首页>
外国专利>
CONSTANT-VOLUME COMBUSTON MODULE FOR A TURBINE ENGINE, COMPRISING COMMUNICATION-BASED IGNITION
CONSTANT-VOLUME COMBUSTON MODULE FOR A TURBINE ENGINE, COMPRISING COMMUNICATION-BASED IGNITION
展开▼
机译:涡轮机的恒定体积燃烧模块,包括基于通信的点火
展开▼
页面导航
摘要
著录项
相似文献
摘要
The invention relates to a turbine engine combustion module (10), in particular for an aircraft turbine engine, designed to carry out constant-volume combustion, comprising: at least two combustion chambers (12A, 12B) arranged about an axis, each chamber (12A, 12B, 12C) comprising a compressed gas intake port (16) and a burnt gas exhaust port (18); and an ignition means that triggers combustion in the combustion chambers (12A, 12B, 12C). The module (10) comprises at least one duct (80) which establishes a communication between a first combustion chamber (12A) and at least one second combustion chamber (12B) in order to inject burnt gases from the first combustion chamber (12A) into the second combustion chamber (12B) so as to trigger combustion in the second combustion chamber (12B).
展开▼