CN208882096U - It is a kind of to be easily installed fixed unmanned plane reinforcing rib attachment device - Google Patents
It is a kind of to be easily installed fixed unmanned plane reinforcing rib attachment device Download PDFInfo
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- CN208882096U CN208882096U CN201820914995.6U CN201820914995U CN208882096U CN 208882096 U CN208882096 U CN 208882096U CN 201820914995 U CN201820914995 U CN 201820914995U CN 208882096 U CN208882096 U CN 208882096U
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- Prior art keywords
- plate
- unmanned plane
- mounting
- reinforcing rib
- vibration damper
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Abstract
Fixed unmanned plane reinforcing rib attachment device is easily installed the utility model discloses a kind of, including welding mounting portion, connecting plate, vibration damper plate and unmanned plane installing zone, connecting plate is installed above the unmanned plane installing zone, and connecting plate is all provided with welding mounting portion close to the two sides of unmanned plane installing zone one end, the bottom end of connecting plate is provided with the second tread plate between the welding mounting portion, and the second middle position inside tread plate is equipped with air sac strip, tuberal part is evenly arranged on the air sac strip, and the middle position at air sac strip both ends is all provided with the wirerope connecting with the second tread plate inside.This is easily installed fixed unmanned plane reinforcing rib attachment device, by being equipped with vibration damper plate, buffer stopper, dashpot and damping spring, so that the device realizes preferable damping, buffering performance in terms of passing through shift transformation and elastic deformation two, to improve the using effect of device.
Description
Technical field
It is specially a kind of to be easily installed fixed unmanned plane and add the utility model relates to unmanned plane attachment device technical field
Strengthening tendons attachment device.
Background technique
China is used as large agricultural country, and 1,800,000,000 mu of basic farmlands need a large amount of agricultural plant protection operation every year, and China is annual
Pesticide poisoning number has 100,000 crowd, lethality 20 about percent, and mortality caused by pesticide residue and pollution is so far still
Without official statistics, presumably an even more surprising number, unmanned Mini Tele-Copter have operation height low, and drift is few, can be empty
Middle hovering, is not necessarily to dedicated landing airport, and the downdraught that rotor generates helps to increase spray to the penetrability of crop, prevention and treatment effect
Fruit is high, and long-distance remote control operation, spraying operation personnel avoid the danger for being exposed to pesticide, improve spraying operation safety etc.
Plurality of advantages, therefore enjoy great popularity, there are a large amount of connection structure in the overall construction of unmanned plane, need to connect dress accordingly
It sets.
However existing unmanned plane attachment device or it is more or less there are some drawbacks, people cannot be met well
Demand cause device inconvenient for use, in addition, existing unmanned plane attachment device is generally deposited similar to being not easy to be fixedly mounted
Lower in structural strength, tension crashworthiness is weak, this causes the service life of device shorter, is unfavorable for the popularization of device, in order to
These defects are solved, provide better usage experience for people, novel are easily installed fixed unmanned plane it is proposed that a kind of
Reinforcing rib attachment device.
Utility model content
It is easily installed fixed unmanned plane reinforcing rib attachment device the purpose of this utility model is to provide a kind of, to solve
It is mentioned above in the background art to be not easy to fixed installation, the problem that structural strength is lower and tension crashworthiness is weak.
To achieve the above object, the utility model provides the following technical solutions: a kind of to be easily installed fixed unmanned plane and add
Strengthening tendons attachment device, including welding mounting portion, connecting plate, vibration damper plate and unmanned plane installing zone, the unmanned plane installing zone it is upper
Side is equipped with connecting plate, and connecting plate is all provided with welding mounting portion, the welding close to the two sides of unmanned plane installing zone one end
The bottom end of connecting plate is provided with the second tread plate between mounting portion, and the middle position inside the second tread plate is equipped with air bag
Item is evenly arranged with tuberal part on the air sac strip, and the middle position at air sac strip both ends is all provided with and the second tread plate
The wirerope of inside connection, the both ends of the connecting plate are all provided with lock seaming bar, and are evenly arranged with reinforcing strip on bar of lockstitching a border, institute
It states top and bottom end inside lock seaming bar and is all evenly arranged with balance weight, the top of the connecting plate is equipped with vibration damper plate, and subtracts
The top and bottom end for shaking intralamellar part are all provided with the first mounting plate, and the described one end of first mounting plate far from vibration damper plate is all provided with
Second mounting plate, and the bottom end of the second mounting plate close to vibration damper plate inner tip is evenly arranged with dashpot, it is described far from subtracting
The top for shaking second mounting plate on intralamellar part top is evenly arranged with the buffer stopper cooperated with dashpot, and buffer stopper top buffers
The inside of slot is evenly arranged with damping spring.
Preferably, the inner sidewall of the mounting hole is provided with thread groove, is all arranged in the mounting disc at the mounting hole both ends
There is the first tread plate, and constitutes bilateral symmetry, the peace about the vertical center line of mounting hole between the first adjacent tread plate
It fills and is all provided with positioning column in the mounting disc of hole two sides, and constituted between adjacent positioning column about the vertical center line of mounting hole
Front and back is symmetrical.
Preferably, the top of the vibration damper plate is equipped with mounting disc, and mounting disc is internally provided with mounting hole, the peace
The vertical center line of hole, mounting disc and vibration damper plate three are filled on same vertical line.
Preferably, the central position inside the connecting plate is provided with reserved chamber, and the inside of reserved chamber is uniformly arranged
There is the titanium alloy reinforcement block equally arranged, the longitudinal section of the titanium alloy reinforcement block is in regular hexagon.
Preferably, convex is presented in the longitudinal section of the welding mounting portion, and that welds mounting portion is internally provided with reinforcement
Layer, the inside of the enhancement layer is evenly arranged in honeycomb arrangement reinforcing rib, and the longitudinal section of reinforcing rib is inverted U shape.
Preferably, the welding mounting portion, connecting plate, vibration damper plate and the lateral wall of mounting disc are all coated with anti oxidation layer,
And the thickness range of the anti oxidation layer is at 2-4 millimeters.
Connect compared with prior art, the utility model has the beneficial effects that this is easily installed fixed unmanned plane reinforcing rib
Connection device, by being equipped with vibration damper plate, buffer stopper, dashpot and damping spring, so that the device passes through shift transformation and elasticity
Preferable damping, buffering performance is realized in terms of deformation two, to improve the using effect of device, is conducive to the length of the device
Phase promotes, and the device is by being equipped with mounting disc, mounting hole, thread groove and tread plate, so that on the one hand the device is convenient for fixing
On the other hand installation and removal enhance firm performance when device is fixed, guarantee that it is not easy to slip, the device is by being equipped with
Mounting portion, enhancement layer and reinforcing rib are welded, so that the device is convenient for and the relevant device of unmanned plane installing zone firmly installs, simultaneously
Loss when device welding is weakened, the service life of device is conducive to extend, meanwhile, the device is anti-oxidant by being provided with
Layer, so that enhancing the functionality of device the arrangement achieves preferable corrosion resistance, the device is by being equipped with reserved chamber
With titanium alloy reinforcement block so that device also reduces the weight of itself while enhancing the structural strength of itself, to be promoted
The using effect of device, is conducive to the long-term popularization of the device.
Detailed description of the invention
Fig. 1 faces the schematic diagram of the section structure for the utility model;
Fig. 2 is that the welding mounting portion of the utility model faces the schematic diagram of the section structure;
Fig. 3 is that the vibration damper plate of the utility model faces the schematic diagram of the section structure;
Fig. 4 is that partial profile structure is overlooked in the mounting disc of the utility model.
In figure: 1, mounting hole;2, dashpot;3, lock seaming bar;4, reinforcing strip;5, chamber is reserved;6, enhancement layer;7, first is anti-skidding
Item;8, vibration damper plate;9, balance weight;10, titanium alloy reinforcement block;11, connecting plate;12, mounting portion is welded;13, unmanned plane installing zone;
14, reinforcing rib;15, wirerope;16, air sac strip;17, tuberal part;18, the second tread plate;19, the first mounting plate;20, damping bullet
Spring;21, the second mounting plate;22, buffer stopper;23, positioning column;24, thread groove;25, mounting disc.
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.
Fig. 1-4 is please referred to, the utility model provides a kind of technical solution: a kind of to be easily installed fixed unmanned plane reinforcing rib
Attachment device, including welding mounting portion 12, connecting plate 11, vibration damper plate 8 and unmanned plane installing zone 13, unmanned plane installing zone 13 it is upper
Side is equipped with connecting plate 11, and connecting plate 11 is all provided with welding mounting portion 12 close to the two sides of 13 one end of unmanned plane installing zone,
Convex is presented in the longitudinal section of welding mounting portion 12, and that welds mounting portion 12 is internally provided with enhancement layer 6, enhancement layer 6 it is interior
Portion is evenly arranged in honeycomb arrangement reinforcing rib 14, and the longitudinal section of reinforcing rib 14 is inverted U shape, it is made to improve device welding
The tension crashworthiness of mounting portion 12 enhances the practicability of device, welding peace to ensure that device is mounted so as to more consolidate
The bottom end of connecting plate 11 is provided with the second tread plate 18 between dress portion 12, and the middle position installation inside the second tread plate 18
Have air sac strip 16, be evenly arranged with tuberal part 17 on air sac strip 16, and the middle position at 16 both ends of air sac strip be all provided with
The wirerope 15 connected inside second tread plate 18, the both ends of connecting plate 11 are all provided with lock seaming bar 3, and on bar 3 of lockstitching a border uniformly
It is provided with reinforcing strip 4, the central position inside connecting plate 11 is provided with reserved chamber 5, and the inside of reserved chamber 5 is evenly arranged with
The longitudinal section of the titanium alloy reinforcement block 10 equally arranged, titanium alloy reinforcement block 10 is in regular hexagon, it is made to enhance dress
The overall structural strength set, and the weight of device is alleviated, so that the using effect of device is improved, the top inside bar 3 of lockstitching a border
End and bottom end are all evenly arranged with balance weight 9, and the top of connecting plate 11 is equipped with vibration damper plate 8, and top vibration damper plate 8 inside with
Bottom end is all provided with the first mounting plate 19, and first one end of mounting plate 19 far from vibration damper plate 8 is all provided with the second mounting plate 21, and
Bottom end close to the second mounting plate 21 of 8 inner tip of vibration damper plate is evenly arranged with dashpot 2, and the top of vibration damper plate 8 is equipped with
Mounting disc 25, and mounting disc 25 is internally provided with mounting hole 1,8 three of mounting hole 1, mounting disc 25 and vibration damper plate it is vertical in
Heart line makes it optimize the structure of device on same vertical line, ensure that the stability of apparatus structure, the inside of mounting hole 1
Wall is provided with thread groove 24, the first tread plate 7 is all provided in the mounting disc 25 at 1 both ends of mounting hole, and adjacent first is anti-skidding
Bilateral symmetry is constituted about the vertical center line of mounting hole 1 between item 7, it is fixed to be all provided in the mounting disc 25 of 1 two sides of mounting hole
Position column 23, and front and back is constituted symmetrically about the vertical center line of mounting hole 1 between adjacent positioning column 23, make it easy to device peace
Securely, to enhance the practicability of device, the top of the second mounting plate 21 far from 8 inner tip of vibration damper plate is uniformly arranged dress
There is the buffer stopper 22 cooperated with dashpot 2, and the inside of 22 top dashpot 2 of buffer stopper is evenly arranged with damping spring 20, weldering
It connects mounting portion 12, connecting plate 11, vibration damper plate 8 and the lateral wall of mounting disc 25 and is all coated with anti oxidation layer, and the anti oxidation layer
Thickness range makes the corrosion resistance which increase device at 2-4 millimeters, to be conducive to extend the service life of device.
Working principle: in use, staff is first with welding mounting portion 12 by the device and unmanned plane installing zone 13
Preferable welding installation is carried out, since welding mounting portion 12 is internally provided with reinforcing rib 14 and enhancement layer 6, so that device reduces
Loss when welding enhances the crush resistance energy of device, is conducive to extend the service life of device, while cooperation second is anti-skidding
The use of item 18, so that device is not easy to slip, then using the effect of the mounting hole 1 in mounting disc 25, by device and accordingly
Equipment firmly installs, so that the functionality of device is enhanced, finally, in the use process of device, since the device is equipped with
Vibration damper plate 8, dashpot 2, buffer stopper 22 and damping spring 20, so that the device is real by shift transformation and two aspect of elastic deformation
Show preferable damping, buffering performance, to improve the using effect of device, is conducive to the long-term popularization of the device, in addition,
The device is by being provided with titanium alloy reinforcement block 10 and reserved chamber 5, so that device is gone back while enhancing the structural strength of itself
The weight of itself is alleviated, to improve the using effect of device, is conducive to the long-term popularization of the device.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of be easily installed fixed unmanned plane reinforcing rib attachment device, including mounting hole (1), welding mounting portion (12), company
Fishplate bar (11), vibration damper plate (8) and unmanned plane installing zone (13), it is characterised in that: pacify the top of the unmanned plane installing zone (13)
Equipped with connecting plate (11), and connecting plate (11) is all provided with welding mounting portion close to the two sides of unmanned plane installing zone (13) one end
(12), the bottom end of connecting plate (11) is provided with the second tread plate (18) between welding mounting portion (12), and the second tread plate
(18) internal middle position is equipped with air sac strip (16), is evenly arranged with tuberal part (17) on the air sac strip (16), and
The middle position at air sac strip (16) both ends is all provided with and the internal wirerope (15) connecting of the second tread plate (18), the company
The both ends of fishplate bar (11) are all provided with lock seaming bar (3), and are evenly arranged with reinforcing strip (4) in lock seaming bar (3), the lock seaming bar
(3) internal top and bottom end are all evenly arranged with balance weight (9), and the top of the connecting plate (11) is equipped with vibration damper plate (8),
And the internal top and bottom end of vibration damper plate (8) is all provided with the first mounting plate (19), first mounting plate (19) is far from damping
One end of plate (8) is all provided with the second mounting plate (21), and the bottom of the second mounting plate (21) close to vibration damper plate (8) inner tip
End is evenly arranged with dashpot (2), and the top of the second mounting plate (21) of separate vibration damper plate (8) inner tip is uniformly arranged
There is the buffer stopper (22) with dashpot (2) cooperation, and the inside of buffer stopper (22) top dashpot (2) is evenly arranged with damping bullet
Spring (20).
2. a kind of fixed unmanned plane reinforcing rib attachment device is easily installed according to claim 1, it is characterised in that: institute
The inner sidewall for stating mounting hole (1) is provided with thread groove (24), and is all provided in the mounting disc (25) at mounting hole (1) both ends
One tread plate (7), and bilateral symmetry, institute are constituted about the vertical center line of mounting hole (1) between adjacent the first tread plate (7)
It states and is all provided with positioning column (23) in the mounting disc (25) of mounting hole (1) two sides, and about peace between adjacent positioning column (23)
The vertical center line for filling hole (1) constitutes front and back symmetrically.
3. a kind of fixed unmanned plane reinforcing rib attachment device is easily installed according to claim 1, it is characterised in that: institute
The top for stating vibration damper plate (8) is equipped with mounting disc (25), and mounting disc (25) is internally provided with mounting hole (1), the installation
The vertical center line in hole (1), mounting disc (25) and vibration damper plate (8) three is on same vertical line.
4. a kind of fixed unmanned plane reinforcing rib attachment device is easily installed according to claim 1, it is characterised in that: institute
The internal central position of connecting plate (11) is stated to be provided with reserved chamber (5), and the inside of reserved chamber (5) be evenly arranged in etc. between
Titanium alloy reinforcement block (10) away from arrangement, the longitudinal section of the titanium alloy reinforcement block (10) are in regular hexagon.
5. a kind of fixed unmanned plane reinforcing rib attachment device is easily installed according to claim 1, it is characterised in that: institute
Convex is presented in the longitudinal section for stating welding mounting portion (12), and welds being internally provided with enhancement layer (6) for mounting portion (12), described
The inside of enhancement layer (6) is evenly arranged in honeycomb arrangement reinforcing rib (14), and the longitudinal section of reinforcing rib (14) is inverted U shape.
6. a kind of fixed unmanned plane reinforcing rib attachment device is easily installed according to claim 1, it is characterised in that: institute
The lateral wall for stating welding mounting portion (12), connecting plate (11), vibration damper plate (8) and mounting disc (25) is all coated with anti oxidation layer, and
The thickness range of the anti oxidation layer is at 2-4 millimeters.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201820914995.6U CN208882096U (en) | 2018-06-13 | 2018-06-13 | It is a kind of to be easily installed fixed unmanned plane reinforcing rib attachment device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201820914995.6U CN208882096U (en) | 2018-06-13 | 2018-06-13 | It is a kind of to be easily installed fixed unmanned plane reinforcing rib attachment device |
Publications (1)
Publication Number | Publication Date |
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CN208882096U true CN208882096U (en) | 2019-05-21 |
Family
ID=66505474
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201820914995.6U Expired - Fee Related CN208882096U (en) | 2018-06-13 | 2018-06-13 | It is a kind of to be easily installed fixed unmanned plane reinforcing rib attachment device |
Country Status (1)
Country | Link |
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CN (1) | CN208882096U (en) |
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2018
- 2018-06-13 CN CN201820914995.6U patent/CN208882096U/en not_active Expired - Fee Related
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Legal Events
Date | Code | Title | Description |
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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: 20190521 |