CN205117843U - A controllable formula forced -air cooling heat dissipation oil tank for early warning plane - Google Patents
A controllable formula forced -air cooling heat dissipation oil tank for early warning plane Download PDFInfo
- Publication number
- CN205117843U CN205117843U CN201520869622.8U CN201520869622U CN205117843U CN 205117843 U CN205117843 U CN 205117843U CN 201520869622 U CN201520869622 U CN 201520869622U CN 205117843 U CN205117843 U CN 205117843U
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- CN
- China
- Prior art keywords
- outer container
- early warning
- fuel tank
- cooling heat
- oil tank
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- 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.)
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- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
The utility model discloses a controllable formula forced -air cooling heat dissipation oil tank for early warning plane, including interior oil tank, outer container and a plurality of heat dissipation muscle, interior oil tank setting is in in the outer container, be provided with a plurality of through -holes on the outer container, it is a plurality of the first end of heat dissipation muscle all passes the through -hole with the lateral wall fixed connection of interior oil tank, be provided with the air -supply line on the side of outer container, be provided with out the tuber pipe on another side of outer container, the air -supply line passes through the trachea and sets up air intlet intercommunication on the early warning plane, the tuber pipe with the last ooff valve that all is provided with of air intlet. The utility model relates to a controllable formula forced -air cooling heat dissipation oil tank for early warning plane installs the outer container additional in the outside of oil tank including through to being connected the outer container with hot blast blowpipe apparatus, making it when needs use forced -air cooling heat dissipation, directly introduce the air to between interior oil tank and the outer container, then can accomplish forced -air cooling heat dissipation, it is better controlled that accessible on -off valve control makes it have.
Description
Technical field
The utility model relates to a kind of heat radiation oil box, particularly relates to a kind of controllable type wind-cooling heat dissipating fuel tank for early warning plane.
Background technique
Fuel tank is for loading the hydraulic oil in the flight fuel of early warning plane or hydraulic system, in the process of flight, if the temperature of the fuel oil of fuel tank or hydraulic oil is too high, early warning plane then may be caused normally to work, traditional fuel tank heat radiation is all only dispelled the heat by fuel tank outer wall, may occur the situation of dispelling the heat not in time, or directly install radiation fan additional, controllability is lower.
Model utility content
The purpose of this utility model is just to provide a kind of controllable type wind-cooling heat dissipating fuel tank for early warning plane to solve the problem.
The utility model is achieved through the following technical solutions above-mentioned purpose:
A kind of controllable type wind-cooling heat dissipating fuel tank for early warning plane, comprise interior fuel tank, outer container and multiple radiating fin, described interior fuel tank is arranged in described outer container, described outer container is provided with multiple through hole, the first end of multiple described radiating fin is all fixedly connected with through the outer side wall of described through hole with described interior fuel tank, a side of described outer container is provided with air intake pipe, another side of described outer container is provided with air outlet tube, described air intake pipe is communicated with the air intlet be arranged on described early warning plane by tracheae, described airduct and described air intlet are provided with switch valve.
Particularly, multiple described radiating fin distributes at the surface uniform of described interior fuel tank, and the distance between two adjacent described radiating fin is equal, and the diameter of described through hole and the equal diameters of described radiating fin, described radiating fin and described outer container are tightly connected.
Particularly, the quantity of described air intake pipe is multiple, and multiple described air intake pipes are evenly distributed on the side of described outer container, and the quantity of described air outlet tube is one or more, and is all arranged on the offside of described air intake pipe.
Particularly, the diameter of described air intake pipe is less than the diameter of described air outlet tube.
The beneficial effects of the utility model are:
A kind of controllable type wind-cooling heat dissipating fuel tank for early warning plane of the utility model is by installing outer container additional in the outside of interior fuel tank, and outer container is connected with air intake device, make it when needs use wind-cooling heat dissipating, directly air is introduced between interior fuel tank and outer container, then can complete wind-cooling heat dissipating, make it have good controlling by control switch valve.
Accompanying drawing explanation
Fig. 1 is the sectional view of the controllable type wind-cooling heat dissipating fuel tank for early warning plane described in the utility model;
Fig. 2 is the plan view of the controllable type wind-cooling heat dissipating fuel tank for early warning plane described in the utility model.
Embodiment
Below in conjunction with accompanying drawing, the utility model is described in further detail:
As depicted in figs. 1 and 2, a kind of controllable type wind-cooling heat dissipating fuel tank for early warning plane of the utility model, comprise interior fuel tank 1, outer container 2 and multiple radiating fin 3, interior fuel tank 1 is arranged in outer container 2, outer container 2 is provided with multiple through hole, the first end of multiple radiating fin 3 is all fixedly connected with through the outer side wall of through hole with interior fuel tank 1, a side of outer container 2 is provided with air intake pipe 4, another side of outer container 2 is provided with air outlet tube 5, air intake pipe 4 is communicated with the air intlet be arranged on early warning plane by tracheae, airduct and air intlet are provided with switch valve, multiple radiating fin 3 distributes at the surface uniform of interior fuel tank 1, distance between two adjacent radiating fin 3 is equal, the diameter of through hole and the equal diameters of radiating fin 3, radiating fin 3 and outer container 2 are tightly connected, the quantity of air intake pipe 4 is multiple, multiple air intake pipes 4 are evenly distributed on the side of outer container 2, the quantity of air outlet tube 5 is one or more, and be all arranged on the offside of air intake pipe 4, the diameter of air intake pipe 4 is less than the diameter of air outlet tube 5.
The working principle that the utility model is used for the controllable type wind-cooling heat dissipating fuel tank of early warning plane is as follows:
Be connected with the air intlet on early warning plane by air intake pipe 4 by airduct, if the temperature of fuel tank is lower, do not need air-cooled auxiliary heat dissipation, then the switch valve on air intlet and the switch valve on airduct are closed, fuel tank is through dispelling the heat by radiating fin 3 and outer container 2.
When the air-cooled auxiliary heat dissipation of needs, switch valve on air intlet and airduct is opened, cool ambient air enters from air intlet, flow between outer container 2 and interior fuel tank 1 through airduct, and flow to air outlet tube 5 place along the gap between outer container 2 and interior fuel tank 1 and discharge, in the process of air current flow, the heat on interior fuel tank 1 is taken away, achieves air-cooled auxiliary heat dissipation.
The utility model can, by the control of control switch valve realization to air-cooled auxiliary heat dissipation, can be selected the need of auxiliary heat dissipation simultaneously according to specific circumstances.If when early warning plane needs high-speed flight, can auxiliary heat dissipating system be closed, reduce the windage of early warning plane, increase flying speed; When early warning plane does not need high-speed flight, can auxiliary heat dissipating system be opened, lower fuel tank temperature.
The technical solution of the utility model is not limited to the restriction of above-mentioned specific embodiment, and every technology distortion made according to the technical solution of the utility model, all falls within protection domain of the present utility model.
Claims (4)
1. the controllable type wind-cooling heat dissipating fuel tank for early warning plane, it is characterized in that: comprise interior fuel tank, outer container and multiple radiating fin, described interior fuel tank is arranged in described outer container, described outer container is provided with multiple through hole, the first end of multiple described radiating fin is all fixedly connected with through the outer side wall of described through hole with described interior fuel tank, a side of described outer container is provided with air intake pipe, another side of described outer container is provided with air outlet tube, described air intake pipe is communicated with the air intlet be arranged on described early warning plane by tracheae, described airduct and described air intlet are provided with switch valve.
2. a kind of controllable type wind-cooling heat dissipating fuel tank for early warning plane according to claim 1, it is characterized in that: multiple described radiating fin distributes at the surface uniform of described interior fuel tank, distance between two adjacent described radiating fin is equal, the diameter of described through hole and the equal diameters of described radiating fin, described radiating fin and described outer container are tightly connected.
3. a kind of controllable type wind-cooling heat dissipating fuel tank for early warning plane according to claim 2, it is characterized in that: the quantity of described air intake pipe is multiple, multiple described air intake pipes are evenly distributed on the side of described outer container, the quantity of described air outlet tube is one or more, and is all arranged on the offside of described air intake pipe.
4. a kind of controllable type wind-cooling heat dissipating fuel tank for early warning plane according to claim 3, is characterized in that: the diameter of described air intake pipe is less than the diameter of described air outlet tube.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520869622.8U CN205117843U (en) | 2015-11-03 | 2015-11-03 | A controllable formula forced -air cooling heat dissipation oil tank for early warning plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520869622.8U CN205117843U (en) | 2015-11-03 | 2015-11-03 | A controllable formula forced -air cooling heat dissipation oil tank for early warning plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205117843U true CN205117843U (en) | 2016-03-30 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520869622.8U Active CN205117843U (en) | 2015-11-03 | 2015-11-03 | A controllable formula forced -air cooling heat dissipation oil tank for early warning plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205117843U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113803634A (en) * | 2020-06-17 | 2021-12-17 | 多立恒（北京）能源技术股份公司 | Inner-cooling air-cooling inflation gun |
-
2015
- 2015-11-03 CN CN201520869622.8U patent/CN205117843U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113803634A (en) * | 2020-06-17 | 2021-12-17 | 多立恒（北京）能源技术股份公司 | Inner-cooling air-cooling inflation gun |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |