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Chuong V Tran

from Burien, WA
Age ~64

Chuong Tran Phones & Addresses

  • 487 S 190Th St, Seattle, WA 98148 (206) 835-5686
  • 2917 Willow St, Seattle, WA 98108
  • Burien, WA
  • Kiona, WA
  • 1234 S 132Nd St, Burien, WA 98168

Work

Position: Executive, Administrative, and Managerial Occupations

Education

Degree: Associate degree or higher

Professional Records

Medicine Doctors

Chuong Tran Photo 1

Chuong T. Tran

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Specialties:
Internal Medicine
Work:
Sutter Pacific Medical FoundationSutter Pacific Medical Foundation Family Health Center
3801 Sacramento St STE 325, San Francisco, CA 94118
(415) 600-2402 (phone), (415) 369-1292 (fax)
Languages:
English
Spanish
Description:
Dr. Tran works in San Francisco, CA and specializes in Internal Medicine. Dr. Tran is affiliated with California Pacific Medical Center.

Resumes

Resumes

Chuong Tran Photo 2

Chuong Tran

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Location:
Seattle, WA
Industry:
Computer Software
Work:
Microsoft Corporations since Aug 2008
Supply Chain Ops. Manager
Education:
Walden University 2009 - 2012
Doctor of Business Administration, Global Supply Chain Management
APICS - CSCP 2010 - 2010
CSCP, Supply Chain Management
California State University-East Bay 2003 - 2005
MBA, Supply Chain Management and E-business
California State University-Sacramento 1998 - 2002
B.S, Management Information System
Skills:
Thailand
Consulting
Suppliers
International Sales
Demand Planning
Windows
Sales
Cost
Apics
Supply Chain Management
Agile Methodologies
Executive Positions
Business Administration
Production Environment
Contract Manufacturing
P&L Review
Production Teams
Australia
Singapore
Embedded Systems
Network Security
On Time Delivery
Cross Functional Team Leadership
Business Requirements
Product Management
Japan
Management
Revenue
Inventory Management
Science
Change Agent
Crm
Indesign
Leadership
Loan Servicing
Lean Manufacturing
Accounting
Sdlc
Quarter
Propose
Execution
Korea
Scorecard
Web Applications
Channel Partners
Forecasting
Customer Satisfaction
Production Planning
English
Team Leadership
Asia
Engineering
Highly Dedicated
Strategy
Inventory
Ecos
Operations Management
Corporations
Pricing Strategy
Implementation Strategies
Distributors
Enterprise Software
Sla
Baan
Taiwan
Engineering Change
Operational Excellence
Supply
Mobile Computing
Project Management
Product Development
Srm
Microsoft
Business Continuity Planning
Concepts
Professional Associations
Sap
Coordination
Indigenous
Accountability
Applications
Network Design
Business Analysis
Erp
Strategic Planning
Cost Savings
Stage
Values
Dell Computers
International Development
Major Accomplishments
Cscp
Social Influence
Bill of Materials
Business Intelligence
Project Planning
Sales Plan
Business Process Improvement
San Jose
Vietnamese
Flows
Sun Java
Engagement
Software Development Life Cycle
Jit
Servers
Cloud Computing
Technical Solutions
Linkedin
Pricing
Responsibility
Logistics Management
Internal Audit
Six Sigma
E Commerce
E Business
Distribution
International
Purchasing
Kpmg
Oracle Enterprise Manager
Operational Planning
Malaysia
Start Ups
Warehousing
Supplier Relationship Management
Vendor Management
Process Improvement
Materials
Software
Oracle
Pmi
San Francisco
Fulfillment Programs
Program Management
India
Business Process
Manufacturing
China
Oems
Onboarding
Platforms
Ecosystem
Budgets
Unlimited
Kaizen
Kanban
Problem Solving
Boms
Meetings
Mis
Supply Chain
Multilingual
Delivery
Mrp
Americas
Coordinated
Coordinate
Gaps
Interests:
Children
Education
Languages:
Vietnamese
English
Certifications:
Certified Supply Chain Professional (Cscp)
Project Management Professional
License Bntyv47K48Ws
License Ht7Vjcscp4W5
Chuong Tran Photo 3

