COMBUSTION CHAMBER
FIELD: combustion chambers of turbo- jet engines; aircraft stationary gas-turbine plants. SUBSTANCE: proposed combustion chamber of gas-jet engine includes circular diffuser, casing, envelopes, flame tube and injectors. Outer wall of diffuser has closed circular cavity formed by load- bearing and pe...
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| creator | MNATSAKANJAN JU.S FEDOROV S.A ANDREEV A.V MARCHUKOV E.JU KUPRIK V.V LEBEDEV V.A KONOVALOVA L.P CHEPKIN V.M |
| description | FIELD: combustion chambers of turbo- jet engines; aircraft stationary gas-turbine plants. SUBSTANCE: proposed combustion chamber of gas-jet engine includes circular diffuser, casing, envelopes, flame tube and injectors. Outer wall of diffuser has closed circular cavity formed by load- bearing and perforated walls which are communicated with cavity of flow section of diffuser by various perforations. Perforated wall is made flush with diffuser profile and load-bearing wall is located at distance from it. EFFECT: enhanced operational stability. 3 cl, 4 dwg |
| format | Patent |
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SUBSTANCE: proposed combustion chamber of gas-jet engine includes circular diffuser, casing, envelopes, flame tube and injectors. Outer wall of diffuser has closed circular cavity formed by load- bearing and perforated walls which are communicated with cavity of flow section of diffuser by various perforations. Perforated wall is made flush with diffuser profile and load-bearing wall is located at distance from it. 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SUBSTANCE: proposed combustion chamber of gas-jet engine includes circular diffuser, casing, envelopes, flame tube and injectors. Outer wall of diffuser has closed circular cavity formed by load- bearing and perforated walls which are communicated with cavity of flow section of diffuser by various perforations. Perforated wall is made flush with diffuser profile and load-bearing wall is located at distance from it. EFFECT: enhanced operational stability. 3 cl, 4 dwg</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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| language | 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 | COMBUSTION CHAMBER |
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