CN206068173U - A kind of unmanned plane protective device of fuel tank - Google Patents
A kind of unmanned plane protective device of fuel tank Download PDFInfo
- Publication number
- CN206068173U CN206068173U CN201621104810.2U CN201621104810U CN206068173U CN 206068173 U CN206068173 U CN 206068173U CN 201621104810 U CN201621104810 U CN 201621104810U CN 206068173 U CN206068173 U CN 206068173U
- Authority
- CN
- China
- Prior art keywords
- baffle
- unmanned plane
- fuel tank
- installing plate
- casing
- 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
Abstract
This utility model is related to unmanned plane fuel tank protective technical field, a kind of especially unmanned plane protective device of fuel tank, including casing, opening is offered at the top of the casing, the box house is vertically arranged with installing plate near the side of opening, and box house offers the chute perpendicular to installing plate relative to the opposite side of installing plate, the installing plate is provided with spring near the side of chute, the spring is connected with first baffle away from one end of installing plate, the first baffle is provided with slide block away from the upper surface of one end of spring, the slide block is connected with slide, the first baffle is provided with contiguous block near one end of slide block, and box house is tiltedly installed with the second baffle corresponding with contiguous block near the side of chute.This utility model is simple in structure and convenient in use, and is effectively reduced the probability of fire generation, and the safety that ensure that unmanned plane fuel tank when in use.
Description
Technical field
This utility model is related to unmanned plane fuel tank protective technical field, more particularly to a kind of unmanned plane protective device of fuel tank.
Background technology
Current police unmanned plane dynamical system mainly have three classes, one be all-electric unmanned plane, Equations of The Second Kind be fuel power
Unmanned plane, the 3rd class are hybrid power unmanned planes.Using fuel power unmanned plane due to fuel oil engine efficiency it is high with it is all-electric
UAS compare, with the big advantage of flight time length, loading capacity, but occur accident post fuel leakage easily draw
Fire is played, there is potential safety hazard.
Utility model content
The purpose of this utility model is and a kind of unmanned sump for proposing in order to solve shortcoming present in prior art
Preventer.The unmanned plane protective device of fuel tank have simple structure, it is easy to use, the features such as be prevented effectively from fire.
To achieve these goals, this utility model employs following technical scheme：
A kind of unmanned plane protective device of fuel tank, including casing are designed, opening, the casing at the top of the casing, is offered
The internal side near opening is vertically arranged with installing plate, and box house relative to installing plate opposite side offer perpendicular to
The chute of installing plate, the installing plate are provided with spring near the side of chute, and the spring connects away from one end of installing plate
There is first baffle, the first baffle is provided with slide block away from the upper surface of one end of spring, and the slide block is connected with slide
Connect, the first baffle is provided with contiguous block near one end of slide block, and box house is tiltedly installed near the side of chute
The second baffle corresponding with contiguous block；
The outside of the casing is provided with Ceramic silicon rubber fireprotection layer, and the periphery setting of Ceramic silicon rubber fireprotection layer
The outside for having air bag protective layer, the air bag protective layer is arranged with metal shell.
Preferably, the second baffle and contiguous block one side close to each other is provided with anti-skid bulge.
Preferably, the chute is set to C-channel.
Preferably, the slide block is set to T-shaped slide block.
Preferably, outside the metal shell, corresponding both sides are provided with mounting blocks.
The utility model proposes a kind of unmanned plane protective device of fuel tank, beneficial effect is：This utility model is being used
When, contiguous block can be made to hang on second baffle spring elongation, due to the contact surface of second baffle and contiguous block be provided with it is anti-
It is sliding raised, the connection between second baffle and contiguous block can be made more to consolidate, be subject to external action to occur in unmanned plane body prominent
When so falling, casing can produce the vibrations of fierceness.Now as second baffle is to be obliquely installed, it is being given a shock or is hitting
When hitting, contiguous block will be slid from second baffle, and opening is covered by first baffle under the action of the spring, can be subtracted to a great extent
In few casing, oil leaks, and the Ceramic silicon rubber fireprotection layer that is arranged on outside casing and air bag protective layer are respectively provided with one
Fixed damping and fireproofing function, can be prevented effectively from fuel tank and the phenomenon such as be caused to catch fire by the leakage of oil in damaged evil idea and fuel tank.This
Utility model is simple in structure and convenient in use, and is effectively reduced the probability of fire generation, and ensure that nobody
The safety of machine fuel tank when in use.
Description of the drawings
Fig. 1 be the utility model proposes a kind of unmanned plane protective device of fuel tank internal structure schematic diagram；
Fig. 2 be the utility model proposes a kind of unmanned plane protective device of fuel tank first baffle structural representation；
Fig. 3 be the utility model proposes a kind of unmanned plane protective device of fuel tank external structure schematic diagram；
Fig. 4 be the utility model proposes a kind of unmanned plane protective device of fuel tank chute and slide block structure schematic diagram.
In figure：Casing 1, first baffle 2, chute 3, spring 4, opening 5, installing plate 6, contiguous block 7, second baffle 8, ceramics
SiClx rubber fire-resistant layer 9, air bag protective layer 10, metal shell 11, slide block 12, mounting blocks 13.
Specific embodiment
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only this utility model a part of embodiment, rather than whole
Embodiment.
