CN213832135U - Soft fuel tank applied to unmanned aerial vehicle - Google Patents
Soft fuel tank applied to unmanned aerial vehicle Download PDFInfo
- Publication number
- CN213832135U CN213832135U CN202021216774.5U CN202021216774U CN213832135U CN 213832135 U CN213832135 U CN 213832135U CN 202021216774 U CN202021216774 U CN 202021216774U CN 213832135 U CN213832135 U CN 213832135U
- Authority
- CN
- China
- Prior art keywords
- oil
- disc
- top cover
- oil outlet
- integral
- 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
- 239000002828 fuel tank Substances 0.000 title claims abstract description 4
- 238000007789 sealing Methods 0.000 claims abstract description 25
- 239000000463 material Substances 0.000 claims abstract description 7
- 239000000446 fuel Substances 0.000 abstract description 4
- 230000001788 irregular Effects 0.000 abstract description 2
- 230000010355 oscillation Effects 0.000 abstract description 2
- 230000001681 protective effect Effects 0.000 abstract 2
- 239000003921 oil Substances 0.000 description 69
- 239000000295 fuel oil Substances 0.000 description 7
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 239000007779 soft material Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Images
Landscapes
- Closures For Containers (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
The utility model discloses a soft fuel tank applied to an unmanned aerial vehicle, which comprises an integral device, a sealing device and an oil outlet device, wherein the integral device is arranged on the ground, the sealing device and the oil outlet device are respectively arranged on two opposite surfaces of the integral device, the oil outlet device is communicated with the integral device, the sealing device comprises a disc, the disc is arranged on the top of the integral device, a top cover is arranged above the disc, a protective pad is arranged between the top cover and the disc, the bottom of the top cover penetrates through the disc and the protective pad and is in threaded connection with the disc, the novel oil-resistant material is formed by high-frequency heat sealing, the weight of the finished product is lighter, because the oil tank is soft and can be randomly deformed in shape and placed in the machine cabin which is irregular in size or larger, the adaptability of the oil tank is improved, because the oil tank is the software, along with the fuel slowly exhausts, the oil tank also can slowly suck flat, can not appear the fuel supply problem that the fuel oscillation causes in the oil tank.
Description
Technical Field
The utility model belongs to the target drone field, concretely relates to use software fuel tank on unmanned aerial vehicle.
Background
A drone is broadly a military aircraft that is targeted for shooting training. The aircraft simulates the aircrafts of enemy army or incoming missiles during military exercises or weapon missions by utilizing remote control or preset flight paths and modes, provides imaginary targets and shooting opportunities for various artillery or missile systems, and belongs to one type of unmanned planes.
At present, oil tanks applied to a plurality of target drone machines are made of plastic, the weight of the oil tanks reaches 260g, the plastic oil tanks are formed, the shape of the oil tanks cannot be randomly and slightly changed and are placed in a drone machine cabin, the size of the oil tanks needs to be completely matched with the drone cabin, otherwise the oil tanks cannot be placed, the fuel oil rocks in the oil tanks along with the reduction of the fuel oil when the fuel oil is in maneuvering flight along with the target drone, particularly the fuel oil can be interrupted when the target drone is in rolling and spiral maneuvering flight, and the engine stalls or the drone aircraft is abnormally broken due to insufficient fuel oil supply.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an use software fuel tank on unmanned aerial vehicle to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an use software fuel tank on unmanned aerial vehicle, includes integrated device, closing cap device and the device of producing oil, integrated device sets up on unmanned aerial vehicle, closing cap device and the device of producing oil set up two opposite faces at integrated device respectively, the device of producing oil communicates with integrated device, closing cap device and the device of producing oil are formed through high frequency heat seal by novel resistant oily material, just the oil tank is the software structure.
Preferably, the closing cap device includes the disc, the disc sets up the top at the integrated device, the top of disc is provided with the top cap, be provided with the protection pad between top cap and the disc, the bottom of top cap run through disc and protection pad and with disc threaded connection, the one end of top cap extends to the top of disc.
Preferably, the oil outlet device comprises a sealing plate, the sealing plate is arranged at the bottom of the whole device, a vertical pipe is arranged in the sealing plate, the vertical pipe penetrates through the sealing plate and extends into the whole device, an oil outlet pipe is arranged in the vertical pipe and is communicated with the vertical pipe, and the oil outlet pipe is arranged below the whole device.
Preferably, the integrated device comprises an oil box, the oil box is arranged in the target drone, the disc and the sealing plate are respectively arranged at two ends of the oil box, the vertical pipe extends into the oil box, and the oil outlet pipe is arranged outside the oil box.
Compared with the prior art, the beneficial effects of the utility model are that: the novel oil-resistant material is formed by high-frequency heat sealing, the weight of a finished product is lighter, the oil tank is soft, the appearance can be randomly deformed and placed into a large or small irregular machine cabin, the adaptability of the oil tank is improved, the oil tank is soft, the oil tank can slowly suck shriveled along with the slow exhaustion of fuel oil, and the problem of fuel supply caused by the oscillation of the fuel oil in the oil tank can be avoided.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a front view of the present invention;
fig. 3 is a side view of the present invention;
fig. 4 is a top view of the present invention;
in the figure: 1. an integral device; 101. an oil box; 2. a capping device; 201. a disc; 202. a protection pad; 203. a top cover; 3. an oil outlet device; 301. a sealing plate; 302. an oil outlet pipe; 303. a standpipe.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention.
