Search

Anna Wei

from San Diego, CA
Age ~61
Get Report
Also known as:
Anna Xin Wei, Xin Wei, Anna Yang, Wei U, Wei Xim
Related to:
Jenny Y LinJenny S Yang, 52Bill YangJui T Yang, 85
Connected to:
Adrienne W Wei, 45Alan C Wei, 39Albert K Wei, 44Angie Wei, 66Ann K Wei, 57Bob Wei, 66Danna Wei, 35Ellie Wei, 59En Wei, 67Evelyn J Wei, 35

Anna Wei Phones & Addresses

  • San Diego, CA
  • Folsom, CA
  • 16 Muriel Rd, Swampscott, MA 01907 (781) 599-9601
  • Sacramento, CA
  • 55 Broadlawn Park, Chestnut Hill, MA 02467
  • Milwaukee, WI
  • Chicago, IL

Resumes

Resumes

Anna Wei Photo 1

Senior Principal Engineer

View page
Location:
San Diego, CA
Industry:
Oil & Energy
Work:
Solar Turbines
Senior Principal Engineer
Education:
University of Arizona 1990 - 1995
Doctorates, Doctor of Philosophy, Engineering, Mechanical Engineering, Philosophy Tsinghua University 1984 - 1986
Masters, Engineering
Skills:
Finite Element Analysis
Gas Turbines
Engineering
Engineering Management
Root Cause Analysis
Ansys
Project Engineering
Mechanical Engineering
Turbomachinery
Anna Wei Photo 2

Anna Wei

View page

Business Records

Name / Title
Company / Classification
Phones & Addresses
Anna Xin Wei
Director
BROADVANTAGE, INCORPORATED
16 Muriel Rd, Swampscott, MA 01907

Publications

Us Patents

Methods And Apparatus For Reducing Vibrations Induced To Airfoils

View page
US Patent:
20070041841, Feb 22, 2007
Filed:
Aug 16, 2005
Appl. No.:
11/204718
Inventors:
Robert Walter - Melrose MA, US
David Christensen - Newbury MA, US
Caroline Granda - Concord MA, US
Jeffrey Nussbaum - Wilmington MA, US
Anna Wei - Swampscott MA, US
Michael Macrorie - Winchester MA, US
Tara Chaidez - Malden MA, US
International Classification:
B64C 27/46
US Classification:
41622300R
Abstract:
Methods and apparatus for fabricating a rotor blade for a gas turbine engine are provided. The rotor blade includes an airfoil having a first sidewall and a second sidewall, connected at a leading edge and at a trailing edge. The method includes forming the airfoil portion bounded by a root portion at a zero percent radial span and a tip portion at a one hundred percent radial span, the airfoil having a radial span dependent chord length C, a respective maximum thickness T, and a maximum thickness to chord length ratio (T/C ratio), forming the root portion having a first T/C ratio, forming the tip portion having a second T/C ratio, and forming a mid portion extending between a first radial span and a second radial span having a third T/C ratio, the third T/C ratio being less than the first T/C ratio and the second T/C ratio.
Control profile
Anna Wei from San Diego, CA, age ~61 Get Report