JET ENGINE Russian patent published in 1999 - IPC

Abstract RU 2142570 C1

FIELD: aerospace equipment, solid-fuel jet engines. SUBSTANCE: technical object of invention consists in increased specific thrust pulse of engine, in increased power and simplification of design which are achieved thanks to manufacture of solid-fuel charge in jet engine that includes body, combustion chamber with solid-fuel charge and nozzle in the form of propellant grain. Central combustion chamber is formed in propellant grain in the form of conical recess, additional combustion chambers located in end face part of propellant grain are formed around central chamber. EFFECT: increased specific thrust pulse, increased power and simplification of design of engine. 4 cl, 2 dwg

Similar patents RU2142570C1

Title Year Author Number
REACTIVE PROPELLANT CELLS 1998
  • Nurmukhametov I.R.
RU2158837C2
SOLID-PROPELLANT JET ENGINE 1997
  • Nurmukhametov I.R.
RU2141571C1
POWDER ROCKET ENGINE 2000
  • Nurmukhametov I.R.
RU2195567C2
AIR-JET ENGINE 2000
  • Nurmukhametov I.R.
RU2243400C2
OPPOSED JET ENGINE 1998
  • Nurmukhametov I.R.
RU2151319C1
STAROVEROV'S CONICAL ROCKET ENGINE 8 (VERSIONS) AND METHOD OF ITS VERTICAL LAUNCHING (VERSIONS) 2013
  • Staroverov Nikolaj Evgen'Evich
RU2524793C1
ROCKET ENGINE OF SOLID FUEL 2018
  • Devyatkin Sergej Petrovich
RU2685751C1
METHOD OF STRAIGHT-AND-LEVEL FLAPPING FLIGHT 1996
RU2129506C1
WING 1998
  • Nurmukhametov I.R.
RU2147544C1
WINDMILL 1998
  • Nurmukhametov I.R.
RU2158848C2

RU 2 142 570 C1

Authors

Nurmukhametov I.R.

Dates

1999-12-10Published

1997-09-29Filed