Reference picture 1-4, a kind of unmanned plane protective device of fuel tank, including casing 1, the top of casing 1 offers opening 5, case
It is vertically arranged with inside installing plate 6, and casing 1 near the side of opening 5 inside body 1 and opens up relative to the opposite side of installing plate 6
There is the chute 3 perpendicular to installing plate 6, installing plate 6 is provided with spring 4, spring 4 away from installing plate 6 near the side of chute 3
End is connected with first baffle 2, and first baffle 2 is provided with slide block 12, slide block 12 and chute 3 away from the upper surface of one end of spring 4
It is slidably connected, chute 3 is set to C-channel, and slide block 12 is set to T-shaped slide block, so arranging can make between chute 3 and slide block 12
Connection more consolidate, while to first baffle 2 also have certain supporting role.
First baffle 2 is provided with inside contiguous block 7, and casing 1 near one end of slide block 12 and inclines near the side of chute 3
The second baffle 8 corresponding with contiguous block 7 is provided with, second baffle 8 and contiguous block 7 one side close to each other is provided with anti-skidding
Projection, is easy to make the connection between second baffle 8 and contiguous block 7 more consolidate.
The outside of casing 1 is provided with Ceramic silicon rubber fireprotection layer 9, and the periphery setting of Ceramic silicon rubber fireprotection layer 9
There is air bag protective layer 10, there is air bag protective layer 10 certain damping, buffering effect can effectively slow down exterior vibration to casing 1
Affect, the outside of air bag protective layer 10 is arranged with metal shell 11, and metal shell 11 has certain guarantor to air bag protective layer 10
Shield is acted on, in order to avoid air bag protective layer 10 is damaged to affect to use, outside metal shell 11, corresponding both sides are provided with mounting blocks
13, the connection being easy between casing 1 and unmanned plane body and dismounting.
Spring 4 when in use, can be stretched by this utility model, contiguous block 7 is hung on second baffle 8, due to second gear
The contact surface of plate 8 and contiguous block 7 is provided with anti-skid bulge, and the connection between second baffle 8 and contiguous block 7 can be made more steady
Gu, when unmanned plane body is subject to external action to occur to fall suddenly, casing 1 can produce the vibrations of fierceness.Now by
In second baffle 8 to be obliquely installed, when being given a shock or clash into, contiguous block 7 will be slid from second baffle 8, and first baffle 2 exists
Opening 5 is covered in the presence of spring 4, leaking for oil can be reduced in casing 1 to a great extent, and be arranged on outside casing 1
The Ceramic silicon rubber fireprotection layer 9 and air bag protective layer 10 in portion is respectively provided with certain damping and fireproofing function, can be prevented effectively from
Fuel tank the phenomenon such as is caused to catch fire by the leakage of oil in damaged evil idea and fuel tank.
The above, only this utility model preferably specific embodiment, but protection domain of the present utility model is not
Be confined to this, any those familiar with the art in the technical scope that this utility model is disclosed, according to this practicality
New technical scheme and its utility model design in addition equivalent or change, should all cover in protection model of the present utility model
Within enclosing.
Claims (5)
1. a kind of unmanned plane protective device of fuel tank, including casing (1), it is characterised in that offer out at the top of the casing (1)
Mouthful (5), the internal side near opening (5) of the casing (1) are vertically arranged with installing plate (6), and casing (1) it is internal relative to
The opposite side of installing plate (6) offers the chute (3) perpendicular to installing plate (6), the installing plate (6) near chute (3)
Side is provided with spring (4), and the spring (4) is connected with first baffle (2), the first baffle away from one end of installing plate (6)
(2) upper surface away from one end of spring (4) is provided with slide block (12), and the slide block (12) is slidably connected with chute (3), described
First baffle (2) is provided with contiguous block (7), and the internal inclination near chute (3) of casing (1) near one end of slide block (12)
The second baffle (8) corresponding with contiguous block (7) is provided with tiltedly；
The outside of the casing (1) is provided with Ceramic silicon rubber fireprotection layer (9), and Ceramic silicon rubber fireprotection layer (9) is outer
Enclose and be provided with air bag protective layer (10), the outside of the air bag protective layer (10) is arranged with metal shell (11).
2. a kind of unmanned plane protective device of fuel tank according to claim 1, it is characterised in that the second baffle (8) and
Contiguous block (7) one side close to each other is provided with anti-skid bulge.
3. a kind of unmanned plane protective device of fuel tank according to claim 1, it is characterised in that the chute (3) is set to C
Shape groove.
4. a kind of unmanned plane protective device of fuel tank according to claim 1, it is characterised in that the slide block (12) is set to
T-shaped slide block.
5. a kind of unmanned plane protective device of fuel tank according to claim 1, it is characterised in that the metal shell (11) is outward
The corresponding both sides in portion are provided with mounting blocks (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621104810.2U CN206068173U (en) | 2016-10-08 | 2016-10-08 | A kind of unmanned plane protective device of fuel tank |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621104810.2U CN206068173U (en) | 2016-10-08 | 2016-10-08 | A kind of unmanned plane protective device of fuel tank |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206068173U true CN206068173U (en) | 2017-04-05 |
Family
ID=58441775
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621104810.2U Expired - Fee Related CN206068173U (en) | 2016-10-08 | 2016-10-08 | A kind of unmanned plane protective device of fuel tank |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206068173U (en) |
-
2016
- 2016-10-08 CN CN201621104810.2U patent/CN206068173U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20171011 Address after: 239400 No. 7 building, Sha Ba District, Huaihe Avenue, Mingguang City, Anhui Patentee after: Sino satellite remote sensing load (Anhui) Technology Co., Ltd. Address before: 100000 Beijing Road, Haidian District, Lane No. 1, building 5, floor 5-1614, 1 Patentee before: China exchange remote sensing load (Beijing) Technology Co., Ltd. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170405 Termination date: 20191008 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |