CN207417115U - A kind of wheeled unmanned plane wing electric foldable unfolding mechanism of bidentate - Google Patents
A kind of wheeled unmanned plane wing electric foldable unfolding mechanism of bidentate Download PDFInfo
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- CN207417115U CN207417115U CN201721543220.4U CN201721543220U CN207417115U CN 207417115 U CN207417115 U CN 207417115U CN 201721543220 U CN201721543220 U CN 201721543220U CN 207417115 U CN207417115 U CN 207417115U
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- wing
- gear
- sleeve
- unmanned plane
- bidentate
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Abstract
The utility model discloses a kind of wheeled unmanned plane wing electric foldable unfolding mechanisms of bidentate, including the first wing, head rod is installed on the right side of first wing, the inner wall of the head rod is equipped with the first sleeve, the right side of first wing is equipped with the second wing, second connecting rod is installed, the inner wall of second connecting rod is equipped with second sleeve on the left of second wing.The wheeled unmanned plane wing electric foldable unfolding mechanism of the bidentate, pass through the cooperation of the first wing and the second wing, achieve the effect that wing-folding, pass through the cooperation of motor and bull stick, motor drives bar rotation, as the power set of unfolding mechanism, pass through the cooperation of first gear and second gear, /V is carried out to the process of the first wing and the second wing-folding, reliability is high, and wing expansion and folding process are controllable, it impacts small, simply, available for the wing-folding unfolding mechanism for becoming sweepback angle, suitable for the different stability requirement of aircraft.
Description
Technical field
The utility model is related to unmanned plane wing technical fields, are specially a kind of wheeled unmanned plane wing electric foldable of bidentate
Unfolding mechanism.
Background technology
It carries and transports in order to facilitate unmanned plane, mostly using the wing and empennage form folded.Existing folding wings unmanned plane
Mostly the reliability that unmanned plane wing is unfolded directly is determined using spring folding and expanding mechanism, the service life of spring and fatigue properties
Unmanned plane is stored by prolonged, and the spring inside fold mechanism is easily permanently deformed, and causes wing that reliability is unfolded
It reduces, proposes a kind of wing unfolding mechanism of unsprung so as to influence the service life of the unmanned plane present invention, i.e. bidentate is wheeled
Electric foldable unfolding mechanism realizes the expansion and folding of wing in opposite direction using steering engine or motor-driven gear transmission, can
It realizes and stores for a long time, it is easy to use, substantially increase the reliability of wing rapid deployment after unmanned plane stores for a long time.
Utility model content
The purpose of this utility model is to provide a kind of wheeled unmanned plane wing electric foldable unfolding mechanism of bidentate, to solve
The problems mentioned above in the background art.
To achieve the above object, the utility model provides following technical solution：A kind of wheeled unmanned plane wing of bidentate is electronic
Folding and expanding mechanism including the first wing, is equipped with head rod on the right side of first wing, the head rod
Inner wall is equipped with the first sleeve, and the right side of first wing is equipped with the second wing, and the is equipped on the left of second wing
Two connecting rods, the inner wall of second connecting rod are equipped with the inside of second sleeve, second connecting rod and head rod
It is equipped with through hole, the top of first sleeve and second sleeve is equipped with top plate, is respectively mounted at left and right sides of the top of the top plate
There is convex block, the convex block is connected by rivet with top plate, and the bottom of first sleeve and second sleeve is equipped with bottom plate, described
First gear on the left of the bottom of bottom plate is installed, second gear is installed on the right side of the bottom of the bottom plate, the first gear with
Second gear engagement is connected, and the bottom of the first gear and second gear is equipped with motor, and the motor passes through bull stick and first
Gear is connected with second gear.
Compared with prior art, the beneficial effects of the utility model are：The wheeled unmanned plane wing electric foldable exhibition of the bidentate
Opening mechanism by the cooperation of the first wing and the second wing, achievees the effect that wing-folding, by the cooperation of motor and bull stick,
Motor drives bar rotation, becomes the power set of unfolding mechanism, by the cooperation of first gear and second gear, to the first machine
The process of the wing and the second wing-folding carries out /V, and reliability is high, and wing expansion and folding process are controllable, impact small, operation side
Just, simply, available for the wing-folding unfolding mechanism for becoming sweepback angle, suitable for the different stability requirement of aircraft.
Description of the drawings
Fig. 1 is the utility model structure diagram.
In figure：1st, the first wing, 2, head rod, 3, top plate, 4, through hole, the 5, first sleeve, 6, convex block, 7, rivet,
8th, second sleeve, the 9, second connecting rod, the 10, second wing, 11, bottom plate, 12, first gear, 13, second gear, 14, bull stick,
15th, motor.
Specific embodiment
The following is a combination of the drawings in the embodiments of the present utility model, and the technical scheme in the embodiment of the utility model is carried out
It clearly and completely describes, 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 embodiment in the utility model, those of ordinary skill in the art are without making creative work
All other embodiments obtained shall fall within the protection scope of the present invention.
Referring to Fig. 1, the utility model provides a kind of technical solution：A kind of wheeled unmanned plane wing electric foldable exhibition of bidentate
Opening mechanism, including the first wing 1, the right side of the first wing 1 is equipped with head rod 2, and the inner wall of head rod 2 is equipped with
First sleeve 5, the right side of the first wing 1 are equipped with the second wing 10, and the left side of the second wing 10 is equipped with the second connecting rod 9, the
The inner wall of two connecting rods 9 is equipped with second sleeve 8, and the inside of the second connecting rod 9 and head rod 2 is equipped with through hole 4, and first
The top of sleeve 5 and second sleeve 8 is equipped with top plate 3, is mounted on convex block 6 at left and right sides of the top of top plate 3, convex block 6 passes through riveting
Nail 7 is connected with top plate 3, and the bottom of the first sleeve 5 and second sleeve 8 is equipped with bottom plate 11, is equipped on the left of the bottom of bottom plate 11
First gear 12, first gear 12 drive the rotation of the first sleeve 5, and the head rod 2 of 5 left side installation of the first sleeve is with first
The rotation of sleeve 5 drives the first wing 1 to be rotated again, and second gear 13, second gear are equipped on the right side of the bottom of bottom plate 11
13 drive the rotation of second sleeves 8, and the second connecting rod 9 of the right side of second sleeve 8 installation drives the again with the rotation of second sleeve 8
The one side of two wings 10 to the first wing 1 is rotated, and realizes the folding of wing, and first gear 12 is nibbled with second gear 13
It closes and is connected, motor 15 drives first gear 12 to rotate by bull stick 14, and motor 15 drives second gear 13 along the by bull stick 14
The opposite direction of one gear 12 rotates, and first gear 12 is intermeshed with second gear 13, first gear 12 and second gear 13
Bottom be equipped with motor 15, when unmanned plane wing is needed to fold or is unfolded, connect the external power supply of motor 15, motor 15 opens
Beginning work, motor 15 are connected by bull stick 14 with first gear 12 and second gear 13, realize wing expansion and folding process
Controllably, impact is small, easy to operate, simply, different suitable for aircraft available for the wing-folding unfolding mechanism for becoming sweepback angle
Stability requirement.
When unmanned plane wing is needed to fold or is unfolded, the external power supply of motor 15 is connected, motor 15 is started to work, electricity
Machine 15 drives first gear 12 to rotate by bull stick 14, and motor 15 drives second gear 13 along 12 phase of first gear by bull stick 14
Anti- direction rotates, and first gear 12 is intermeshed with second gear 13, is rotated in first gear 12 and second gear 13 same
When, first gear 12 drives the rotation of the first sleeve 5, and the head rod 2 of 5 left side installation of the first sleeve is with the first sleeve 5
Rotation drives the first wing 1 to be rotated again, and second gear 13 drives the rotation of second sleeve 8,8 right side installation of second sleeve
Second connecting rod 9 drives the one side of the second wing 10 to the first wing 1 to be rotated again with the rotation of second sleeve 8, realizes
The folding of wing.
