FIELD: engines and pumps.
SUBSTANCE: invention refers to LNG-powered internal combustion engines. Fuel-feed turbine pump assembly to LNG-powered internal combustion engine comprises a shaft-mounted air compressor wheel, a fuel pump impeller, a turbine with an engine disk provided in a housing of the turbine pump assembly and a gas generator with its case being coaxial with the turbine. A starter is attached to the shaft of the turbine pump assembly, while outlets of the air compressor wheel and the fuel pump are connected to the gas generator. At the outlet of the fuel pump, there is an exchanger-gasifier. At the outlet of the fuel pump, a receiver is fixed. At the outlet of the fuel pump, in front of the gas generator, there is a fuel-flow controller.
EFFECT: invention provides increasing efficiency of the turbine pump assembly.
5 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
TURBOPUMP SET OF LIQUID-PROPELLANT ROCKET ENGINE | 2006 |
|
RU2302548C1 |
TURBO-PUMP UNIT OF LIQUID-PROPELLANT ENGINE | 2006 |
|
RU2318129C1 |
ROCKET ENGINE THREE-COMPONENT FUEL TURBOPUMPING SYSTEM | 2008 |
|
RU2384724C1 |
TURBOPUMP UNIT FOR THREE-COMPONENT LIQUID PROPELLANT ROCKET ENGINE | 2008 |
|
RU2383766C1 |
TURBOPUMP SET OF ROCKET ENGINE | 2006 |
|
RU2299346C1 |
MULTI-STAGE | 2008 |
|
RU2390476C1 |
MULTISTAGE CARRIER ROCKET, METHOD OF ITS LAUNCHING, FOUR-COMPONENT ROCKET ENGINE AND FOUR COMPONENT GAS GENERATOR | 2009 |
|
RU2397116C1 |
THREE-COMPONENT LIQUID-PROPELLANT ROCKET ENGINE AND METHOD OF ITS OPERATION | 2008 |
|
RU2386844C1 |
THREE-COMPONENT LIQUID-PROPELLANT ENGINE | 2011 |
|
RU2484287C1 |
GAS TURBO-LOCOMOTIVE | 2008 |
|
RU2387556C2 |
Authors
Dates
2009-07-27—Published
2008-04-07—Filed