CN215554142U - Unmanned aerial vehicle flight stabilising arrangement - Google Patents
Unmanned aerial vehicle flight stabilising arrangement Download PDFInfo
- Publication number
- CN215554142U CN215554142U CN202122431772.9U CN202122431772U CN215554142U CN 215554142 U CN215554142 U CN 215554142U CN 202122431772 U CN202122431772 U CN 202122431772U CN 215554142 U CN215554142 U CN 215554142U
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- unmanned aerial
- aerial vehicle
- base
- fixed
- vehicle body
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- 230000003019 stabilising effect Effects 0.000 title claims abstract description 9
- 230000000087 stabilizing effect Effects 0.000 claims abstract description 25
- 230000006835 compression Effects 0.000 claims abstract description 19
- 238000007906 compression Methods 0.000 claims abstract description 19
- 238000000034 method Methods 0.000 abstract description 34
- 230000005484 gravity Effects 0.000 abstract description 5
- 230000003139 buffering effect Effects 0.000 abstract description 2
- 238000009434 installation Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle flight stabilizing device which comprises a base, wherein an unmanned aerial vehicle body is arranged at the top end of the base, lamp holders are respectively fixed at two ends of two sides of the bottom of the base, a reserved groove is formed in the top end of the base, and fixing pins are respectively vertically fixed at two sides of two ends of the base. This unmanned aerial vehicle flight stabilising arrangement installs when using on unmanned aerial vehicle through flight stabilising arrangement, at the in-process that unmanned aerial vehicle descends, the base bottom is provided with two sets of chassis, after the chassis contacts ground in the process of descending, the action of gravity of unmanned aerial vehicle body can push down the chassis, the limiting plate that the chassis top was fixed this moment can upwards promote second compression spring in the inside of spout, come to descend the inertia that the in-process falls to ground to the unmanned aerial vehicle body and cushion and offset, reduce the damage of the equipment of the hard contact between when the unmanned aerial vehicle body descends and the ground, the problem of being not convenient for carry out the buffering at unmanned aerial vehicle descending in-process has been solved.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a flight stabilizing device of an unmanned aerial vehicle.
Background
Unmanned aerial vehicle is an unmanned aerial vehicle who utilizes radio remote control equipment to control operation, can divide into some military and civilian fields, wherein some civilian unmanned aerial vehicle need use the flight stabilising arrangement at the in-process of flight and reduce the danger such as the turn on one's side of unmanned aerial vehicle flight in-process, but some unmanned aerial vehicle flight stabilising arrangement that have now still exist some not enoughly at the in-process that uses, for example, be not convenient for buffer at unmanned aerial vehicle landing in-process, there is not one kind simultaneously and be convenient for install fixed measure between device and the unmanned aerial vehicle, and also there is not one kind and be convenient for carry out safety warning's measure at the in-process that unmanned aerial vehicle flies.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a flight stabilizing device of an unmanned aerial vehicle, which aims to solve the problem that the unmanned aerial vehicle is inconvenient to buffer in the landing process in the background technology.
In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides an unmanned aerial vehicle flight stabilising arrangement, includes the base, the top of base is provided with the unmanned aerial vehicle body, the both ends of base bottom both sides are fixed with the lamp stand respectively, the inside on base top is provided with the reservation groove, the both sides at base both ends are vertical fixed with fixed foot respectively, the bottom mounting of base has the end cover, the inside intermediate position department of end cover is provided with the steady piece, the inside both ends of end cover and both sides are fixed with first compression spring respectively, fixed connection between one side of first compression spring and the outside of steady piece.
Preferably, the inside of fixed foot is vertically provided with the spout, the inside bottom mounting of spout has the inner tube, the both sides of base bottom are provided with the chassis respectively, the inside top vertical mounting of spout has the second compression spring, the top of chassis runs through the inside of inner tube and is fixed with the limiting plate.
Preferably, the bottom end of the second compression spring is fixedly connected with the top end of the limiting plate, the outer diameter of the limiting plate is smaller than the inner diameter of the sliding chute, and the outer diameter of the limiting plate is larger than the outer diameter of the inner barrel.
