Multi-fuseable shaft

Aeronautics and astronautics – Aircraft control

Patent

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Details

74665F, 74665G, 74665H, 464 32, 464 97, B64C 1324

Patent

active

049712675

ABSTRACT:
A fuseable torsion shaft for use within an aircraft flight control surface actuation system. The fuseable torsion shaft includes a shear tube which exhibits high strength elastic characteristics during normal operation up to a predetermined shear torque level. Thereafter, a torsion shaft having lower strength plastic characteristics provides torque transmission capability for a limited deflection.

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