Abstract: A mechanical load fuse assembly, particularly designed for lifting cables used with helicopters, consists of first and second end assemblies. An axial shear pin is releasably secured between the first and second end assemblies; and this shear pin is calibrated to have a breaking point of a pre-established amount when axial forces are applied to it. A protective sleeve is located over the shear pin between the first and second end assemblies when the shear pin is releasably secured. This protective sleeve has first and second positions of operation. A coil spring is used to normally bias the protective sleeve to the first position. In this position, radially projecting pins on the first and second end assemblies engage corresponding slots on the protective sleeve to prevent relative rotation of the first and second end assemblies relative to one another, so long as the sleeve is in the first position.

Abstract: In a NOTAR.TM. (No tail rotor) system for a helicopter, the addition of vortex generators in the longitudinal slots or nozzles which produce the circulation control portion of the system which combines with a jet thruster and fluid resource to replace the tail rotor.