An arm restraint assembly configured to pierce a canopy in response to expulsion of an ejection seat from a cockpit may comprise a primary arm configured to pivot relative to the ejection seat. A canopy piercer may be coupled to the primary arm. The primary arm may be configured to rotate to a fully-deployed position while located within the cockpit. An apex of the canopy piercer may be oriented toward the canopy, when the primary arm is in the fully-deployed position.
Collins Aerospace
Engineering Manager
Utc Aerospace Systems Nov 2012 - Jun 2017
Design Engineer Actuation Systems
Sikorsky Aircraft Apr 2008 - Nov 2012
Senior Mechanical Engineer
Goodrich Sep 2006 - Apr 2008
Lead Mechanical Engineer
General Dynamics Armament and Technical Sep 2004 - Jan 2006
Associate Testing and Design Engineer
Education:
University of New Haven 2010 - 2012
Master of Business Administration, Masters
Drexel University 2003 - 2003
Bachelors, Bachelor of Science, Mechanical Engineering
Champlain Valley Uhsd #15