FUEL TANK SUPERCHARGING SYSTEM (VERSIONS) Russian patent published in 2008 - IPC F02K9/50 

Abstract RU 2341675 C2

FIELD: engines and pumps.

SUBSTANCE: invention relates to space engineering, particularly, to designing and operation of jet engines of space vehicles. The fuel tank supercharging system comprising high-pressure cylinders communicating, via pneumatic lines, with gas chambers of appropriate tanks containing fuel and oxidiser and start-and-shut-off valves consecutively fitted on the said pneumatic lines and gas pressure control valve differs from the known device, in compliance with the first version, in that it incorporates a heater representing a multi-channel tubular-casing heat exchanger connected to the thermal control system. Note that every pipe of the said heat exchanger houses a displacer arranged over the entire pipe length to form a uniform circular gap in the annular channel between the pipe wall and displacer. Note here that the pipes represent coils and heat exchanger channels are connected into appropriate circuits of pneumatic lines behind the gas pressure control valves and throttling devices arranged therebefore. Note also that the heat exchanger tubular annulus is connected to onboard thermal control system. In compliance with the second version, the fuel tank supercharging system incorporates a heater representing the said multi-channel tubular-casing heat exchanger connected to the thermal control system with every pipe accommodating a displacer arranged along the pipe entire length. Note that every pipe of the said heat exchanger houses a displacer arranged over the entire pipe length to form a uniform circular gap in the annular channel between the pipe wall and displacer. Note here that the pipes represent coils and heat exchanger channels are connected into appropriate circuits of pneumatic lines behind the gas pressure control valves and throttling devices arranged therebefore. Note also that the heat exchanger tubular annulus is connected to onboard thermal control system.

EFFECT: higher efficiency and reliability provided for by ruling out creation of cold gas flows into fuel-and-oxidiser tanks.

2 cl, 2 dwg

Similar patents RU2341675C2

Title Year Author Number
FUEL TANK SUPERCHARGING SYSTEM 2006
  • Banin Viktor Nikitovich
  • Gorelikov Vladimir Ivanovich
  • Khitev Nikolaj Ivanovich
RU2339834C2
FUEL-TANK PRESSURISATION SYSTEM 2006
  • Banin Viktor Nikitovich
  • Gorelikov Vladimir Ivanovich
RU2339833C2
PRESSURIZATION SYSTEM FOR SPACECRAFT ENGINE PLANT PROPELLANT TANKS (FUEL TANKS AND OXIDIZER TANKS) 1998
  • Gorelikov V.I.
  • Sobolev V.M.
RU2143579C1
COMBINED PUMPING-DISPLACEMENT SYSTEM FOR FEED OF HYDROREACTIVE FUEL (HRF) LIQUID COMPONENTS TO CONSUMING HARDWARE 2014
  • Belchikov Andrej Valerevich
  • Savchenko Grigorij Borisovich
RU2582372C2
FUEL FEED SYSTEM 2006
  • Banin Viktor Nikitovich
  • Gorelikov Vladimir Ivanovich
RU2339832C2
FUEL FEED SYSTEM 2009
  • Banin Viktor Nikitovich
  • Gorelikov Vladimir Ivanovich
RU2407907C1
FUEL-TANK PRESSURISATION SYSTEM 2006
  • Banin Viktor Nikitovich
  • Gorelikov Vladimir Ivanovich
RU2339835C2
FUEL AND OXIDIZER TANK PRESSURIZATION SYSTEM OF SPACECRAFT ENGINE PLANT 1998
  • Gorelikov V.I.
  • Sobolev V.M.
RU2147344C1
PRESSURIZATION SYSTEM OF FUEL AND OXIDIZER TANKS OF SPACE FLYING VEHICLE ENGINE PLANT 1997
  • Gorelikov V.I.
RU2140003C1
PROPELLANT TANK (FUEL AND OXIDIZER TANKS) PRESSURIZATION SYSTEM OF SPACE-CRAFT ENGINE PLANT 1997
  • Gorelikov V.I.
  • Sarychev L.N.
RU2132477C1

RU 2 341 675 C2

Authors

Banin Viktor Nikitovich

Gorelikov Vladimir Ivanovich

Dates

2008-12-20Published

2006-05-26Filed