CN209617488U - A kind of modularization head - Google Patents
A kind of modularization head Download PDFInfo
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- CN209617488U CN209617488U CN201920021351.9U CN201920021351U CN209617488U CN 209617488 U CN209617488 U CN 209617488U CN 201920021351 U CN201920021351 U CN 201920021351U CN 209617488 U CN209617488 U CN 209617488U
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- head
- fuselage
- modularization
- mounting hole
- hole
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Abstract
The utility model discloses a kind of modularization heads, including head and fuselage, wherein, multiple bolts are fixed at the head tail end inner wall, multiple connecting tubes are provided at the fuselage inner wall, the bolt is protruded into the connecting tube, and is fixedly connected by fixing bolt.The problems in the utility model is not only simple in structure, easy for installation, and is easy to implement the replacement of unmanned plane internal motivation accessory, and be able to solve head stress collection.
Description
Technical field
The utility model belongs to air vehicle technique field, more particularly to a kind of modularization head.
Background technique
Unmanned plane, that is, UAV is manipulated not using radio robot and the presetting apparatus provided for oneself
Manned aircraft, unmanned plane are mainly made of head and fuselage, are mostly one after head and the fuselage cooperation of current unmanned plane
Formula structure, the accessory structure inside unmanned plane are not easy to replace.
Therefore, the problem of how to provide a kind of modularization head becomes those skilled in the art's urgent need to resolve.
Utility model content
In view of this, the present invention provides a kind of modularization heads, are not only simple in structure, easy for installation, Er Qiebian
The problems in the replacement of realization unmanned plane internal motivation accessory, and be able to solve head stress collection.
To achieve the goals above, the utility model adopts the following technical solution:
A kind of modularization head, comprising: head and fuselage, wherein multiple bolts are fixed at the head tail end inner wall,
Multiple connecting tubes are provided at the fuselage inner wall, the bolt protrudes into the connecting tube, and connects by the way that fixing bolt is fixed
It connects.
Preferably, mounting hole one is offered on the bolt, is provided in the connecting tube and is matched with the mounting hole one
The mounting hole two of conjunction, the fixing bolt are connected through the mounting hole two and with the mounting hole one.
Preferably, head tail end setting is there are two spare hole one, the fuselage head end setting there are two with it is described standby
The spare hole two to be matched with hole one.It, can be by spare hole one and standby when needing to increase other equipment or replacement is electric-powered
Increase required interface with hole two.
Preferably, the spare hole one and two upper cover of spare hole are equipped with sealing cover.Spare hole one and spare hole two exist
When not in use, covering sealing cover makes head and fuselage keep sealing.
Preferably, the head tail end is provided with spininess aviation plug female, the fuselage head end be provided with it is described more
The spininess aviation plug male connector that needle aviation plug female matches.The sealing wire of electronic equipment needed for head is mounted on spininess aviation
In plug female and spininess aviation plug male connector, and realized and electricity by spininess aviation plug female and spininess aviation plug male connector
The connection in source.
Preferably, the head tail end is provided with engine oil pipe fitting female, the fuselage head end be provided with it is described
The engine oil pipe fitting male connector that engine oil pipe fitting female matches.Engine oil inlet pipe sequentially passes through engine oil tube and connects
After head female, engine oil pipe fitting male connector, it is connected with fuel tank.
Preferably, clump weight is additionally provided in the head.Increase the counterweight module of clump weight and afterbody in head
Cooperation increases the stability of equilibrium of unmanned plane, solves the problems, such as drone center of unmanned aerial vehicle offset.
Preferably, CDI igniter and engine apparatus are installed in the head.The setting of CDI igniter is convenient for starting
The starting of machine equipment can provide flying power by engine apparatus for unmanned plane.
Preferably, airborne control equipment and power supply are provided in the fuselage, the CDI igniter, the engine are set
Standby, the described airborne control equipment is electrically connected with the power supply.Power supply can be CDI igniter, engine apparatus and airborne
Control the electric energy needed for equipment provides；The wireless connection with ground control centre can be realized by airborne control equipment, thus real
The control of existing unmanned plane during flying state.
The utility model has the beneficial effects that:
The utility model structure is simple, easy for installation, and head and fuselage are convenient for by the mating connection of bolt and connecting tube
It realizes the replacement of unmanned plane internal motivation accessory, and fuselage is transmitted to by the power that connecting tube can be born head, can solve
Certainly the problems in head stress collection.
Detailed description of the invention
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, the accompanying drawings in the following description is only
It is the embodiments of the present invention, for those of ordinary skill in the art, without creative efforts, also
Other attached drawings can be obtained according to the attached drawing of offer.
Fig. 1 attached drawing is the structural schematic diagram of the utility model.
Fig. 2 attached drawing is a kind of assembly state diagram of the utility model bolt and connecting tube.
