CN109018425A - A kind of small drone steering engine exchanging structure of low cost - Google Patents
A kind of small drone steering engine exchanging structure of low cost Download PDFInfo
- Publication number
- CN109018425A CN109018425A CN201810982538.5A CN201810982538A CN109018425A CN 109018425 A CN109018425 A CN 109018425A CN 201810982538 A CN201810982538 A CN 201810982538A CN 109018425 A CN109018425 A CN 109018425A
- Authority
- CN
- China
- Prior art keywords
- changeover base
- connecting plate
- steering engine
- small drone
- low cost
- 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.)
- Pending
Links
- 238000009434 installation Methods 0.000 abstract description 11
- 238000012545 processing Methods 0.000 abstract description 8
- 238000013461 design Methods 0.000 abstract description 7
- 239000007769 metal material Substances 0.000 abstract description 4
- 238000005457 optimization Methods 0.000 abstract description 4
- 238000003754 machining Methods 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 2
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 2
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/40—Maintaining or repairing aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Steering Controls (AREA)
Abstract
The application belongs to field of machining, more particularly to a kind of small drone steering engine exchanging structure of low cost, including main changeover base, support plate there are two being vertically arranged in the main changeover base, the two sides of the main changeover base are respectively arranged with the first connecting plate and the second connecting plate, it is connected with the first changeover base on first connecting plate, the second changeover base is provided on second connecting plate, is provided with lid above the main changeover base.This structure is suitable for the installation of general small drone standard steering engine, and installation and the mode dismantled are simple, fast；Structure is added using common metal material numerical control machine, and difficulty of processing is small, and processing cost is low；Screw selects the fastener of the national universal standard, is easy to purchase, high reliablity；The outer dimension of lid passes through optimization design, and the shape coordinate design with empennage utmostly reduces resistance.
Description
Technical field
The application belongs to the small drone steering engine exchanging structure of field of machining more particularly to a kind of low cost.
Background technique
Chinese Small-sized unmanned plane industry upsurge is sprung up, dog-eat-dog, and control cost becomes the target of small drone development
One of.How under the premise of guaranteeing quality and meeting functional requirement, the pass that cost is also small drone is maximumlly reduced
One of key technology.Cost control, first aspect experience the complexity in structure, and second aspect is embodied in the difficulty or ease journey of processing
Degree, the third aspect are embodied in the lengthy and jumbled degree of assembly.Fourth aspect is embodied in maintainability.The outer wing and empennage of general small drone
Selection standard steering engine.After standard steering engine occurs using failure, need that steering engine is repaired or replaced in time.
Summary of the invention
For the requirement of the above-mentioned prior art, a kind of small drone steering engine exchanging structure of low cost is provided, it is this
Structure can not only realize being rapidly assembled and disassembled for steering engine, while effectively increase the aerodynamic configuration of empennage.
In order to realize the above technical effect, the technical solution of the application is as follows:
A kind of small drone steering engine exchanging structure of low cost, which is characterized in that including main changeover base, the main switching
It is vertically arranged on pedestal there are two support plate, the two sides of the main changeover base are respectively arranged with the first connecting plate and the second connection
Plate is connected with the first changeover base on first connecting plate, the second changeover base is provided on second connecting plate, described
Lid is provided with above main changeover base.
Fixing screws are provided in the support plate.
First changeover base is connect with the first connecting plate by fixing screws, and second changeover base connects with second
Fishplate bar is connected by fixing screws.
The lid passes through fixing screws respectively and is connected with the first connecting plate and the second connecting plate.
It is provided with lug boss in the middle part of the lid, the lower section of the lug boss is supporting plate structure, by the lug boss
It is provided with uncovered structure.
The installation steps of the application are as follows:
Steering engine is quick for installation, and the process of process implementing is broadly divided into 3 steps: in outside, the machine of steering is placed on main changeover base
On, it is fixed by 4 fixing screws；
The main changeover base for installing steering engine is assembled to the first changeover base and the second changeover base by 2 fixing screws
On；
Lid is mounted in main changeover base by fixing screws.
The advantages of the application, is:
This structure is suitable for the installation of general small drone standard steering engine, and installation and the mode dismantled are simple, fast；
Structure is added using common metal material numerical control machine, and difficulty of processing is small, and processing cost is low；Screw selects the national universal standard
Fastener, be easy to purchase, high reliablity；The outer dimension of lid is by optimization design, the shape coordinate design with empennage, most
Big degree reduces resistance.
Detailed description of the invention
Fig. 1 is the main changeover base structural schematic diagram of the application.
Fig. 2 is the application assemble sequence schematic diagram.
In figure:
The main changeover base of 1-, 2- support plate, the first connecting plate of 3-, the second connecting plate of 4-, the first changeover base of 5-, 6- second transfer
Pedestal, 7- lid, 8- fixing screws, 9- lug boss, 10- uncovered structure.
Specific embodiment
Embodiment 1
A kind of small drone steering engine exchanging structure of low cost includes main changeover base 1, vertical in the main changeover base 1
There are two support plates 2 for setting, and the two sides of the main changeover base 1 are respectively arranged with the first connecting plate 3 and the second connecting plate 4, institute
It states and is connected with the first changeover base 5 on the first connecting plate 3, the second changeover base 6 is provided on second connecting plate 4, it is described
Lid 7 is provided with above main changeover base 1.This structure is suitable for the installation of general small drone standard steering engine, installation
And the mode of disassembly is simple, fast；Structure is added using common metal material numerical control machine, and difficulty of processing is small, is processed into
This is low；Screw selects the fastener of the national universal standard, is easy to purchase, high reliablity；The outer dimension of lid 7 is set by optimization
Meter, the shape coordinate design with empennage utmostly reduce resistance.
Embodiment 2
A kind of small drone steering engine exchanging structure of low cost includes main changeover base 1, vertical in the main changeover base 1
There are two support plates 2 for setting, and the two sides of the main changeover base 1 are respectively arranged with the first connecting plate 3 and the second connecting plate 4, institute
It states and is connected with the first changeover base 5 on the first connecting plate 3, the second changeover base 6 is provided on second connecting plate 4, it is described
Lid 7 is provided with above main changeover base 1.
Fixing screws 8 are provided in the support plate 2.
First changeover base 5 and the first connecting plate 3 are connect by fixing screws 8, second changeover base 6 and the
Two connecting plates 4 are connected by fixing screws 8.
The lid 7 is connected by fixing screws 8 with the first connecting plate 3 and the second connecting plate 4 respectively.
The middle part of the lid 7 is provided with lug boss 9, and the lower section of the lug boss 9 is 2 structure of support plate, the protrusion
Uncovered structure 10 is provided with by portion 9.
Steering engine is quick for installation, and the process of process implementing is broadly divided into 3 steps: in outside, the machine of steering is placed on main switching bottom
It is fixed by 4 fixing screws 8 on seat 1；
The main changeover base 1 for installing steering engine is assembled to the first changeover base 5 and the second switching bottom by 2 fixing screws 8
On seat 6；
Lid 7 is mounted in main changeover base 1 by fixing screws 8.
This structure is suitable for the installation of general small drone standard steering engine, and installation and the mode dismantled are simple,
Fast；Structure is added using common metal material numerical control machine, and difficulty of processing is small, and processing cost is low；Screw selects country logical
With the fastener of standard, it is easy to purchase, high reliablity；The outer dimension of lid 7 passes through optimization design, coordinates with the shape of empennage
Design, utmostly reduces resistance.
Claims (5)
1. a kind of small drone steering engine exchanging structure of low cost, which is characterized in that described including main changeover base (1)
There are two being vertically arranged on main changeover base (1) support plate (2), the two sides of the main changeover base (1) are respectively arranged with first
Connecting plate (3) and the second connecting plate (4) are connected with the first changeover base (5) on first connecting plate (3), and described second connects
It is provided on fishplate bar (4) the second changeover base (6), is provided with lid (7) above the main changeover base (1).
2. a kind of small drone steering engine exchanging structure of low cost according to claim 1, which is characterized in that described
Fixing screws (8) are provided in support plate (2).
3. a kind of small drone steering engine exchanging structure of low cost according to claim 1, which is characterized in that described
First changeover base (5) is connect with the first connecting plate (3) by fixing screws (8), and second changeover base (6) connects with second
Fishplate bar (4) is connected by fixing screws (8).
4. a kind of small drone steering engine exchanging structure of low cost according to claim 1, which is characterized in that described
Lid (7) is connected by fixing screws (8) with the first connecting plate (3) and the second connecting plate (4) respectively.
