CHRIS CAMPBELL, MD
Anesthesiologist Assistant at Kingsley Ave, Orange Park, FL
License number
Florida ME49692
Category
Osteopathic Medicine
Type
Anesthesiology
Address
Address
2
1665 Kingsley Ave SUITE 105, Orange Park, FL 32073
PO Box 850001, Orlando, FL 32885
PO Box 850001, Orlando, FL 32885
Phone
(904) 215-7015
Personal information
See more information about CHRIS CAMPBELL at radaris.comName
Address
Phone
4510 New Dawn Ct, Lutz, FL 33558
4875 Augusta Ave, Oldsmar, FL 34677
417 SE 14Th St, Dania, FL 33004
48 Plantation Dr, Vero Beach, FL 32966
539 Shady Pine Way APT B2, Greenacres, FL 33415
Organization information
See more information about CHRIS CAMPBELL at bizstanding.comChris Campbell MD
2021 Kingsley Ave, Orange Park, FL 32073
Industry:
Anesthesiology
Phone:
(904) 276-5400 (Phone)
Chris John Campbell
Professional information
Digital Media Specialist, Dyna Interactive
Position:
Owner - Deisgner, Developer at Dyna Interactive
Location:
Orlando, Florida
Industry:
Online Media
Work:
Dyna Interactive
- Orlando, FL since Jan 2002
-
Owner - Deisgner, Developer
GMD Studios
Nov 2006 - Feb 2011
-
Production Supervisor
Premiere Trade
Apr 2006 - Nov 2006
-
Web Developer
MindComet
- Maitland, FL Aug 2005 - Apr 2006
-
Production Assistant
Education:
University of Central Florida 2002 - 2006
Digital Media, Internet & Interactive Systems West Orange High School 1998 - 2002
Digital Media, Internet & Interactive Systems West Orange High School 1998 - 2002
Skills:
Wordpress, HTML, CSS, CSS3, jQuery, PHP, MySQL, Graphic Design, Web Design, Web Development, Brand Development, Blogging, Social Media Marketing, XHTML
Interests:
UCF Sports, Orlando Magic, Golf, Apple, and my DVR!
Creative Director At Diversitile Custom Clothing Llc
Position:
Creative Director at Diversitile Custom Clothing LLC, Owner at Diversitile Custom Clothing
Location:
Orlando, Florida Area
Industry:
Apparel & Fashion
Work:
Diversitile Custom Clothing LLC
- Orlando, Florida Area since Jan 2010
-
Creative Director
Diversitile Custom Clothing
since Jan 2009
-
Owner
Education:
UCF 2006 - 2008
Bachelor of Art, Animation University of Central Florida 2005 - 2008
BFA, Animation
Bachelor of Art, Animation University of Central Florida 2005 - 2008
BFA, Animation
Skills:
Fine Artist, Musician, Creative Direction, Illustration, Logo Design, Graphic Design, Digital Illustration
Dr. Chris Campbell, Orange Park FL - MD (Doctor of Medicine)
Specialties:
Anesthesiology
Address:
Anesthesia Associates
2001 Kingsley Ave, Orange Park 32073
(904) 276-5400 (Phone)
2001 Kingsley Ave, Orange Park 32073
(904) 276-5400 (Phone)
Languages:
English
Education:
Medical School
Pennsylvania State University College Of Medicine
Graduated: 1985
Pennsylvania State University College Of Medicine
Graduated: 1985
Owner At Carpet
Position:
owner at carpet
Location:
Orlando, Florida Area
Industry:
Construction
Work:
carpet
-
owner
Ceramic Matrix Composite Gas Turbine Vane
US Patent:
6709230, Mar 23, 2004
Filed:
May 31, 2002
Appl. No.:
10/158946
Inventors:
Jay A. Morrison - Ovledo FL
Chris Campbell - Orlando FL
Gary Brian Merrill - Orlando FL
Jay Edgar Lane - Murrysville PA
Daniel George Thompson - Pittsburgh PA
Harry A. Albrecht - Hobe Sound FL
Yevgeniy P. Shteyman - West Palm Beach FL
Chris Campbell - Orlando FL
Gary Brian Merrill - Orlando FL
Jay Edgar Lane - Murrysville PA
Daniel George Thompson - Pittsburgh PA
Harry A. Albrecht - Hobe Sound FL
Yevgeniy P. Shteyman - West Palm Beach FL
Assignee:
Siemens Westinghouse Power Corporation - Orlando FL
International Classification:
F01D 904
US Classification:
415115, 415200, 416 97 R, 416 97 A, 416229 A, 416224, 416241 B
Abstract:
A hybrid vane ( ) for a gas turbine engine having a ceramic matrix composite (CMC) airfoil member ( ) bonded to a substantially solid core member ( ). The airfoil member and core member are cooled by a cooling fluid ( ) passing through cooling passages ( ) formed in the core member. The airfoil member is cooled by conductive heat transfer through the bond (( ) between the core member and the airfoil member and by convective heat transfer at the surface directly exposed to the cooling fluid. A layer of insulation ( ) bonded to the external surface of the airfoil member provides both the desired outer aerodynamic contour and reduces the amount of cooling fluid required to maintain the structural integrity of the airfoil member. Each member of the hybrid vane is formulated to have a coefficient of thermal expansion and elastic modulus that will minimize thermal stress during fabrication and during turbine engine operation.