Chuong Tran

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Location:
P/O Box 18003, Tucson, AZ
Industry:
Information Technology And Services
Work:
Ibm Jun 1, 2015 - Oct 2017
Software Engineer at Ibm
Education:
University of Arizona 2013 - 2014
Bachelors, Biology
University of Arizona 2003 - 2008
Bachelors, Bachelor of Science, Electrical Engineering
Pima Community College 2008 - 2008
Skills:
Testing
Linux
Storage
Engineering Support
Software Development
Shell Scripting
Unix
Nas
Network Attached Storage
Ras
Bash
Networking
Virtualization
Agile Methodologies
Software Engineering
Debugging
Xml
Switches
Integration
Javascript
Operating Systems
Databases
Hardware
Java
Aix
San
Computer Hardware
Interests:
Computers
Cars
Reading
Sports
Digital Photography
Health
Networking
Engine Swaps
Electronics
Outdoors
Education
Science and Technology
Paintball
Custom Built
Disaster and Humanitarian Relief
Home Storage Solutions
Career
Boating
Investing
Turbo Installation
Vehicle Maintenance
Languages:
English
Vietnamese
Certifications:
Emergency Medical Technician
Emergency Medical Care Technician (Emct)
National Registry of Emergency Medical Technicians
Arizona Department of Health Services
Chuong Tran Photo 4

Chuong Tran

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Location:
1906 Osprey Dr, Florence, SC 29501
Industry:
Design
Work:
Northeastern University
Teaching Assistant

Air Force Research Lab at Rome May 2016 - Aug 2016
Smart Scholar Research Scientist Intern

First Choice Health Jan 2015 - Sep 2015
Provider Information Specialist at First Choice Health

University of Washington Sep 2013 - Dec 2013
Student Researcher

The Aerospace Corporation Jun 2012 - Sep 2012
Laboratory Technician and Test Engineer
Education:
University of Washington 2010 - 2014
Bachelors, Mathematics, Biochemistry, Chemistry
Northeastern University
Masters, Mathematics, Computer Science
Skills:
Web Development
Web Design
Ui
Matlab
Data Analysis
Machine Learning
Labview
C++
Programming
Databases
Access
C
Engineering
Analysis
R
Laboratory
Cad
Research
Java
Program Management
Python
Experimentation
Testing
Spectroscopy
Nanotechnology
Physical Chemistry
Materials Science
Mathematical Modeling
Microsoft Office
Healthcare Industry
Healthcare Analytics
Microsoft Excel
Data Entry
Languages:
English
French
Chuong Tran Photo 5

Engineer At Boeing

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Location:
22118 41St Pl south, Kent, WA 98032
Industry:
Aviation & Aerospace
Work:
Boeing
Engineer at Boeing
Chuong Tran Photo 6

Chuong Tran

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Chuong Tran Photo 7

Chuong Tran

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Chuong Tran Photo 8

Chuong Tran

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Chuong Tran Photo 9

Chuong Tran

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Business Records

Name / Title
Company / Classification
Phones & Addresses
Chuong Tran
#1 BILLIARDS, LLC
Chuong Tran
Principal
Apex Hardwood Floor L L C
Floor Covering Stores · Ret Floor Covering
17429 34 Pl W, Lynnwood, WA 98037

Publications

Us Patents

Aircraft Multi-Axis Modal Suppression System

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US Patent:
6915989, Jul 12, 2005
Filed:
May 1, 2002
Appl. No.:
10/136907
Inventors:
Kioumars Najmabadi - Bellevue WA, US
Chuong B. Tran - Mukilteo WA, US
John Koon-Hung Ho - Shoreline WA, US
Assignee:
The Boeing Company - Seattle WA
International Classification:
B64C013/16
US Classification:
244195, 244177, 244 75 R
Abstract:
Vibrations due to excitation of the natural modes of an aircraft's body are suppressed by an active multi-axis modal suppression system. Dedicated sensors are positioned in the aircraft at optimal locations for sensing modal induced vibrations. The sensor produced signals are processed through control logic which, in response thereto, and in response to aircraft inertial, velocity and altitude related signals produces output control signals. The control signals effect control surface deployment creating forces to suppress the natural mode induced vibrations on multiple geometric axis's. More particularly, symmetric and anti-symmetric control surface deployments are used on one or more geometric axis's to damp lateral, longitudinal, vertical and most importantly torsional vibrational modes.

Aircraft Multi-Axis Modal Suppression System

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US Patent:
7191985, Mar 20, 2007
Filed:
Jul 12, 2005
Appl. No.:
11/180309
Inventors:
Kioumars Najmabadi - Bellevue WA, US
Chuong B. Tran - Mukilteo WA, US
John Koon-Hung Ho - Shoreline WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64C 13/16
US Classification:
244195, 244177, 244 751
Abstract:
Vibrations due to excitation of the natural modes of an aircraft's body are suppressed by an active multi-axis modal suppression system. Dedicated sensors are positioned in the aircraft at optimal locations for sensing modal induced vibrations. The sensor produced signals are processed through control logic which, in response thereto, and in response to aircraft inertial, velocity and altitude related signals produces output control signals. The control signals effect control surface deployment creating forces to suppress the natural mode induced vibrations on multiple geometric axis's. More particularly, a symmetric and anti-symmetric control surface deployments are used on one or more geometric axis'to damp lateral, longitudinal, vertical and most importantly torsional vibrational modes.

