CN104743126A - Aircraft oil tank casting device - Google Patents
Aircraft oil tank casting device Download PDFInfo
- Publication number
- CN104743126A CN104743126A CN201310736223.XA CN201310736223A CN104743126A CN 104743126 A CN104743126 A CN 104743126A CN 201310736223 A CN201310736223 A CN 201310736223A CN 104743126 A CN104743126 A CN 104743126A
- Authority
- CN
- China
- Prior art keywords
- oil tank
- control mechanism
- casting device
- aircraft
- fuel tank
- 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
Landscapes
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
The invention is practical for reducing the generation probability of aviation accident fire, and provides an aircraft oil tank casting device. The oil tank casting device is designed to consist of a tracker, an oil tank control mechanism and the like; the tracker tracks an aviation accident generation signal to transfer to the oil tank control mechanism; and the oil tank control mechanism controls an oil tank to be separated from an aircraft body, so that the oil tank is cast before an aircraft lands, and no fuel is left in landing collision as shown in figure. The aircraft oil tank casting device has the beneficial effects of reducing the fire generation probability and preventing the mass casualties.
Description
Technical field
The present invention is practically applicable to reduce airplane crash fire odds.
Background technology
Airplane crash occurs, and usually with fire, the loss caused cannot be retrieved, and cause of fire is fuel tank mainly.
Summary of the invention
In order to overcome the problem such as fire in airplane crash, the invention provides a kind of fuel tanker slinger, this fuel tank slinger designs is tracker, the formations such as fuel tank control mechanism, tracker traces into the signal transmission oil dropping apparatus control mechanism that airplane crash occurs, fuel tank control mechanism controls fuel tank and is separated with airframe, makes aircraft jettisoning fuel tank before landing, and lands when clashing into and does not have fuel oil.As shown in the figure.The invention has the beneficial effects as follows, reduce fire odds, avoid a large amount of injures and deaths of personnel.
Accompanying drawing explanation
Fig. 1 is the structural representation of fuel tanker slinger:
Wherein 1 is body, and 2 is trackers, and 3 is fuel tanks, and 4 is fuel tank control mechanisms.
Detailed description of the invention
As in Fig. 1, fuel tank slinger designs is tracker (2), the formations such as fuel tank control mechanism (4), tracker (2) traces into the signal transmission of airplane crash generation to controlling fuel tank mechanism (4), fuel tank control mechanism (4) controls fuel tank and is separated with airframe (1), make aircraft jettisoning fuel tank before landing, land when clashing into and there is no fuel oil.
Claims (1)
1. a fuel tanker slinger, by tracker, fuel tank control mechanism is formed, and it is characterized in that: tracker traces into the signal transmission oil dropping apparatus control mechanism that airplane crash occurs, and fuel tank control mechanism controls fuel tank and is separated with airframe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310736223.XA CN104743126A (en) | 2013-12-29 | 2013-12-29 | Aircraft oil tank casting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310736223.XA CN104743126A (en) | 2013-12-29 | 2013-12-29 | Aircraft oil tank casting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104743126A true CN104743126A (en) | 2015-07-01 |
Family
ID=53583542
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310736223.XA Pending CN104743126A (en) | 2013-12-29 | 2013-12-29 | Aircraft oil tank casting device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104743126A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108382601A (en) * | 2018-03-30 | 2018-08-10 | 贵州大鸟创新科技有限公司 | A kind of unmanned plane protective device of fuel tank |
| CN111731492A (en) * | 2020-06-04 | 2020-10-02 | 天津爱思达新材料科技有限公司 | Fuel tank of aircraft |
-
2013
- 2013-12-29 CN CN201310736223.XA patent/CN104743126A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108382601A (en) * | 2018-03-30 | 2018-08-10 | 贵州大鸟创新科技有限公司 | A kind of unmanned plane protective device of fuel tank |
| CN111731492A (en) * | 2020-06-04 | 2020-10-02 | 天津爱思达新材料科技有限公司 | Fuel tank of aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150701 |
|
| WD01 | Invention patent application deemed withdrawn after publication |