基本信息:
- 专利标题： 터빈엔진 시동방법
- 专利标题（英）：Method for starting a turbomachine
- 专利标题（中）：启动涡轮机的方法
- 申请号：KR1020137019498 申请日：2012-01-03
- 公开(公告)号：KR1020140008330A 公开(公告)日：2014-01-21
- 发明人： 베르디에,휴버트,파스칼 , 에쉐파레,필리페 , 쥐랄트,피에르 , 레베르가,루크
- 申请人： 사프란 헬리콥터 엔진스
- 申请人地址： F-***** Bordes, France
- 专利权人： 사프란 헬리콥터 엔진스
- 当前专利权人： 사프란 헬리콥터 엔진스
- 当前专利权人地址： F-***** Bordes, France
- 代理人： 김윤배; 이상목; 강철중
- 优先权： FR1150206 2011-01-11
- 国际申请： PCT/FR2012/050005 2012-01-03
- 国际公布： WO2012095590 2012-07-19
- 主分类号： F02C7/262
- IPC分类号： F02C7/262 ; F02C7/26
The present invention relates to a turbine engine start-up procedure. It is characterized attempting step to the fact that further comprising, re-present invention the shaft is re-performed in the case the first set when it reaches the speed value is not the main injectors do not ignition attempt step is: the starter and the ignition is stopped stopping step (S210) during which; The ignition device is activated while the fuel is injected into the combustion chamber, the rotational speed of the shaft, both when it reaches the second predetermined speed value, the second the second ignition phase the ignition step is carried out (S230): and to drive to rotate the shaft It consists of a second start-up phase during which the starter is working once more.
公开/授权文献:
- KR101895642B1 터빈엔진 시동방법 公开/授权日：2018-10-04