CN205113680U - Fin quick -insertion structure - Google Patents
Fin quick -insertion structure Download PDFInfo
- Publication number
- CN205113680U CN205113680U CN201520903201.2U CN201520903201U CN205113680U CN 205113680 U CN205113680 U CN 205113680U CN 201520903201 U CN201520903201 U CN 201520903201U CN 205113680 U CN205113680 U CN 205113680U
- Authority
- CN
- China
- Prior art keywords
- empennage
- fuselage
- fin
- plug
- quick detach
- 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.)
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Links
- 238000003780 insertion Methods 0.000 title abstract 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 8
- 229910052799 carbon Inorganic materials 0.000 claims description 8
- 238000000034 method Methods 0.000 description 4
- 238000004806 packaging method and process Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
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- Mutual Connection Of Rods And Tubes (AREA)
Abstract
The utility model discloses a fin quick -insertion structure, including fuselage and fin, be provided with a fin owner bolt on the fin, the fuselage is provided with corresponding fin owner bolt sleeve, and, still be provided with a quick detach hasp on the fuselage, be equipped with one on the quick detach hasp and press the stopper, the fin is provided with the plug that corresponds with the quick detach hasp and presses spacing seat, and the plug is pressed spacing seat and is set up and press that the stopper is corresponding presses spacing hole. The utility model discloses a fin sets up fin owner bolt, and the fuselage is provided with corresponding fin owner bolt sleeve to and the fuselage sets up the quick detach hasp, and the fin sets up corresponding plug and presses spacing seat, so, when connecting the fin with the fuselage, need insert fin owner bolt with fin owner bolt in to through the locking of quick detach hasp, can realize the quick dismantlement of fin and fuselage, the structure is very simple.
Description
Technical field
The utility model relates to unmanned plane equipment, in particular the fast inserting structure of a kind of empennage.
Background technology
In prior art, the empennage of unmanned plane is generally non-dismountable, and it is bulky that non-removable structure causes it to exist in transport and packaging, occupies the huge space of packaging, the not convenient property of transport difficult, reduces the complete machine safety under unmanned plane traffic condition.
Therefore, prior art existing defects, needs to improve.
Utility model content
Technical problem to be solved in the utility model is: provide a kind of quick release, the fast inserting structure of the simple empennage of structure.
The technical solution of the utility model is as follows: the fast inserting structure of a kind of empennage, comprises fuselage and empennage, empennage is provided with the main latch of an empennage, and fuselage is provided with the corresponding main pin bushing of empennage; Further, fuselage is also provided with a quick detach snap close, quick disassemble lock is buckled and is provided with one and presses limiting stopper; Empennage is provided with the plug corresponding with quick detach snap close and presses limit base, plug press limit base arrange with press limiting stopper corresponding press spacing hole.
Be applied to technique scheme, in the fast inserting structure of described empennage, empennage be also provided with an empennage fastening screw, fuselage is provided with corresponding empennage fastening screw cover.
Be applied to each technique scheme, in the fast inserting structure of described empennage, the main pin bushing of empennage and empennage fastening screw cover are installed respectively and are arranged on the carbon pipe bracket of its correspondence.
Being applied to each technique scheme, in the fast inserting structure of described empennage, fuselage being also provided with one for installing the plug firm banking of quick detach snap close.
Be applied to each technique scheme, in the fast inserting structure of described empennage, fuselage interior is provided with an integral support, and each carbon pipe bracket and plug firm banking are all fixedly installed on integral support.
Adopt such scheme, the utility model arranges the main latch of empennage by empennage, fuselage is provided with the corresponding main pin bushing of empennage, and fuselage arranges quick detach snap close, and limit base is pressed in the plug that empennage arranges correspondence, so, when connecting empennage and fuselage, only need main for empennage latch to insert in the main latch of empennage, and tight by quick disassemble lock padlock, can realize the quick-detachment of empennage and fuselage, structure is very simple.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the utility model is described in detail.
