SIM card converter | |
| CN205854479U (en) | Unmanned plane wing device for quickly disassembling | |
| CN204407651U (en) | A kind of USB joint with expansion mouth | |
| CN205277183U (en) | Novel arc glass briquetting | |
| CN204124253U (en) | Novel portable Kickboard Scooter | |
| CN202053797U (en) | Dust sucking eraser | |
| CN202806922U (en) | Transportation semi trailer body structure | |
| CN203198998U (en) | Convenient and rapid feeding carriage | |
| CN203180265U (en) | Movable socket | |
| CN207843646U (en) | A kind of plastic sucking disc facilitating installation | |
| CN109080308A (en) | A kind of accounting invoice storing unit | |
| CN104443748A (en) | Furniture carrying protection tool | |
| CN203267565U (en) | Blackboard easy to move | |
| CN206501686U (en) | Sunshading board presss from both sides axle | |
| CN204836263U (en) | Glue frame structure | |
| CN204130871U (en) | The plug of rotatable band sucker | |
| CN204978445U (en) | Novel automobile -used cell phone stand | |
| CN208007275U (en) | Undercarriage applied to four axis unmanned planes | |
| CN204859250U (en) | Glue frame structure | |
| CN109017080A (en) | A kind of pen container | |
| CN206619573U (en) | A kind of fuse sheath connecting structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| PP01 | Preservation of patent right | ||
| PP01 | Preservation of patent right |
Effective date of registration: 20181212 Granted publication date: 20170104 |
|
| PD01 | Discharge of preservation of patent | ||
| PD01 | Discharge of preservation of patent |
Date of cancellation: 20201212 Granted publication date: 20170104 |
|
| 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: 20170104 Termination date: 20180803 |