CN208947585U - A kind of unmanned plane that foot prop is convenient for disassembly and assembly - Google Patents
A kind of unmanned plane that foot prop is convenient for disassembly and assembly Download PDFInfo
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- CN208947585U CN208947585U CN201821422888.8U CN201821422888U CN208947585U CN 208947585 U CN208947585 U CN 208947585U CN 201821422888 U CN201821422888 U CN 201821422888U CN 208947585 U CN208947585 U CN 208947585U
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Abstract
Foot prop described in the utility model unmanned plane convenient for disassembly and assembly, including fuselage, foot prop, its main feature is that: the foot prop is U-shaped frame, the foot prop is connected on fuselage in which can be removably mounted by fastening device, the fastening device include be set on fuselage bottom case can with the screw structure of the first end rotary clamping of foot prop, the elasticity pressing fastening structure of holding can be cooperated with the second end of foot prop.The utility model is when dismounting foot prop, it does not need by tool, can be directly clamped with hand by one end that compression elasticity Pressing fastener binding structure disengages foot prop, then rotate foot prop and disengage other end clamping, foot prop can be made rapidly to dismantle with fuselage, dismantled very convenient, quick.
Description
Technical field
The utility model relates to unmanned plane field, especially a kind of unmanned plane that foot prop is convenient for disassembly and assembly.
Background technique
The relevant technologies of multiaxis unmanned vehicle (abbreviation unmanned plane) and application flourish in recent years, the utilization of unmanned plane
Field is popularized for ordinary consumer from profession shooting gradually, and portable volume is the acceptable principal element of consumer,
In the case where not influencing performance and overall weight, how effective and quick and convenient dismantling assembling increases to reduce small product size
Storage property and the convenience for promoting the maintenance replacement of components are the technical issues that need to address.
It include fuselage in the housing construction of traditional unmanned plane, fuselage connects horn, is provided with power device and paddle on horn
Leaf.The lower end of fuselage is connected with foot prop, and foot prop is fixed by screws in bottom case lower end.This foot stand connecting structure, due to
It needs to carry out by tool (such as screwdriver) when dismounting, so dismounting is inconvenient, dismounting speed is also relatively slow.
Summary of the invention
The purpose of this utility model is that not needing to borrow when providing a kind of disassembly of foot prop for above-mentioned there are problem and shortage
Assistant engineer's tool, convenient for disassembly and assembly, efficiently unmanned plane.
The technical solution of the utility model is achieved in that
Foot prop described in the utility model unmanned plane convenient for disassembly and assembly, including fuselage, foot prop, its main feature is that: the foot prop is U
Shape frame (or approximate U shape frame), the foot prop are connected on fuselage in which can be removably mounted by fastening device, and the fastening device includes setting
Be placed on fuselage bottom case can with the screw structure of the first end rotary clamping of foot prop, can cooperate with the second end of foot prop and block
The elasticity pressing fastening structure set.
Wherein, above-mentioned fuselage bottom case is equipped with the inserting mouth for foot prop the second end inserting, above-mentioned elasticity pressing snapping
Structure includes the elastic pressing piece for being installed on the band buckle at fuselage bottom case inserting mouth, corresponding is set to foot prop the second end
Can be clasped holding locking bayonet arrangement.
To make its more convenient operation while structure is reliable, one end of above-mentioned elasticity pressing piece is to be connected to fuselage bottom case
Be fixedly connected with portion, the other end is that can be placed through the button portion of fuselage bottom case up and down, and be connected in the button portion multiple
Position spring, above-mentioned buckle are set to the middle part of elastic pressing piece and stretch downwards and be placed in inserting mouth, and above-mentioned fuselage bottom case is located at inserting
Mouth beside is provided with the perforation placed for the button portion accordingly.
Further technical solution is: above-mentioned fuselage bottom case inserting mouth is that length jaggy is opened in the side far from above-mentioned button portion
Slotted hole structure, sleeve column protruding upward is equipped on the end face of above-mentioned foot prop the second end accordingly, and above-mentioned bayonet arrangement is to open up
In the card slot on sleeve column, after the second end of above-mentioned foot prop inserts the side notch insertion of mouth by its sleeve column from fuselage bottom case,
It is promoted to the button portion direction and slides to above-mentioned buckle and realize locking in the bayonet arrangement, and is described pressing up
It takes off buckle from bayonet arrangement and realizes unlock.
To keep its structure simpler, above-mentioned screw structure includes the T shape card convex for being set to foot prop first end, corresponding setting
In the card hole of above-mentioned fuselage bottom case, rotation is (general after the first end of the foot prop is packed into the card hole by its T shape card convex
It is 60 ~ 90 degree of rotation) realize locking.