Preferably, the inside at base top both ends transversely is provided with the draw-in groove respectively, the both ends of unmanned aerial vehicle body bottom transversely are fixed with the card strip respectively.
Preferably, the inside of base both sides intermediate position department is provided with respectively reserves the battery compartment, the inside of reserving the battery compartment is provided with the battery, the top of lamp stand is fixed with the warning light.
Preferably, the lamp holder and the battery are respectively arranged symmetrically with respect to a vertical center line of the base.
Compared with the prior art, the utility model has the beneficial effects that: the unmanned aerial vehicle flight stabilizing device not only realizes the convenience of buffering in the landing process of the unmanned aerial vehicle, realizes the convenience of mounting and fixing the device and the unmanned aerial vehicle, but also realizes the convenience of safety warning in the flying process of the unmanned aerial vehicle;
(1) by arranging the fixing legs, the second compression springs, the sliding groove, the limiting plates, the inner barrel and the underframe, when the flight stabilizing device is installed on an unmanned aerial vehicle for use, in the landing process of the unmanned aerial vehicle, the two groups of underframe are arranged at the bottom end of the base, after the underframe contacts the ground in the landing process, the underframe can be pressed downwards under the action of gravity of the unmanned aerial vehicle body, at the moment, the limiting plates fixed at the top end of the underframe can upwards push the second compression springs in the sliding groove to buffer and offset the inertia falling to the ground in the landing process of the unmanned aerial vehicle body, and the damage to equipment caused by hard contact between the unmanned aerial vehicle body and the ground when the unmanned aerial vehicle body lands is reduced;
(2) by arranging the reserved groove, the clamping strips and the clamping grooves, in the process of connecting and installing the flight stabilizing device and the unmanned aerial vehicle body, the unmanned aerial vehicle body can slide into the clamping grooves from one sides of the two groups of clamping grooves in the base by utilizing the two groups of clamping strips arranged at the two ends of the bottom, and the clamping strips and the clamping grooves are connected and fixed, so that the unmanned aerial vehicle body and the stabilizing device can be conveniently installed and detached;
(3) through being provided with the lamp stand, reserve battery compartment, battery and warning light, unmanned aerial vehicle is at the in-process that light is not good or uses under the dark condition, can be through with the battery after the installation again get into the inside of reserving battery compartment, provide the electric quantity by the battery for the warning light and light, come to carry out outside warning and discernment to the in-process of unmanned aerial vehicle flight, improve the security of unmanned aerial vehicle use.
Drawings
FIG. 1 is a schematic front sectional view of the present invention;
FIG. 2 is an enlarged partial cross-sectional view taken at A in FIG. 1 according to the present invention;
FIG. 3 is an enlarged side view of a card slot of the present invention;
fig. 4 is an enlarged partial sectional view of the warning light according to the present invention.
