KENNETH D OLSON
Medical Practice at Dixie Hwy, West Palm Beach, FL
License number
Florida 511866
Issued Date
Oct 27, 2005
Effective Date
Jun 17, 2011
Expiration Date
Dec 1, 2010
Category
Health Care
Type
Emergency Medical Technician
Address
Address
500 N Dixie Hwy, West Palm Beach, FL 33401
Phone
(561) 804-4700
Personal information
See more information about KENNETH D OLSON at radaris.comName
Address
Phone
5 Shady Ln, Mary Esther, FL 32569
5400 Collins Lake Dr APT 110, Jacksonville, FL 32244
5524 Cord Grass Ln, Melbourne Bch, FL 32951
645 SW Wisper Bay Dr #SW, Palm City, FL 34990
5620 Collins Rd #103, Jacksonville, FL 32244
Professional information
See more information about KENNETH D OLSON at trustoria.com
Low Rotor Vibration Avoidance In Aircraft Gas Turbine Engines
Low Rotor Vibration Avoidance In Aircraft Gas Turbine Engines
US Patent:
5687564, Nov 18, 1997
Filed:
Dec 4, 1995
Appl. No.:
8/566846
Inventors:
James B. Kelly - Lake Worth FL
Kenneth D. Olson - Royal Palm Beach FL
Johnny B. Davis - Jupiter FL
Gerald Bracci - Tequesta FL
Kenneth D. Olson - Royal Palm Beach FL
Johnny B. Davis - Jupiter FL
Gerald Bracci - Tequesta FL
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
F02K 115
US Classification:
60235
Abstract:
Corrected fan speed (N1C2) and engine pressure ratio (EPR) are controlled, by controlling exhaust nozzle area (EA) according to a schedule or map so that as altitude increases (P2 decreases) the axial forces on the low rotor are sufficient to minimize low rotor vibrations. The altitude band (critical load region) is determined that produces loading levels in which vibrations appear. As this band is approached, conventional control of N1C2 and EPR is automatically over-ridden. N1C2 is decreased with altitude and exhaust area is reduced, thereby increasing the axial force (load) on the low rotor. When the upper limit of the band is reached, conventional control of N1C2 and EPR is automatically resumed, resulting in crossing the critical load region rapidly over a narrow altitude band.
Rotor Inlet Temperature Control For Turbo Machine
Rotor Inlet Temperature Control For Turbo Machine
US Patent:
6931857, Aug 23, 2005
Filed:
May 30, 2003
Appl. No.:
10/448900
Inventors:
Craig W. Irwin - Jupiter FL, US
Richard W. McBride - Palm Beach Gardens FL, US
Kenneth D. Olson - Royal Palm Beach FL, US
Carl F. Simmons - Palm Beach Gardens FL, US
Richard W. McBride - Palm Beach Gardens FL, US
Kenneth D. Olson - Royal Palm Beach FL, US
Carl F. Simmons - Palm Beach Gardens FL, US
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
G02C009/48
US Classification:
60773, 60 39281
Abstract:
A method of synthesizing rotor inlet temperature in a turbine comprising the steps of determining a burner fuel flow (WFGG), a burner inlet pressure (PS32), and a compressor discharge temperature (T3) of a turbine, calculating a ratio unit parameter from the burner fuel flow, the burner inlet pressure, and the compressor discharge temperature, and calculating a synthesized rotor inlet temperature from the ratio unit parameter.