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Sidney Xue Phones & Addresses

  • Houston, TX
  • Colleyville, TX
  • 315 Bristol Ct, Longmont, CO 80501 (303) 485-2033
  • 3837 Staghorn Dr, Longmont, CO 80503
  • Katy, TX
  • Pleasanton, CA
  • Euless, TX
  • Sunnyvale, CA
  • Fort Worth, TX

Work

Company: Wind turbine aeroacoustics consulting Jun 2012 Position: Aero-acoustics specialist

Education

Degree: Ph.D School / High School: University of Minnesota 1990 to 1994 Specialities: Aerospace Engineering

Skills

Fluid Dynamics • Wind Turbines • Aerodynamics • Turbines • Cfd • Wind Tunnel Testing • Wind • Aeroacoustics • Fluid Mechanics • Aerospace • Simulations • R&D • Acoustics • Structural Dynamics • Engineering • Turbulence

Industries

Renewables & Environment

Resumes

Resumes

Sidney Xue Photo 1

Aero-Acoustics Specialist

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Location:
Katy, TX
Industry:
Renewables & Environment
Work:
Wind Turbine Aeroacoustics Consulting since Jun 2012
Aero-Acoustics Specialist

Vestas Technology R&D Americas, Inc. Mar 2009 - May 2012
Principal engineer/Project technical lead

Bell Helicopter, Textron Feb 2003 - Feb 2009
Principal engineer

Maxtor Corporation 2000 - 2003
Senior Staff Engineer

Western Digitial 1996 - 2000
Principal engineer
Education:
University of Minnesota 1990 - 1994
Ph.D, Aerospace Engineering
Syracuse University 1987 - 1989
MS, Mechanical Engineering
Shanghai Jiao Tong University 1980 - 1984
BS, Power Machinary Engineering
Skills:
Fluid Dynamics
Wind Turbines
Aerodynamics
Turbines
Cfd
Wind Tunnel Testing
Wind
Aeroacoustics
Fluid Mechanics
Aerospace
Simulations
R&D
Acoustics
Structural Dynamics
Engineering
Turbulence

Business Records

Name / Title
Company / Classification
Phones & Addresses
Sidney Xue
Director
XY WORKS LLC
Nonclassifiable Establishments
27914 Iberville Gln Dr, Katy, TX 77494
Sidney Y. Xue
Director
GALE POWER SYSTEMS INC
6620 Sapphire Cir S, Colleyville, TX 76034
PO Box 21, Colleyville, TX 76034

Publications

Us Patents

Counter-Torque Device For A Helicopter

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US Patent:
8286908, Oct 16, 2012
Filed:
Jul 15, 2005
Appl. No.:
11/632421
Inventors:
John M. Kebrle - Dallas TX, US
Justin Daw - Fort Worth TX, US
Jim Hurdle - Fort Worth TX, US
Paul Sherrill - Grapevine TX, US
Jimmy C. Narramore - Bedford TX, US
Sidney Xue - Colleyville TX, US
Charles Hollimon - Fort Worth TX, US
Dudley Smith - Arlington TX, US
Bryce Docker - Arlington TX, US
John T. Brieger - Colleyville TX, US
Assignee:
Bell Helicopter Textron Inc. - Hurst TX
International Classification:
B64C 27/82
US Classification:
244 1719, 416203
Abstract:
A ducted fan for a helicopter includes a transverse duct and a counter-torque device supported within the duct. The counter-torque device includes a rotor rotatably mounted within the duct and a stator fixedly mounted within the duct downstream from the rotor. The rotor includes a rotor hub having a rotor axis, and rotor blades extending from the hub. The Rotor blades have a modulated angular distribution about the rotor axis. The stator includes a stator hub, and a plurality of stator vanes distributed around the stator hub. The stator vanes are angularly modulated around the stator hub.

Counter-Torque Device For A Helicopter

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US Patent:
8640984, Feb 4, 2014
Filed:
Aug 7, 2012
Appl. No.:
13/568262
Inventors:
John M. Kebrle - Dallas TX, US
James R. Andrews - Mansfield TX, US
Justin Daw - Fort Worth TX, US
Jim Hurdle - Fort Worth TX, US
Paul Sherrill - Grapevine TX, US
Jimmy C. Narramore - Bedford TX, US
Sidney Xue - Colleyville TX, US
Charles Hollimon - Forth Worth TX, US
Dudley Smith - Arlington TX, US
Bryce Docker - Arlington TX, US
John T. Brieger - Colleyville TX, US
Assignee:
Bell Helicopter Textron Inc. - Hurst TX
International Classification:
B64C 27/82
US Classification:
244 1719, 416203
Abstract:
A ducted fan for a helicopter includes a transverse duct and a counter-torque device supported within the duct. The counter-torque device includes a rotor rotatably mounted within the duct and a stator fixedly mounted within the duct downstream from the rotor. The rotor includes a rotor hub having a rotor axis, and rotor blades extending from the hub. The Rotor blades have a modulated angular distribution about the rotor axis. The stator includes a stator hub, and a plurality of stator vanes distributed around the stator hub. The stator vanes are angularly modulated around the stator hub.
Sidney Xue from Houston, TX Get Report