EXHAUST GAS VORTEX EJECTOR OF CARB AND DIESEL ENGINES Russian patent published in 2015 - IPC F01N1/08 F02B27/04 

Abstract RU 2548330 C1

FIELD: engines and pumps.

SUBSTANCE: vortex ejector comprises exhaust gas ejection booster, adapter sleeve and jet sleeve. Vortex chamber is composed of thin-wall hollow cone at vertex angle not exceeding 15 degrees arranged behind the adapter sleeve facing the exhaust gas flow and hollow conical cylinder. N lengthwise direct-flow plates are arranged between cone and hollow conical cylinder surfaces. Cross-section of flow channels changes from triangular to trapezoidal cross-section from cone vertex to its end. Ejector is composed by the end of thin-wall hollow cone, N flow channels and direct-flow circular channel composed of outer surfaces of hollow conical cylinder and air intake directed along the car motion. Spring blades are arranged at 30-60 degrees to the flow to make the lengthwise plates extension at the vortex chamber inlet. Exhaust gas inlet flow cross-section area and cross-sections of other functional elements are in the ratio of ~ 1:1.38:1.626:1.38. Jet chamber length and vortex chamber length and outlet diffuser length are in the ratio of ~ 1:1,2:0,4 mm. Through circular channel inlet cross-section and inlet exhaust gas flow cross-section as well as outlet diffuser convergence diameter and vortex chamber inlet cross-section are in the ratio of ~ 0,65:1.

EFFECT: higher wear resistance and reliability of brush seal, higher ICE efficiency, lower toxicity, fuel consumption and exhaust noise.

4 dwg

Similar patents RU2548330C1

Title Year Author Number
ICE EXHAUST GAS EJECTOR 2022
  • Vozisov Nikolaj Ivanovich
RU2804988C1
VORTEX WIND-POWER PLANT 1996
  • Serebrjakov Rudol'F Anatol'Evich
RU2093702C1
STRAIGHT-FLOW VORTEX EJECTOR WITH ROTATING CYCLONES 2023
  • Vozisov Nikolaj Ivanovich
RU2823502C1
INTERNAL COMBUSTION ENGINE EXHAUST ACCELERATOR 2006
  • Nikolaev Andrej Sergeevich
  • Ivanishchev Pavel Ivanovich
  • Velikanov Aleksej Viktorovich
RU2330165C2
EJECTION-VORTEX ENGINE 2023
  • Nippard Igor Viktorovich
RU2827018C1
VORTEX GAS COMPRESSOR DEVICE FOR COMBINED AIR-JET ENGINE 2019
  • Frolov Mikhail Petrovich
RU2766496C2
GASIFIER FOR INTERNAL COMBUSTION ENGINE 1993
  • Bulatov Anatolij Vasil'Evich
  • Bulatov Mikhail Anatol'Evich
RU2076231C1
RAMJET-EJECTOR ROCKET CARRIER 2001
  • Zemljakov N.V.
RU2181849C1
RAMJET LAUNCH VEHICLE 1999
  • Zemljakov N.V.
RU2150598C1
METHOD OF AND DEVICE FOR OPERATION OF RAMJET ENGINE 2003
  • Lebedenko I.S.
  • Lebedenko Ju.I.
  • Lebedenko V.I.
RU2264554C2

RU 2 548 330 C1

Authors

Serebrjakov Rudol'F Anatol'Evich

Dates

2015-04-20Published

2014-01-22Filed