Engineer Manufacturing

PHILLIP M. KING

PO Box ***

BRISTOL, NH *****

Cell603-***-****

**********@*****.***

SUMMARY

Engineering professional with over thirty years of experience in both the aerospace and electronics industries, combining design skills with common sense to meet project objectives. Strong interpersonal skills allow quick integration into a team environment.

EMPLOYMENT HISTORY

Titeflex Aerospace, Laconia, New Hampshire 3/2011 to 11/6/2015

Senior CAD Designer/Applications Engineer

Designed product for production

Revised Drawings

Designed for prototype and final production release

Reviewed Job Quotes for Engineering Approval

Reviewed Orders submitted to the shop floor for Engineering Approval

Responded to Vendor Information Requests

Reviewed and designed Tooling

Submitted Engineering Design Changes

CAD-Unigraphics NX 8.5

Lehigh Technical, Long Island, New York 4/2010 to 2/25/2011

Manufacturing Engineer at ITT Fiber Innovations Walpole, Ma

Supported Operations of shop floor. Resin Transfer Molding of composite Jet Engine Parts.

Ordered parts and material to keep shop floor Operational.

Facilitated any issues with shop floor employees.

Worked with and supported (KOMO) Milling machine operator.

Maintained Resin Transfer equipment for composite aircraft parts.

Part Material Graphite Non-Metallic

Interfaced with vendors regarding service contracts.

Used power points and spreadsheet to discuss with management project goals.

Worked with RTM tooling for composite parts.

Programmed ovens with Thermal Profile.

CAD-CATIA 5.0

Butler America, Shelton, Connecticut 11/2009 to 3/2010

Structural Designer

Designed Structural composite Details for Helicopter.

Geometric Tolerance in 3D model.

Designed Metal parts-2024 Aluminum.

Prepared power points for Design review meetings.

CAD-CATIA 5.0

Comforce, Long Island, New York 08/2008 to 11/2009

Manufacturing Engineer at ITT Defense Amityville, New York

Concept Design of Major Composite Assembly Tooling for Sponson and Tail Rotor Pylon/Composite material

Designed Major Assembly Tooling.

Designed Structural Composite parts.

Tooling Material Steel AISI 1330 and Inconel.

Prepared Power Points for Major Assembly Tooling concept review.

CAD-CATIA

Butler International Shelton, Connecticut 09/2007 to 06/2008

Structural Designer

Structural Designer

Geometric Tolerance in 3D model.

Design details for Wing.

Part Material Non-Metalic

Designed Air passage skin for airframe.

CAD-CATIA

NorthropGrumman Bethpage, New York 11/2005 to 08/2007 Structural Designer

Designed Structural composite aircraft parts and used PDM Enovia.

Geometric Tolerance in 3D model.

Material of parts Titanium and Non-Metalic

Prepared power points for design review meeting

CAD-CATIA

Smiths Tubular systems Laconia, New Hampshire 4/2004 to 11/2005

CAD Designer

Designed Detail tubing for Jet Engines.

Designed Jigs & Fixtures for aircraft tubing

Materials 304 Stainless Steel, Titanium & Aluminum 2024

Geometric Tolerance in 2D

CAD-CATIA 5.0 and UNIGRAPHICS NX 6.0

IBM, Essex Junction, VT 1995 to 2004

Mechanical Designer

Designed Tooling & handling equipment for the microelectronics Manufacturing.

CAD-CATIA.

Grumman Bethpage, New York 11/1985 to 08/1995 Structural and Tool Designer

Designed Structural composite aircraft parts.

Designed tooling for part fabrication.

Geometric Tolerance in 3D model.

Material of parts Titanium and Non-Metalic

Metallurgical Department prepared specimens with Bakelite

Analyzed grain structure using acid etch and microscope

Used Rockwell Hardness and Brunel to determine tensile strength

CAD-CATIA

EDUCATION

Bachelors of Manufacturing Engineering Technology

State University of New York at Farmingdale, 1991

CAD/CAM AND COMPUTER EXPERIENCE

Proficient on CATIA 5.0

Proficient on Unigraphics NX 8.5

Proficient with Windows for text, data, and graphics processing.

REFERENCES AND ADDITIONAL INFO PROVIDED ON REQUEST

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