The utility model due to passing through screw structure and elasticity pressing fastening structure energy using by the both ends of U-shaped foot prop respectively
It is removably connected on fuselage, so the utility model is not needed when dismounting foot prop by tool, can directly be pressed with hand
Elasticity pressing fastening structure disengages one end clamping of foot prop, and rotation foot prop disengages other end clamping, can make foot prop rapidly
It is dismantled with fuselage, dismantles so very convenient, quick, unmanned plane is also convenient for collecting, transports, carries and part replacement maintenance,
The needs of the majority of consumers can be met.
The utility model will be further described below with reference to the accompanying drawings.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the assembling structure schematic diagram of the utility model middle fuselage bottom case and foot prop；
Fig. 3 is that structural schematic diagram cuts open in the office of the utility model；
Fig. 4 is the structure enlargement diagram in Fig. 3 at A.
Specific embodiment
As Figure 1-Figure 4, foot prop described in the utility model unmanned plane convenient for disassembly and assembly, including fuselage 1, foot prop 2,
In, the foot prop 2 is U-shaped frame, and the foot prop 2 is connected on fuselage 1 in which can be removably mounted by fastening device, the fastening device packet
Include be set on 1 bottom case of fuselage can with the screw structure of the first end rotary clamping of foot prop 2, can be with the second end of foot prop 2
Portion cooperates the elasticity pressing fastening structure of holding.The utility model is not needed when dismounting foot prop 2 by tool, can be direct
One end clamping of foot prop 2 is disengaged by compression elasticity Pressing fastener binding structure with hand, and rotation foot prop disengages other end clamping, so that it may make foot
Frame is rapidly dismantled with fuselage, is dismantled very convenient, quick.To keep the utility model structure simpler, above-mentioned 1 bottom case of fuselage is set
There is the inserting mouth 11 for 2 the second end of foot prop inserting, above-mentioned elasticity pressing fastening structure includes being installed on 1 bottom of fuselage
The elastic pressing piece 3 with buckle 31, corresponding be set at shell inserting mouth 11 block capable of cooperating with buckle 31 for 2 the second end of foot prop
Set the bayonet arrangement 20 of locking.One end of above-mentioned elasticity pressing piece 3 be connected to 1 bottom case of fuselage be fixedly connected with portion, the other end
For the button portion 32 that can be placed through 1 bottom case of fuselage up and down, and reset spring is connected in the button portion 32 and (is also possible to
Other return units), above-mentioned buckle 31 is set to the middle part of elastic pressing piece 3 and stretches downwards and is placed in inserting mouth 11, above-mentioned 1 bottom of fuselage
Shell is located at inserting 11 beside of mouth and is provided with the perforation placed for the button portion 32 accordingly.To keep its inserting more convenient, on
Stating 1 bottom case of fuselage inserting mouth 11 is elongated slot pore structure, which is provided with notch far from the side of above-mentioned button portion 32, on
It states and is equipped with sleeve column 21 protruding upward on the end face of 2 the second end of foot prop accordingly, above-mentioned bayonet arrangement 20 is to be opened in sleeve column
Card slot on 21, after the second end of above-mentioned foot prop 2 inserts the side notch insertion of mouth by its sleeve column from 1 bottom case of fuselage, to
The button portion direction promotes and slides to above-mentioned buckle 31 and realize locking in the bayonet arrangement 20, and pressing up
So that the abjection from bayonet arrangement 20 of buckle 31 is realized unlock when stating button portion 32, operates extremely convenient.Further to simplify it
Structure, above-mentioned screw structure include the T shape card convex 22 for being set to 2 first end of foot prop, are accordingly set to above-mentioned 1 bottom case of fuselage
Card hole 12, rotation (certain angle) is realized after the first end of the foot prop 2 is packed into the card hole 12 by its T shape card convex 22
Locking.After the end of the T shape card convex 22 has two edges, the T shape card convex 22 of the first end of foot prop 2 to pack into card hole 12, rotation
90 degree, so that it may so that two edge of end of card convex is transferred to simultaneously overhead and realize positive lock in the hole edge of 12 inside of card hole.To prevent
Card convex rotation is excessively deviate from, and the inner surface at above-mentioned card hole 12 is equipped with limited block.To reinforce the structural strength at card hole 12,
Reinforcing rib can be also equipped with around above-mentioned card hole 12.To keep foot prop support more stable, the bottom center of above-mentioned U-shaped frame is bent up
And then two pin points are formed in 2 bottom of foot prop.The utility model structure is simple, foot prop disassembly is very convenient, quick, facilitates receipts
It receives, transport, the replacement maintenance of carrying and part.
