Stabilizer for strengthening oil-gas mixing for ramjet engine
The invention provides a stabilizer for strengthening oil-gas mixing for a ramjet engine. The problem that an existing stabilizer cannot achieve reliable ignition and stable combustion under the low-temperature and low-pressure conditions is solved. The stabilizer comprises an annular evaporation pi...
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| creator | HUANG YUN SHI TENG CHEN KAITUO LIANG JUNLONG ZHOU JIE SONG YAHENG WANG YUQING MU YANG |
| description | The invention provides a stabilizer for strengthening oil-gas mixing for a ramjet engine. The problem that an existing stabilizer cannot achieve reliable ignition and stable combustion under the low-temperature and low-pressure conditions is solved. The stabilizer comprises an annular evaporation pipe and an annular turbulent flow body which are concentrically arranged. An annular protrusion is arranged on the front side wall of the annular evaporation pipe and provided with an annular fuel oil pipeline, and a fuel oil inlet is formed in the side wall of the annular protrusion. A plurality of air inlet pipes are arranged on the front side of the annular protrusion in the circumferential direction. Each air inlet pipe comprises an inner pipe body and an outer pipe body, an annular fuel oil liquid collecting cavity communicated with the annular fuel oil pipeline is formed between the inner pipe body and the outer pipe body, and an inner cavity of the inner pipe body is communicated with an inner cavity of the a |
| format | Patent |
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The problem that an existing stabilizer cannot achieve reliable ignition and stable combustion under the low-temperature and low-pressure conditions is solved. The stabilizer comprises an annular evaporation pipe and an annular turbulent flow body which are concentrically arranged. An annular protrusion is arranged on the front side wall of the annular evaporation pipe and provided with an annular fuel oil pipeline, and a fuel oil inlet is formed in the side wall of the annular protrusion. A plurality of air inlet pipes are arranged on the front side of the annular protrusion in the circumferential direction. 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The problem that an existing stabilizer cannot achieve reliable ignition and stable combustion under the low-temperature and low-pressure conditions is solved. The stabilizer comprises an annular evaporation pipe and an annular turbulent flow body which are concentrically arranged. An annular protrusion is arranged on the front side wall of the annular evaporation pipe and provided with an annular fuel oil pipeline, and a fuel oil inlet is formed in the side wall of the annular protrusion. A plurality of air inlet pipes are arranged on the front side of the annular protrusion in the circumferential direction. 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| language | chi ; eng |
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| subjects | BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | Stabilizer for strengthening oil-gas mixing for ramjet engine |
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