CN210258816U - Unmanned aerial vehicle damping mechanism that rises and falls - Google Patents
Unmanned aerial vehicle damping mechanism that rises and falls Download PDFInfo
- Publication number
- CN210258816U CN210258816U CN201921105200.8U CN201921105200U CN210258816U CN 210258816 U CN210258816 U CN 210258816U CN 201921105200 U CN201921105200 U CN 201921105200U CN 210258816 U CN210258816 U CN 210258816U
- Authority
- CN
- China
- Prior art keywords
- base
- unmanned aerial
- aerial vehicle
- pole
- organism
- Prior art date
- 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
- 238000013016 damping Methods 0.000 title claims abstract description 12
- 230000003139 buffering effect Effects 0.000 claims description 22
- 230000006835 compression Effects 0.000 claims description 3
- 238000007906 compression Methods 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 13
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 4
- 230000003014 reinforcing effect Effects 0.000 abstract description 3
- 238000010276 construction Methods 0.000 abstract 1
- 239000006185 dispersion Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
Images
Landscapes
- Vibration Dampers (AREA)
Abstract
The utility model provides an unmanned aerial vehicle damping mechanism that rises and falls belongs to tunnel construction technical field, including organism and wing, the bottom fixed surface of organism is connected with the regulation pole, adjusts the pole and is provided with the junction embedding of organism and connects the cross axle, and the bottom of adjusting the pole sets up the base, and the base is sliding connection with adjusting the pole, and the inboard embedding of base is provided with embedded connecting rod, and embedded connecting rod sets up to cup jointing the telescopic link, and the bottom surface of base evenly imbeds and is provided with the bottom block. The utility model discloses a setting up to scalable regulation pole, being convenient for drive the base and carrying out the lift adjustment, when unmanned aerial vehicle descended, the cooperation leaned out the regulation pole that sets up, and the area of contact on extension base and ground reaches the stability when reinforcing unmanned aerial vehicle descended, and the angle department is the tilt up arcuation setting simultaneously, the effectual effect that plays the water conservancy diversion when unmanned aerial vehicle flies.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, more specifically relates to a damping mechanism technical field.
Background
Unmanned aerial vehicles can be classified into military and civil according to application fields. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, self-shooting, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
Current unmanned aerial vehicle undercarriage security is poor in the use, when unmanned aerial vehicle descending in-process, because the weight of self is great impact force occasionally at the landing, make the unmanned aerial vehicle organism take place to empty easily, and then make wing or organism impaired, be unfavorable for the problem of unmanned aerial vehicle safety landing, the undercarriage simultaneously, reduce unmanned aerial vehicle absorbing effect, the degree of difficulty undercarriage that has also increased and has carried makes unmanned aerial vehicle flight inconvenient longer easily, make unmanned aerial vehicle damage when flying in narrow and small space easily, airflow resistance when great undercarriage increases the flight easily, unmanned aerial vehicle stable flight is not convenient for.
SUMMERY OF THE UTILITY MODEL
The utility model discloses aim at solving current most unmanned aerial vehicle undercarriage, reduce unmanned aerial vehicle absorbing effect, also increased the degree of difficulty undercarriage that carries simultaneously and longer make unmanned aerial vehicle flight inconvenient easily, make unmanned aerial vehicle damage easily when flying in narrow and small space, airflow resistance when great undercarriage increases the flight easily, the problem of unmanned aerial vehicle stable flight of not being convenient for.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle damping mechanism that rises and falls, including organism and wing, the rotatory embedding of wing is on the top of organism, the bottom fixed surface of organism is connected with the regulation pole, the embedding of the junction of adjusting pole and organism is provided with the connection cross axle, the bottom of adjusting the pole sets up the base, the base is sliding connection with adjusting the pole, the inboard embedding of base is provided with embedded connecting rod, embedded connecting rod sets up to cup jointing the telescopic link, the even embedding in bottom surface of base is provided with the bottom block, in the protruding half embedding base of bottom block, the one end fixedly connected with buffering frame in the bottom block embedding base, the fixed surface of buffering frame is connected.
Further preferred embodiments: adjust the pole along the bottom four corners setting of organism, and adjust the pole and set up to straight cylinder telescopic link, adjust two and be a set of, be and lean out the setting.
Further preferred embodiments: the base is provided with two, is located the bottom both sides of organism, and the base is surperficial curved trapezoidal of falling.
Further preferred embodiments: the base is of a two-section splicing type, and the guide angle at the bottom end of the base is in an upward inclined arc shape.
Further preferred embodiments: the buffer frame is of a cross structure, and a cross shaft is embedded in the cross position.
Further preferred embodiments: the quantity that sets up of buffering post sets up according to the quantity of buffering frame, and the three is a set of, and every buffering post is located between the buffering frame main part both ends and sets up with the bottom, and the buffering post sets up to the compression spring post.
