Method of monitoring a mount system for an aircraft engine

Details Method of monitoring a mount system for an aircraft engine Method of monitoring a mount system for an aircraft engine

1990-01-31

1991-02-12

Raevis, Robert

Measuring and testing

Simulating operating condition

Marine

G01M 1500

Patent

active

049914316

ABSTRACT:
A method of monitoring a mount system for an aircraft propulsion turbo-prop engine including the steps of dynamically measuring the fraction of output shaft torque being reacted by a selected one of the mount elements of the mount system and comparing the dynamically measured fraction with a predetermined fraction for the selected mount element corresponding to normal operation of the mount system. Variation between dynamic fraction and the predetermined fraction indicates a change of load distribution between the mount elements of the mount system.

REFERENCES:
patent: 3135487 (1964-06-01), Kottsieper
patent: 3288404 (1966-11-01), Schmidt et al.
patent: 3764098 (1973-10-01), Dickinson

Affiliated with

Also associated with

Rating

Method of monitoring a mount system for an aircraft engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method of monitoring a mount system for an aircraft engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method of monitoring a mount system for an aircraft engine will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-12806