Synchronous signal generator for trim balancing of jet engine

Details Synchronous signal generator for trim balancing of jet engine Synchronous signal generator for trim balancing of jet engine

G - Physics

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M

G01M 1/02 (2006.01) F01D 5/10 (2006.01) G01M 15/14 (2006.01) F16F 15/28 (2006.01) G01M 1/16 (2006.01)

Patent

CA 2636407

A synchronous signal generator (80) is provided for use in conjunction with an aircraft engine (20) having a spool (46) and an engine output shaft (66) driven by the spool (46). The synchronous signal generator includes a generator housing (82), a generator output member (86) rotatably mounted in the generator housing, a once-per- revolution timing mark (98) on the generator output member, and conversion gearing (84) disposed within the generator housing and configured to couple the engine output shaft to the generator output member. The conversion gearing rotates the generator output member at substantially the same rotational frequency as the spool when the conversion gearing is coupled to the engine output shaft.

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