Fig. 3 attached drawing is another assembly state diagram of the utility model bolt and connecting tube.
Fig. 4 attached drawing is a kind of assembly state diagram of the utility model head and fuselage.
Fig. 5 attached drawing is another assembly state diagram of the utility model head and fuselage.
Wherein, in figure,
1- head；2- fuselage；3- bolt；4- connecting tube；5- fixing bolt；6- mounting hole one；7- mounting hole two；8- is spare
Kong Yi；The spare hole two 9-；10- spininess aviation plug female；11- needle aviation plug male connector；12- sealing wire；13- power supply；14- hair
Motivation oil connection female；15- engine oil pipe fitting male connector；16- engine oil inlet pipe；17- fuel tank；18- clump weight；19-
CDI igniter；20- engine apparatus；The airborne control equipment of 21-.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Attached drawing 1-5 is please referred to, the utility model provides a kind of modularization head, comprising: head 1 and fuselage 2, wherein
It is fixed with multiple bolts 3 at 1 tail end inner wall of head, multiple connecting tubes 4 are provided at 2 inner wall of fuselage, bolt 3 protrudes into connecting tube 4
It is interior, and be fixedly connected by fixing bolt 5, it is quick and easy for installation.
In order to further optimize the above technical scheme, bolt 3 is set as 4, be all made of 7075 solid aluminum alloys production and
At connecting tube is also configured as 4, is made using aluminum alloy square tube, and fixing bolt uses high-strength bolt, to improve
The bonding strength of head 1 and fuselage 2.
Mounting hole 1 is offered on bolt 3, and the mounting hole 27 matched with mounting hole 1 is provided in connecting tube 4, Gu
The diameter for determining 5 head of bolt is greater than the diameter of mounting hole 27, and 5 penetrating mounting holes 27 of fixing bolt are simultaneously connected with mounting hole 1,
To realize the assembly connection of head 1 Yu fuselage 2, no longer needs to add other reinforcing members, facilitate installation.
For the setting of 1 tail end of head there are two spare hole 1, the setting of 2 head end of fuselage is standby there are two matching with spare hole 1
With hole 29.When needing to increase other equipment or replacement is electric-powered, needed for being increased by spare hole 1 and spare hole 29
Interface.
In order to further optimize the above technical scheme, spare hole 1 and 29 upper cover of spare hole are equipped with sealing cover.Spare hole
1 and spare hole 29 so that head 1 and fuselage 2 is kept sealing when not in use, covering sealing cover.
1 tail end of head is provided with spininess aviation plug female 10, and 2 head end of fuselage is provided with and spininess aviation plug female 10
The spininess aviation plug male connector 11 to match.The sealing wire 12 of electronic equipment needed for head 1 is mounted on spininess aviation plug female
10 and spininess aviation plug male connector 11 in, when installation, 11 grafting of spininess aviation plug female 10 and spininess aviation plug male connector, i.e.,
The connection of electronic equipment and power supply 13 needed for head 1 can be achieved.
1 tail end of head is provided with engine oil pipe fitting female 14, and 2 head end of fuselage is provided with female with engine oil pipe fitting
The first 14 engine oil pipe fitting male connectors 15 to match.Engine oil inlet pipe 16 sequentially pass through engine oil pipe fitting female 14,
After engine oil pipe fitting male connector 15, it is connected with fuel tank 17, by engine oil pipe fitting female 14 and engine oil when installation
Oil circuit conducting can be realized in 15 grafting of pipe fitting male connector.
In order to further optimize the above technical scheme, clump weight 18 is additionally provided in head 1.Increase clump weight in head 1
18 increase the stability of equilibrium of unmanned plane with the counterweight module cooperation of 2 tail portion of fuselage, solve asking for drone center of unmanned aerial vehicle offset
Topic.
The ancillary equipment of CDI igniter 19, engine apparatus 20 and engine apparatus is installed in head 1.CDI igniting
The starting of engine apparatus 20 is convenient in the setting of device 19, can provide flying power by engine apparatus 20 for unmanned plane.
Airborne control equipment 21 and power supply 13, CDI igniter 19, engine apparatus 20, airborne control are provided in fuselage 2
Equipment 21 is electrically connected with power supply 13.Power supply 13 can be CDI igniter 19, engine apparatus 20 and airborne control equipment 21
Electric energy needed for providing；The wireless connection with ground control centre can be realized by airborne control equipment 21, to realize nobody
The control of machine state of flight.
The utility model structure is simple, easy for installation, and head 1 passes through the mating connection of bolt 3 and connecting tube 4 with fuselage 2,
It is easy to implement the replacement of unmanned plane internal motivation accessory, and the power that head 1 is born can be transmitted to by fuselage 2 by connecting tube 4,
It is able to solve the problems in 1 stress collection of head.
