Objective:

To obtain the performance test and analysis of the Gas Turbine Engine as

the assistant engineering or etc.

Education:

Newton International College, Computer Applications Courses

(2008.7~present, Garden Grove, CA)

Grace Mission University, Christian Education Master Course

(2006.8~2008.7, Fullerton, CA)

California State Fullerton University American Language Program,

(2006.3~11, Fullerton, CA)

Korea Chosun University Master Degree of Aerospace Engineering

Department (2002.2, Gwangju, Korea)

Experience in USA:

< Surveillance System(Cables, PC-DVR system assembly, installation

and Network setup)

< Samsung Digital Camera A/S and Computer Repair

Gas Turbine Engineering Experience in Korea:

( Hybrid propulsion system: Gas Turbine Engine (A250-C18) Performance

Test for UAV's Propulsion System(tilting rotors) Development Project-

KARI (Korea Aerospace Research Institute) 09/02~07/05

< Tested the engine performance, and operated the propulsion system

integration test (engine, propellers, system control operator) on

the ground condition

< Tested the load power by adjusting the propellers rpm and checked

the data (turbine inlet temp., fuel consumption, pressures and

etc.) for analyzing the gas turbine engine performance

< Performed the propulsion system certification check for the flight

tests

< Performed the real time data analysis of propulsion systems for

flying the UAV and after returning the ground field

< Maintained and found the propulsion system fault cause (FTA: Fault

Tree Analysis)

< Rechecked the engine performance with Software Program (GSP 10,

Gas Turbo with maps)

( Gas Turbine Performance Program Development Project

ADD (Agency for Defense Development)

03/00~07/02

< Gas turbine Engine(PT6A-62) performance program upgrade for Korea

Trainer Aircraft Engine, studied the output and tested data

( Compressor and gas turbine engine performance improvement with using

Moisture -RSC

03/00~12/02

< Developed MAT (Moisture Air Turbine) cycle diagram for Free-shaft

gas turbine engine.

< Developed the performance program for MAT

< Modeled computer simulation of thermodynamic cycles for rubber

engine

< Tested the small gas turbine engine(P9005) for MAT system

application

( Reverse Brayton Thermal Cycle Engine Study (Osaka Prefecture

University, Aerospace

propulsion engineering, Japan)

01/00~08/00

( Centrifugal Compressor Performance Test field Education for Turbo

Compressor

(Samsung Techwin) 12/99~01/00

Related Skills:

( Computer Programming: Basic Understanding of C++ and FORTRAN, expert

using of GSP10, Gas Turbo program ( Software: Engineer Computer Design,

Lab view, Origin, Microsoft PowerPoint, and Word ( Hardware: Computer

Assembly, Security system management & maintenance

Leadership:

Project Director - Gas turbine lab. Of Chosun University, Korea (01

~02),

Managed and arranged the job schedules for developing the propulsion

system with the association company

Led meetings, events, and conducted the university campus service

outreaches

Honors / Involvement / Community Service:

BK21 (Brain Korea) scholarship (Jan. 00 ~ Aug. 02)

New Life Mission Church (Presbyterians) Fullerton

Korean-American Aerospace Scientists Association (KASA) Member

Korean Society of propulsion Engineers Member

Korean Society for Aeronautical & Space Sciences Member

EGT (Easy Gas Turbine) R&D Co., Ltd. (Korea) cooperation Member

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