Referring to fig. 1-4, the present invention provides the following technical solutions: the utility model provides an use software fuel tank on unmanned aerial vehicle, includes integrated device 1, closing cap device 2 and oil outlet device 3, integrated device 1 sets up on unmanned aerial vehicle, and closing cap device 2 and oil outlet device 3 set up respectively at two opposite faces of integrated device 1, and oil outlet device 3 and integrated device 1 intercommunication, integrated device 1, closing cap device 2 and oil outlet device 3 are formed by novel resistant oily material through high frequency heat seal, and the oil tank is the software structure.
In order to seal the top of the oil box 101 and avoid the oil leakage phenomenon of the oil box 101, in this embodiment, preferably, the cover device 2 includes a circular disc 201, the circular disc 201 is disposed on the top of the whole device 1, a top cover 203 is disposed above the circular disc 201, a protection pad 202 is disposed between the top cover 203 and the circular disc 201, the bottom of the top cover 203 penetrates through the circular disc 201 and the protection pad 202 and is in threaded connection with the circular disc 201, one end of the top cover 203 extends to the top of the circular disc 201, the top of the oil box 101 is sealed by the top cover 203, and the oil leakage of the oil box 101 is prevented.
In order to make the oil in the oil box 101 flow out through the standpipe 303 and the oil outlet pipe 302, in this embodiment, preferably, the oil outlet device 3 includes a sealing plate 301, the sealing plate 301 is disposed at the bottom of the whole device 1, the standpipe 303 is disposed in the sealing plate 301, the standpipe 303 penetrates through the sealing plate 301 and extends into the whole device 1, the oil outlet pipe 302 is disposed in the standpipe 303, the oil outlet pipe 302 is communicated with the standpipe 303, the oil outlet pipe 302 is disposed below the whole device 1, and the sealing plate 301 can prevent the oil in the oil box 101 from leaking out.
In order to enable the oil box 101 to change along with the volume change of the oil in the oil box 101, the novel oil-resistant material of the oil box 101 is formed by high-frequency heat sealing, and the material selected for the oil box 101 is a soft material, in this embodiment, preferably, the whole device 1 includes the oil box 101, the oil box 101 is disposed in a target drone, the discs 201 and the sealing plates 301 are disposed at two ends of the oil box 101 respectively, the vertical pipe 303 extends into the oil box 101, and the oil outlet pipe 302 is disposed outside the oil box 101.
The utility model discloses a theory of operation and use flow: the utility model discloses after having installed, at first inspect the utility model discloses an installation is fixed and safety protection, then just can use, during the use, place top cap 203 at the top of oil box 101 to twist and move top cap 203 and make the bottom of top cap 203 enter into disc 201, through the threaded connection of top cap 203 bottom and disc 201, make top cap 203 can fix at the top of oil box 101, make the top seal of oil box 101, then oil in the oil box 101 flows standpipe 303 and play oil pipe 302 through closing plate 301, and flows by play oil pipe 302.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (2)
1. The utility model provides an use software fuel tank on unmanned aerial vehicle, includes integrated device (1), closing cap device (2) and oil outlet device (3), its characterized in that: the integral device (1) is arranged on an unmanned aerial vehicle, the sealing device (2) and the oil outlet device (3) are respectively arranged on two opposite surfaces of the integral device (1), the oil outlet device (3) is communicated with the integral device (1), the sealing device (2) comprises a disc (201), the disc (201) is arranged at the top of the integral device (1), a top cover (203) is arranged above the disc (201), a protection pad (202) is arranged between the top cover (203) and the disc (201), the bottom of the top cover (203) penetrates through the disc (201) and the protection pad (202) and is in threaded connection with the disc (201), one end of the top cover (203) extends to the upper side of the disc (201), the oil outlet device (3) comprises a sealing plate (301), the sealing plate (301) is arranged at the bottom of the integral device (1), a vertical pipe (303) is arranged in the sealing plate (301), standpipe (303) run through sealing plate (301) and extend to in integrated device (1), be provided with out oil pipe (302) in standpipe (303), go out oil pipe (302) and standpipe (303) intercommunication, it sets up the below at integrated device (1) to go out oil pipe (302), integrated device (1), closing cap device (2) and play oil device (3) are formed through high frequency heat seal by novel resistant oily material, just the oil tank is the software structure.
2. The soft fuel tank applied to the unmanned aerial vehicle as claimed in claim 1, wherein: the integral device (1) comprises an oil box (101), wherein the oil box (101) is arranged in a target machine, the disc (201) and the sealing plate (301) are respectively arranged at two ends of the oil box (101), the vertical pipe (303) extends into the oil box (101), and the oil outlet pipe (302) is arranged outside the oil box (101).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021216774.5U CN213832135U (en) | 2020-06-28 | 2020-06-28 | Soft fuel tank applied to unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021216774.5U CN213832135U (en) | 2020-06-28 | 2020-06-28 | Soft fuel tank applied to unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213832135U true CN213832135U (en) | 2021-07-30 |
Family
ID=76987329
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021216774.5U Expired - Fee Related CN213832135U (en) | 2020-06-28 | 2020-06-28 | Soft fuel tank applied to unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213832135U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116767493A (en) * | 2023-05-04 | 2023-09-19 | 中国人民解放军军事科学院系统工程研究院 | Air-drop liquid cargo device and air-drop liquid cargo unmanned aerial vehicle with same |
-
2020
- 2020-06-28 CN CN202021216774.5U patent/CN213832135U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116767493A (en) * | 2023-05-04 | 2023-09-19 | 中国人民解放军军事科学院系统工程研究院 | Air-drop liquid cargo device and air-drop liquid cargo unmanned aerial vehicle with same |
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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: 20210730 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |