CN105923142A - Unmanned aerial vehicle waterproof structure - Google Patents
Unmanned aerial vehicle waterproof structure Download PDFInfo
- Publication number
- CN105923142A CN105923142A CN201610317409.5A CN201610317409A CN105923142A CN 105923142 A CN105923142 A CN 105923142A CN 201610317409 A CN201610317409 A CN 201610317409A CN 105923142 A CN105923142 A CN 105923142A
- Authority
- CN
- China
- Prior art keywords
- upper cover
- lower cover
- cover
- screw
- silica gel
- 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.)
- Pending
Links
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical group O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims abstract description 18
- 239000000741 silica gel Substances 0.000 claims abstract description 13
- 229910002027 silica gel Inorganic materials 0.000 claims abstract description 13
- 238000010276 construction Methods 0.000 claims description 9
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 7
- 229910052710 silicon Inorganic materials 0.000 claims description 7
- 239000010703 silicon Substances 0.000 claims description 7
- 230000000694 effects Effects 0.000 claims description 4
- 238000007789 sealing Methods 0.000 abstract description 6
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 238000004078 waterproofing Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B43/00—Washers or equivalent devices; Other devices for supporting bolt-heads or nuts
- F16B43/001—Washers or equivalent devices; Other devices for supporting bolt-heads or nuts for sealing or insulation
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Building Environments (AREA)
Abstract
The invention provides an unmanned aerial vehicle waterproof structure. The unmanned aerial vehicle waterproof structure comprises an upper cover and a lower cover, and the lower cover and the upper cover are buckled together and are fixed through screws. A groove is formed in the lower cover along an edge combination part of the lower cover. A sealing silica gel ring is arranged in the groove. A protruding block is arranged on the upper cover along an edge combination part of the upper cover. When the upper cover and the lower cover are fixed together, the protruding block is tightly pressed on the sealing silica gel ring, so that moisture is prevented from entering an unmanned aerial vehicle, and the waterproof function is achieved. By arranging the sealing silica gel ring between the upper cover and the lower cover of the unmanned aerial vehicle, moisture can be prevented from entering the unmanned aerial vehicle through a gap between the combination part of the upper cover and the combination part of the lower cover; and meanwhile, by combining the screw for fixation and added silica gel gaskets, the unmanned aerial vehicle reaches higher waterproof grade.
Description
Technical field
The present invention relates to unmanned vehicle, particularly relate to a kind of unmanned plane waterproof construction.
Background technology
Unmanned air vehicle technique is fast-developing, and the range of application of unmanned plane is more extensive, has in the market
Part has waterproof unmanned plane, but this part unmanned plane is typically only limited to protection against the tide, and waterproof rank is inadequate,
Can not flight near sea level.
Summary of the invention
The technical problem to be solved in the present invention is: provide a kind of unmanned plane waterproof construction with water-proof function.
For achieving the above object, a kind of unmanned plane waterproof construction that the present invention provides, including upper cover and with described
The lower cover that upper cover snaps together and is screwed, described lower cover is being provided with recessed along its edge juncture
Groove, is provided with sealed silicon cushion rubber in described groove；Described upper cover is being provided with projection along its edge juncture；
When described upper cover is fixed together with described lower cover, described projection is pressed on described sealed silicon cushion rubber, from
And prevent moisture from entering and play waterproof effect.
Further, cover on described and be provided with multiple screw column for installing screw, in described screw column
Being provided with silica gel pad, described screw passes described silica gel pad；Cover under described be provided with multiple for solid
Determine the Nut column of screw；After described upper cover is fixing with described lower cover, described silica gel pad is pressed on described nut
On the upper surface of post, thus prevent moisture from entering from Nut column or screw column.
The unmanned plane of the present invention by arrange between upper cover and lower cover sealed silicon cushion rubber be possible to prevent moisture from
Enter inside unmanned plane at upper cover and the gap of described lower cover joint portion；In combination with the fixed form to screw
Increase silica gel pad, make this unmanned plane reach higher waterproof rank, it is possible to ensure that moisture will not enter nothing
Man-machine inside.Expanded the scope of application by the unmanned plane of the waterproof present invention, can fly near sea level
OK.
Accompanying drawing explanation
Below in conjunction with the accompanying drawings, by the detailed description of the invention of the present invention is described in detail, the skill of the present invention will be made
Art scheme and other beneficial effect are apparent.