In the description of the utility model, it is to be understood that term " coaxial ", " bottom ", " one end ", " top ", " in
Portion ", " other end ", " on ", " one side ", " top ", " interior ", " forepart ", " center ", the orientation of the instructions such as " both ends " or position close
Be for based on orientation shown in the drawings or position relationship, be for only for ease of description the utility model and simplify description rather than
Indicate or imply that signified device or element there must be specific orientation, with specific azimuth configuration and operation, therefore cannot
It is interpreted as the limitation to the utility model.
In the utility model, unless otherwise clearly defined and limited, term " installation ", " setting ", " connection ", " Gu
It is fixed ", the terms such as " being screwed on " should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected or integral；
Can be mechanical connection or electrical connection；It can be directly connected, can also be indirectly connected by intermediary, it can be with
It is the interaction relationship of connection inside two elements or two elements, unless otherwise restricted clearly, for this field
For those of ordinary skill, concrete meaning of the above-mentioned term in the utility model can be understood as the case may be.
While there has been shown and described that the embodiment of the utility model, for the ordinary skill in the art,
It is appreciated that in the case where not departing from the principle of the utility model and spirit can these embodiments be carried out with a variety of variations, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (1)
1. a kind of wheeled unmanned plane wing electric foldable unfolding mechanism of bidentate, including the first wing (1), it is characterised in that：It is described
Head rod (2) is installed, the inner wall of the head rod (2) is equipped with the first sleeve on the right side of the first wing (1)
(5), the right side of first wing (1) is equipped with the second wing (10), and the second company is equipped on the left of second wing (10)
Extension bar (9), the inner wall of second connecting rod (9) are equipped with second sleeve (8), second connecting rod (9) and the first connection
The inside of bar (2) is equipped with through hole (4), and the top of first sleeve (5) and second sleeve (8) is equipped with top plate (3), the top
Convex block (6) is mounted at left and right sides of the top of plate (3), the convex block (6) is connected by rivet (7) with top plate (3), and described the
The bottom of one sleeve (5) and second sleeve (8) is equipped with bottom plate (11), and the first tooth is equipped on the left of the bottom of the bottom plate (11)
It takes turns (12), second gear (13), the first gear (12) and second gear is installed on the right side of the bottom of the bottom plate (11)
(13) engagement is connected, and the bottom of the first gear (12) and second gear (13) is equipped with motor (15), and the motor (15) is logical
Bull stick (14) is crossed with first gear (12) and second gear (13) to be connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721543220.4U CN207417115U (en) | 2017-11-17 | 2017-11-17 | A kind of wheeled unmanned plane wing electric foldable unfolding mechanism of bidentate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721543220.4U CN207417115U (en) | 2017-11-17 | 2017-11-17 | A kind of wheeled unmanned plane wing electric foldable unfolding mechanism of bidentate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207417115U true CN207417115U (en) | 2018-05-29 |
Family
ID=62302626
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721543220.4U Active CN207417115U (en) | 2017-11-17 | 2017-11-17 | A kind of wheeled unmanned plane wing electric foldable unfolding mechanism of bidentate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207417115U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109110094A (en) * | 2018-07-19 | 2019-01-01 | 芜湖籁余新能源科技有限公司 | A kind of underwater autonomous underwater vehicle flank telescopic device |
| CN112046742A (en) * | 2020-09-13 | 2020-12-08 | 西北工业大学 | Flapping wing mechanism with wing spreading capability |
-
2017
- 2017-11-17 CN CN201721543220.4U patent/CN207417115U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109110094A (en) * | 2018-07-19 | 2019-01-01 | 芜湖籁余新能源科技有限公司 | A kind of underwater autonomous underwater vehicle flank telescopic device |
| CN112046742A (en) * | 2020-09-13 | 2020-12-08 | 西北工业大学 | Flapping wing mechanism with wing spreading capability |
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