Catalyst Element Having A Thermal Barrier Coating As The Catalyst Substrate
US Patent:
7371352, May 13, 2008
Filed:
May 30, 2002
Appl. No.:
10/158372
Inventors:
Chris Campbell - Orlando FL, US
Ramesh Subramanian - Oviedo FL, US
Andrew Jeremiah Burns - Orlando FL, US
Ramesh Subramanian - Oviedo FL, US
Andrew Jeremiah Burns - Orlando FL, US
Assignee:
Siemens Power Generation, Inc. - Orlando FL
International Classification:
B01D 50/00, B32B 18/00
US Classification:
422177, 428325, 428335
Abstract:
A combustion catalyst coating () applied to the surface of a ceramic thermal barrier coating () which is supported by a metal substrate (). The microstructure of the thermal barrier coating surface provides the necessary turbulent flow and surface area for interaction of the catalyst and a fuel-air mixture in a catalytic combustor of a gas turbine engine. The temperature gradient developed across the thermal barrier coating protects the underlying metal substrate from a high temperature combustion process occurring at the catalyst surface. The thermal barrier coating deposition process may be controlled to form a microstructure having at least one feature suitable to interdict a flow of fuel-air mixture and cause the flow to become more turbulent than if such feature did not exist.
Method Of Forming A Catalyst Element Having A Thermal Barrier Coating As The Catalyst Substrate
US Patent:
7691341, Apr 6, 2010
Filed:
Apr 8, 2008
Appl. No.:
12/099280
Inventors:
Chris Campbell - Orlando FL, US
Andrew J. Burns - Orlando FL, US
Ramesh Subramanian - Oviedo FL, US
Andrew J. Burns - Orlando FL, US
Ramesh Subramanian - Oviedo FL, US
Assignee:
Siemens Energy, Inc. - Orlando FL
International Classification:
B01D 50/00, B32B 18/00
US Classification:
422177, 428335
Abstract:
A combustion catalyst coating () applied to the surface of a ceramic thermal barrier coating () which is supported by a metal substrate (). The microstructure of the thermal barrier coating surface provides the necessary turbulent flow and surface area for interaction of the catalyst and a fuel-air mixture in a catalytic combustor of a gas turbine engine. The temperature gradient developed across the thermal barrier coating protects the underlying metal substrate from a high temperature combustion process occurring at the catalyst surface. The thermal barrier coating deposition process may be controlled to form a microstructure having at least one feature suitable to interdict a flow of fuel-air mixture and cause the flow to become more turbulent than if such feature did not exist.
High Temperature Insulation With Enhanced Abradability
US Patent:
2008027, Nov 6, 2008
Filed:
Dec 1, 2006
Appl. No.:
11/607344
Inventors:
Gary B. Merrill - Orlando FL, US
Jay E. Lane - Mims FL, US
Chris Campbell - Orlando FL, US
Jay A. Morrison - Oviedo FL, US
Jay E. Lane - Mims FL, US
Chris Campbell - Orlando FL, US
Jay A. Morrison - Oviedo FL, US
International Classification:
B32B 3/02, B32B 5/16, B32B 3/30, B32B 3/28, B32B 3/00, C23C 14/30
US Classification:
428168, 428172, 4283133, 427596
Abstract:
A enhanced abradable friable graded insulator FGI results from the laser patterning of a coating where a series of top surfaces reside on a series of columns such that the walls of the columns are not significantly densified relative to the interior of the columns. Patterns can be generated where the columns are oriented independently normal to or at an acute angle to the top surfaces. The cross sections of the top surfaces are formed to conform to the average dimensions of the spheres of the FGI coating. The cross sections of the top surfaces can be more than 1.5 times the diameter of the spheres. Various patterns of top surfaces can be used including regular, random, quasiperiodic patterns. A gradient of abradability can be imposed on the coating.