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
Title | Year | Author | Number |
---|---|---|---|
ICE EXHAUST GAS EJECTOR | 2022 |
|
RU2804988C1 |
VORTEX WIND-POWER PLANT | 1996 |
|
RU2093702C1 |
STRAIGHT-FLOW VORTEX EJECTOR WITH ROTATING CYCLONES | 2023 |
|
RU2823502C1 |
INTERNAL COMBUSTION ENGINE EXHAUST ACCELERATOR | 2006 |
|
RU2330165C2 |
EJECTION-VORTEX ENGINE | 2023 |
|
RU2827018C1 |
VORTEX GAS COMPRESSOR DEVICE FOR COMBINED AIR-JET ENGINE | 2019 |
|
RU2766496C2 |
GASIFIER FOR INTERNAL COMBUSTION ENGINE | 1993 |
|
RU2076231C1 |
RAMJET-EJECTOR ROCKET CARRIER | 2001 |
|
RU2181849C1 |
RAMJET LAUNCH VEHICLE | 1999 |
|
RU2150598C1 |
METHOD OF AND DEVICE FOR OPERATION OF RAMJET ENGINE | 2003 |
|
RU2264554C2 |
Authors
Dates
2015-04-20—Published
2014-01-22—Filed