Although the utility model is to be described with reference to specific embodiments, this description is not meant to the utility model
It is construed as limiting.Referring to the description of the utility model, other variations of the disclosed embodiments are all for those skilled in the art
It is anticipated that, this variation should belong in appended claims limited range.
Claims (8)
1. a kind of unmanned plane that foot prop is convenient for disassembly and assembly, including fuselage (1), foot prop (2), it is characterised in that: the foot prop (2) is U
Shape frame, the foot prop (2) are connected on fuselage (1) in which can be removably mounted by fastening device, and the fastening device includes being set to machine
On the bottom case of body (1) can with the screw structure of the first end rotary clamping of foot prop (2), can be with the second end of foot prop (2)
Cooperate the elasticity pressing fastening structure of holding.
2. unmanned plane according to claim 1, it is characterised in that: above-mentioned fuselage (1) bottom case is equipped with for the foot prop (2) the
The inserting mouth (11) of two ends inserting, above-mentioned elasticity pressing fastening structure include being installed on the fuselage (1) bottom case inserting mouth
(11) at buckle (31) elastic pressing piece (3), be accordingly set to capable of cooperating with buckle (31) for foot prop (2) the second end
The bayonet arrangement (20) of holding locking.
3. unmanned plane according to claim 2, it is characterised in that: one end of above-mentioned elasticity pressing piece (3) is to be connected to machine
Body (1) bottom case is fixedly connected with portion, and the other end is the button portion (32) that can be placed through fuselage (1) bottom case up and down, and should
Be connected with reset spring in button portion (32), above-mentioned buckle (31) be set to the middle part of elastic pressing piece (3) and stretching downwards be placed in it is slotting
It fills in mouth (11), above-mentioned fuselage (1) bottom case is provided with accordingly positioned at inserting mouth (11) beside and wears for the button portion (32)
The perforation set.
4. unmanned plane according to claim 3, it is characterised in that: above-mentioned fuselage (1) bottom case inserting mouth (11) is long slot hole
Structure, the elongated slot pore structure are provided with notch far from the side of above-mentioned button portion (32), on the end face of above-mentioned foot prop (2) the second end
It is equipped with sleeve column (21) protruding upward accordingly, above-mentioned bayonet arrangement (20) is the card slot being opened on sleeve column (21), above-mentioned foot
After the second end of frame (2) inserts the side notch insertion of mouth by its sleeve column from fuselage (1) bottom case, Xiang Suoshu button portion direction
It promotes and slides to above-mentioned buckle (31) and realize locking in the bayonet arrangement (20), and pressing up the button portion
(32) make to buckle (31) abjection realization unlock from bayonet arrangement (20) when.
5. unmanned plane according to claim 1, it is characterised in that: above-mentioned screw structure includes being set to foot prop (2) first
The first end of the T shape card convex (22) of end, the card hole (12) for being accordingly set to above-mentioned fuselage (1) bottom case, the foot prop (2) is logical
It crosses rotation after its T shape card convex (22) packs into the card hole (12) and realizes locking.
6. unmanned plane according to claim 5, it is characterised in that: the inner surface at above-mentioned card hole (12) is equipped with limiting block
Block.
7. unmanned plane according to claim 5, it is characterised in that: be equipped with reinforcing rib around above-mentioned card hole (12).
8. unmanned plane according to claim 1, it is characterised in that: the bottom center of above-mentioned U-shaped frame is bent into upwards.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821422888.8U CN208947585U (en) | 2018-08-31 | 2018-08-31 | A kind of unmanned plane that foot prop is convenient for disassembly and assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821422888.8U CN208947585U (en) | 2018-08-31 | 2018-08-31 | A kind of unmanned plane that foot prop is convenient for disassembly and assembly |
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| Publication Number | Publication Date |
|---|---|
| CN208947585U true CN208947585U (en) | 2019-06-07 |
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ID=66736427
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821422888.8U Active CN208947585U (en) | 2018-08-31 | 2018-08-31 | A kind of unmanned plane that foot prop is convenient for disassembly and assembly |
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| Country | Link |
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| CN (1) | CN208947585U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115180125A (en) * | 2022-09-09 | 2022-10-14 | 致导创新(天津)科技有限公司 | Unmanned aerial vehicle foot rest connection structure |
-
2018
- 2018-08-31 CN CN201821422888.8U patent/CN208947585U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115180125A (en) * | 2022-09-09 | 2022-10-14 | 致导创新(天津)科技有限公司 | Unmanned aerial vehicle foot rest connection structure |
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