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GYROSCOPIC LOADING [1 record]

Record 1 2008-03-18

English

Subject field(s)
  • Aircraft Propulsion Systems
  • Aircraft Piloting and Navigation
CONT

In conjunction with this damage was the observation that all engine fan blade sets also exhibited extremely severe localized rubbing on a small arc of blades sufficient to remove over a half inch of material length. Analysis of this damage concluded that it could only have occurred as gyroscopic loading as a result of a rapid change of axis of the engine centerlines while all four engines were spinning at high speed/power.

French

Domaine(s)
  • Propulsion des aéronefs
  • Pilotage et navigation aérienne
CONT

On rappelle que l'ensemble des aubages sont soumis : -à des sollicitations mécaniques : appui des gaz sur les aubages et les ailettes, force centrifuge sur les ailettes, effort gyroscopique sur les ailettes, vibrations liées au passage des gaz [...]

Spanish

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