公开(公告)号：WO2010007277A9

公开(公告)日：2010-09-23

申请号：PCT/FR2009051158

申请日：2009-06-18

Applicant: SNECMA ,  GALIVEL JEAN-PIERRE

Inventor： GALIVEL JEAN-PIERRE

IPC: F01D21/00 ,  G01H1/00

CPC classification number: F01D21/003 ,  F05D2260/80 ,  F05D2270/44 ,  G01H1/006

Abstract: The invention relates to a method for determining the angular position of a first turbojet engine rotor, which consists in: generating at least one vibration while the first rotor is rotating, each vibration being generated as the first rotor passes through one and the same reference angular position; detecting the vibrations generated; obtaining (E30) the angular position at a given moment of a second rotor of the turbojet engine with respect to the angular position that it occupied at a reference instant representative of the detection of one of the vibrations, this second rotor being rotationally coupled to the first rotor and having a rotational speed different from that of the first rotor; and determining (E40), from the angular position of the second rotor, the angular position of the first rotor at this given instant.

Abstract translation: 本发明涉及一种用于确定第一涡轮喷气发动机转子的角位置的方法，该方法包括：在第一转子旋转时产生至少一个振动，当第一转子通过相同的参考角 位置; 检测产生的振动; 在涡轮喷气发动机的第二转子的给定时刻获得（E30）相对于其在代表振动之一的基准瞬间所占据的角位置的角位置，该第二转子被旋转地联接到 第一转子并具有不同于第一转子的转速; 以及从所述第二转子的角位置确定（E40）所述第一转子在该给定时刻的角位置。