Has the advantages that:
1. the utility model discloses a for curved inverted trapezoid base in surface, when unmanned aerial vehicle descends, the cooperation leans out the regulation pole that sets up, and the area of contact on extension base and ground reaches stability when reinforcing unmanned aerial vehicle descends, and the bottom lead angle department is the tilt up arcuation setting simultaneously, the effectual effect that plays the water conservancy diversion when unmanned aerial vehicle flies, and the setting of two sections concatenation formulas is convenient for make the base shrink and adjust.
2. Secondly, reach the effect that reaches the support when the bottom block receives external force through the buffering frame, the setting of activity crossing simultaneously, main part reaction deformation when receiving external force reaches the effect of buffering.
3. Moreover, through the buffering post, when the buffering frame received external force and produced deformation, cushion the dispersion to the external force of its main part, reach absorbing effect.
Drawings
Fig. 1 is a plan view of the whole front structure of the present invention.
Fig. 2 is a plan view of the base of the present invention in the retracted state.
Fig. 3 is a top view of the main structure of the present invention.
Fig. 4 is a sectional view of the bottom block connecting structure of the present invention.
In FIGS. 1-4: 1-machine body, 2-wing, 3-connecting cross shaft, 4-adjusting rod, 5-base, 6-embedded connecting rod, 7-buffer frame, 8-buffer column and 9-bottom block.
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.
Please refer to fig. 1 to 4, in the embodiment of the utility model, an unmanned aerial vehicle damping mechanism that rises and falls, including organism 1 and wing 2, the rotatory embedding of wing 2 is on the top of organism 1, the bottom fixed surface of organism 1 is connected with adjusts pole 4, it is provided with and is connected cross axle 3 to adjust the embedding of pole 4 and the junction of organism 1, the bottom of adjusting pole 4 sets up base 5, base 5 is sliding connection with adjusting pole 4, the inboard embedding of base 5 is provided with embedded connecting rod 6, embedded connecting rod 6 sets up to cup jointing the telescopic link, the even embedding in bottom surface of base 5 is provided with bottom block 9, bottom block 9 protrudes in half embedding base 5, the one end fixedly connected with cushion frame 7 in bottom block 9 embedding base 5, the fixed surface of cushion frame 7 is connected with cushion column 8.
Wherein, adjust pole 4 along organism 1's bottom four corners setting, and adjust pole 4 and set up to straight cylinder telescopic link, adjust pole 4 two and be a set of, be and lean out the setting, through setting up to scalable regulation pole 4, be convenient for drive base 5 and carry out the lift adjustment.
Wherein, base 5 is provided with two, is located the bottom both sides of organism 1, and base 5 is surperficial curved trapezoidal of falling.
Wherein, base 5 is two sections concatenation formulas, and the bottom lead angle department of base 5 is the tilt up arcuation setting, through for surperficial curved inverted trapezoid base 5, when unmanned aerial vehicle descends, the cooperation leans out the regulation pole that sets up, the area of contact on extension base 5 and ground, reach the stability when reinforcing unmanned aerial vehicle descends, bottom lead angle department is the tilt up arcuation setting simultaneously, the effectual effect that plays the water conservancy diversion when unmanned aerial vehicle flies, and the setting of two sections concatenation formulas is convenient for make base 5 shrink and adjust.
Wherein, the buffer frame 7 is arranged into a cross structure, the cross part is embedded into the cross shaft, the effect of supporting when the bottom block 9 receives external force is achieved through the buffer frame 7, meanwhile, the main body is deformed in a reaction mode when external force is received through the movable cross arrangement, and the effect of buffering is achieved.
Wherein, the quantity that sets up of buffering post 8 sets up according to the quantity of buffering frame 7, and three be a set of, every buffering post 8 is located between 7 main part both ends of buffering frame and sets up with the bottom, and buffering post 8 sets up to the compression spring post, through buffering post 8, when buffering frame 7 receives external force and produces deformation, cushions the dispersion to the external force of its main part, reaches absorbing effect.
Use the utility model relates to an unmanned aerial vehicle damping mechanism that rises and falls, at first, when unmanned aerial vehicle descends, the external force that base 5 received conducts to buffer frame 7 on through the bottom 9 of bottom embedding, buffer frame 7 receives the inside shrink of external force, it cushions to be located 8 dispersed external forces of buffer column wherein simultaneously, reduce the vibrations that organism 1 received, when unmanned aerial vehicle takes off, adjust pole 4 and stretch out and draw back, drive base 5 upwards packs up to organism 1's bottom, and the arc surface in the base 5 outside and the trapezoidal setting of falling, the effectual air water conservancy diversion that carries on, make organism 1 be in stable state.
The above is only the preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, without departing from the concept of the present invention, several modifications and improvements can be made, which should also be regarded as the protection scope of the present invention, and these will not affect the effect of the implementation of the present invention and the practicability of the patent.