In accompanying drawing,
Fig. 1 is unmanned plane waterproof construction entirety exploded perspective view of the present invention；
Fig. 2 is upper cover of the present invention and lower cap fixing structure schematic diagram；
Fig. 3 is screw fixed structure schematic diagram of the present invention.
Drawing reference numeral illustrates:
100, upper cover；11, projection；200, lower cover；21, groove；300, sealed silicon cushion rubber；400、
Screw column；500, Nut column；600, silica gel pad；700, screw.
Detailed description of the invention
By further illustrating the technological means and effect thereof that the present invention taked, below in conjunction with the present invention's
Preferred embodiment and accompanying drawing thereof are described in detail.
Referring to Fig. 1, the unmanned plane waterproof construction that the present invention provides includes: upper cover 100, lower cover 200, edge
Upper cover 100 or lower cover 200 edge are fixed on the sealed silicon cushion rubber 300 within upper cover 100 or lower cover 200, and this is close
Envelope silica gel ring 300 is after described upper cover 100 is fixing with described lower cover 200, it is possible to prevent moisture from entering described nothing
Man-machine.
As in figure 2 it is shown, concrete, described lower cover 200 is being provided with groove 21 along edge juncture, described close
Envelope silica gel ring 300 is arranged in described groove 21；Described upper cover 100 is provided with projection 11 along edge juncture；
After described upper cover 100 is fixed together with described lower cover 200, described projection 11 is pressed on described sealing silica gel
On circle 300, thus play waterproof effect.
In the present embodiment, described groove 21 is corresponding with the position of described projection 11, described projection 11
The guarantee that is sized to be contained in shown groove 21.Utilize the structure that the present invention is above-mentioned, by increasing capacitance it is possible to increase described
Upper cover 100 and the sealing property of described lower cover 200, improve fire resistance characteristic.
Such as Fig. 3, further, described upper cover 100 is provided with multiple screw column 400 for installing screw,
Being provided with silica gel pad 600 in described screw column 400, described screw 700 is fixed through described silica gel pad 600
In the Nut column 500 being positioned at described lower cover 200 correspondence position；Fix with described lower cover 200 at described upper cover 100
After, described silica gel pad 600 is pressed on the upper surface of described Nut column 500, thus prevents moisture from nut
Post 500 or screw column 400 enter inside unmanned plane.
In the present embodiment, the fixed form of screw 700 has been done water-proofing treatment, has further improve
The water resistance that nobody connects.
The unmanned plane waterproof construction of the present invention, respectively fixing, screw 700 from upper cover 100 and lower cover 200
Sealing has carried out waterproofing design, so that this unmanned plane has extremely strong water resistance.
The above, for the person of ordinary skill of the art, can be according to technical scheme
Make other various corresponding changes and deformation with technology design, and all these change and deformation all should belong to
The protection domain of the claims in the present invention.
Claims (2)
1. a unmanned plane waterproof construction, including upper cover and snap together with described upper cover and pass through screw
Fixing lower cover, it is characterised in that described lower cover is being provided with groove along its edge juncture, described recessed
Sealed silicon cushion rubber it is provided with in groove；Described upper cover is being provided with projection along its edge juncture；When described upper cover
When being fixed together with described lower cover, described projection is pressed on described sealed silicon cushion rubber, thus prevents moisture
Enter and play waterproof effect.
