RU95121284A - LIQUID ROCKET ROCKET ENGINE - Google Patents

LIQUID ROCKET ROCKET ENGINE

Info

Publication number
RU95121284A
RU95121284A RU95121284/06A RU95121284A RU95121284A RU 95121284 A RU95121284 A RU 95121284A RU 95121284/06 A RU95121284/06 A RU 95121284/06A RU 95121284 A RU95121284 A RU 95121284A RU 95121284 A RU95121284 A RU 95121284A
Authority
RU
Russia
Prior art keywords
rocket
gas duct
combustion chamber
rods
engine
Prior art date
Application number
RU95121284/06A
Other languages
Russian (ru)
Other versions
RU2161263C2 (en
Inventor
В.Г. Чикалов
Г.М. Горелов
В.Н. Орлов
В.А. Барышевский
С.В. Михайлов
Original Assignee
Акционерное общество открытого типа "Самарский научно-технический комплекс "Двигатели НК"
Filing date
Publication date
Application filed by Акционерное общество открытого типа "Самарский научно-технический комплекс "Двигатели НК" filed Critical Акционерное общество открытого типа "Самарский научно-технический комплекс "Двигатели НК"
Priority to RU95121284/06A priority Critical patent/RU2161263C2/en
Priority claimed from RU95121284/06A external-priority patent/RU2161263C2/en
Publication of RU95121284A publication Critical patent/RU95121284A/en
Application granted granted Critical
Publication of RU2161263C2 publication Critical patent/RU2161263C2/en

Links

Claims (1)

Жидкостный ракетный двигатель с дожиганием, содержащий камеру сгорания с газоводом и опорными элементами на корпусе головки камеры, карданный шаровой подвес с неподвижным опорным конусом и полым подвижным, скрепленным с камерой сгорания, систему рулевых приводов качания двигателя с тягами, силовыми цилиндрами и кронштейнами для тяг, отличающийся тем, что, с целью повышения надежности, уменьшения массы и унификации камеры сгорания, газовод камеры расположен внутри подвижного опорного конуса, снабженного отверстием для прохода газовода и силовым фланцем, состыкованным с опорными элементами головки камеры, а кронштейны для подсоединения тяг рулевых приводов установлены в плоскостях качания на наружной поверхности подвижного опорного конуса.A post-combustion liquid propellant rocket engine containing a combustion chamber with a gas duct and supporting elements on the camera head housing, a cardan ball suspension with a fixed support cone and a hollow movable fastened with a combustion chamber, a system of steering gear drives for the engine with rods, power cylinders and brackets for rods, characterized in that, in order to increase reliability, reduce weight and unify the combustion chamber, the gas duct of the chamber is located inside the movable support cone, equipped with an opening for the passage of the gas duct and a power flange docked with the support elements of the camera head, and the brackets for connecting the tie rods of the steering drives are installed in the swing planes on the outer surface of the movable support cone.
RU95121284/06A 1995-12-19 1995-12-19 Liquid-propellant afterburner rocket engine RU2161263C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU95121284/06A RU2161263C2 (en) 1995-12-19 1995-12-19 Liquid-propellant afterburner rocket engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU95121284/06A RU2161263C2 (en) 1995-12-19 1995-12-19 Liquid-propellant afterburner rocket engine

Publications (2)

Publication Number Publication Date
RU95121284A true RU95121284A (en) 1997-12-20
RU2161263C2 RU2161263C2 (en) 2000-12-27

Family

ID=20174772

Family Applications (1)

Application Number Title Priority Date Filing Date
RU95121284/06A RU2161263C2 (en) 1995-12-19 1995-12-19 Liquid-propellant afterburner rocket engine

Country Status (1)

Country Link
RU (1) RU2161263C2 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2455515C1 (en) * 2011-04-04 2012-07-10 Николай Борисович Болотин Three-stage booster-rocket, liquid propellant rocket engine and roll nozzle block
RU2455514C1 (en) * 2011-04-04 2012-07-10 Николай Борисович Болотин Multistage booster-rocket, liquid propellant rocket engine and roll nozzle block
RU2458245C1 (en) * 2011-04-20 2012-08-10 Николай Борисович Болотин Liquid-propellant rocket engine and turbopump unit
RU2490508C1 (en) * 2012-04-24 2013-08-20 Открытое акционерное общество "Конструкторское бюро химавтоматики" Liquid-propellant engine with afterburning of generator gas
RU2556762C1 (en) * 2014-06-24 2015-07-20 Открытое Акционерное Общество "Кузнецов" Cardan suspension of liquid-fuel rocket engine
RU2703883C1 (en) * 2018-12-29 2019-10-22 Акционерное общество "НПО Энергомаш имени академика В.П. Глушко" Liquid rocket engine chamber rocking assembly with generator gas afterburning

Similar Documents

Publication Publication Date Title
IL101697A0 (en) Ring support for vectoring nozzle of gas turbine engine
RU95121284A (en) LIQUID ROCKET ROCKET ENGINE
FR2767356B1 (en) MIXING HEAD OF THE COMBUSTION CHAMBER OF A PROPERGOL LIQUID ROCKET ENGINE
IT1168988B (en) IMPROVEMENT SUPPLIED TO THE AIR INTAKES OF GAS TURBINE ENGINES MOUNTED ON AIRCRAFT
DE69715084D1 (en) Thrust reverser device of a jet engine with a wall part connected to the front of the flaps
RU96122836A (en) MULTI-STAGE TRANSPORT SYSTEM FOR SPACE FLIGHT AND HORIZONTAL STARTING METHOD
RU2161263C2 (en) Liquid-propellant afterburner rocket engine
BR9002946A (en) INJECTOR TO PROVIDE A FUEL AND AIR LOAD DIRECTLY INSIDE THE COMBUSTION CHAMBER OF AN ENGINE
JPH06107283A (en) Lower unit for ship propulsion device
RU95100182A (en) Rocket-propelled flying vehicle (versions) and rocket engine
FR2731471B1 (en) SOLID PROPERGOL ROCKET ENGINE WITH EXTERNAL COMBUSTION AND INTERNAL COMBUSTION PROPULSIVE CHARGES
RU2119081C1 (en) Engine for liquid-propellant rocket power plant
GB1224230A (en) Improvements in devices for coaxially securing a centrebody inside a hollow body
RU96121673A (en) ENGINE FOR ROCKET POWER PLANT OF LIQUID FUEL (OPTIONS)
RU96114396A (en) ACCELERATION UNIT
JPS6293131U (en)
GB2265184B (en) Gas turbine engine support structure
RU2002131694A (en) SOLID FUEL ROCKET ENGINE
SU1119926A1 (en) Ship
JPS6455881A (en) Dither mechanism of ring laser gyroscope
RU95111975A (en) RING COMBUSTION CAMERA OF A GAS-TURBINE ENGINE
RU95111720A (en) Launch pedestal for launch vehicle water surface start
RU2000111674A (en) ROCKET SOLID FUEL ENGINE INSTALLATION
RU96103923A (en) BIKALIBER CONTROLLED ROCKET
TH12960B (en) Exhaust with exhaust gas purification device