Aircraft Frequency Adaptive Modal Suppression System

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US Patent:
58606254, Jan 19, 1999
Filed:
Dec 30, 1996
Appl. No.:
8/827875
Inventors:
Chuong B. Tran - Lynnwood WA
Stephen White - Bothell WA
Assignee:
The Boeing Company - Seattle WA
International Classification:
B64C 1700
G05D 100
US Classification:
244195
Abstract:
An aircraft modal suppression system which recognizes that the frequency and phase of the body bending mode varies when the weight of the aircraft differs from the design gross weight. An active damper notch filter which is tabulated as a function of aircraft gross weight is utilized, thereby enabling not only the frequency, but also the width and depth of the notch filter to vary according to the gross weight of the aircraft.

Aircraft Frequency Adaptive Modal Suppression System

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US Patent:
54528658, Sep 26, 1995
Filed:
Jun 28, 1993
Appl. No.:
8/086447
Inventors:
Chuong B. Tran - Lynnwood WA
Stephen White - Bothell WA
Assignee:
The Boeing Company - Seattle WA
International Classification:
B64C 1316
G05D 100
G06G 770
US Classification:
244 75A
Abstract:
An aircraft modal suppression system which recognizes that the frequency and phase of the body bending mode varies when the weight of the aircraft differs from the design gross weight. An active damper notch filter which is tabulated as a function of aircraft gross weight is utilized, thereby enabling not only the frequency, but also the width and depth of the notch filter to vary according to the gross weight of the aircraft.

Aircraft Modal Suppression System

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US Patent:
50728938, Dec 17, 1991
Filed:
May 28, 1987
Appl. No.:
7/055801
Inventors:
Abhijit J. M. Chakravarty - Renton WA
Steven R. Cooper - Seattle WA
John K. H. Ho - Renton WA
Chuong B. Tran - Everett WA
Assignee:
The Boeing Company - Seattle WA
International Classification:
B64L 1316
US Classification:
244 76R
Abstract:
Accelerations due to excitation of the natural modes of an aircraft's body are suppressed by an active suppression system. Dedicated accelerometers are positioned in the aircraft at optimal locations for sensing modal induced lateral accelerations. The accelerometer produced signals are processed through control logic which, in response thereto, and in response to aircraft velocity and altitude related signals produces output control signals. The control signals effect rudder deployment creating forces to suppress the natural mode induced accelerations.

Aircraft Frequency Adaptive Modal Suppression System

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US Patent:
58331735, Nov 10, 1998
Filed:
Oct 8, 1996
Appl. No.:
8/731043
Inventors:
Chuong B. Tran - Lynnwood WA
Stephen White - Bothell WA
Assignee:
The Boeing Company - Seattle WA
International Classification:
B64C 1316
G05D 108
US Classification:
244 75A
Abstract:
An aircraft modal suppression system which recognizes that the frequency and phase of the body bending mode varies when the weight of the aircraft differs from the design gross weight. An active damper notch filter which is tabulated as a function of aircraft gross weight is utilized, thereby enabling not only the frequency, but also the width and depth of the notch filter to vary according to the gross weight of the aircraft.

Method And Apparatus For Turn Coordination Gain As A Function Of Flap Position

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US Patent:
58396977, Nov 24, 1998
Filed:
May 14, 1996
Appl. No.:
8/645616
Inventors:
Chuong B. Tran - Lynnwood WA
Assignee:
The Boeing Company - Seattle WA
International Classification:
G05D 108
US Classification:
244195
Abstract:
An improved method and apparatus for determining the amount of turn coordination gain in an aircraft yaw damper during a turn maneuver is disclosed. The yaw damper includes inputs from the inertial reference units of the aircraft and also from the flight management computer of the aircraft. The flight management computer provides to the yaw damper a signal indicative of the position of the flaps of the aircraft. The yaw damper includes a turn coordination gain box that receives the flap position signal and outputs a turn coordination gain value, dependent upon the flap position. Generally, the turn coordination gain value increases as the flap position is more extended. The precise turn coordination gain value for each flap position is dependent upon the particular aerodynamic characteristics of the aircraft.

Aircraft Frequency Adaptive Modal Suppression System

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US Patent:
56671660, Sep 16, 1997
Filed:
Feb 13, 1996
Appl. No.:
8/600779
Inventors:
Chuong B. Tran - Lynnwood WA
Stephen White - Bothell WA
Assignee:
The Boeing Company - Seattle WA
International Classification:
B64C 1300
B64C 1316
US Classification:
244 76C
Abstract:
An aircraft modal suppression system which recognizes that the frequency and phase of the body bending mode varies when the weight of the aircraft differs from the design gross weight. An active damper notch filter which is tabulated as a function of aircraft gross weight is utilized, thereby enabling not only the frequency, but also the width and depth of the notch filter to vary according to the gross weight of the aircraft.
Chuong V Tran from Burien, WA, age ~64 Get Report