CN208165249U - A kind of high continuation of the journey unmanned plane - Google Patents
A kind of high continuation of the journey unmanned plane Download PDFInfo
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- CN208165249U CN208165249U CN201820544491.XU CN201820544491U CN208165249U CN 208165249 U CN208165249 U CN 208165249U CN 201820544491 U CN201820544491 U CN 201820544491U CN 208165249 U CN208165249 U CN 208165249U
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- fixedly connected
- unmanned plane
- side wall
- plate
- fuselage
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
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Abstract
The utility model discloses a kind of high continuation of the journey unmanned planes, including fuselage, annular is equidistantly fixedly connected with multiple aviation mechanisms on the side wall of the fuselage, the lower end of the fuselage is fixedly connected with fixed plate, the lower end two sides of the fixed plate are fixedly connected to buffer gear, the lower end of two buffer gears is fixedly connected to connecting plate, the lower end of two connecting plates is fixedly connected to undercarriage, the lower end side of two undercarriages is fixedly connected to coasting mechanism, the lower end two sides of the fixed plate are fixedly connected to support column corresponding with two connecting plate positions, the opposing sidewalls of two support columns are equipped with strip groove.The utility model is compact-sized, by the way that solar panel is arranged, the cruising ability of unmanned plane is improved to a certain extent, and by the way that buffer gear is arranged on undercarriage, to reduce unmanned plane impact force suffered during landing, the service life of unmanned plane is extended to a certain extent.
Description
Technical field
The utility model relates to air vehicle technique field more particularly to a kind of high continuation of the journey unmanned planes.
Background technique
Height continuation of the journey unmanned plane in landing since each rotating device is to be operated alone, generally under the fuselage of unmanned plane
End setting undercarriage, existing undercarriage are generally made of metal tube, and undercarriage vibration in landing is very big, lead to high continuation of the journey nothing
Man-machine descent is simultaneously unstable, especially in no special stop position, can make the dress inside high continuation of the journey unmanned plane
It sets and is impacted, when service life is too long, will result in the plant failure inside unmanned plane, reduce unmanned plane uses the longevity
Life, prospect of the application is not fine.
Utility model content
Purpose of the utility model is to solve disadvantage existing in the prior art, and what is proposed a kind of high continues a journey nobody
Machine.
To achieve the goals above, the utility model uses following technical solution：
A kind of high continuation of the journey unmanned plane, including fuselage, annular is equidistantly fixedly connected with multiple fly on the side wall of the fuselage
Row mechanism, the lower end of the fuselage are fixedly connected with fixed plate, and the lower end two sides of the fixed plate are fixedly connected to buffer
Structure, the lower end of two buffer gears are fixedly connected to connecting plate, and the lower end of two connecting plates is fixedly connected to
Undercarriage, the lower end side of two undercarriages are fixedly connected to coasting mechanism, and the lower end two sides of the fixed plate are solid
Surely it is connected with support column corresponding with two connecting plate positions, the opposing sidewalls of two support columns are equipped with strip groove, and two
Guiding axis is fixedly connected in a strip groove, the connecting plate is fixedly connected to two slidings close to the side of support column
Set, two sliding sleeves run through the side wall of strip groove and are slidably socketed on guiding axis, and the lower end of the fixed plate is fixed
It is connected with T-type plate, the lower end of the T-type plate is fixedly connected with parcel shelf, fixes in the opposing sidewalls of two connecting plates
It is connected with guide rod, the lower end of two guide rods is fixedly connected to guiding mechanism, and the side wall of the parcel shelf is equipped with
Two guide grooves corresponding with guiding mechanism position, the lower end of two guiding mechanisms are slidably connected in guide groove, institute
The upper end for stating fuselage is fixedly connected with placing box, and the interior bottom of the placing box is equipped with solar panel, the placing box
Upper end two sides are equipped with the position-limit mechanism limited to solar panel, and the inner wall of the placing box is fixedly connected with rubber
The side wall of plate, the solar panel and rubber slab offsets.
Preferably, the aviation mechanism includes the flank being fixedly connected on fuselage side wall, and the flank is far from fuselage
Propeller is rotatably connected to by driving motor on the side wall of one end.
