公开(公告)号：US20130239653A1

公开(公告)日：2013-09-19

申请号：US13792537

申请日：2013-03-11

Applicant: SNECMA

Inventor： Geoffroy NICQ ,  Valerio GEREZ

IPC: G01N3/30

CPC classification number: G01N3/30 ,  F01D21/003 ,  F01D21/14

Abstract: A method and an on-board system for detecting impact on an impeller wheel of an aircraft engine. Deflection signals representative of the deflections on the blades of the impeller wheel are acquired. Each of the deflection signals is correlated with a pulse signal typical of an impact on a sound blade at the rotation frequency of the engine, in order to identify impacts on the impeller wheel. The impact signals are extracted from among the deflection signals. The impact signals are transmitted to the ground in order that the signals are analysed to detect defects on the blades of the impeller wheel.

Abstract translation: 一种用于检测对飞机发动机的叶轮的冲击的方法和车载系统。 获得表示叶轮的叶片上的偏转的偏转信号。 每个偏转信号与典型的在发动机的旋转频率下对声音叶片的冲击的脉冲信号相关，以便识别对叶轮的影响。 从偏转信号中提取冲击信号。 撞击信号被传递到地面，以便分析信号以检测叶轮的叶片上的缺陷。

公开(公告)号：US20160178531A1

公开(公告)日：2016-06-23

申请号：US14900388

申请日：2014-06-20

Applicant: SNECMA

Inventor： Geoffroy NICQ

IPC: G01N21/88 ,  F01D21/00 ,  G01N21/21

CPC classification number: G01N21/8806 ,  B64C11/26 ,  B64D2027/005 ,  B64D2045/0085 ,  F01D21/003 ,  G01N21/21 ,  G01N2021/8848 ,  G01N2201/061 ,  G01N2201/0683 ,  G01N2201/08 ,  Y02T50/66

Abstract: The present description relates to a remote connection system suitable for being incorporated in an aircraft (1A, 1B, 1C) comprising at least one engine propeller (50A, 50B, 50C) having a plurality of blades (52A, 52B, 52C) suitable for rotating relative to a stationary module (10A, 10B, 10C) of the aircraft about an engine axis (X). The remote connection system comprises: a light emitter device configured, when the remote connection system is incorporated in the aircraft (1A, 1B, 1C), to emit a light beam that emerges to the outside of the propeller (50A, 50B, 50C), from at least one emission surface (54A, 54B, 54C) of said propeller (50A, 50B, 50C).

Abstract translation: 本说明书涉及一种适用于结合在飞行器（1A，1B，1C）中的远程连接系统，该飞机包括至少一个具有多个叶片（52A，52B，52C）的发动机推进器（50A，50B，50C） 相对于飞行器的关于发动机轴线（X）的固定模块（10A，10B，10C）旋转。 远程连接系统包括：发光器件，当远程连接系统被结合在飞行器（1A，1B，1C）中时，配置为发射出到螺旋桨外部的光束（50A，50B，50C） 来自所述螺旋桨（50A，50B，50C）的至少一个发射表面（54A，54B，54C）。

公开(公告)号：US20150315914A1

公开(公告)日：2015-11-05

申请号：US14650043

申请日：2013-12-03

Applicant: SNECMA

Inventor： Geoffroy NICQ

IPC: F01D5/10 ,  G01M1/32 ,  F16F15/34

CPC classification number: F01D5/10 ,  F01D5/027 ,  F16B1/0071 ,  F16F15/32 ,  F16F15/34 ,  G01M1/32 ,  Y02T50/671 ,  Y10T29/49334

Abstract: A method of balancing a turbine engine rotor, the method including mounting screws forming balance weights on the rotor in order to form a balance configuration, each screw possessing a predetermined weight and a screw head having a visual characteristic previously associated with its weight. A rotor balanced by such a method is also disclosed.

Abstract translation: 一种平衡涡轮发动机转子的方法，所述方法包括在转子上形成平衡重的螺钉，以形成平衡构型，每个螺钉具有预定的重量，以及具有先前与其重量相关联的视觉特性的螺钉头。 还公开了通过这种方法平衡的转子。