Claims (6)
1. The utility model provides an unmanned aerial vehicle damping mechanism that rises and falls, includes organism (1) and wing (2), the rotatory top of embedding at organism (1) of wing (2), its characterized in that: the utility model discloses a telescopic rod, including organism (1), bottom fixed surface is connected with regulation pole (4), the junction embedding of adjusting pole (4) and organism (1) is provided with and connects cross axle (3), the bottom of adjusting pole (4) sets up base (5), base (5) are sliding connection with adjusting pole (4), the inboard embedding of base (5) is provided with embedded connecting rod (6), embedded connecting rod (6) set up to cup joint the telescopic link, the even embedding in bottom surface of base (5) is provided with bottom block (9), bottom block (9) salient half imbeds in base (5), the one end fixedly connected with buffering frame (7) in bottom block (9) embedding base (5), the fixed surface of buffering frame (7) is connected with buffering post (8).
2. The unmanned aerial vehicle landing gear damping mechanism of claim 1, wherein: adjust pole (4) along the bottom four corners setting of organism (1), and adjust pole (4) and set up to straight cylinder telescopic link, adjust pole (4) two and be a set of, be and lean out the setting.
3. The unmanned aerial vehicle landing gear damping mechanism of claim 1, wherein: the two bases (5) are located on two sides of the bottom end of the machine body (1), and the bases (5) are in an inverted trapezoid shape with an arc-shaped surface.
4. An unmanned aerial vehicle landing gear according to any of claims 1 or 3, wherein: the base (5) is of a two-section splicing type, and the bottom end guide angle of the base (5) is arranged in an upwards inclined arc shape.
5. The unmanned aerial vehicle landing gear damping mechanism of claim 1, wherein: the buffer frame (7) is arranged into a cross structure, and a cross shaft is embedded in the cross position.
6. The unmanned aerial vehicle landing gear damping mechanism of claim 1, wherein: the number of the buffer columns (8) is set according to the number of the buffer frames (7), the three buffer columns are in a group, each buffer column (8) is located between two ends of the main body of each buffer frame (7) and is arranged at the bottom of the main body, and the buffer columns (8) are set to be compression spring columns.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921105200.8U CN210258816U (en) | 2019-07-15 | 2019-07-15 | Unmanned aerial vehicle damping mechanism that rises and falls |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921105200.8U CN210258816U (en) | 2019-07-15 | 2019-07-15 | Unmanned aerial vehicle damping mechanism that rises and falls |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210258816U true CN210258816U (en) | 2020-04-07 |
Family
ID=70012568
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921105200.8U Expired - Fee Related CN210258816U (en) | 2019-07-15 | 2019-07-15 | Unmanned aerial vehicle damping mechanism that rises and falls |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210258816U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114455074A (en) * | 2022-04-13 | 2022-05-10 | 徐州飞梦电子科技有限公司 | High-stability multifunctional rescue unmanned aerial vehicle |
-
2019
- 2019-07-15 CN CN201921105200.8U patent/CN210258816U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114455074A (en) * | 2022-04-13 | 2022-05-10 | 徐州飞梦电子科技有限公司 | High-stability multifunctional rescue unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN111301665A (en) | Landing auxiliary balancing device for unmanned aerial vehicle | |
| CN211196666U (en) | Cargo-carrying unmanned aerial vehicle take-off and landing platform | |
| CN210258816U (en) | Unmanned aerial vehicle damping mechanism that rises and falls | |
| CN110683038A (en) | Combined type unmanned aerial vehicle vibration damping mount | |
| CN212290333U (en) | Unmanned aerial vehicle protection device | |
| CN211766288U (en) | Vertical forced landing protection device for unmanned aerial vehicle | |
| CN113335505A (en) | Combined type unmanned aerial vehicle vibration damping mount and have its unmanned aerial vehicle | |
| CN108275261A (en) | A kind of collapsible unmanned plane undercarriage | |
| CN215972143U (en) | Environmental detection is with unmanned aerial vehicle that barrier propterty is good | |
| CN213200087U (en) | Carbon fiber unmanned machine shell | |
| CN212448092U (en) | A unmanned aerial vehicle for dam body patrols | |
| CN212685899U (en) | Multifunctional landing support for surveying and mapping unmanned aerial vehicle landing | |
| CN213384685U (en) | Unmanned aerial vehicle with descending shock-absorbing function | |
| CN211568293U (en) | Adjustable shock-absorbing support for unmanned aerial vehicle | |
| CN211468760U (en) | A undercarriage for unmanned aerial vehicle | |
| CN210852979U (en) | Unmanned aerial vehicle parking support for surveying and mapping | |
| CN210310880U (en) | Unmanned aerial vehicle topography survey device | |
| CN210503161U (en) | A undercarriage and protective structure for unmanned aerial vehicle | |
| CN220448179U (en) | Surveying and mapping unmanned aerial vehicle with RTK | |
| CN215323262U (en) | Unmanned aerial vehicle undercarriage | |
| CN215399359U (en) | Unmanned aerial vehicle is used in survey and drawing with protection device | |
| CN210503171U (en) | Unmanned aerial vehicle with slowly fall device | |
| CN211996122U (en) | Unmanned aerial vehicle that satisfies airworthiness requirement is with frame shock-absorbing structure that plays | |
| CN213473503U (en) | Effectual unmanned aerial vehicle of descending shock attenuation | |
| CN112278244B (en) | Unmanned aerial vehicle falling foot stand capable of increasing sliding resistance |
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: 20200407 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |