CN208024771U - A kind of unmanned plane vibration damping medicine-chest - Google Patents
A kind of unmanned plane vibration damping medicine-chest Download PDFInfo
- Publication number
- CN208024771U CN208024771U CN201721870628.2U CN201721870628U CN208024771U CN 208024771 U CN208024771 U CN 208024771U CN 201721870628 U CN201721870628 U CN 201721870628U CN 208024771 U CN208024771 U CN 208024771U
- Authority
- CN
- China
- Prior art keywords
- medicine
- damping
- chest
- unmanned plane
- plane vibration
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Landscapes
- Catching Or Destruction (AREA)
- Special Spraying Apparatus (AREA)
Abstract
The utility model discloses a kind of unmanned plane vibration damping medicine-chest, belong to air vehicle technique field, including medicine-chest, the first damping device for being arranged below medicine-chest and multiple second damping devices；First damping device includes the casing and sliding block being arranged in casing, the first damping spring and cushion block, second damping device includes the decoupling rod being connect with medicine-chest and the second damping spring being arranged on decoupling rod, the lower section of decoupling rod is equipped with cushion socket, the bottom that cushion socket is equipped with cushion socket is equipped with pedestal, pedestal is arranged on the second fixed frame, and the second fixed mount setting is on fuselage.The damping spring of the utility model contacts or in spray drug operation when unmanned plane landing with ground, it is elastic potential energy by the vibrational energy sorption enhanced that medicine-chest and fuselage generate, vibrations when can effectively reduce body landing and spray drug operation operating to medicine-chest, reduce the damage to fuselage and medicine-chest, improves spray drug operation effect.
Description
Technical field
The utility model is related to a kind of unmanned plane medicine-chests to belong to unmanned plane more particularly to a kind of unmanned plane vibration damping medicine-chest
Technical field.
Background technology
With the continuous rise of the appropriate scale of agriculture, agricultural unmanned plane is increasingly appearing in agricultural plant protection operation neck in recent years
Domain, as a kind of unmanned plane for the purpose of plant protection, the rational design of unmanned plane drug reservoir, especially unmanned plane drug reservoir
The rational design of damping medicine-chest directly affect agricultural plant protection unmanned plane working efficiency, when existing unmanned plane landing and ground
When contact, larger vibrations are will produce, are easy to damage unmanned plane entirety and unmanned plane medicine-chest, moreover, unmanned plane is spraying
It is larger due to vibrating when medicine operation operates, spray drug operation effect can be reduced, therefore we make this improvement, propose a kind of nothing
Man-machine vibration damping medicine-chest.
Utility model content
The main purpose of the utility model is to provide for a kind of unmanned plane vibration damping medicine-chest, can effectively reduce body landing
To the vibrations of medicine-chest when being operated with spray drug operation, reduce the damage to fuselage and medicine-chest, improves spray drug operation effect.
The purpose of this utility model can reach by using following technical solution：
A kind of unmanned plane vibration damping medicine-chest, including medicine-chest, the first damping device and multiple for being arranged below the medicine-chest
Two damping devices；First damping device includes the casing and sliding block being arranged in described sleeve pipe, the first damping spring and pad
Block, the sliding block are arranged by connecting rod on the first fixed frame, and the connecting rod and first fixed frame are arranged at machine
With；Multiple second damping devices are distributed in dispersed, and second damping device includes subtracting with what the medicine-chest was connect
The lower section of shake bar and the second damping spring being arranged on the decoupling rod, the decoupling rod is equipped with cushion socket, the cushion socket
It is equipped with the spring limiting part limited to second damping spring, the bottom of the cushion socket is equipped with pedestal, the bottom
Seat is arranged on the second fixed frame, and second fixed mount setting is on the fuselage.
Preferably, the medicine-chest is equipped with transparency window, and the transparency window is equipped with scale, and the transparency window is windowpane.
Preferably, there is the pedestal groove, the cushion socket to be arranged in the groove, and the cushion socket is equipped with limit
Position block, the pedestal are equipped with damping trough, and the limited block slides in the damping trough.
Preferably, the bottom portion of groove of the pedestal is equipped with damping soft formation, and the cushion socket is arranged on the damping soft formation,
The damping soft formation is rubber layer.
Preferably, first fixed frame and second fixed frame are metal holder, and shape is arc, section
Face shape is cylinder.
Preferably, second fixed frame is fixed on by fixing nut on the fuselage, the connecting rod and described the
One fixed frame is fixedly connected, and buffer gap is equipped between the fuselage after the connecting rod and first fixed frame connection.
Preferably, first damping spring is arranged between the sliding block and the cushion block, and the top of the sliding block is logical
Cross first damping spring and the cushion block elastic connection.
Preferably, described sleeve pipe is internally provided with notch sliding slot directed downwardly, and the cushion block is fixed at the sliding slot
The top of cell wall.
Preferably, the positive stop lug boss limited to the sliding block, the positive stop lug boss are equipped at the notch of the sliding slot
It is fixedly connected between described sleeve pipe.
Preferably, first damping spring and second damping spring are metal damping spring, and the pedestal is
Metab, the cushion socket are metal cushion socket, and the decoupling rod is metal decoupling rod.
The advantageous effects of the utility model：According to the unmanned plane vibration damping medicine-chest of the utility model, the utility model carries
The unmanned plane vibration damping medicine-chest of confession, by the way that damping spring is arranged, when unmanned plane landing is contacted with ground or in spray drug operation, is subtracted
Shaking connecting rod of the spring in sliding slot pushes sliding block to move upwards, in fuselage descent, by the vibration of medicine-chest and fuselage generation
Energy sorption enhanced is elastic potential energy, vibrations when can effectively reduce body landing and spray drug operation operating to medicine-chest, reduction pair
The damage of fuselage and medicine-chest improves spray drug operation effect.
Description of the drawings
Fig. 1 is the overall structure diagram according to a preferred embodiment of the unmanned plane vibration damping medicine-chest of the utility model；
Fig. 2 is the cushion socket structural schematic diagram according to a preferred embodiment of the unmanned plane vibration damping medicine-chest of the utility model；
Fig. 3 is to be looked up according to the first damping device of a preferred embodiment of the unmanned plane vibration damping medicine-chest of the utility model
Figure.
In figure：1- pedestals, 2- cushion sockets, 3- spring limiting parts, 4- decoupling rods, the second damping springs of 5-, 6- first are fixed
Frame, 7- damping troughs, 8- connecting rods, 9- casings, 10- sliding blocks, the first damping springs of 11-, 12- cushion blocks, 13- positive stop lug boss, 14- limits
Position block, 15- fuselages, the second fixed frames of 16-, 17- fixing nuts, 18- medicine-chests, 19- transparency windows, 20- scales, 21- spray mouths,
22- damping soft formations.
Specific implementation mode
To make the more clear and clear the technical solution of the utility model of those skilled in the art, with reference to embodiment and
Attached drawing is described in further detail the utility model, and however, the embodiments of the present invention are not limited thereto.
As shown in Figure 1, Figure 2 and Figure 3, a kind of unmanned plane vibration damping medicine-chest provided in this embodiment, including medicine-chest 18, setting exist
The first damping device and multiple second damping devices of 18 lower section of the medicine-chest；First damping device includes casing 9 and sets
Set sliding block 10, the first damping spring 11 and cushion block 12 in described sleeve pipe 9, the sliding block 10 is arranged by connecting rod 8 the
On one fixed frame 6, the connecting rod 8 and first fixed frame 6 are arranged on fuselage 15；Multiple second damping devices
It is distributed in dispersed, second damping device includes the decoupling rod 4 being connect with the medicine-chest 18 and is arranged in the decoupling rod 4
On the second damping spring 5, the lower section of the decoupling rod 4 is equipped with cushion socket 2, and the cushion socket 2 is equipped with to be subtracted to described second
The bottom of the spring limiting part 3 that shake spring 5 is limited, the cushion socket 2 is equipped with pedestal 1, and the setting of the pedestal 1 is solid second
Determine on frame 16, second fixed frame 16 is arranged on the fuselage 15.
Further, in the present embodiment, as shown in Figure 1, the medicine-chest 18 is equipped with transparency window 19, the transparency window 19
It is equipped with scale 20, the transparency window 19 is windowpane.
Further, in the present embodiment, as depicted in figs. 1 and 2, there is the pedestal 1 groove, the cushion socket 2 to set
It sets in the groove, the cushion socket 2 is equipped with limited block 14, and the pedestal 1 is equipped with damping trough 7, the limited block 14
The bottom portion of groove of the sliding in the damping trough 7, the pedestal 1 is equipped with damping soft formation 22, and the setting of the cushion socket 2 subtracts described
It shakes on soft formation 22, the damping soft formation 22 is rubber layer.
Further, in the present embodiment, as shown in Figure 1, first fixed frame 6 and second fixed frame 16 are
Metal holder, shape are arc, and cross sectional shape is cylinder, and second fixed frame 16 is fixed by fixing nut 17
On the fuselage 15, the connecting rod 8 is fixedly connected with first fixed frame 6, and the connecting rod 8 is fixed with described first
Frame 6 is equipped with buffer gap between the fuselage 15 after connecting, first damping spring 11 is arranged in the sliding block 10 and institute
Between stating cushion block 12, the top of the sliding block 10 passes through first damping spring 11 and 12 elastic connection of the cushion block.
