CN213735505U - Novel aircraft bonnet of unmanned aerial vehicle - Google Patents
Novel aircraft bonnet of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN213735505U CN213735505U CN202022785148.4U CN202022785148U CN213735505U CN 213735505 U CN213735505 U CN 213735505U CN 202022785148 U CN202022785148 U CN 202022785148U CN 213735505 U CN213735505 U CN 213735505U
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- CN
- China
- Prior art keywords
- wall
- protecting crust
- cover body
- unmanned aerial
- aerial vehicle
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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
Links
- 238000003466 welding Methods 0.000 claims abstract description 15
- 230000004224 protection Effects 0.000 claims description 40
- 230000001681 protective effect Effects 0.000 claims description 9
- 230000008878 coupling Effects 0.000 abstract description 2
- 238000010168 coupling process Methods 0.000 abstract description 2
- 238000005859 coupling reaction Methods 0.000 abstract description 2
- 230000004888 barrier function Effects 0.000 description 3
- 239000000428 dust Substances 0.000 description 2
- 239000008187 granular material Substances 0.000 description 2
- 230000008859 change Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000009979 protective mechanism Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model discloses a novel aircraft bonnet of unmanned aerial vehicle, including the cover body and protecting crust, it has the constant head tank to open on the top outer wall of the cover body, and it has the guiding hole to open on the bottom inner wall of constant head tank, the welding of the center department of protecting crust bottom outer wall has the guide bar, and the guide bar is pegged graft in the inside of guiding hole, the welding has main spring on the bottom outer wall of protecting crust, and main spring cup joints in the outside of guide bar, the one end joint that the protecting crust was kept away from to main spring is in the inside of constant head tank, it has the fixed slot that is the equidistance and distributes to open on the top outside of the cover body, the welding has the secondary spring that becomes the equidistance and distributes on the bottom outer wall of protecting crust, and the inside of the one end joint of protecting crust is kept away from to secondary spring at the fixed slot. The utility model discloses the top that the cover body is the easiest to receive the collision uses the protecting crust to protect, and the protecting crust passes through main spring and vice spring coupling with the cover body for the protecting crust can only transmit the vibration that receives for the cover body with soft vibrations, has protected the cover body, prevents that the cover body from receiving great damage.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to a novel aircraft bonnet of unmanned aerial vehicle.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
Current unmanned aerial vehicle aircraft bonnet is mostly overall structure, because when the misoperation fuselage bumps, fuselage and barrier direct contact cause the damage of fuselage easily. Therefore, it is highly desirable to design a new hood for unmanned aerial vehicles to solve the above problems.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that exists among the prior art, and the novel aircraft bonnet of unmanned aerial vehicle that proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides a novel aircraft bonnet of unmanned aerial vehicle, includes the cover body and protecting crust, it has the constant head tank to open on the top outer wall of the cover body, and opens on the bottom inner wall of constant head tank and have the guiding hole, the welding of the center department of protecting crust bottom outer wall has the guide bar, and the guide bar pegs graft in the inside of guiding hole, the welding has main spring on the bottom outer wall of protecting crust, and main spring cup joints in the outside of guide bar, the one end joint that the protecting crust was kept away from to main spring is in the inside of constant head tank.
Furthermore, open on the top outside of the cover body and be the fixed slot that the equidistance distributes, the welding has the auxiliary spring that becomes the equidistance and distributes on the bottom outer wall of protecting crust, and the one end joint that the protecting crust was kept away from to the auxiliary spring is in the inside of fixed slot.
Furthermore, threaded connection has the protection knob on the top inner wall of the cover body, and it has the cushion hole to open on the top outer wall of protection knob, the guide bar is pegged graft in the inside of cushion hole, it has the blotter to bond on the bottom inner wall of cushion hole.
Further, the welding has the connecting rod that is the equidistance and distributes on the side outer wall of the cover body, and the outside of connecting rod has cup jointed protection machanism, the joint has last fixed cover and lower fixed cover on the side outer wall of connecting rod, and goes up fixed cover and lower fixed cover be the rotation with one side outer wall through the hinge and connect, protection machanism is located one side outer wall of connecting rod and goes up between the outer wall of fixed cover one side.
Further, protection machanism is including the protection frame, all install the guard plate through the screw on the top outer wall of protection frame and on the bottom outer wall, it has the gas tank that is the equidistance and distributes to open on the top outer wall of guard plate, and the inside joint in gas tank has the filter screen.
Further, it has the jack to open on one side outer wall of protection frame, and the protection frame cup joints the outside at the connecting rod through the jack, it has the draw-in groove that is the equidistance and distributes to open on the side inner wall of jack, the welding has the fixture block that is the equidistance and distributes on one side outer wall of connecting rod, and the fixture block joint is in the inside of draw-in groove.
Furthermore, the top outer wall and the bottom outer wall of the connecting rod are provided with fixing holes distributed equidistantly, the bottom inner wall of the upper fixing sleeve and the top inner wall of the lower fixing sleeve are welded with fixing pins distributed equidistantly, and the fixing pins are inserted into the fixing holes.
The utility model has the advantages that:
1. through the protecting crust that sets up, the top that receives the collision most of the cover body uses the protecting crust to protect, and the protecting crust passes through main spring and vice spring coupling with the cover body for the protecting crust can absorb the vibration that receives, only transmits soft vibrations for the cover body, has protected the cover body, prevents that the cover body from receiving great damage.
2. Through the protection machanism who sets up, the protection frame can protect the screw, can prevent when touching with the barrier that the screw is direct to touch the emergence that causes the crash accident with the barrier to the filter screen can filter the air of screw contact, makes unmanned aerial vehicle can fly in the more environment of granule dust in the air.
Drawings
Fig. 1 is a schematic structural view of a novel hood of an unmanned aerial vehicle provided by the present invention;
fig. 2 is a schematic view of a connecting rod structure of a novel hood of an unmanned aerial vehicle according to the present invention;
fig. 3 is a sectional view of a cover body structure of a novel hood of an unmanned aerial vehicle, which is provided by the utility model;
fig. 4 is the utility model provides a protection machanism structure explosion schematic diagram of novel aircraft bonnet of unmanned aerial vehicle.
In the figure: the protective cover comprises a cover body 1, a protective shell 2, a connecting rod 3, a protective mechanism 4, a guide rod 5, a main spring 6, a positioning groove 7, a fixing groove 8, a pair of springs 9, a protective knob 10, a buffer hole 11, a buffer pad 12, a guide hole 13, an upper fixing sleeve 14, a lower fixing sleeve 15, a fixing pin 16, a fixing hole 17, a clamping block 18, a protective frame 19, a protective plate 20, an air groove 21, a filter screen 22, a jack 23 and a clamping groove 24.
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.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When a component is referred to as being "connected" to another component, it can be directly connected to the other component or intervening components may also be present. When a component is referred to as being "disposed on" another component, it can be directly on the other component or intervening components may also be present. The terms "vertical," "horizontal," "left," "right," and the like as used herein are for illustrative purposes only.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
Referring to fig. 1-4, a novel aircraft bonnet of unmanned aerial vehicle, including the cover body 1 and protecting crust 2, it has constant head tank 7 to open on the top outer wall of the cover body 1, and it has guiding hole 13 to open on the bottom inner wall of constant head tank 7, the welding of the center department of 2 bottom outer walls of protecting crust has guide bar 5, and guide bar 5 pegs graft in the inside of guiding hole 13, for main spring 6 direction, prevent that main spring 6 from taking place deformation on the horizontal direction, the welding has main spring 6 on the bottom outer wall of protecting crust 2, and main spring 6 cup joints the outside at guide bar 5, the inside at constant head tank 7 of one end joint that protecting crust 2 was kept away from to main spring 6, main spring 6 is used for absorbing the shock.
Further, open on the top outside of the cover body 1 and be the fixed slot 8 that the equidistance distributes, the welding has the vice spring 9 that becomes the equidistance and distributes on the bottom outer wall of protecting crust 2, and the one end joint that the protecting crust 2 was kept away from to vice spring 9 is in the inside of fixed slot 8, further absorbs the vibrations and assaults.
Further, threaded connection has protection knob 10 on the top inner wall of the cover body 1, and it has buffer hole 11 to open on protection knob 10's the top outer wall, and guide bar 5 pegs graft in buffer hole 11's inside, and it has blotter 12 to bond on buffer hole 11's the bottom inner wall, and blotter 12 is used for preventing that guide bar 5 is direct to be in hard contact with protection knob 10.
Further, the welding has the connecting rod 3 that is the equidistance and distributes on the side outer wall of the cover body 1, and the protection machanism 4 has been cup jointed to the outside of connecting rod 3, and the joint has last fixed cover 14 and lower fixed cover 15 on the side outer wall of connecting rod 3, and goes up fixed cover 14 and lower fixed cover 15 be the rotation with one side outer wall through the hinge and connect, and protection machanism 4 is located one side outer wall of connecting rod 3 and goes up between fixed cover 14 one side outer wall.
Further, protection machanism 4 includes protection frame 19, all installs protection plate 20 through the screw on the top outer wall of protection frame 19 and on the bottom outer wall, and it has the air tank 21 that is the equidistance and distributes to open on the top outer wall of protection plate 20, and the inside joint of air tank 21 has filter screen 22, and filter screen 22 is arranged in the dust granule of filtered air.
Further, it has jack 23 to open on one side outer wall of protection frame 19, and protection frame 19 cup joints the outside at connecting rod 3 through jack 23, and it has the draw-in groove 24 that is the equidistance and distributes to open on the side inner wall of jack 23, and the welding has the fixture block 18 that is the equidistance and distributes on one side outer wall of connecting rod 3, and the inside at draw-in groove 24 of fixture block 18 joint, prevents that protection frame 19 from rotating.
Further, all open on the top outer wall of connecting rod 3 and on the bottom outer wall and be the fixed orifices 17 that the equidistance distributes, all weld on the bottom inner wall of last fixed cover 14 and on the top inner wall of fixed cover 15 down and become the fixed pin 16 that the equidistance distributes, and fixed pin 16 pegs graft in the inside of fixed orifices 17, and fixed pin 16 is interference fit with fixed orifices 17 for fixed cover 14 and fixed cover 15 down.
