RU2008130741A - FENCE DEVICE - Google Patents
FENCE DEVICE Download PDFInfo
- Publication number
- RU2008130741A RU2008130741A RU2008130741/11A RU2008130741A RU2008130741A RU 2008130741 A RU2008130741 A RU 2008130741A RU 2008130741/11 A RU2008130741/11 A RU 2008130741/11A RU 2008130741 A RU2008130741 A RU 2008130741A RU 2008130741 A RU2008130741 A RU 2008130741A
- Authority
- RU
- Russia
- Prior art keywords
- liner
- compartment
- tank
- intake
- drain pipe
- Prior art date
Links
- 239000000446 fuel Substances 0.000 claims abstract 2
- 239000002828 fuel tank Substances 0.000 claims abstract 2
- 238000005192 partition Methods 0.000 claims abstract 2
Landscapes
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
1. Заборное устройство топливного бака с кольцевым днищем, содержащее кольцевую пластину, установленную над днищем бака, и сливной трубопровод, отличающееся тем, что оно снабжено желобом, выполненным эквидистантно днищу бака и образующим с кольцевой пластиной полый вкладыш с переменным по высоте сечением, содержащий перегородки для разделения вкладыша на отсеки, заборники топлива, размещенные в каждом отсеке и трубопроводы для последовательного сообщения каждого заборника с полостью соседнего отсека, при этом в отсеке с наименьшим сечением выполнено отверстие для сообщения вкладыша с полостью бака, а заборник последнего отсека соединен со сливным трубопроводом. ! 2. Заборное устройство по п.1, отличающееся тем, что вкладыш выполнен разъемным.1. The intake device of the fuel tank with an annular bottom, comprising an annular plate mounted above the bottom of the tank, and a drain pipe, characterized in that it is provided with a groove made equidistant to the bottom of the tank and forming a hollow liner with an annular plate with a variable cross-section, containing partitions for separating the liner into compartments, fuel intakes located in each compartment and pipelines for sequential communication of each intake with the cavity of the adjacent compartment, while in the compartment with the smallest section A hole is made for communication between the liner and the tank cavity, and the intake of the last compartment is connected to the drain pipe. ! 2. The intake device according to claim 1, characterized in that the liner is made detachable.
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008130741/11A RU2384487C1 (en) | 2008-07-24 | 2008-07-24 | Intake device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008130741/11A RU2384487C1 (en) | 2008-07-24 | 2008-07-24 | Intake device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2008130741A true RU2008130741A (en) | 2010-01-27 |
| RU2384487C1 RU2384487C1 (en) | 2010-03-20 |
Family
ID=42121804
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2008130741/11A RU2384487C1 (en) | 2008-07-24 | 2008-07-24 | Intake device |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2384487C1 (en) |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3903924A (en) * | 1973-07-23 | 1975-09-09 | Sundstrand Corp | Compartmented fuel tank |
| RU2156723C1 (en) * | 1999-11-03 | 2000-09-27 | Государственный космический научно-производственный центр им. М.В. Хруничева | Cryogenic stage |
| RU2187010C2 (en) * | 2000-05-03 | 2002-08-10 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им. С.П.Королева" | Liquid propellant rocket engine installation |
-
2008
- 2008-07-24 RU RU2008130741/11A patent/RU2384487C1/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| RU2384487C1 (en) | 2010-03-20 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20130725 |