发明授权
US09472026B2 Avionics method and device for monitoring a turbomachine at startup
有权
用于在起动时监测涡轮机的航空电子方法和装置
- 专利标题: Avionics method and device for monitoring a turbomachine at startup
- 专利标题(中): 用于在起动时监测涡轮机的航空电子方法和装置
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申请号: US14183820申请日: 2014-02-19
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公开(公告)号: US09472026B2公开(公告)日: 2016-10-18
- 发明人: Valerio Gerez , Serge Christian Joel Blanchard , Julien Alexis Louis Ricordeau
- 申请人: SNECMA
- 申请人地址: FR Paris
- 专利权人: SNECMA
- 当前专利权人: SNECMA
- 当前专利权人地址: FR Paris
- 代理机构: Oblon, McClelland, Maier & Neustadt, L.L.P.
- 优先权: FR1351421 20130220
- 主分类号: G06F19/00
- IPC分类号: G06F19/00 ; G07C5/00 ; F01D19/02 ; F01D21/06 ; F01D25/04
摘要:
A method of characterizing a turbine engine, the method comprising: steps of using measurements from an accelerometer monitoring a particular turbine engine while it is starting to detect the energy released by any contact during said starting between the rotor and the stator of the turbine engine, and of associating any such detection of contact with thermodynamic data measured on the particular turbine engine; and then a recognition training step, based on the associations, to enable a thermal context of the turbine engine to be used to recognize the presence of a rotor thermal unbalance to be taken into account in order to avoid contacts between the rotor and the stator on starting.
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