CN210653672U - Unmanned aerial vehicle system for special equipment detection - Google Patents
Unmanned aerial vehicle system for special equipment detection Download PDFInfo
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- CN210653672U CN210653672U CN201920480311.0U CN201920480311U CN210653672U CN 210653672 U CN210653672 U CN 210653672U CN 201920480311 U CN201920480311 U CN 201920480311U CN 210653672 U CN210653672 U CN 210653672U
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Abstract
The utility model provides an unmanned aerial vehicle system for detecting special equipment, which relates to the technical field of unmanned aerial vehicles, and comprises a body, wherein the top of the body is provided with wings, the top of the body is adhered with a switch and a wireless receiver electrically connected with the switch, the bottom side of the side wall of the body is fixedly connected with an arc rod, the bottom of the arc rod is connected with a fixed block, one side of the fixed block close to the body is adhered with an annular air bag, the unmanned aerial vehicle system for detecting special equipment is provided with the annular air bag at the bottom side of the outer wall of the body, the annular air bag in an inflation state can surround the bottom of the side wall of the body, the impact strength between the unmanned aerial vehicle and the ground when falling is reduced, a small catapult parachute is arranged at the top of the body, the top of the unmanned aerial vehicle can be lifted, the unmanned aerial vehicle which falls can correct the, the annular air bag is ensured to be firstly contacted with the ground.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle system is used in special equipment detection.
Background
The quantity of special equipment presents the rapid growth trend, its structure and theory of operation are becoming complicated day by day, make special equipment inspection task climb year by year, consequently need effectively to use current advanced technology fast to improve inspection efficiency and quality, solve the restriction of complicated inspection environment to people, there is at present to use unmanned aerial vehicle to detect, detection efficiency has been improved greatly, but unmanned aerial vehicle flies in complicated environment, also easily strike the foreign object and produce the danger of falling, application number is CN201820476092.4 an unmanned aerial vehicle who has the safety protection function, although solved the influence to unmanned aerial vehicle when sideslipping, nevertheless can't reduce the damage to unmanned aerial vehicle when falling in the high altitude, the unmanned aerial vehicle that falls in the high altitude very easily causes the damage of internals, maintenance cost has been increased.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Not enough to prior art, the utility model provides a special equipment detects uses unmanned aerial vehicle system has solved the unmanned aerial vehicle that the high altitude falls and has very easily caused the damage of internals, has increased cost of maintenance's problem.
(II) technical scheme
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: the utility model provides a special type equipment detects uses unmanned aerial vehicle system, includes the fuselage, the wing is installed at the top of fuselage, the top of fuselage bond have the switch and with switch electric connection's wireless receiver, the lateral wall bottom side fixedly connected with arc pole of fuselage, the bottom of arc pole is connected with the fixed block, one side that the fixed block is close to the fuselage bonds and has annular gasbag, the outer wall of fuselage bonds and has miniature air pump, and miniature air pump passes through the trachea and is connected with annular gasbag, miniature air pump passes through wire and switch electric connection.
Further, the top joint of fuselage has the top section of thick bamboo on top, it has the slidable shrouding to peg graft at the lateral wall top of top section of thick bamboo, the lateral wall of shrouding is connected with the connecting rod, the bottom of connecting rod is connected with electric liquid push rod, electric liquid push rod riveting in the top of fuselage, electric liquid push rod passes through wire and switch electric connection, the inner wall bottom joint of top section of thick bamboo has the powerful spring of compression, and the joint has little parachute between powerful spring and the shrouding.
Furthermore, the bottom plate of fixed block bonds has the telescopic link, and the bottom of telescopic link bonds has the rubber block, buffer spring has been cup jointed to the outer wall of telescopic link.
Further, the bottom of the machine body is bonded with a rubber disc, and the bottom of the rubber plate is downwards smoothly protruded.
Furthermore, a notch is formed in one side, close to the machine body, of the fixing block, and the annular air bag is located inside the notch.
Furthermore, a rubber ring is bonded on one side, away from the machine body, of the fixed block, and the rubber ring surrounds the bottom side of the outer wall of the machine body.
Furthermore, the top of fuselage fixed mounting has the frame that protects, and protects the frame and encircle the outer wall of wing.
Furthermore, the outer wall of the protective frame is bonded with a reinforcing ring, and the reinforcing ring is sleeved on the outer wall of the protective frame.
(III) advantageous effects
The utility model provides a special equipment detects uses unmanned aerial vehicle system. The method has the following beneficial effects:
1. this special type equipment detects uses unmanned aerial vehicle system has installed annular gasbag in the outer wall bottom side of fuselage, and the annular gasbag of gas filled state can encircle the lateral wall bottom of fuselage, can carry out effectual protection to it when unmanned aerial vehicle falls in the high altitude, reduces the striking dynamics on unmanned aerial vehicle and ground, reduces the damage degree, the effectual loss of property that has reduced.
2. This unmanned aerial vehicle system is used in special equipment detection has installed the little parachute that can launch at the top of fuselage, can lift unmanned aerial vehicle's top, plays the effect of correcting the state of falling to the unmanned aerial vehicle that falls, makes unmanned aerial vehicle's bottom ground, guarantees that annular gasbag earlier with ground contact, can alleviate the speed of falling simultaneously, buffering striking dynamics.
3. This special type equipment detects uses unmanned aerial vehicle system, telescopic link and buffer spring can cushion when unmanned aerial vehicle descends with the rigid contact on ground, the too big stability that influences its inner structure of recoil power of avoiding receiving, the telescopic link inclines to the outside simultaneously, also can play the effect of stabilizing the buffering to it when unmanned aerial vehicle descends sideslipping, the effectual normal operating who guarantees unmanned aerial vehicle.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is an enlarged view of A in FIG. 1;
FIG. 3 is an enlarged view of B in FIG. 1;
fig. 4 is an internal schematic view of the top cylinder of the present invention.
In the figure: the device comprises a machine body 1, wings 2, a protective frame 3, a reinforcing ring 4, an arc rod 5, a fixing block 6, an annular air bag 7, a miniature air pump 8, a notch 9, a telescopic rod 10, a rubber block 11, a rubber ring 12, a rubber disc 13, a top cylinder 14, a sealing plate 15, a small parachute 16, a powerful spring 17, a connecting rod 18, an electro-hydraulic push rod 19, a switch 20, a wireless receiver 21 and a buffer spring 22.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
The embodiment of the utility model provides an unmanned aerial vehicle system for special equipment detection, as shown in figure 1-4, including fuselage 1, the camera for detection is installed to the lateral wall of fuselage 1, the internally mounted of fuselage 1 has the battery, the memory, system devices such as motor that control unmanned aerial vehicle flies, wing 2 is installed at the top of fuselage 1, switch 20 and the wireless receiver 21 of being connected with switch 20 electricity are bonded to the top of fuselage 1, the wireless transmitter that is fit for with wireless receiver 21 is installed on the remote controller of unmanned aerial vehicle, can carry out remote control to it, the lateral wall bottom side of fuselage 1 is fixedly connected with arc pole 5, the quantity of arc pole 5 has four, the equidistance encircles the outer wall of fuselage 1, the bottom of arc pole 5 is connected with fixed block 6, one side of fixed block 6 near fuselage 1 is bonded with annular gasbag 7, the outer wall of fuselage 1 is bonded with miniature air pump 8, the model of miniature air pump 8 is ZQ370-01PM, rated voltage is 6V, miniature air pump 8 passes through the trachea and is connected with annular gasbag 7, miniature air pump 8 passes through wire and switch 20 electric connection, miniature air pump 8 starts to aerify annular gasbag 7 is inside, the annular gasbag 7 of the gas filled state can encircle the lateral wall bottom of fuselage 1, can carry out effectual protection to it when unmanned aerial vehicle high altitude falls, reduce the striking dynamics on unmanned aerial vehicle and ground, reduce the damage degree, the effectual loss of property that has reduced.
