FIELD: engines and pumps.
SUBSTANCE: each of lengthwise walls is fitted between appropriate chamber bottom flanges and fairing. Lengthwise walls, chamber bottom and fairing are interconnected via multiple first fasteners, only between lengthwise walls and chamber bottom. That alternate with multiple second fasteners other than first fasteners, only between lengthwise walls and fairing. The number of first fasteners between lengthwise walls and chamber bottom correspond to that of second fasteners between lengthwise walls and fairing.
EFFECT: combustion chamber that features ease of assembly, sufficient flexibility and reliable tightening.
6 cl, 4 dwg
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| COMBUSTION CHAMBER OF GAS TURBINE ENGINE | 2006 |
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| GAS TURBINE ENGINE STRUCTURAL CARCASS AND GAS TURBINE ENGINE | 2009 |
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| AIR-FUEL MIXTURE SPRAY DEVICE, COMBUSTION CHAMBER AND GAS TURBINE ENGINE | 2007 |
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| EXTERNAL COVER OF AIR PIPE OF GAS-TURBINE ENGINE FAN | 2008 |
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RU2462601C2 |
