RU2008115367A - GAS TURBOCHEMISTER AND GAS TURBOCHARGET MISSION - Google Patents
GAS TURBOCHEMISTER AND GAS TURBOCHARGET MISSION Download PDFInfo
- Publication number
- RU2008115367A RU2008115367A RU2008115367/11A RU2008115367A RU2008115367A RU 2008115367 A RU2008115367 A RU 2008115367A RU 2008115367/11 A RU2008115367/11 A RU 2008115367/11A RU 2008115367 A RU2008115367 A RU 2008115367A RU 2008115367 A RU2008115367 A RU 2008115367A
- Authority
- RU
- Russia
- Prior art keywords
- gas turbine
- gas
- locomotive
- roof
- side walls
- Prior art date
Links
- 230000003137 locomotive effect Effects 0.000 claims abstract 6
- 239000000446 fuel Substances 0.000 claims abstract 4
- 238000002485 combustion reaction Methods 0.000 claims abstract 2
- 239000007800 oxidant agent Substances 0.000 claims abstract 2
- 239000003381 stabilizer Substances 0.000 claims abstract 2
Landscapes
- Supercharger (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
1. Газотурбовоз, содержащий корпус, имеющий крышу и боковые стенки, основную силовую установку в виде двух газотурбинных двигателей, а также вспомогательный дизель, соединенные кинематически, отличающийся тем, что применено два ракетных двигателя, установленных в мотогондолах, прикрепленных к боковым стенкам корпуса газотурбовоза, на крыше корпуса установлен, по меньшей мере, один аэродинамический стабилизатор. ! 2. Ракетный двигатель газотурбовоза, содержащий камеру сгорания с турбонасосным агрегатом, выход насосов окислителя и горючего которого соединен с газогенератором, установленным соосно с турбиной, отличающийся тем, что турбонасосный агрегат содержит дополнительный насос горючего и пусковую турбину, соединенную с источником сжатого воздуха.1. A gas turbine locomotive comprising a housing having a roof and side walls, a main power unit in the form of two gas turbine engines, and an auxiliary diesel engine connected kinematically, characterized in that two rocket engines installed in engine nacelles attached to the side walls of the gas turbine locomotive are used, at least one aerodynamic stabilizer is installed on the roof of the casing. ! 2. A gas turbine locomotive rocket engine containing a combustion chamber with a turbopump unit, the output of the oxidizer and fuel pumps of which is connected to a gas generator installed coaxially with the turbine, characterized in that the turbopump unit contains an additional fuel pump and a starting turbine connected to a source of compressed air.
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008115367/11A RU2387556C2 (en) | 2008-04-18 | 2008-04-18 | Gas turbo-locomotive |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008115367/11A RU2387556C2 (en) | 2008-04-18 | 2008-04-18 | Gas turbo-locomotive |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2008115367A true RU2008115367A (en) | 2009-10-27 |
| RU2387556C2 RU2387556C2 (en) | 2010-04-27 |
Family
ID=41352548
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2008115367/11A RU2387556C2 (en) | 2008-04-18 | 2008-04-18 | Gas turbo-locomotive |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2387556C2 (en) |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4233908A (en) * | 1978-12-28 | 1980-11-18 | Omar Alejandro G | Construction of reactor-driven articulated trains with elevated tracks |
| RU2038504C1 (en) * | 1992-01-22 | 1995-06-27 | Московский авиационный институт им.С.Орджоникидзе | Combined gas-turbine engine |
| RU2251505C1 (en) * | 2003-11-17 | 2005-05-10 | Самарская государственная академия путей сообщения (СамГАПС) | Jet gas-turbine locomotive |
-
2008
- 2008-04-18 RU RU2008115367/11A patent/RU2387556C2/en active
Also Published As
| Publication number | Publication date |
|---|---|
| RU2387556C2 (en) | 2010-04-27 |
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