发明名称 |
GAS TURBINE ENGINE AFTERBURNER CHAMBER |
摘要 |
FIELD: engines and pumps. ^ SUBSTANCE: proposed afterburner chamber comprises outlet channel with its rear accommodating invariable-cross section outer nozzle, flame stabiliser arranged inside channel front part and fuel nozzle arranged inside flame stabiliser to inject fuel therein. Afterburner chamber incorporates also inner ablation nozzle that makes a protective enclosure for outer nozzle and contains combustible material to be fired in afterburner operation. ^ EFFECT: simplified design of afterburner for supersonic flight. ^ 9 cl, 5 dwg |
申请公布号 |
RU2382894(C2) |
申请公布日期 |
2010.02.27 |
申请号 |
RU20050106776 |
申请日期 |
2005.03.09 |
申请人 |
DZHENERAL EHLEKTRIK KOMPANI |
发明人 |
KOSHOFFER DZHON MAJKL;L'JUIS REHNDI LI |
分类号 |
F02K1/06;F02K1/82;F02K3/10;F02K9/10;F02K9/97;F23M5/00;F23R3/20 |
主分类号 |
F02K1/06 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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