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NASA NTRS ยท 19940000344

Releasable High-Mechanical-Advantage Linear Actuator

Abstract

Proposed linear actuator includes ball-screw mechanism made to engage or disengage piston as needed. Requires low power to maintain release and no power to maintain engagement. Pins sliding radially in solenoids in yoke engage or disengage slot in piston. With help of optoelectronic feedback, yoke made to follow free piston during disengagement so always in position to "grab" piston.

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BibTeXRIS

Young, Gordon H.. 1994-06-01. Releasable High-Mechanical-Advantage Linear Actuator. https://ntrs.nasa.gov/citations/19940000344

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