The working principle is as follows: during the use, operating personnel firstly fix the cover body 1 outside the frame through the bolt, then cup joint the protection frame 19 outside the connecting rod 3, make the inside of fixture block 18 joint in draw-in groove 24, cup joint the upper fixing sleeve 14 and the lower fixing sleeve 15 outside the connecting rod 3, make the locating pin 16 peg graft inside the fixed orifices 17, make the upper fixing sleeve 14 and the lower fixing sleeve 15 fix the protection frame 19, install unmanned aerial vehicle's power unit in the one end of connecting rod 3 again, install the antiskid ribbed tile 20 at the top outer wall and the bottom outer wall of protection frame 19 through the screw at last; when a collision occurs, the shield case 2 compresses the main spring 6 and the sub spring 9, so that the guide rod 5 moves inside the guide hole 13 and the buffer hole 11 to absorb the impact.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (7)
1. The utility model provides a novel aircraft bonnet of unmanned aerial vehicle, includes the cover body (1) and protecting crust (2), its characterized in that, it has constant head tank (7) to open on the top outer wall of the cover body (1), and opens on the bottom inner wall of constant head tank (7) has guiding hole (13), the welding of center department of protecting crust (2) bottom outer wall has guide bar (5), and guide bar (5) pegs graft in the inside of guiding hole (13), the welding has main spring (6) on the bottom outer wall of protecting crust (2), and main spring (6) cup joint in the outside of guide bar (5), the inside of one end joint at constant head tank (7) that protecting crust (2) were kept away from in main spring (6).
2. The novel hood for unmanned aerial vehicle as claimed in claim 1, wherein fixing grooves (8) are formed in the top outer portion of the hood body (1) and are distributed equidistantly, secondary springs (9) are welded on the bottom outer wall of the protective shell (2) and are distributed equidistantly, and one ends, far away from the protective shell (2), of the secondary springs (9) are clamped inside the fixing grooves (8).
3. The novel aircraft bonnet of unmanned aerial vehicle of claim 1, wherein the top inner wall of the cover body (1) is connected with a protection knob (10) in a threaded manner, the top outer wall of the protection knob (10) is provided with a buffer hole (11), the guide rod (5) is inserted into the buffer hole (11), and the bottom inner wall of the buffer hole (11) is bonded with a cushion pad (12).
4. The novel hood for unmanned aerial vehicle as claimed in claim 1, wherein connecting rods (3) are welded on the outer side wall of the hood body (1) and are distributed equidistantly, a protection mechanism (4) is sleeved outside the connecting rods (3), an upper fixing sleeve (14) and a lower fixing sleeve (15) are clamped on the outer side wall of the connecting rods (3), the outer wall of the same side of the upper fixing sleeve (14) and the outer wall of the same side of the lower fixing sleeve (15) are rotatably connected through a hinge, and the protection mechanism (4) is located between the outer wall of one side of the connecting rods (3) and the outer wall of one side of the upper fixing sleeve (14).
5. The novel hood for unmanned aerial vehicle as claimed in claim 4, wherein the protection mechanism (4) comprises a protection frame (19), protection plates (20) are mounted on the top outer wall and the bottom outer wall of the protection frame (19) through screws, air grooves (21) are formed in the top outer wall of the protection plate (20) and are distributed equidistantly, and a filter screen (22) is clamped inside the air grooves (21).
6. The novel aircraft bonnet of unmanned aerial vehicle of claim 5, wherein the protective frame (19) is provided with a jack (23) on the outer wall of one side, the protective frame (19) is sleeved outside the connecting rod (3) through the jack (23), the inner wall of the side surface of the jack (23) is provided with clamping grooves (24) distributed equidistantly, the outer wall of one side of the connecting rod (3) is welded with clamping blocks (18) distributed equidistantly, and the clamping blocks (18) are clamped inside the clamping grooves (24).
7. The novel hood for unmanned aerial vehicle as claimed in claim 4, wherein the top outer wall and the bottom outer wall of the connecting rod (3) are provided with fixing holes (17) distributed equidistantly, the bottom inner wall of the upper fixing sleeve (14) and the top inner wall of the lower fixing sleeve (15) are welded with fixing pins (16) distributed equidistantly, and the fixing pins (16) are inserted into the fixing holes (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022785148.4U CN213735505U (en) | 2020-11-26 | 2020-11-26 | Novel aircraft bonnet of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022785148.4U CN213735505U (en) | 2020-11-26 | 2020-11-26 | Novel aircraft bonnet of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213735505U true CN213735505U (en) | 2021-07-20 |
Family
ID=76830571
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022785148.4U Expired - Fee Related CN213735505U (en) | 2020-11-26 | 2020-11-26 | Novel aircraft bonnet of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213735505U (en) |
-
2020
- 2020-11-26 CN CN202022785148.4U patent/CN213735505U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210720 |