Further, in the present embodiment, as shown in figures 1 and 3, described sleeve pipe 9 to be internally provided with notch directed downwardly
Sliding slot, the cushion block 12 are fixed at the top of the sliding slot cell wall, are equipped with to the sliding block 10 at the notch of the sliding slot
The positive stop lug boss 13 limited, is fixedly connected between the positive stop lug boss 13 and described sleeve pipe 9, first damping spring 11
It is metal damping spring with second damping spring 5, the pedestal 1 is metab, and the cushion socket 2 is metal damping
Seat, the decoupling rod 4 are metal decoupling rod.
Further, in the present embodiment, as shown in Figure 1, first damping spring 11 setting the sliding block 10 with
Between the cushion block 12, the sliding block 10 and the cushion block 12 are circle, and the top of the sliding block 10 subtracts by described first
Spring 11 and 12 elastic connection of the cushion block are shaken, the sliding block 10 is metal block, and the cushion block 12 is flexible cushion block, described soft
Property cushion block be nonmetallic cushion block.
Further, in the present embodiment, as depicted in figs. 1 and 2, the connecting rod 8 be metal tie rods, described first
Fixed frame 6 is metal machine frame, is welded between the connecting rod 8 and first fixed frame 6, and the connecting rod 8 is cylindrical bar,
First damping spring 11 and second damping spring 5 are metal damping spring, and the pedestal 1 can also be rubber-sole
Seat, the cushion socket 2 can also be rubber shock-absorbing seat, and the decoupling rod 4 is cylindrical metal decoupling rod.
Further, in the present embodiment, by the unmanned plane vibration damping medicine-chest, by the way that damping spring is arranged, when this nobody
Machine landing contacts with ground or in spray drug operation, and connecting rod of the damping spring in sliding slot pushes sliding block to move upwards, fuselage
In descent, the vibrational energy sorption enhanced that medicine-chest and fuselage are generated is elastic potential energy, can effectively reduce body landing and
Vibrations when spray drug operation operates to medicine-chest reduce the damage to fuselage and medicine-chest, improve spray drug operation effect.
The above, only the utility model further embodiment, but the scope of protection of the utility model is not limited to
In this, any one skilled in the art is according to the present utility model in range disclosed in the utility model
Technical solution and its design are subject to equivalent substitution or change, belong to the scope of protection of the utility model.
Claims (10)
1. a kind of unmanned plane vibration damping medicine-chest, including medicine-chest (18), the first damping device for being arranged below the medicine-chest (18) and
Multiple second damping devices；It is characterized in that, first damping device includes that casing (9) and setting are interior in described sleeve pipe (9)
Sliding block (10), the first damping spring (11) and cushion block (12), the sliding block (10) by connecting rod (8) be arranged first fix
On frame (6), the connecting rod (8) and first fixed frame (6) are arranged on fuselage (15)；Multiple second damping dresses
It sets and is distributed in dispersed, second damping device includes the decoupling rod (4) being connect with the medicine-chest (18) and is arranged described
The second damping spring (5) on decoupling rod (4), the lower section of the decoupling rod (4) are equipped with cushion socket (2), on the cushion socket (2)
Equipped with the spring limiting part (3) limited to second damping spring (5), the bottom of the cushion socket (2) is equipped with pedestal
(1), the pedestal (1) is arranged on the second fixed frame (16), and second fixed frame (16) is arranged on the fuselage (15).
2. a kind of unmanned plane vibration damping medicine-chest according to claim 1, it is characterised in that：The medicine-chest (18) is equipped with transparent
Window (19), the transparency window (19) are equipped with scale (20), and the transparency window (19) is windowpane.
3. a kind of unmanned plane vibration damping medicine-chest according to claim 1, it is characterised in that：The pedestal (1) has groove, institute
It states cushion socket (2) to be arranged in the groove, the cushion socket (2) is equipped with limited block (14), and the pedestal (1), which is equipped with, to be subtracted
Shake slot (7), the limited block (14) sliding in the damping trough (7).
4. a kind of unmanned plane vibration damping medicine-chest according to claim 3, it is characterised in that：The bottom portion of groove of the pedestal (1)
Equipped with damping soft formation (22), the cushion socket (2) is arranged on the damping soft formation (22), and the damping soft formation (22) is rubber
Layer.
5. a kind of unmanned plane vibration damping medicine-chest according to claim 1, it is characterised in that：First fixed frame (6) and institute
It is metal holder to state the second fixed frame (16), and shape is arc, and cross sectional shape is cylinder.
6. a kind of unmanned plane vibration damping medicine-chest according to claim 5, it is characterised in that：Second fixed frame (16) passes through
Fixing nut (17) is fixed on the fuselage (15), and the connecting rod (8) is fixedly connected with first fixed frame (6), institute
It states and is equipped with buffer gap after connecting rod (8) is connect with first fixed frame (6) between the fuselage (15).
7. a kind of unmanned plane vibration damping medicine-chest according to claim 1, it is characterised in that：First damping spring (11) sets
It sets between the sliding block (10) and the cushion block (12), the top of the sliding block (10) passes through first damping spring (11)
With the cushion block (12) elastic connection.
8. a kind of unmanned plane vibration damping medicine-chest according to claim 1, it is characterised in that：The inside of described sleeve pipe (9) is arranged
There are notch sliding slot directed downwardly, the cushion block (12) to be fixed at the top of the sliding slot cell wall.
9. a kind of unmanned plane vibration damping medicine-chest according to claim 8, it is characterised in that：At the notch of the sliding slot be equipped with pair
The positive stop lug boss (13) that the sliding block (10) is limited is fixedly connected between the positive stop lug boss (13) and described sleeve pipe (9).
10. a kind of unmanned plane vibration damping medicine-chest according to claim 1, it is characterised in that：First damping spring (11)
It is metal damping spring with second damping spring (5), the pedestal (1) is metab, and the cushion socket (2) is gold
Belong to cushion socket, the decoupling rod (4) is metal decoupling rod.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721870628.2U CN208024771U (en) | 2017-12-27 | 2017-12-27 | A kind of unmanned plane vibration damping medicine-chest |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721870628.2U CN208024771U (en) | 2017-12-27 | 2017-12-27 | A kind of unmanned plane vibration damping medicine-chest |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208024771U true CN208024771U (en) | 2018-10-30 |
Family
ID=63900608
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721870628.2U Expired - Fee Related CN208024771U (en) | 2017-12-27 | 2017-12-27 | A kind of unmanned plane vibration damping medicine-chest |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208024771U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109781234A (en) * | 2019-01-29 | 2019-05-21 | 浙江厚达智能科技股份有限公司 | If the rack of oscillation crosswise transferring structure |
| CN109781235A (en) * | 2019-01-29 | 2019-05-21 | 浙江厚达智能科技股份有限公司 | Chinese medicine weighing system vibration damping open frame |
-
2017
- 2017-12-27 CN CN201721870628.2U patent/CN208024771U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109781234A (en) * | 2019-01-29 | 2019-05-21 | 浙江厚达智能科技股份有限公司 | If the rack of oscillation crosswise transferring structure |
| CN109781235A (en) * | 2019-01-29 | 2019-05-21 | 浙江厚达智能科技股份有限公司 | Chinese medicine weighing system vibration damping open frame |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN208024771U (en) | A kind of unmanned plane vibration damping medicine-chest | |
| CN206374975U (en) | A kind of aircraft wheel group containing two sets of shock mitigation systems | |
| CN204776052U (en) | Damping structure of cloud platform | |
| CN204921809U (en) | Elevator from area buffering vibration damper | |
| CN204956199U (en) | Vibration -damping seat | |
| CN206939060U (en) | Undercarriage for vertically taking off and landing flyer | |
| CN205217215U (en) | Connecting rod formula sprayer | |
| CN209654520U (en) | A kind of unmanned machine support damping device of aerial survey remote sensing | |
| CN203402344U (en) | Linkage type front fork structure of bicycle | |
| CN208053638U (en) | A kind of novel plant protection machine unmanned plane pulling buckle | |
| CN203214660U (en) | Dustproof bearing seat | |
| CN208149596U (en) | A kind of unmanned plane shock bracket | |
| CN207843307U (en) | A kind of plant protection drone undercarriage with pooling feature | |
| CN201102567Y (en) | Shock absorbing device of babies' barrow | |
| CN205203216U (en) | Basket damping device | |
| CN210971512U (en) | Four-wheel aircraft front wheel steering shock absorber | |
| CN208897314U (en) | A kind of novel unmanned plane elasticity undercarriage | |
| CN108609163A (en) | A kind of mapping unmanned plane lifting shock bracket | |
| CN205220257U (en) | Snowmobile hangs rocking arm | |
| CN204784369U (en) | Baby's handcart damper | |
| CN212125529U (en) | Unmanned aerial vehicle is used in plant protection reconnaissance with vibration damping mount | |
| CN212448049U (en) | Unmanned aerial vehicle for plant protection exploration of easy maintenance | |
| CN206813217U (en) | Shock-absorbing device for bicycle | |
| CN208558929U (en) | A kind of automobile front suspension structure | |
| CN208745680U (en) | A kind of automobile swing arm that can detect damaged condition automatically |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181030 Termination date: 20191227 |