MR. THOMAS ANTHONY RICHARDSON, COTA
Restorative Service Providers at Keystone Xing, Indianapolis, IN
License number
Indiana 32001033A
Category
Restorative Service Providers
Type
Environmental Modification
Address
Address
2
8900 Keystone Xing STE 600, Indianapolis, IN 46240
9699 N Wanda Ct, Mooresville, IN 46158
9699 N Wanda Ct, Mooresville, IN 46158
Phone
(317) 218-0654
(317) 834-4929
(317) 834-4929
Professional information
Thomas Richardson - Mooresville, IN
Work:
Repustaff (FT)
COTA Select Rehab (PRN)
COTA Healthcare Therapy Services (PRN)
COTA Select Rehab Hospital (PRN)
COTA Aegis/Beverly Corporation (FT)
COTA Genesis Eldercare (PRN)
COTA VRS Rehab Services (PRN)
COTA OPS Quality Care (Outpatient Hand Clinic) (FT)
COTA Highland Occupational Therapy Rehab Services (Outpatient Hand Clinic) (FT)
COTA
COTA Select Rehab (PRN)
COTA Healthcare Therapy Services (PRN)
COTA Select Rehab Hospital (PRN)
COTA Aegis/Beverly Corporation (FT)
COTA Genesis Eldercare (PRN)
COTA VRS Rehab Services (PRN)
COTA OPS Quality Care (Outpatient Hand Clinic) (FT)
COTA Highland Occupational Therapy Rehab Services (Outpatient Hand Clinic) (FT)
COTA
Education:
Ivy Tech State College - Indianapolis, IN
Associates in Occupational Therapy Assistant
Associates in Occupational Therapy Assistant
Gas Turbine Engine And Fuel Injection System
US Patent:
2012019, Aug 9, 2012
Filed:
Dec 23, 2011
Appl. No.:
13/336276
Inventors:
Jushan Chin - Irvine CA, US
Nader K. Rizk - Carmel IN, US
Thomas Richardson - Indianapolis IN, US
Mohan K. Razdan - Indianapolis IN, US
Duane Smith - Carmel IN, US
Nader K. Rizk - Carmel IN, US
Thomas Richardson - Indianapolis IN, US
Mohan K. Razdan - Indianapolis IN, US
Duane Smith - Carmel IN, US
International Classification:
F23R 3/28
US Classification:
60738
Abstract:
One embodiment of the present invention is a unique gas turbine engine. Another embodiment is a unique fuel injection system for a gas turbine engine. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines and fuel injection systems for gas turbine engines. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.