Unmanned plane waterproof construction the most according to claim 1, it is characterised in that cover setting on described
Having multiple screw column for installing screw, be provided with silica gel pad in described screw column, described screw passes
Described silica gel pad；Cover under described and be provided with multiple Nut column for fixed screw；Described upper cover and institute
State lower cover fixing after, described silica gel pad is pressed on the upper surface of described Nut column, thus prevent moisture from
Nut column or screw column enter.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610317409.5A CN105923142A (en) | 2016-05-13 | 2016-05-13 | Unmanned aerial vehicle waterproof structure |
| US15/264,600 US20170327220A1 (en) | 2016-05-13 | 2016-09-14 | Waterproof unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610317409.5A CN105923142A (en) | 2016-05-13 | 2016-05-13 | Unmanned aerial vehicle waterproof structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105923142A true CN105923142A (en) | 2016-09-07 |
Family
ID=56835946
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610317409.5A Pending CN105923142A (en) | 2016-05-13 | 2016-05-13 | Unmanned aerial vehicle waterproof structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105923142A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110116798A (en) * | 2019-05-20 | 2019-08-13 | 苏州臻迪智能科技有限公司 | A kind of unmanned thermomechanical components and unmanned plane |
| CN110356576A (en) * | 2019-07-30 | 2019-10-22 | 南京精微迅智能科技有限公司 | A kind of unmanned machine head waterproof construction and waterproof method |
| CN111090287A (en) * | 2018-10-23 | 2020-05-01 | 深圳市斯威普科技有限公司 | Remote control for controlling an aircraft |
| CN111361752A (en) * | 2017-12-29 | 2020-07-03 | 深圳市大疆创新科技有限公司 | Driving device, cloud platform, shooting device and unmanned vehicles |
| WO2021016816A1 (en) * | 2019-07-29 | 2021-02-04 | 深圳市大疆创新科技有限公司 | Photographing apparatus, gimbal device, and unmanned aerial vehicle |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201627812U (en) * | 2009-11-23 | 2010-11-10 | 平高集团有限公司 | Combination gasket and bolt sealing structure |
| US20130256464A1 (en) * | 2010-06-29 | 2013-10-03 | Pavel Belik | Uav having hermetically sealed modularized compartments and fluid drain ports |
| CN204131040U (en) * | 2014-07-30 | 2015-01-28 | 广西地凯科技有限公司 | A kind of waterproof junction box |
| CN204223172U (en) * | 2014-10-27 | 2015-03-25 | 广州极飞电子科技有限公司 | Rotor craft battery fastening structure |
| CN204399461U (en) * | 2015-01-13 | 2015-06-17 | 杭州乐卡麦尔工业设计有限公司 | The removable unmanned plane of fuselage |
| CN105059528A (en) * | 2015-07-23 | 2015-11-18 | 致导科技（北京）有限公司 | Foldable unmanned aerial vehicle |
| CN205615701U (en) * | 2016-05-13 | 2016-10-05 | 深圳市斯威普科技有限公司 | Unmanned aerial vehicle waterproof construction |
-
2016
- 2016-05-13 CN CN201610317409.5A patent/CN105923142A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201627812U (en) * | 2009-11-23 | 2010-11-10 | 平高集团有限公司 | Combination gasket and bolt sealing structure |
| US20130256464A1 (en) * | 2010-06-29 | 2013-10-03 | Pavel Belik | Uav having hermetically sealed modularized compartments and fluid drain ports |
| CN204131040U (en) * | 2014-07-30 | 2015-01-28 | 广西地凯科技有限公司 | A kind of waterproof junction box |
| CN204223172U (en) * | 2014-10-27 | 2015-03-25 | 广州极飞电子科技有限公司 | Rotor craft battery fastening structure |
| CN204399461U (en) * | 2015-01-13 | 2015-06-17 | 杭州乐卡麦尔工业设计有限公司 | The removable unmanned plane of fuselage |
| CN105059528A (en) * | 2015-07-23 | 2015-11-18 | 致导科技（北京）有限公司 | Foldable unmanned aerial vehicle |
| CN205615701U (en) * | 2016-05-13 | 2016-10-05 | 深圳市斯威普科技有限公司 | Unmanned aerial vehicle waterproof construction |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111361752A (en) * | 2017-12-29 | 2020-07-03 | 深圳市大疆创新科技有限公司 | Driving device, cloud platform, shooting device and unmanned vehicles |
| CN111090287A (en) * | 2018-10-23 | 2020-05-01 | 深圳市斯威普科技有限公司 | Remote control for controlling an aircraft |
| CN110116798A (en) * | 2019-05-20 | 2019-08-13 | 苏州臻迪智能科技有限公司 | A kind of unmanned thermomechanical components and unmanned plane |
| WO2021016816A1 (en) * | 2019-07-29 | 2021-02-04 | 深圳市大疆创新科技有限公司 | Photographing apparatus, gimbal device, and unmanned aerial vehicle |
| CN110356576A (en) * | 2019-07-30 | 2019-10-22 | 南京精微迅智能科技有限公司 | A kind of unmanned machine head waterproof construction and waterproof method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160907 |