DR. ROBERT PARKER MITCHELL, DMD
Dentist at Via Soleri Dr, Scottsdale, AZ
License number
Arizona D009863
Category
Dentist
Type
General Practice
Address
Address
7025 E Via Soleri Dr UNIT 4013, Scottsdale, AZ 85251
Phone
(941) 961-4448
Professional information
Elearning Director, Producer; Interactive Media Strategist, Musician, Composer
Position:
Director of Media Development; Director of Awesome at Glynlyon
Location:
Phoenix, Arizona
Industry:
E-Learning
Work:
Glynlyon
- Chandler, AZ since Mar 2013
-
Director of Media Development; Director of Awesome
CORECareers Global
- Los Angeles, Phoenix, Atlanta, London, Mumbai Jan 2012 - Jan 2013
-
Director of eLearning, Producer; Product Strategist
Arizona State University
Nov 2011 - Dec 2011
-
Business Analyst
Arizona State University
- Tempe, AZ Dec 1997 - Dec 2011
-
Instructional Designer, Trainer, Presenter
Arizona State University
- Tempe, AZ 1997 - Nov 2011
-
Web Application Developer, UX Specialist
Education Management Group
- Scottsdale, AZ 1995 - 1997
-
Education Multimedia Developer
The Evergreen State College
1990 - 1995
-
Accounts Receivable Rep and part-time Computer Operator
The Evergreen State College
1990 - 1995
-
Student Accounts Receivable Rep
Education:
The Evergreen State College 1992 - 1995
Bachelor of Science, Software Development, Instructional Design, Educational Multimedia University of Oklahoma 1981 - 1983
Bachelor of Science, Software Development, Instructional Design, Educational Multimedia University of Oklahoma 1981 - 1983
Apparatus And Method For Testing Jet Engine Fuel Manifold Flow Distribution
US Patent:
6672145, Jan 6, 2004
Filed:
Sep 21, 2001
Appl. No.:
09/960897
Inventors:
Robert D. Mitchell - Scottsdale AZ
John R. Webber - Clarksburg CA
Joseph M. Oloffo - Phoenix AZ
Michael S. Englund - Phoenix AZ
John R. Webber - Clarksburg CA
Joseph M. Oloffo - Phoenix AZ
Michael S. Englund - Phoenix AZ
Assignee:
Honeywell International, Inc. - Morristown NJ
International Classification:
G01M 1500
US Classification:
731181, 73119 A
Abstract:
An apparatus and method for testing the flow distribution through a turbine engine fuel manifold and one or more nozzles connected to the manifold. A plurality of individual fluid measurement vessels, at least one for each of the nozzles being tested, collects test fluid pumped through the manifold and the connected nozzles. The level in each of the measurement vessels is periodically sampled during the test. The test fluid flow rate through each of the nozzles is periodically determined based on the periodically sampled levels.
Compact Mixer With Trimmable Open Centerbody
US Patent:
7506501, Mar 24, 2009
Filed:
Sep 9, 2005
Appl. No.:
11/223556
Inventors:
Morris G. Anderson - Mesa AZ, US
John C. Gerrard - Gilbert AZ, US
Ron G. Ruiz - Scottsdale AZ, US
Robert D. Mitchell - Scottsdale AZ, US
John C. Gerrard - Gilbert AZ, US
Ron G. Ruiz - Scottsdale AZ, US
Robert D. Mitchell - Scottsdale AZ, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
F02K 1/34
US Classification:
60262, 23926517
Abstract:
Compact exhaust mixer assemblies comprising a compact mixer and a trimmable open centerbody are provided. The trimmable center body allows for adjustments of the open centerbody after manufacturing and during production testing. The trimmable open centerbody may be used to compensate for production tolerances making it possible to obtain the desired core effective area for proper engine operation. The compact mixer may be either lobed or serrated. The compact exhaust mixer assemblies have a length of about half that of conventional exhaust mixer assemblies.
Apparatus And Method For Testing Jet Engine Fuel Manifold Flow Distribution
US Patent:
2003017, Sep 11, 2003
Filed:
Mar 14, 2003
Appl. No.:
10/388967
Inventors:
Robert Mitchell - Scottsdale AZ, US
John Webber - Clarksburg CA, US
Joseph Oloffo - Phoenix AZ, US
Michael Englund - Phoenix AZ, US
John Webber - Clarksburg CA, US
Joseph Oloffo - Phoenix AZ, US
Michael Englund - Phoenix AZ, US
International Classification:
G01F001/00
US Classification:
702/046000
Abstract:
An apparatus and method for testing the flow distribution through a turbine engine fuel manifold and one or more nozzles connected to the manifold. A plurality of individual fluid measurement vessels, at least one for each of the nozzles being tested, collects test fluid pumped through the manifold and the connected nozzles. The level in each of the measurement vessels is periodically sampled during the test. The test fluid flow rate through each of the nozzles is periodically determined based on the periodically sampled levels.