In the figure: 1. a base; 2. a lamp socket; 3. an unmanned aerial vehicle body; 4. reserving a groove; 5. a fixing leg; 6. a first compression spring; 7. a stabilizing block; 8. a bottom cover; 9. a second compression spring; 10. a chute; 11. a limiting plate; 12. an inner barrel; 13. a chassis; 14. clamping the strip; 15. a card slot; 16. reserving a battery compartment; 17. a storage battery; 18. a warning light.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Example 1: referring to fig. 1-4, an unmanned aerial vehicle flight stabilizing device comprises a base 1, wherein an unmanned aerial vehicle body 3 is arranged at the top end of the base 1, lamp holders 2 are respectively fixed at two ends of two sides of the bottom of the base 1, a reserved groove 4 is arranged inside the top end of the base 1, fixing pins 5 are respectively vertically fixed at two sides of two ends of the base 1, a bottom cover 8 is fixed at the bottom end of the base 1, a stabilizing block 7 is arranged at the middle position inside the bottom cover 8, first compression springs 6 are respectively fixed at two ends and two sides inside the bottom cover 8, and one side of each first compression spring 6 is fixedly connected with the outside of the stabilizing block 7;
a sliding chute 10 is vertically arranged in the fixed foot 5, an inner cylinder 12 is fixed at the bottom end in the sliding chute 10, two sides of the bottom end of the base 1 are respectively provided with an underframe 13, a second compression spring 9 is vertically fixed at the top end in the sliding chute 10, the top end of the underframe 13 penetrates through the inner cylinder 12 and is fixed with a limiting plate 11, the bottom end of the second compression spring 9 is fixedly connected with the top end of the limiting plate 11, the outer diameter of the limiting plate 11 is smaller than the inner diameter of the sliding chute 10, and the outer diameter of the limiting plate 11 is larger than the outer diameter of the inner cylinder 12;
specifically, as shown in fig. 1 and fig. 2, when the flight stabilising arrangement was installed and is used on unmanned aerial vehicle, at the in-process that unmanned aerial vehicle descended, 1 bottom of base is provided with two sets of chassis 13, after descending in-process chassis 13 contacts ground, unmanned aerial vehicle body 3's action of gravity can push down chassis 13, chassis 13 fixed limiting plate 11 in top this moment can upwards promote second compression spring 9 in the inside of spout 10, come to descend 3 in-process to the inertia on ground of landing to cushion and offset, reduce the damage of unmanned aerial vehicle body 3 when descending and the hard contact between the ground to equipment.
Example 2: clamping grooves 15 are respectively and transversely formed in the two ends of the top of the base 1, and clamping strips 14 are respectively and transversely fixed at the two ends of the bottom of the unmanned aerial vehicle body 3;
specifically, as shown in fig. 1 and 3, in the process of installing being connected between stabilizing device and the unmanned aerial vehicle body 3 will fly, can slide into from one side of two sets of draw-in grooves 15 of base 1 inside and go into the inside of going into draw-in groove 15 through utilizing two sets of card strips 14 that bottom both ends set up with unmanned aerial vehicle body 3, will block and be connected fixedly between strip 14 and the draw-in groove 15, be convenient for to installation and dismantlement between unmanned aerial vehicle body 3 and the stabilizing device.
Example 3: reserved battery bins 16 are respectively arranged in the middle positions of two sides of the base 1, a storage battery 17 is arranged in each reserved battery bin 16, a warning lamp 18 is fixed at the top end of the lamp holder 2, and the lamp holder 2 and the storage battery 17 are respectively symmetrically arranged about the vertical center line of the base 1;
specifically, as shown in fig. 1 and 4, unmanned aerial vehicle is at the in-process that light is not good or use under the dark condition, can be through the inside of installing again after charging battery 17 and getting into reserve battery compartment 16, light for warning light 18 provides the electric quantity by battery 17, carries out outside warning and discernment to the in-process of unmanned aerial vehicle flight, improves the security in the unmanned aerial vehicle use.
The working principle is as follows: when the unmanned aerial vehicle is used, in the process of connecting and installing the flight stabilizing device and the unmanned aerial vehicle body 3, the unmanned aerial vehicle body 3 can slide into and be clamped into the clamping grooves 15 from one side of the two groups of clamping grooves 15 in the base 1 by utilizing the two groups of clamping strips 14 arranged at the two ends of the bottom part, the clamping strips 14 and the clamping grooves 15 are connected and fixed, the unmanned aerial vehicle body 3 and the stabilizing device are convenient to install and disassemble, when the unmanned aerial vehicle body 3 encounters different wind speeds and wind directions in the flight process, the stabilizing block 7 arranged in the bottom cover 8 can move to a corresponding position according to the position of the unmanned aerial vehicle body 3, the stabilizing block 7 can move leftwards and rightwards in the bottom cover 8 according to the change of the wind speeds and the wind directions, so that the gravity center of the unmanned aerial vehicle body 3 in the flight process is constantly kept at an optimal position, and the stability of the unmanned aerial vehicle body 3 in the flight process is improved, meanwhile, when the flight stabilizing device is installed on an unmanned aerial vehicle for use, in the process of landing of the unmanned aerial vehicle, two groups of underframe 13 are arranged at the bottom end of the base 1, after the underframe 13 is in contact with the ground in the landing process, the underframe 13 is pressed downwards under the action of gravity of the unmanned aerial vehicle body 3, at the moment, the limiting plate 11 fixed at the top end of the underframe 13 pushes the second compression spring 9 upwards in the sliding chute 10 to buffer and offset the inertia falling to the ground in the landing process of the unmanned aerial vehicle body 3, the damage to equipment caused by hard contact between the unmanned aerial vehicle body 3 and the ground in the landing process is reduced, in the process of using the unmanned aerial vehicle under the condition of poor light or darkness, the unmanned aerial vehicle can be installed into the reserved battery bin 16 after the storage battery 17 is charged, the storage battery 17 provides electric quantity for the warning lamp 18 to light, so as to perform external warning and identification in the process of flying the unmanned aerial vehicle, improve the security in the unmanned aerial vehicle use.