Present embodiments provide the fast inserting structure of a kind of empennage, be mainly used in the connection between the empennage of unmanned plane and fuselage, as shown in Figure 1, the fast inserting structure of empennage comprises fuselage 111 and empennage 101, wherein, empennage 101 is provided with the main latch 103 of an empennage and an empennage fastening screw 112, fuselage 111 is provided with the main pin bushing 104 of the corresponding empennage of latch 103 main with empennage, and the empennage fastening screw corresponding with empennage fastening screw 112 overlaps 110, and, fuselage 111 is also provided with a quick detach snap close 107, quick detach snap close 107 is provided with one and presses limiting stopper 113, equally, empennage 101 is provided with the plug corresponding with quick detach snap close 107 and presses limit base 102, plug press limit base 102 arrange with press limiting stopper corresponding press spacing hole 114.
So, when connecting fuselage 111 and empennage 101, the main latch of empennage 103 is inserted in the main pin bushing 104 of empennage, empennage fastening screw 112 is inserted in empennage fastening screw cover 110, simultaneously, quick detach snap close 107 is fixed on plug and presses on limit base 102, and be fixed on press in spacing hole 114 by pressing limiting stopper 113, thus fuselage and empennage are locked, when dismantling, only need will to press limiting stopper 113 to press disengaging and press spacing hole 114, thus quick disassemble lock can be tipped in row unblock, realize fast speed Assembly &Disassembly.
Or, the main pin bushing 104 of empennage is mounted on the carbon pipe bracket 105 of its correspondence, empennage fastening screw cover 110 is installed and is arranged on the carbon pipe bracket 109 of its correspondence, and, quick detach snap close 107 is fixed on the plug firm banking 108 of fuselage setting, carbon pipe bracket 105, carbon pipe bracket 109 and plug firm banking 108 are all fixedly installed on integral support 106, so, by the integral support 106 arranged, can carry out module words to each connection result to install, mounting structure is more simple and convenient.
These are only preferred embodiment of the present utility model, be not limited to the utility model, all do within spirit of the present utility model and principle any amendment, equivalent to replace and improvement etc., all should be included within protection domain of the present utility model.
Claims (5)
1. the fast inserting structure of empennage, comprises fuselage and empennage, it is characterized in that:
Empennage is provided with the main latch of an empennage, fuselage is provided with the corresponding main pin bushing of empennage;
Further, fuselage is also provided with a quick detach snap close, quick disassemble lock is buckled and is provided with one and presses limiting stopper; Empennage is provided with the plug corresponding with quick detach snap close and presses limit base, plug press limit base arrange with press limiting stopper corresponding press spacing hole.
2. the fast inserting structure of empennage according to claim 1, is characterized in that: empennage is also provided with an empennage fastening screw, and fuselage is provided with corresponding empennage fastening screw cover.
3. the fast inserting structure of empennage according to claim 2, is characterized in that: the main pin bushing of empennage and empennage fastening screw cover are installed respectively and arranged on the carbon pipe bracket of its correspondence.
4. the fast inserting structure of empennage according to claim 3, is characterized in that: fuselage is also provided with one for installing the plug firm banking of quick detach snap close.
5. the fast inserting structure of empennage according to claim 4, is characterized in that: fuselage interior is provided with an integral support, and each carbon pipe bracket and plug firm banking are all fixedly installed on integral support.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520903201.2U CN205113680U (en) | 2015-11-13 | 2015-11-13 | Fin quick -insertion structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520903201.2U CN205113680U (en) | 2015-11-13 | 2015-11-13 | Fin quick -insertion structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205113680U true CN205113680U (en) | 2016-03-30 |
Family
ID=55569313
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520903201.2U Active CN205113680U (en) | 2015-11-13 | 2015-11-13 | Fin quick -insertion structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205113680U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106218850A (en) * | 2016-07-27 | 2016-12-14 | 东莞前沿技术研究院 | Dirigible |
-
2015
- 2015-11-13 CN CN201520903201.2U patent/CN205113680U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106218850A (en) * | 2016-07-27 | 2016-12-14 | 东莞前沿技术研究院 | Dirigible |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 518000, 13th Floor, Building A4, Nanshan Zhiyuan, No. 1001 Xueyuan Avenue, Changyuan Community, Taoyuan Street, Nanshan District, Shenzhen, Guangdong Province Patentee after: Shenzhen Pegasus Robotics Co.,Ltd. Country or region after: China Address before: 518000, 1st Floor, 16th Building, Zhiheng Industrial Park, Nantou Street, Nanshan District, Shenzhen City, Guangdong Province Patentee before: SHENZHEN FEIMA ROBOTICS Co.,Ltd. Country or region before: China |
|
| CP03 | Change of name, title or address |