LIQUID-PROPELLANT ENGINE CHAMBER Russian patent published in 2013 - IPC F02K9/52 

Abstract RU 2490505 C1

FIELD: engines and pumps.

SUBSTANCE: liquid-propellant engine chamber includes a regeneratively cooled combustion chamber with critical section and a nozzle, a mixing head including a housing, an oxidiser supply unit, mainly oxygen, main fuel supply unit, additional fuel supply unit and a fire bottom unit. In the above units there installed in concentric circles are coaxial uniaxial-jet injectors forming central and peripheral zones. The above coaxial uniaxial-jet injectors include a hollow tip attaching the oxidiser cavity to combustion zone, a sleeve enveloping the tip with a gap and attaching the cavity of the first fuel to combustion zone; in tips at least of injectors if the central zone in the outlet part there are radially located slots mad in the form of alternating projections and cavities. Radially located slots are made so that perimetre of central part of the jet part, which is restricted with beam generatrixes, is not more than 3s, and beam length is 2.3…2.5s, where s is beam thickness. Number of beams is equal to three; in the sleeve between projections of the tip there are channels, the outlet part of which opens to combustion zone made in the sleeve housing, and the inlet part is connected to the additional fuel cavity. The above cavity in the sleeve housing is connected through tangential channels to a annular groove made on the sleeve end and connected to combustion zone.

EFFECT: invention provides increased economy of an operating process at operation of a mixing head of the chamber.

6 dwg

Similar patents RU2490505C1

Title Year Author Number
LIQUID PROPELLANT ROCKET ENGINE 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
RU2497012C1
CHAMBER OF LIQUID-PROPELLANT ROCKET ENGINE 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
RU2493405C1
LIQUID PROPELLANT ROCKET ENGINE 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
  • Chernyshov Valerij Aleksandrovich
RU2493410C1
LIQUID-PROPELLANT ENGINE 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
  • Chernyshov Valerij Aleksandrovich
RU2490503C1
LIQUID-PROPELLANT ENGINE 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
  • Solzhenikin Pavel Anatol'Evich
RU2490506C1
MIXING HEAD OF LIQUID PROPELLANT ROCKET ENGINE CHAMBER 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
  • Solzhenikin Pavel Anatol'Evich
RU2493408C1
LIQUID-PROPELLANT ENGINE CHAMBER MIXING HEAD 2012
RU2490502C1
MIXING HEAD OF LIQUID ROCKET ENGINE CHAMBER 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
  • Solzhenikin Pavel Anatol'Evich
RU2498102C1
LIQUID-PROPELLANT ENGINE 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
  • Chernyshov Valerij Aleksandrovich
RU2490507C1
LIQUID PROPELLANT ROCKET ENGINE 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
  • Chernyshov Valerij Aleksandrovich
RU2493406C1

RU 2 490 505 C1

Authors

Chernichenko Vladimir Viktorovich

Shepelenko Vitalij Borisovich

Chernyshov Valerij Aleksandrovich

Dates

2013-08-20Published

2012-06-27Filed