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Benny T Cheung

from Fremont, CA
Age ~50
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Also known as:
Benny C Cheung, Benny T Truong, Benny T Troung
Related to:
Ha To Truong, 63Julie TruongXay TruongTrang TruongVincent Nguyen, 53John Truong, 74
Connected to:
Adeline Cheung, 34Allen C Cheung, 47Angelica L Cheung, 32Anita J Cheung, 60Ava C Cheung, 57Barbara H Cheung, 75Beata Y Cheung, 45Catherine K Cheung, 42Cedric P Cheung, 50Celina W Cheung, 27

Benny Cheung Phones & Addresses

  • Fremont, CA
  • 2090 167Th Ave, San Leandro, CA 94578
  • 2347 20Th St, Oakland, CA 94601 (510) 434-1888
  • 17012 Robey Dr, Castro Valley, CA 94546
  • Alameda, CA
  • Las Vegas, NV
  • San Francisco, CA

Resumes

Resumes

Benny Cheung Photo 1

Chief Executive Officer - Self

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Location:
1536 La Mesa Dr, Burlingame, CA 94010
Industry:
E-Learning
Work:
Employed
Chief Executive Officer - Self
Languages:
English
Benny Cheung Photo 2

Benny Cheung

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Benny Cheung Photo 3

Dispatcher At Vta

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Position:
Dispatcher at VTA
Location:
San Francisco Bay Area
Industry:
Transportation/Trucking/Railroad
Work:
VTA
Dispatcher

Business Records

Name / Title
Company / Classification
Phones & Addresses
Benny Cheung
President
WENTWORTH PROPERTY MANAGEMENT, INC
Real Estate Agent/Manager · Real Estate Agents
383 Rhode Is St STE 101, San Francisco, CA 94103
(415) 255-8888
Benny Chin Kiu Cheung
Director
Shandong Swan USA, Inc
Real/personal Property
Benny Cheung
President
CHEUNG INVESTMENT GROUP, INC
383 Rhode Is St STE 200, San Francisco, CA 94103

Publications

Us Patents

System For Determining Aerodynamic Imbalance

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US Patent:
53520904, Oct 4, 1994
Filed:
Aug 7, 1992
Appl. No.:
7/926117
Inventors:
Gary B. Churchill - San Jose CA
Benny K. Cheung - San Francisco CA
Assignee:
The United States of America as represented by the Administrator of the
National Aeronautics and Space Administration - Washington DC
International Classification:
B64C 1100
US Classification:
416 61
Abstract:
A system is provided for determining tracking error in a propeller or rotor driven aircraft by determining differences in the aerodynamic loading on the propeller or rotor blades of the aircraft. The system includes a microphone disposed relative to the blades during the rotation thereof so as to receive separate pressure pulses produced by each of the blades during the passage thereof by the microphone. A low pass filter filters the output signal produced by the microphone, the low pass filter having an upper cut-off frequency set below the frequency at which the blades pass by the microphone. A sensor produces an output signal after each complete revolution of the blades, and a recording display device displays the outputs of the low pass filter and sensor so as to enable evaluation of the relative magnitudes of the pressure pulses produced by passage of the blades by the microphone during each complete revolution of the blades.
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Benny T Cheung from Fremont, CA, age ~50 Get Report