5. a kind of small drone steering engine exchanging structure of low cost according to claim 1, which is characterized in that described
It is provided in the middle part of lid (7) lug boss (9), the lower section of the lug boss (9) is support plate (2) structure, the lug boss (9)
Side is provided with uncovered structure (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810982538.5A CN109018425A (en) | 2018-08-27 | 2018-08-27 | A kind of small drone steering engine exchanging structure of low cost |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810982538.5A CN109018425A (en) | 2018-08-27 | 2018-08-27 | A kind of small drone steering engine exchanging structure of low cost |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109018425A true CN109018425A (en) | 2018-12-18 |
Family
ID=64624679
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810982538.5A Pending CN109018425A (en) | 2018-08-27 | 2018-08-27 | A kind of small drone steering engine exchanging structure of low cost |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109018425A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20130137336A1 (en) * | 2010-08-13 | 2013-05-30 | Kanghan Ni | Linkage device for remote control model helicopter with coaxial and counter rotating double-propeller |
| CN105217019A (en) * | 2015-10-16 | 2016-01-06 | 河南翱翔航空科技有限公司 | Unmanned plane horizontal tail wing control mechanism |
| CN205971884U (en) * | 2016-08-30 | 2017-02-22 | 北方天途航空技术发展（北京）有限公司 | Can protect light fixed wing uavs of carry equipment |
| CN107010244A (en) * | 2017-04-06 | 2017-08-04 | 观典防务技术股份有限公司 | A kind of split type unmanned plane |
| CN206417186U (en) * | 2017-01-13 | 2017-08-18 | 重庆星环航空科技有限公司 | A kind of steering wheel mounting structure |
| CN206704521U (en) * | 2017-05-17 | 2017-12-05 | 仲恺农业工程学院 | A kind of device for integrating function of foot rest and protective cover function |
| CN107697272A (en) * | 2017-09-11 | 2018-02-16 | 西安冰果智能航空科技有限公司 | A kind of unmanned plane rudder face drive mechanism |
| CN207157495U (en) * | 2017-08-05 | 2018-03-30 | 北京海利天梦科技有限公司 | Unmanned plane hides tail vane linkage |
-
2018
- 2018-08-27 CN CN201810982538.5A patent/CN109018425A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20130137336A1 (en) * | 2010-08-13 | 2013-05-30 | Kanghan Ni | Linkage device for remote control model helicopter with coaxial and counter rotating double-propeller |
| CN105217019A (en) * | 2015-10-16 | 2016-01-06 | 河南翱翔航空科技有限公司 | Unmanned plane horizontal tail wing control mechanism |
| CN205971884U (en) * | 2016-08-30 | 2017-02-22 | 北方天途航空技术发展（北京）有限公司 | Can protect light fixed wing uavs of carry equipment |
| CN206417186U (en) * | 2017-01-13 | 2017-08-18 | 重庆星环航空科技有限公司 | A kind of steering wheel mounting structure |
| CN107010244A (en) * | 2017-04-06 | 2017-08-04 | 观典防务技术股份有限公司 | A kind of split type unmanned plane |
| CN206704521U (en) * | 2017-05-17 | 2017-12-05 | 仲恺农业工程学院 | A kind of device for integrating function of foot rest and protective cover function |
| CN207157495U (en) * | 2017-08-05 | 2018-03-30 | 北京海利天梦科技有限公司 | Unmanned plane hides tail vane linkage |
| CN107697272A (en) * | 2017-09-11 | 2018-02-16 | 西安冰果智能航空科技有限公司 | A kind of unmanned plane rudder face drive mechanism |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204747867U (en) | Cabinet welding jig is pieced together to cabinet body | |
| CN208746270U (en) | A kind of small drone steering engine exchanging structure of low cost | |
| CN206533656U (en) | Structure is fixedly mounted in a kind of pcb board | |
| CN109018425A (en) | A kind of small drone steering engine exchanging structure of low cost | |
| CN211490380U (en) | Variable-force press-fitting machine for thermostat seat | |
| CN207385975U (en) | The multidirectional quick light-dividing device of feed type | |
| CN107414711B (en) | Novel assembly jig for cementing of rear machine body | |
| CN205525019U (en) | Unmanned aerial vehicle aerial survey camera supporting structure | |
| CN210774593U (en) | Vibration experiment tool compatible with various types of steering engines | |
| CN209938963U (en) | Novel modularization unmanned aerial vehicle | |
| CN203882054U (en) | Intelligent touch all-in-one machine structure capable of being achieved quickly | |
| CN208483364U (en) | A kind of driving side plate of electric resistance welding X-type welding gun | |
| CN204613356U (en) | A kind of transistor test device | |
| CN109227448A (en) | Aircraft spherical surface frame guarantor's type positioning tool | |
| CN204372458U (en) | A kind of 3D printer frame | |
| CN216265609U (en) | Fixing tool for processing antenna base | |
| CN205651262U (en) | Positioning anchor clamps | |
| CN206471267U (en) | A kind of isolator operating mechanism connected without standard component | |
| CN215035127U (en) | Double-station composite bearing press-fitting machine for shaft parts | |
| CN208837721U (en) | A kind of exchange cooking machine | |
| CN207611720U (en) | A kind of riveting mechanism of relay spring and yoke | |
| CN209999348U (en) | cutting device convenient to mount | |
| CN204179234U (en) | The assembled adjusting device of radio telescope unit panel of reflecting surface subelement | |
| CN204135974U (en) | High accuracy MSASM assembly machine | |
| CN213566435U (en) | Unmanned aerial vehicle frame of mortise and tenon joint structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20181218 |