COAXIAL SPRAY INJECTOR Russian patent published in 2013 - IPC F02K9/52 

Abstract RU 2481490 C1

FIELD: engines and pumps.

SUBSTANCE: coaxial spray injector includes a tubular housing with the main axial channel, which has an axial inlet and outlet, as well as a blind tube fixed at least on one pylon coaxially to the housing inside it, which is made as an integral part of the pylon and the tubular housing. At least one inlet through hole is made in the pylon, which is spread along the pylon from outer surface of the injector to the axial channel in the blind tube on the side of its blind end. Stepped change of the flow passage of the tubular housing is made so that the flow passage of the above housing reduces from pylons to the outlet part mainly in the form of one confuser. A sleeve is installed on the outlet part of the tubular housing so that an annular cavity, in which screw channels are arranged, is formed between outer surface of the above housing and inner surface of the sleeve. On the side of the axial inlet of the tubular housing there made is an adjustment element in the form of a chamfer provided with possibility of changing its geometrical parameters during adjustment. Tubular housing is split-type. On outer surface of the blind tube, which is arranged in outlet part of the tubular housing, there made are pylons interacting with their outer surface to inner surface of the tubular housing. Longitudinal axes of the above pylons are installed at an angle to longitudinal axis of the injector axis. Channels are made in the pylons, the inlet part of which is connected to the cavity of the blind tube, and the outlet part of which is connected to the annular cavity formed with the tubular housing and the blind tube. Blind tube is split-type and consists of a pylon part and a tip; at that, a jet nozzle is installed at their interface point; blind tube is fixed coaxially to the housing inside it on two radially directed pylons, which are equally spaced in a circumferential direction, inside each of which there arranged are two transverse inlet through holes relative to the injector axis, the tube is fixed inside the housing on two radially directed pylons, which are equally spaced in a circumferential direction, inside each of which there arranged are two transverse inlet through holes relative to the injector axis; injector is split-type and consists of two parts, inlet and outlet ones, which are tightly attached with a weld; the tubular housing is equipped at least with one annular swelling.

EFFECT: increasing the economy of the working process both at operation of the injector as three-component (oxygen-kerosene-hydrogen) and as two-component (oxygen-hydrogen).

4 cl, 3 dwg

Similar patents RU2481490C1

Title Year Author Number
METHOD FOR SUPPLYING FUEL COMPONENTS TO LIQUID-PROPELLANT ENGINE CHAMBER 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
RU2482320C1
METHOD FOR SUPPLYING FUEL COMPONENTS TO LIQUID-PROPELLANT ENGINE CHAMBER 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
RU2481492C1
METHOD FOR SUPPLYING FUEL COMPONENTS TO LIQUID-PROPELLANT ENGINE CHAMBER 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
RU2482317C1
MIXING HEAD OF LIQUID-PROPELLANT ENGINE CHAMBER 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
RU2481491C1
LIQUID-PROPELLANT ROCKET ENGINE MIXING CHAMBER 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
RU2479741C1
LIQUID-PROPELLANT ENGINE CHAMBER 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
RU2481485C1
METHOD FOR SUPPLYING FUEL COMPONENTS TO LIQUID-PROPELLANT ENGINE CHAMBER 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
RU2482319C1
METHOD FOR SUPPLYING FUEL COMPONENTS TO LIQUID-PROPELLANT ENGINE CHAMBER 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
RU2481493C1
METHOD FOR SUPPLYING FUEL COMPONENTS TO LIQUID-PROPELLANT ENGINE CHAMBER 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
RU2481494C1
LIQUID-PROPELLANT ROCKET ENGINE COMBUSTION CHAMBER 2012
  • Chernichenko Vladimir Viktorovich
  • Shepelenko Vitalij Borisovich
RU2479740C1

RU 2 481 490 C1

Authors

Chernichenko Vladimir Viktorovich

Shepelenko Vitalij Borisovich

Dates

2013-05-10Published

2012-03-15Filed