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 PDF

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Publication number
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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CN
China
Prior art keywords
plate
unmanned plane
mounting
reinforcing rib
vibration damper
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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
Application number
CN201820914995.6U
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Chinese (zh)
Inventor
吴建杭
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Nanjing Jim Pogson Aviation Technology Co Ltd
Original Assignee
Nanjing Jim Pogson Aviation Technology Co Ltd
Priority date (The priority date 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 date listed.)
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Priority to CN201820914995.6U priority Critical patent/CN208882096U/en
Application granted granted Critical
Publication of CN208882096U publication Critical patent/CN208882096U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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

It is a kind of to be easily installed fixed unmanned plane reinforcing rib attachment device
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.
CN201820914995.6U 2018-06-13 2018-06-13 It is a kind of to be easily installed fixed unmanned plane reinforcing rib attachment device Expired - Fee Related CN208882096U (en)

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
CN208882096U true CN208882096U (en) 2019-05-21

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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
CN (1) CN208882096U (en)

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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