CN209719915U - A kind of rotor internally-arranged type bilayer leaf unmanned plane - Google Patents
A kind of rotor internally-arranged type bilayer leaf unmanned plane Download PDFInfo
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- CN209719915U CN209719915U CN201920393425.1U CN201920393425U CN209719915U CN 209719915 U CN209719915 U CN 209719915U CN 201920393425 U CN201920393425 U CN 201920393425U CN 209719915 U CN209719915 U CN 209719915U
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- Prior art keywords
- support rod
- circular
- leaf
- unmanned plane
- hole
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- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 4
- 229910052799 carbon Inorganic materials 0.000 claims description 4
- 239000000835 fiber Substances 0.000 claims description 4
- 239000000463 material Substances 0.000 claims description 4
- 238000000034 method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003749 cleanliness Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
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Abstract
The utility model relates to a kind of rotor internally-arranged type bilayer leaf unmanned planes, including body, multiple circular through holes are offered on body, wing body in each circular through hole, wing body includes the mounting shell positioned at circular through hole the center point, mounting base is provided through in the middle part of mounting shell, mounting base is intermediate with demarcation plate, the two sides of demarcation plate are respectively and fixedly provided with driving motor, the output shaft end of driving motor is connected with wing, the upper and lower ends of mounting base are integrally formed with bracket, bracket includes strut and axle sleeve, one end of strut is fixed on the side wall of mounting base, the output shaft of driving motor passes through axle sleeve and is connected on wing；2 support rods are symmetrically arranged in the middle part of mounting shell, one end and the mounting shell of support rod are detachably connected, and the other end of support rod is fixed by screws on the inner sidewall of circular through hole；The utility model have the advantages that stability it is strong, it is easy to disassemble, worn convenient for route, convenient for keep overall aesthetics.
Description
Technical field
The utility model belongs to air vehicle technique field, and in particular to a kind of rotor internally-arranged type bilayer leaf unmanned plane.
Background technique
In recent years, with the continuous development of China's science and technology, unmanned plane is widely applied to every field, with unmanned plane skill
The development of art, the double-deck leaf unmanned plane have good running stability in the process of running.However, the current double-deck leaf nobody
Machine is extremely inconvenient in reassembling type, seriously affects the packaging efficiency of unmanned plane.
Utility model content
There is provided the purpose of the utility model is to overcome the deficiencies in the prior art it is a kind of have stability it is strong, it is easy to disassemble,
It is worn convenient for route, the rotor internally-arranged type bilayer leaf unmanned plane convenient for keeping overall aesthetics.
The technical solution of the utility model is under:
A kind of rotor internally-arranged type bilayer leaf unmanned plane, including body, the square structure that the body is integrally formed, body
On offer multiple circular through holes, wing body in each circular through hole, the wing body includes being located at the circular through hole center of circle
The mounting shell at place, is provided through longitudinally disposed mounting base in the middle part of the mounting shell, and the mounting base is intermediate to have point
The barreled structure of partition, the two sides of demarcation plate are respectively and fixedly provided with driving motor, and the output shaft end connection of the driving motor is organic
The wing, for the upper and lower ends of mounting base integrally formed with bracket, the bracket includes strut and axle sleeve, and one end of the strut is solid
It is scheduled on the side wall for being fixed on mounting base, the other end and axle sleeve of strut are integrally formed, and the output shaft of the driving motor passes through
Axle sleeve is connected on wing；2 support rods are symmetrically arranged in the middle part of mounting shell, one end of the support rod and mounting shell are removable
Connection is unloaded, the other end of support rod is fixed by screws on the inner sidewall of circular through hole.
Further, the connecting pin of the support rod and mounting shell is provided with miner diameter end, and the miner diameter end has with support rod
One end of miner diameter end is provided with screw thread.
Further, the miner diameter end of the support rod is threadingly attached in demarcation plate, and support rod is threadingly attached to
On mounting shell.
Further, the line of the support rod in relatively described two circular through hole is straight line.
Further, the extended line of the support rod of relatively described two circular through hole is in 90 °.
Further, the middle part of the body is the installing zone for installing battery and control system, the installing zone
Openable cover board is arranged in top.
Further, the height of the body is greater than in circular through hole the distance of two wing lower edges up and down.
Further, the support rod is the carbon fibre materials of hollow structure.
Compared with prior art, the utility model has the beneficial effects that
1, it in the circular through hole that wing is set to body in the utility model is total to, avoids when storing unmanned plane, due to people
The damage for leading to wing is not paid attention to for misoperation or；
2, the utility model is connected on the circular through hole inner sidewall of body by wing body by dismountable support rod,
Consequently facilitating the maintenance to body, while stability when body operation is effectively ensured；
3, the support rod of the utility model uses the carbon fibre materials of hollow structure, effectively improves the resistance to mechanical energy of support rod
Convenient for the laying to unmanned machine circuit while power, the connection line of driving motor and control system and battery need to only be worn
In support rod, the aesthetics of unmanned plane entirety is effectively ensured；
In short, the utility model is strong, easy to disassemble with stability, wears convenient for route, convenient for holding overall aesthetics
The advantages of.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model.
Fig. 2 is the wing body structural schematic diagram of the utility model.
Wherein, 1, body, 2, circular through hole, 3, mounting shell, 4, mounting base, 5, demarcation plate, 6, driving motor, 7, wing,
8, bracket, 801, strut, 802, axle sleeve, 9, support rod, 901, miner diameter end, 10, cover board.
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.
According to Fig. 1-2, a kind of rotor internally-arranged type bilayer leaf unmanned plane, including body 1, the body 1 are integrated into
The square structure of type offers multiple circular through holes 2, wing body in each circular through hole 2, the wing body on body 1
Mounting shell 3 including being located at 2 the center point of circular through hole, the middle part of the mounting shell 3 is provided through longitudinally disposed mounting base
4, the mounting base 4 is the intermediate barreled structure with demarcation plate 5, and the two sides of the demarcation plate 5 are respectively and fixedly provided with driving motor
6, the output shaft end of the driving motor 6 is connected with wing 7, and the upper and lower ends of mounting base 4 are described integrally formed with bracket 8
Bracket 8 includes strut 801 and axle sleeve 802, and one end of the strut 801 is fixed on the side wall of mounting base 4, strut
801 other end and axle sleeve 802 is integrally formed, and the output shaft of the driving motor 6 passes through axle sleeve 802 and is connected on wing 7, from
And it is limited by output shaft of the bracket 8 to driving motor 6；The middle part of mounting shell 3 is symmetrically arranged with 2 support rods 9, institute
The one end and mounting shell 3 for stating support rod 9 are detachably connected by screw thread, and the other end of support rod 9 is fixed by screws in circle
On the inner sidewall of through-hole 2.
In the present embodiment, the connecting pin of the support rod 9 and mounting shell 3 is provided with miner diameter end 901, the miner diameter end 901
With support rod 9 there is one end of miner diameter end 901 to be provided with screw thread, consequently facilitating the dismounting between support rod 9 and mounting shell 3.
In the present embodiment, the miner diameter end 901 of the support rod 9 is threadingly attached in demarcation plate 5, and support rod 9 passes through
It is threadedly connected on mounting shell 3.
In the utility model, the line of the support rod 9 in relatively described two circular through hole 2 is straight line, relatively described
The extended line of the support rod 9 of two circular through holes 2 is in 90 °, thus when the overall aesthetics and operation of the utility model is effectively ensured
Cleanliness.
In the present embodiment, the middle part of the body 1 is the installing zone for installing battery and control system, the installation
Openable cover board 10 is arranged in the top in area.
In the utility model, the height of the body 1 is greater than in circular through hole 2 distance of two wing lower edges up and down.
In the present embodiment, the support rod 9 is the carbon fibre materials of hollow structure, thus being convenient for wearing driving motor 6
While line, the mechanical performance of support rod is effectively improved, good supporting role is played to wing body.
The utility model during installation, after mounting rod 9 is connected through a screw thread in mounting shell 3, by the another of support rod 9
End is fixed by screws on the inner sidewall of circular through hole 2, wherein for wearing driving in the support rod 9 of installing zone side
The route of motor 6；Wherein, wing body install when, mounting base 4 is socketed in mounting shell 3 so that the threaded hole on mounting shell 3 with
Threaded hole in mounting base 4 is corresponding.
Although the utility model is described in detail with reference to the foregoing embodiments, come for those skilled in the art
Say, it is still possible to modify the technical solutions described in the foregoing embodiments, or to part of technical characteristic into
Row equivalent replacement, within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on should all
It is included within the scope of protection of this utility model.
Claims (8)
1. a kind of rotor internally-arranged type bilayer leaf unmanned plane, including body (1), it is characterised in that: the body (1) is integrally formed
Square structure, offer multiple circular through holes (2) on body (1), each interior wing body of circular through hole (2), the machine
Wing body includes the mounting shell (3) positioned at circular through hole (2) the center point, and longitudinal set is provided through in the middle part of the mounting shell (3)
The mounting base (4) set, the mounting base (4) are the intermediate barreled structure with demarcation plate (5), the two sides of the demarcation plate (5)
Face is respectively and fixedly provided with driving motor (6), and the output shaft end of the driving motor (6) is connected with wing (7), above and below mounting base (4)
Both ends are integrally formed with bracket (8), and the bracket (8) includes strut (801) and axle sleeve (802), the strut (801)
One end is fixed on the side wall of mounting base (4), and the other end of strut (801) and axle sleeve (802) are integrally formed, the drive
The output shaft of dynamic motor (6) passes through axle sleeve (802) and is connected on wing (7)；2 branch are symmetrically arranged in the middle part of mounting shell (3)
One end of strut (9), the support rod (9) is detachably connected with mounting shell (3) by screw thread, and the other end of support rod (9) is logical
Screw is crossed to be fixed on the inner sidewall of circular through hole (2).
2. rotor internally-arranged type bilayer leaf unmanned plane according to claim 1, it is characterised in that: the support rod (9) and peace
The connecting pin of dress shell (3) is provided with miner diameter end (901), and the miner diameter end (901) and support rod (9) have miner diameter end (901)
One end is provided with screw thread.
3. rotor internally-arranged type bilayer leaf unmanned plane according to claim 1, it is characterised in that: the support rod (9) it is small
Diameter end (901) is threadingly attached in demarcation plate (5), and support rod (9) is threadingly attached on mounting shell (3).
4. rotor internally-arranged type bilayer leaf unmanned plane according to claim 1, it is characterised in that: relatively described two circular through hole
(2) line of the support rod (9) in is straight line.
5. rotor internally-arranged type bilayer leaf unmanned plane according to claim 2, it is characterised in that: relatively described two circular through hole
(2) extended line of support rod (9) is in 90 °.
6. rotor internally-arranged type bilayer leaf unmanned plane according to claim 1, it is characterised in that: the middle part of the body (1)
Openable cover board (10) is arranged in top for the installing zone for installing battery and control system, the installing zone.
7. rotor internally-arranged type bilayer leaf unmanned plane according to claim 1, it is characterised in that: the height of the body (1)
Greater than the distance of two wing lower edges upper and lower in circular through hole (2).
8. rotor internally-arranged type bilayer leaf unmanned plane according to claim 1-7, it is characterised in that: the support rod
It (9) is the carbon fibre materials of hollow structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920393425.1U CN209719915U (en) | 2019-03-26 | 2019-03-26 | A kind of rotor internally-arranged type bilayer leaf unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920393425.1U CN209719915U (en) | 2019-03-26 | 2019-03-26 | A kind of rotor internally-arranged type bilayer leaf unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209719915U true CN209719915U (en) | 2019-12-03 |
Family
ID=68688730
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920393425.1U Expired - Fee Related CN209719915U (en) | 2019-03-26 | 2019-03-26 | A kind of rotor internally-arranged type bilayer leaf unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209719915U (en) |
-
2019
- 2019-03-26 CN CN201920393425.1U patent/CN209719915U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230109 Address after: 450044 Room 1502, Building 21, Beijun Phase II, southwest corner of the intersection of Xincheng Road and Jinhe Road, Huiji District, Zhengzhou City, Henan Province Patentee after: Guyi (Henan) Intelligent Equipment Co.,Ltd. Address before: No. 120, Floor 1, Building D2, Zone A, Henan Outsourcing Industrial Park, No. 139, Yangjin Road, Jinshui District, Zhengzhou City, Henan Province, 450000 Patentee before: HENAN GUYI AUTOMATION TECHNOLOGY CO.,LTD. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20191203 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |