FIELD: engines and pumps.
SUBSTANCE: this turbo pump assy comprises oxidizer pump impeller fitted on the shaft, propellant pump and turbine wheel arranged in turbo pump housing. Note here that it comprises electrical generator with stator and rotor with shaft coupled with turbo pump unit shaft. Note also that magnetic clutch is fitted between turbo pump unit shaft and electrical generator clutch. Said magnetic clutch can be arranged between oxidizer pump and propellant pump. Magnetic clutch can be arranged between propellant pump and extra propellant pump.
EFFECT: ruled out turbo pump explosion at start or in flight.
4 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TURBOPUMP SET OF LIQUID-PROPELLANT ROCKET ENGINE | 2006 |
|
RU2302548C1 |
| TURBO-PUMP UNIT OF LIQUID-PROPELLANT ENGINE | 2006 |
|
RU2318129C1 |
| LIQUID-PROPELLANT ENGINE AND TURBO-PUMP UNIT | 2009 |
|
RU2418970C1 |
| TURBO-PUMP UNIT OF LIQUID MISSILE ENGINE | 2014 |
|
RU2560656C1 |
| TURBOPUMP SET OF ROCKET ENGINE | 2006 |
|
RU2299346C1 |
| LIQUID-PROPELLANT ROCKET ENGINE FUEL FEED PLANT | 2014 |
|
RU2574192C1 |
| LIQUID PROPELLANT ROCKET ENGINE | 2014 |
|
RU2545613C1 |
| LIQUID-PROPELLANT ROCKET ENGINE TURBOPUMP UNIT | 2014 |
|
RU2539315C1 |
| LIQUID-PROPELLANT ROCKET ENGINE | 2006 |
|
RU2300657C1 |
| ROCKET ENGINE THREE-COMPONENT FUEL TURBOPUMPING SYSTEM | 2008 |
|
RU2384724C1 |