It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (6)
1. The utility model provides an unmanned aerial vehicle flight stabilising arrangement, includes base (1), its characterized in that: the top of base (1) is provided with unmanned aerial vehicle body (3), the both ends at base (1) bottom both sides are fixed with lamp stand (2) respectively, the inside on base (1) top is provided with reservation groove (4), the both sides at base (1) both ends are vertical fixed with fixed foot (5) respectively, the bottom mounting of base (1) has end cover (8), the inside intermediate position department of end cover (8) is provided with stabilizing block (7), the inside both ends of end cover (8) and both sides are fixed with first compression spring (6) respectively, fixed connection between one side of first compression spring (6) and the outside of stabilizing block (7).
2. The unmanned aerial vehicle flight stabilizing device of claim 1, wherein: the inside of fixed foot (5) is vertical to be provided with spout (10), the inside bottom mounting of spout (10) has inner tube (12), the both sides of base (1) bottom are provided with chassis (13) respectively, the inside top vertical fixation of spout (10) has second compression spring (9), the top of chassis (13) runs through the inside of inner tube (12) and is fixed with limiting plate (11).
3. The unmanned aerial vehicle flight stabilizing device of claim 2, wherein: the bottom end of the second compression spring (9) is fixedly connected with the top end of the limiting plate (11), the outer diameter of the limiting plate (11) is smaller than the inner diameter of the sliding groove (10), and the outer diameter of the limiting plate (11) is larger than the outer diameter of the inner cylinder (12).
4. The unmanned aerial vehicle flight stabilizing device of claim 1, wherein: the inside at base (1) top both ends transversely is provided with draw-in groove (15) respectively, the both ends of unmanned aerial vehicle body (3) bottom transversely are fixed with card strip (14) respectively.
5. The unmanned aerial vehicle flight stabilizing device of claim 1, wherein: the inside of base (1) both sides intermediate position department is provided with respectively reserves battery compartment (16), the inside of reserving battery compartment (16) is provided with battery (17), the top of lamp stand (2) is fixed with warning light (18).
6. The unmanned aerial vehicle flight stabilizing device of claim 1, wherein: the lamp holder (2) and the storage battery (17) are respectively arranged symmetrically relative to the vertical center line of the base (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122431772.9U CN215554142U (en) | 2021-10-10 | 2021-10-10 | Unmanned aerial vehicle flight stabilising arrangement |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122431772.9U CN215554142U (en) | 2021-10-10 | 2021-10-10 | Unmanned aerial vehicle flight stabilising arrangement |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215554142U true CN215554142U (en) | 2022-01-18 |
Family
ID=79853341
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122431772.9U Expired - Fee Related CN215554142U (en) | 2021-10-10 | 2021-10-10 | Unmanned aerial vehicle flight stabilising arrangement |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215554142U (en) |
-
2021
- 2021-10-10 CN CN202122431772.9U patent/CN215554142U/en not_active Expired - Fee Related
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| 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: 20220118 |
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| CF01 | Termination of patent right due to non-payment of annual fee |