Each embodiment in this specification is described in a progressive manner, the highlights of each of the examples are with other
The difference of embodiment, the same or similar parts in each embodiment may refer to each other.For device disclosed in embodiment
For, since it is corresponded to the methods disclosed in the examples, so being described relatively simple, related place is said referring to method part
It is bright.
The foregoing description of the disclosed embodiments can be realized professional and technical personnel in the field or using originally practical new
Type.Various modifications to these embodiments will be readily apparent to those skilled in the art, and determine herein
The General Principle of justice can be realized in other embodiments without departing from the spirit or scope of the present utility model.Cause
This, the present invention will not be limited to the embodiments shown herein, and is to fit to and principles disclosed herein
The widest scope consistent with features of novelty.
Claims (9)
1. a kind of modularization head characterized by comprising head (1) and fuselage (2), wherein in head (1) tail end
It is fixed with multiple bolts (3), is provided with multiple connecting tubes (4) at fuselage (2) inner wall, the bolt (3) protrudes into institute at wall
It states in connecting tube (4), and is fixedly connected by fixing bolt (5).
2. a kind of modularization head according to claim 1, which is characterized in that offer mounting hole on the bolt (3)
One (6) are provided with the mounting hole two (7) matched with the mounting hole one (6), the fixing bolt on the connecting tube (4)
(5) run through the mounting hole two (7) and be connected with the mounting hole one (6).
3. a kind of modularization head according to claim 1, which is characterized in that there are two head (1) the tail end settings
Spare hole one (8), there are two the spare holes two (9) to match with the spare hole one (8) for fuselage (2) the head end setting.
4. a kind of modularization head according to claim 3, which is characterized in that the spare hole one (8) and described spare
Hole two (9) upper cover is equipped with sealing cover.
5. a kind of modularization head according to claim 1, which is characterized in that head (1) tail end is provided with spininess
Aviation plug female (10), fuselage (2) head end are provided with the spininess to match with the spininess aviation plug female (10)
Aviation plug male connector (11).
6. according to claim 1 or a kind of 5 described in any item modularization heads, which is characterized in that head (1) tail end is set
It is equipped with engine oil pipe fitting female (14), fuselage (2) head end is provided with and the engine oil pipe fitting female (14)
The engine oil pipe fitting male connector (15) to match.
7. a kind of modularization head according to claim 1, which is characterized in that be additionally provided with counterweight in the head (1)
Block (18).
8. a kind of modularization head according to claim 1, which is characterized in that be equipped with CDI igniting in the head (1)
Device (19) and engine apparatus (20).
9. a kind of modularization head according to claim 8, which is characterized in that be provided with airborne control in the fuselage (2)
Control equipment (21) and power supply (13), the CDI igniter (19), the engine apparatus (20), the airborne control equipment
(21) it is electrically connected with the power supply (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920021351.9U CN209617488U (en) | 2019-01-07 | 2019-01-07 | A kind of modularization head |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920021351.9U CN209617488U (en) | 2019-01-07 | 2019-01-07 | A kind of modularization head |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209617488U true CN209617488U (en) | 2019-11-12 |
Family
ID=68448894
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920021351.9U Active CN209617488U (en) | 2019-01-07 | 2019-01-07 | A kind of modularization head |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209617488U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109665101A (en) * | 2019-01-07 | 2019-04-23 | 浙江自贸区协同科技有限公司 | A kind of modularization head |
| CN113581477A (en) * | 2021-06-29 | 2021-11-02 | 成都纵横大鹏无人机科技有限公司 | Functional module mounting structure and aircraft adopting same |
-
2019
- 2019-01-07 CN CN201920021351.9U patent/CN209617488U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109665101A (en) * | 2019-01-07 | 2019-04-23 | 浙江自贸区协同科技有限公司 | A kind of modularization head |
| CN113581477A (en) * | 2021-06-29 | 2021-11-02 | 成都纵横大鹏无人机科技有限公司 | Functional module mounting structure and aircraft adopting same |
| CN113581477B (en) * | 2021-06-29 | 2024-04-26 | 成都纵横大鹏无人机科技有限公司 | Function module mounting structure and adopt its aircraft |
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230626 Address after: 710000, 4th Floor, Guangde Garden, West Gate, Xigong University, No.127 Youyi West Road, Beilin District, Xi'an City, Shaanxi Province Patentee after: Xi'an Hangke Intelligent Information Technology Co.,Ltd. Address before: 316000 East side of the first floor of standard plant 9, Small and Micro Enterprise Park, No. 220, Xinma Avenue, Xingang Industrial Park, Dinghai District, Zhoushan, Zhejiang Province Patentee before: ZHEJIANG FREE TRADE ZONE XIETONG TECHNOLOGY Co.,Ltd. |
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| TR01 | Transfer of patent right |