Further, a top barrel 14 without a top is clamped at the top of the machine body 1, a slidable sealing plate 15 is inserted at the top of the side wall of the top barrel 14, the side wall of the sealing plate 15 is connected with a connecting rod 18, the bottom of the connecting rod 18 is connected with an electro-hydraulic push rod 19, the electro-hydraulic push rod 19 is riveted at the top of the machine body 1, the electro-hydraulic push rod 19 is electrically connected with a switch 20 through a lead, a compressed strong spring 17 is clamped at the bottom of the inner wall of the top barrel 14, and a small parachute 16 is clamped between the strong spring 17 and the sealing plate, when the unmanned aerial vehicle is out of control and falls, the electro-hydraulic push rod 19 contracts to drive the sealing plate 15 to move out of the top cylinder 14, the compressed strong spring 17 can eject the small parachute 16 to lift the top of the unmanned aerial vehicle, play the effect of correcting the state of falling to the unmanned aerial vehicle that falls, make unmanned aerial vehicle's bottom ground, guarantee annular gasbag 7 earlier with ground contact, can alleviate the speed of falling simultaneously, buffering striking dynamics.
Wherein, the bottom plate of fixed block 6 bonds there is telescopic link 10, telescopic link 10 is to keeping away from the lopsidedness of fuselage 1, and the bottom of telescopic link 10 bonds there is rubber block 11, buffer spring 22 has been cup jointed to the outer wall of telescopic link 10, telescopic link 10 and buffer spring 22 can cushion the rigid contact on ground when unmanned aerial vehicle descends, the too big stability that influences its inner structure of recoil power of avoiding receiving, simultaneously telescopic link 10 inclines to the outside, also can play the effect of stabilizing the buffering to it when unmanned aerial vehicle descends and sideslips, the effectual normal operating who guarantees unmanned aerial vehicle.
Wherein, the bottom of fuselage 1 bonds there is rubber disc 13, and the downward rounding off of bottom of rubber slab 13 is protruding, and rubber disc 13's shape helps upwards exporting the air current of unmanned aerial vehicle bottom, is in the horizontality when guaranteeing unmanned aerial vehicle whereabouts.
Wherein, fixed block 6 has seted up notch 9 near one side of fuselage 1, and annular gasbag 7 is located the inside of notch 9, and the notch 9 inner wall is slick and sly, and notch 9 protects annular gasbag 7, avoids annular gasbag 7 and external object wearing and tearing, and the influence is to unmanned aerial vehicle's protection effect.
Wherein, one side bonding that fuselage 1 was kept away from to fixed block 6 has rubber ring 12, and rubber ring 12 encircles in the bottom side of fuselage 1 outer wall, and rubber ring 12 links together four fixed blocks 6, helps stabilizing its orientation, avoids using 6 slopes of fixed block to influence the supporting effect to unmanned aerial vehicle for a long time.
Wherein, the top fixed mounting of fuselage 1 has protecting frame 3, and protects frame 3 and encircles the outer wall of wing 2, protects frame 3 and can encircle the protection with the outside of wing 2, and it causes the damage to avoid wing 2 to contact with external object when rotatory.
Wherein, the outer wall of protecting frame 3 bonds and has beaded finish 4, and beaded finish 4 cover is located the outer wall of protecting frame 3, and beaded finish 4 has increased the intensity of protecting frame 3, has further improved the protection effect to wing 2.
The working principle is as follows: when the unmanned aerial vehicle lands, the telescopic rod 10 and the buffer spring 22 can buffer the hard contact with the ground when the unmanned aerial vehicle lands, the influence of overlarge recoil force on the stability of the internal structure of the unmanned aerial vehicle is avoided, meanwhile, the telescopic rod 10 inclines to the outer side, and the function of stable buffer can be also played when the unmanned aerial vehicle lands and sideslips, so that the normal operation of the unmanned aerial vehicle is effectively ensured, the protective frame 3 and the reinforcing ring 4 can protect the rotating wings 2, the wings 2 are prevented from being greatly damaged on foreign objects, when the unmanned aerial vehicle is out of control and falls, a remote controller of the unmanned aerial vehicle sends an instruction to the wireless receiver 21, the start switch 20 controls the micro air pump 8 to start, so that the annular air bag 7 is inflated to surround the bottom of the side wall of the body 1, the unmanned aerial vehicle can be effectively protected when falling in high altitude, and the impact, reduce the damage degree, the 19 shrink of switch 20 control electricity liquid push rod simultaneously drives shrouding 15 and shifts out the outside of top cylinder 14, and compressed powerful spring 17 can pop out little parachute 16, lifts unmanned aerial vehicle's top, plays the effect of correcting the state of falling to the unmanned aerial vehicle that falls, makes unmanned aerial vehicle's bottom ground, guarantees annular gasbag 7 earlier with ground contact, can alleviate the speed of falling simultaneously, buffering striking dynamics.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (8)
1. Unmanned aerial vehicle system is used in special type equipment detection, its characterized in that, including fuselage (1), wing (2) are installed at the top of fuselage (1), the top of fuselage (1) bonds switch (20) and wireless receiver (21) with switch (20) electric connection, the lateral wall bottom side fixedly connected with arc pole (5) of fuselage (1), the bottom of arc pole (5) is connected with fixed block (6), one side that fixed block (6) are close to fuselage (1) bonds and has annular gasbag (7), the outer wall of fuselage (1) bonds and has miniature air pump (8), and miniature air pump (8) are connected with annular gasbag (7) through the trachea, miniature air pump (8) pass through wire and switch (20) electric connection.
2. The unmanned aerial vehicle system for special equipment detection of claim 1, wherein: the top joint of fuselage (1) has top section of thick bamboo (14) on top or not, it has slidable shrouding (15) to peg graft at the lateral wall top of top section of thick bamboo (14), the lateral wall of shrouding (15) is connected with connecting rod (18), the bottom of connecting rod (18) is connected with electric liquid push rod (19), electric liquid push rod (19) are riveted in the top of fuselage (1), electric liquid push rod (19) pass through wire and switch (20) electric connection, the inner wall bottom joint of top section of thick bamboo (14) has compressed powerful spring (17), and the joint has little parachute (16) between powerful spring (17) and shrouding (15).
3. The unmanned aerial vehicle system for special equipment detection of claim 1, wherein: the bottom plate of fixed block (6) bonds has telescopic link (10), and the bottom of telescopic link (10) bonds has rubber block (11), buffer spring (22) have been cup jointed to the outer wall of telescopic link (10).
4. The unmanned aerial vehicle system for special equipment detection of claim 1, wherein: the bottom of the machine body (1) is bonded with a rubber disc (13), and the bottom of the rubber disc (13) is downwards smoothly protruded.
5. The unmanned aerial vehicle system for special equipment detection of claim 1, wherein: one side of the fixed block (6) close to the machine body (1) is provided with a notch (9), and the annular air bag (7) is positioned in the notch (9).
6. The unmanned aerial vehicle system for special equipment detection of claim 1, wherein: one side of the fixed block (6) far away from the machine body (1) is bonded with a rubber ring (12), and the rubber ring (12) surrounds the bottom side of the outer wall of the machine body (1).
7. The unmanned aerial vehicle system for special equipment detection of claim 1, wherein: the top fixed mounting of fuselage (1) has protective frame (3), and protective frame (3) encircles the outer wall of wing (2).
8. The unmanned aerial vehicle system for special equipment detection of claim 7, wherein: the outer wall of the protective frame (3) is bonded with a reinforcing ring (4), and the reinforcing ring (4) is sleeved on the outer wall of the protective frame (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920480311.0U CN210653672U (en) | 2019-04-10 | 2019-04-10 | Unmanned aerial vehicle system for special equipment detection |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201920480311.0U CN210653672U (en) | 2019-04-10 | 2019-04-10 | Unmanned aerial vehicle system for special equipment detection |
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| CN210653672U true CN210653672U (en) | 2020-06-02 |
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| CN201920480311.0U Active CN210653672U (en) | 2019-04-10 | 2019-04-10 | Unmanned aerial vehicle system for special equipment detection |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113137892A (en) * | 2020-12-25 | 2021-07-20 | 北京理工大学 | Low-slow small target cluster countercheck device based on flexible network capture and countercheck method thereof |
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2019
- 2019-04-10 CN CN201920480311.0U patent/CN210653672U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113137892A (en) * | 2020-12-25 | 2021-07-20 | 北京理工大学 | Low-slow small target cluster countercheck device based on flexible network capture and countercheck method thereof |
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