MARK STEPHEN WAGNER, MD
Osteopathic Medicine at Memorial Dr, Seneca, SC
License number
South Carolina 31391
Category
Osteopathic Medicine
Type
Internal Medicine
Address
Address
2
298 Memorial Dr, Seneca, SC 29672
1 Independence Pt STE 212, Greenville, SC 29615
1 Independence Pt STE 212, Greenville, SC 29615
Phone
(864) 885-7758
(864) 885-7749 (Fax)
(864) 797-6306
(864) 885-7749 (Fax)
(864) 797-6306
Professional information
Manager, New Product Systems At Ge
Position:
Manager, New Product Systems at GE
Location:
Greenville, South Carolina Area
Industry:
Mechanical or Industrial Engineering
Work:
GE
-
Manager, New Product Systems
Dr. Mark Wagner, Seneca SC - MD (Doctor of Medicine)
Specialties:
Internal Medicine
Address:
Oconee Hospitalists
298 Memorial Dr, Seneca 29672
(864) 885-7758 (Phone)
298 Memorial Dr, Seneca 29672
(864) 885-7758 (Phone)
Certifications:
Internal Medicine, 1987
Awards:
Healthgrades Honor Roll
Languages:
English
Hospitals:
Oconee Hospitalists
298 Memorial Dr, Seneca 29672
Musc Medical Center
169 Ashley Ave, Charleston 29425
298 Memorial Dr, Seneca 29672
Musc Medical Center
169 Ashley Ave, Charleston 29425
Education:
Medical School
University of Florida
Graduated: 1984
Rhode Island Hospital
University of Florida
Graduated: 1984
Rhode Island Hospital
Mark Stephen Wagner, Seneca SC
Specialties:
Internal Medicine, Hospitalist
Work:
Oconee Memorial Hospital
298 Memorial Dr, Seneca, SC 29672
298 Memorial Dr, Seneca, SC 29672
Education:
University of Florida (1984)
Turbomachine Configured To Burn Ash-Bearing Fuel Oils And Method Of Burning Ash-Bearing Fuel Oils In A Turbomachine
US Patent:
2013007, Mar 28, 2013
Filed:
Sep 23, 2011
Appl. No.:
13/242200
Inventors:
Mark Joseph Wagner - Greenville SC, US
Gunnar Leif Siden - Greenville SC, US
Ravi-Kumar Vipperla - Greenville SC, US
Gunnar Leif Siden - Greenville SC, US
Ravi-Kumar Vipperla - Greenville SC, US
Assignee:
GENERAL ELECTRIC COMPANY - Schenectady NY
International Classification:
F02C 3/24, F04D 29/70
US Classification:
60772, 60 39461, 4151212
Abstract:
According to one aspect of the exemplary embodiment, a turbomachine includes a compressor portion, a combustor fluidly connected to the compressor portion, and a turbine portion fluidly connected to the combustor portion and mechanically coupled to the compressor portion. The combustor portion is configured and disposed to burn ash-bearing fuel oils. The turbine portion includes a first stage having a first plurality of airfoils, and a second stage having a second plurality of airfoils. The first plurality of airfoils have a trailing edge discharge member. The second plurality of airfoils is clocked circumferentially relative to the first plurality of airfoils. The first plurality of airfoils are configured and disposed to direct an ash depleted flow upon corresponding adjacent ones of the second plurality of airfoils.