FRANK Y.S. LIN
*** **** ****, *******, ** *****
Mobile 626-***-****
***********@*****.***
EDUCATION
Master of Science in Mechanical Engineering, Texas A&M University, College Station, Texas
EXPERIENCE
HARRIS RADAR SYSTEMS – VAN NNUYS, California 2016-2017
Sr. Mechanical Engineer
Packaged airborne (UAV) and ground based radar systems using Solidworks and ANSY to perform solid modeling, stress and thermal analyzes.
CRANE AEROSPACE - Burbank, California 2011-2015
Sr. Mechanical Engineer
Design aircraft seat actuation system using Soliddrworks and Cosmosworks to perform solid modeling, stress, vibration and coolingl analyses. Package motorized system and power supply module to include internal harness, PCB stacks, and sheet metal enclosure. Propose environmental and life cycle test for product validation.
Represent Engineering in MRB activities and review engineering change requests and returned units (NCR), perform failure investigation and formulate product improvement plan. Disposed parts in stock with MRP and parts tracking.
Designed injection molded parts, such as transducer housing and buttons support assembly for high volume, low cost production.
PRATT & WHITNEY ROCKETDYNE - Chatsworth, California 2008-2011
Sr. Mechanical Engineer
Used non-linear finite element analysis (ANSYS) to simulate temperature shock and validated interconnect components for sealing hot gas and cryogenic fluids; Prepared analysis and test reports on critical joints for PDR, CDR and document deliverables, Prepared cost/schedule/budget estimates, issued Statement Of Work for seal validation and leakage test,
Acted as the design focal for interconnect components, such as flanges, seals, specialty fasteners, and separable fittings, etc. Performed failure investigation on sealing related incidents for launch and hot fire test.
Developed company standard work (eSW) and analysis tools for designing heat exchanger and ancillary system components. Developed work instructions for selecting metallic and elastomer seal materials under extreme environments. Developed verification and validation work flow maps for interconnect components to support rocket engine certification.
SPACE VECTOR - Chatsworth, California 2004-2008
Sr. Mechanical Engineer
Developed components for air-launched spacecraft, including rocket engines, thrust vectoring devices, and cold gas control valves, Participated in engine hot firings, and testing of downcomer, cryogenic isolation valves.
As project lead in various programs to prepared technical proposals and presented in various design reviews. Developed proprietary electromechanical products such as cryogenic solenoid valve, non-explosive stage separation system, non-explosive isolation
valves, air launched vehicle restraint and release systems, vibration dampener for battery packaging.
Responsible for all engineering analyses to validated stress, dynamic and thermal designs; prepared formal analysis reports and deliverables for control fin, aft skirt, re-entry vehicle adapter, mobile missile erector/transporter, battery rack, GPS receiver and fuel tanks, e