Preferably, the buffer gear includes the placement plate for being fixedly connected on fixed plate lower end, the lower end of the placement plate
Equipped with multiple dashpots, the inner top of the dashpot is fixedly connected with damping spring, and the lower end of the damping spring is through slow
Jet-bedding is simultaneously fixedly connected with stripe board, and the stripe board is fixedly connected on the upper end of connecting plate.
Preferably, the coasting mechanism includes the walking seat for being fixedly connected on undercarriage lower end side, the walking seat
Traveling wheel is rotatably connected on side wall.
Preferably, the guiding mechanism includes the catch bar for being fixedly connected on guide rod lower end, the lower end of the catch bar
Through guide groove and it is fixedly connected with limited block, and limited block is slidably connected in guide groove.
Preferably, the position-limit mechanism includes the mounting plate on placing box side wall, and the lower end of the mounting plate is fixed
It is connected with the stripper plate limited to solar panel, the side wall of the mounting plate is fixed in placement equipped with multiple
Lock-screw on case side wall.
In the utility model, by the way that solar panel is arranged in fuselage upper end, solar panel carries out unmanned plane
Electric power storage can extend the hours underway of unmanned plane to a certain extent, in unmanned plane landing, when the lower end and ground of two undercarriages
When face is in contact, two buffer gears play certain shock absorbing effect to two undercarriages respectively, and undercarriage can pass through
Sliding sleeve is moved on guiding axis, and guiding axis plays certain guiding role, and two guide rods to the movement of undercarriage
The guiding mechanism of lower end further functions as guiding role to the movement of undercarriage in the vertical direction, exists to improve unmanned plane
Stability when landing.The utility model is compact-sized, by the way that solar panel is arranged, improves unmanned plane to a certain extent
Cruising ability, and by the way that buffer gear is arranged on undercarriage, to reduce, unmanned plane is suffered during landing to be rushed
Power is hit, extends the service life of unmanned plane to a certain extent.
Detailed description of the invention
Fig. 1 be the utility model proposes it is a kind of it is high continuation of the journey unmanned plane structural schematic diagram；
Fig. 2 be the utility model proposes it is a kind of it is high continuation of the journey unmanned plane structure top view；
Fig. 3 is enlarged drawing at A in Fig. 1；
Fig. 4 is enlarged drawing at B in Fig. 1；
Fig. 5 is enlarged drawing at C in Fig. 1.
In figure：1 fuselage, 2 flanks, 3 propellers, 4 placing boxes, 5 solar panels, 6 fixed plates, 7 support columns, 8 connections
Plate, 9 undercarriages, 10 walking seats, 11 traveling wheels, 12T template, 13 guide rods, 14 mounting plates, 15 stripper plates, 16 lock-screws, 17
Guiding axis, 18 sliding sleeves, 19 stripe boards, 20 damping springs, 21 placement plates, 22 parcel shelf, 23 catch bars, 24 limited blocks, 25 rubbers
Offset plate.
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.
- 5 Figure of description referring to Fig.1, a kind of high continuation of the journey unmanned plane, including fuselage 1, between annular is equal on the side wall of fuselage 1
Away from multiple aviation mechanisms are fixedly connected with, the lower end of fuselage 1 is fixedly connected with fixed plate 6, and the lower end two sides of fixed plate 6 are fixed
It is connected with buffer gear, the lower end of two buffer gears is fixedly connected to connecting plate 8, and the lower end of two connecting plates 8 is fixed
It is connected with undercarriage 9, two buffer gears play certain shock absorbing effect to two undercarriages 9 respectively, when unmanned plane exists
During landing, buffer gear reduces impact force suffered by undercarriage 9 to a certain extent, under two undercarriages 9
End side is fixedly connected to coasting mechanism, and the lower end two sides of fixed plate 6 are fixedly connected to corresponding with two 8 positions of connecting plate
Support column 7, the opposing sidewalls of two support columns 7 are equipped with strip groove, guiding axis 17 are fixedly connected in two strip grooves, even
Fishplate bar 8 is fixedly connected to two sliding sleeves 18 close to the side of support column 7, and two sliding sleeves 18 run through the side wall of strip groove
And be slidably socketed on guiding axis 17, when unmanned plane is during landing lands, since buffer gear is to the buffering of connecting plate 8
Effect, undercarriage 9 drive connecting plate 8 to carry out certain movement in the vertical direction, and guiding axis 17 plays the movement of connecting plate 8
Guiding role, the lower end of fixed plate 6 are fixedly connected with T-type plate 12, and the lower end of T-type plate 12 is fixedly connected with parcel shelf 22, and two
Guide rod 13 is fixedly connected in the opposing sidewalls of connecting plate 8, the lower end of two guide rods 13 is fixedly connected to Guiding machine
Structure is set on the side wall of parcel shelf 22 there are two guide groove corresponding with guiding mechanism position, and the lower end of two guiding mechanisms is sliding
Dynamic to be connected in guide groove, two guiding mechanisms further play guiding role to the movement of two connecting plates 8, thus to two
Undercarriage 9 plays certain guiding role, and the upper end of fuselage 1 is fixedly connected with placing box 4, and the interior bottom of placing box 4 is equipped with too
Positive energy solar panel 5, solar panel 5 with electric storage means by being attached, to carry out electric power storage to unmanned plane, improves unmanned plane
Cruising ability, the upper end two sides of placing box 4 are equipped with the position-limit mechanism limited to solar panel 5, placing box 4
Inner wall is fixedly connected with rubber slab 25, and solar panel 5 and the side wall of rubber slab 25 offset.
In the utility model, aviation mechanism includes the flank 2 being fixedly connected on 1 side wall of fuselage, and flank 2 is far from fuselage 1
One end side wall on propeller 3 is rotatably connected to by driving motor.Buffer gear includes being fixedly connected on 6 lower end of fixed plate
The lower end of placement plate 21, placement plate 21 is equipped with multiple dashpots, and the inner top of dashpot is fixedly connected with damping spring 20, damping
The lower end of spring 20 is through dashpot and is fixedly connected with stripe board 19, and stripe board 19 is fixedly connected on the upper end of connecting plate 8, subtracts
Shaking spring 20 has certain elastic reaction, to play certain shock absorbing effect to undercarriage 9 by connecting plate 8, drops
The vibration caused in landing of low unmanned plane.Coasting mechanism includes the walking seat for being fixedly connected on 9 lower end side of undercarriage
10, walk seat 10 side wall on be rotatably connected to traveling wheel 11.Guiding mechanism includes being fixedly connected on pushing away for 13 lower end of guide rod
The lower end of lever 23, catch bar 23 through guide groove and is fixedly connected with limited block 24, and limited block 24 is slidably connected at guiding
In slot, when connecting plate 8 is just moved in the vertical direction by impact force, catch bar 23 drives limited block 24 in guide groove
It is inside moved, to further play guiding role to the movement of connecting plate 8.Position-limit mechanism includes being located at 4 side wall of placing box
On mounting plate 14, the lower end of mounting plate 14 is fixedly connected with the stripper plate 15 limited to solar panel 5, mounting plate
14 side wall is equipped with multiple lock-screws 16 being fixed on 4 side wall of placing box.
In the utility model, by hold on the fuselage 1 setting solar panel 5, solar panel 5 to unmanned plane into
Row electric power storage can extend the hours underway of unmanned plane to a certain extent, in unmanned plane landing, when the lower end of two undercarriages 9
When touching with ground, two buffer gears play certain shock absorbing effect, and undercarriage 9 to two undercarriages 9 respectively
It can be moved on guiding axis 17 by sliding sleeve 18, guiding axis 17 plays certain guiding role to the movement of undercarriage 9,
And the guiding mechanism of two 13 lower ends of guide rod further functions as guiding role to the movement of undercarriage 9 in the vertical direction, from
And improve stability of the unmanned plane in landing.
The preferable specific embodiment of the above, only the utility model, but the protection scope of the utility model is not
It is confined to this, anyone skilled in the art is within the technical scope disclosed by the utility model, practical according to this
Novel technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model
Within enclosing.
Claims (6)
1. a kind of high continuation of the journey unmanned plane, including fuselage (1), which is characterized in that annular is equidistant solid on the side wall of the fuselage (1)
Surely multiple aviation mechanisms are connected with, the lower end of the fuselage (1) is fixedly connected with fixed plate (6), the lower end of the fixed plate (6)
Two sides are fixedly connected to buffer gear, and the lower end of two buffer gears is fixedly connected to connecting plate (8), described in two
The lower end of connecting plate (8) is fixedly connected to undercarriage (9), and the lower end side of two undercarriages (9) is fixedly connected to
Coasting mechanism, the lower end two sides of the fixed plate (6) are fixedly connected to support column corresponding with two connecting plate (8) positions
(7), the opposing sidewalls of two support columns (7) are equipped with strip groove, are fixedly connected with guiding axis in two strip grooves
(17), the connecting plate (8) is fixedly connected to two sliding sleeves (18), two slidings close to the side of support column (7)
Set (18) through the side wall of strip groove and is slidably socketed on guiding axis (17), and the lower end of the fixed plate (6) is fixedly connected
Have T-type plate (12), the lower end of the T-type plate (12) is fixedly connected with parcel shelf (22), the opposite side of two connecting plates (8)
It is fixedly connected on wall guide rod (13), the lower end of two guide rods (13) is fixedly connected to guiding mechanism, described
It is set on the side wall of parcel shelf (22) there are two guide groove corresponding with guiding mechanism position, the lower end of two guiding mechanisms is equal
It is slidably connected in guide groove, the upper end of the fuselage (1) is fixedly connected with placing box (4), the interior bottom of the placing box (4)
Equipped with solar panel (5), the upper end two sides of the placing box (4), which are equipped with, limits solar panel (5)
The inner wall of position-limit mechanism, the placing box (4) is fixedly connected rubber slab (25), the solar panel (5) and rubber slab
(25) side wall offsets.
2. a kind of high continuation of the journey unmanned plane according to claim 1, which is characterized in that the aviation mechanism includes being fixedly connected
Flank (2) on fuselage (1) side wall, the flank (2) far from fuselage (1) one end side wall on by driving motor rotation company
It is connected to propeller (3).
3. a kind of high continuation of the journey unmanned plane according to claim 1, which is characterized in that the buffer gear includes being fixedly connected
Placement plate (21) in fixed plate (6) lower end, the lower end of the placement plate (21) are equipped with multiple dashpots, the dashpot it is interior
Top is fixedly connected with damping spring (20), and the lower end of the damping spring (20) through dashpot and is fixedly connected with stripe board
(19), the stripe board (19) is fixedly connected on the upper end of connecting plate (8).
4. a kind of high continuation of the journey unmanned plane according to claim 1, which is characterized in that the coasting mechanism includes being fixedly connected
Walking seat (10) in undercarriage (9) lower end side, it is described walking seat (10) side wall on be rotatably connected to traveling wheel (11).
5. a kind of high continuation of the journey unmanned plane according to claim 1, which is characterized in that the guiding mechanism includes being fixedly connected
The lower end of catch bar (23) in guide rod (13) lower end, the catch bar (23) through guide groove and is fixedly connected with limited block
(24), and limited block (24) is slidably connected in guide groove.
6. a kind of high continuation of the journey unmanned plane according to claim 1, which is characterized in that the position-limit mechanism includes being located to place
Mounting plate (14) on case (4) side wall, the lower end of the mounting plate (14), which is fixedly connected with, limits solar panel (5)
The side wall of the stripper plate (15) of position, the mounting plate (14) is equipped with multiple lockings being fixed on placing box (4) side wall
Screw (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820544491.XU CN208165249U (en) | 2018-04-17 | 2018-04-17 | A kind of high continuation of the journey unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820544491.XU CN208165249U (en) | 2018-04-17 | 2018-04-17 | A kind of high continuation of the journey unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208165249U true CN208165249U (en) | 2018-11-30 |
Family
ID=64369632
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820544491.XU Active CN208165249U (en) | 2018-04-17 | 2018-04-17 | A kind of high continuation of the journey unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208165249U (en) |
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2018
- 2018-04-17 CN CN201820544491.XU patent/CN208165249U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: Room 605, Building 1, Internet Industry Park, No. 1, Binhan Road, Weibin District, Baoji City, Shaanxi Province, 721000 Patentee after: Baoji Xinzhengda Science and Technology Co., Ltd. Address before: Room 605, Building 1, Internet Industry Park, No. 1, Binhan Road, Weibin District, Baoji City, Shaanxi Province, 721000 Patentee before: Baoji new Zhengda Technology Development Co., Ltd. |
|
| CP01 | Change in the name or title of a patent holder |