BING TONG
Pilots at Seabreeze Farms Dr, San Diego, CA
License number
California A5236971
Issued Date
Mar 2015
Expiration Date
Mar 2016
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
12985 Seabreeze Farms Dr, San Diego, CA 92130
Personal information
See more information about BING TONG at radaris.comName
Address
Phone
12985 Seabreeze Farms Dr, San Diego, CA 92130
1801 39Th Ave, San Francisco, CA 94122
2027 Mayflower Pl, San Leandro, CA 94579
801 Franklin St APT 1104, Oakland, CA 94607
940 Cayuga Ave, San Francisco, CA 94112
Professional information
Chief Systems Engineer At Ht Engineering Company
Position:
Chief Systems Engineer at HT Engineering Company, Consultant at Company Confidential
Location:
Greater San Diego Area
Industry:
Aviation & Aerospace
Work:
HT Engineering Company
- Southern California since Jun 2012
-
Chief Systems Engineer
Company Confidential
since Jun 2010
-
Consultant
Hamilton Sundstrand
Jan 2002 - Jun 2010
-
Project and Systems Engineer
Pratt & Whitney
Jan 2001 - Dec 2001
-
Operability Engineer
Honeywell International
May 2000 - Dec 2000
-
Senior Project Engineer
Pratt & Whitney
Jan 1998 - May 1999
-
System Software Engineer
Honeywell
Jan 1996 - Jan 1999
-
Senior Project Engineer
Education:
Arizona State University 1995 - 1998
MS (to be), Electrical Engineering University of Baltimore 1990 - 1992
MBA, General Management Tianjin No. 20 Middle School
MS (to be), Electrical Engineering University of Baltimore 1990 - 1992
MBA, General Management Tianjin No. 20 Middle School
Skills:
Aerospace, Systems Engineering, DO-178B, Engineering Management, Avionics, Root Cause Analysis, Embedded Systems, Labview, Aircraft, Continuous Improvement, Matlab, Embedded Software, Program Management, Simulink
Interests:
PADI Certified Open Water Diver
USSA Captain in-training
Fixed-Wing Private Pilot in-training
Honor & Awards:
Holder of US Patent #7,559,696 - Active Thrust Management System
Main inventor of US Patent #8,245,517 - Gas Turbine Starting With Stepping Speed Control
Active Thrust Management System
US Patent:
2006004, Mar 2, 2006
Filed:
Aug 30, 2004
Appl. No.:
10/929803
Inventors:
Carlos Oncina - Ellensburg WA, US
Michael Mehrer - San Diego CA, US
Bing Tong - San Diego CA, US
Pete Suttie - San Diego CA, US
William Dornfield - San Diego CA, US
Michael Mehrer - San Diego CA, US
Bing Tong - San Diego CA, US
Pete Suttie - San Diego CA, US
William Dornfield - San Diego CA, US
International Classification:
F16C 32/06
US Classification:
384121000
Abstract:
An active thrust management system varies pressure responsive to changes in rotor assembly thrust to maintain a desired position. The system includes a bearing supporting rotation of a rotor assembly within a pressurizing chamber. The rotor assembly is supported on a cushion of air generated between the bearing and the rotor assembly. Pressure within a cavity adjacent the rotor assembly opposes a thrust force to maintain a desired position of the rotor assembly. Modulating airflow into the pressurizing chamber adjacent the rotor assembly compensates for changes in the thrust generated by the rotor assembly to maintain the desired rotor assembly position.
Gas Turbine Starting With Stepping Speed Control
US Patent:
8245517, Aug 21, 2012
Filed:
May 19, 2009
Appl. No.:
12/468390
Inventors:
Bing Tong - San Diego CA, US
Timothy J. Sullivan - La Mesa CA, US
Paul E. Hilgeman - Santee CA, US
Tarrence L. Mack - Santee CA, US
Timothy J. Sullivan - La Mesa CA, US
Paul E. Hilgeman - Santee CA, US
Tarrence L. Mack - Santee CA, US
Assignee:
Hamilton Sundstrand Corporation - Rockford IL
International Classification:
F02C 7/26
US Classification:
60778, 60786, 60787, 60788, 60772
Abstract:
The system and method of the present invention provides stepping speed control of a gas turbine engine to reliably light-off a gas turbine engine. During starting, the speed of the gas turbine engine is incremented by stepped amounts through the light-off window from a minimum speed value to a maximum speed value, with the speed of the gas turbine dwelling at each stepped value for a period of time before incrementing the speed of the engine to the next stepped level. If the gas turbine engine is stepped through the entire light-off window without success, the controller decreases the speed of the gas turbine engine to the minimum value and begins the process again. The process continues until successful light-off is initiated or until the light-off window is traversed a certain number of times, after which the start process is aborted.