DR. ROBERT SCOTT WATSON, MD, MPH
Medical Practice at Sand Point Way, Seattle, WA
License number
Washington MD071712L
Category
Medical Practice
Type
Specialist
License number
Washington MD00032885
Category
Medical Practice
Type
Pediatric Critical Care Medicine
Address
Address
4800 Sand Point Way NE, Seattle, WA 98105
Phone
(206) 987-2000
Personal information
See more information about ROBERT SCOTT WATSON at radaris.comName
Address
Phone
5224 S Dayton St, Kennewick, WA 99337
5207 128Th St E, Tacoma, WA 98446
Professional information
Software Engineer At Nimbleuser
Position:
Software Engineer at NimbleUser
Location:
Greater Seattle Area
Industry:
Information Technology and Services
Work:
NimbleUser
- Pittsford, NY since Jun 2012
-
Software Engineer
Rochester Institute of Technology
- Rochester, NY Dec 2010 - May 2012
-
Student Government Director of Services
Rochester Institute of Technology
- Rochester, NY Sep 2008 - May 2012
-
Wallace Center Desk Worker
Rochester Institute of Technology
- Rochester, NY Apr 2011 - Sep 2011
-
Orientation Assistant
NimbleUser
- Pittsford, NY May 2011 - Aug 2011
-
Web Developer Intern
First Quality
- McElhattan, PA May 2010 - Nov 2010
-
IT Intern
Rochester Institute of Technology
- Rochester, NY Sep 2008 - May 2010
-
Residence Halls Association Director of Services
Education:
Rochester Institute of Technology 2008 - 2012
Bachelor of Science (B.S.), Information Technology
Bachelor of Science (B.S.), Information Technology
Skills:
Apex Programming, Salesforce.com, SOQL, SQL, MySQL, PHP, Java, ASP.NET, C#, HTML 5, CSS, AJAX, JavaScript, Microsoft SQL Server, XML, Oracle SQL, Amazon Web Services (AWS), Web Applications, Agile Methodologies, Web Development
Interests:
running, biking, hiking, camping, traveling, reading, technology, web design, community service
Honor & Awards:
Dean's List, 2008-2012
RIT Outstanding Undergraduate Scholar, 2011-2012
RIT Presidential Scholarship Recipient, 2008-2011
1st Place Economics PA Business Plan Challenge, 2008
1st Place Database Applications, FBLA Nationals 2008
1st Place Virtual Business Challenge, FBLA Nationals 2007
Certifications:
Salesforce.com Certified Force.com Developer, Salesforce.com
It Programmer Analyst Sr At Ttm Technologies
Position:
Web Programmer Analyst (ITS4) at Washington State Employment Security Department
Location:
Greater Seattle Area
Industry:
Information Technology and Services
Work:
Washington State Employment Security Department
- Lacey, WA since Aug 2011
-
Web Programmer Analyst (ITS4)
TTM Technologies
- Redmond,WA Aug 2006 - May 2009
-
IT Programmer Analyst Sr
City University of Seattle
- Bellevue,Wa Oct 1988 - Mar 2006
-
Senior Programmer Analsyt
Education:
Olympic College 2009 - 2011
AAS, Information Systems Specialist - Web Development City University of Seattle 1990 - 2005
ITT Technical Institute 1986 - 1988
AS, Business Application and Information Systems
AAS, Information Systems Specialist - Web Development City University of Seattle 1990 - 2005
ITT Technical Institute 1986 - 1988
AS, Business Application and Information Systems
Skills:
Access, VB.NET, HTML, Requirements Analysis, SQL, Visual Basic, CSS, Microsoft SQL Server, ASP.NET, Java, Project Management, SharePoint
Robert Watson
Location:
Greater Seattle Area
Industry:
Real Estate
Methods For Manufacturing Composite Sections For Aircraft Fuselages And Other Structures
US Patent:
8303758, Nov 6, 2012
Filed:
Mar 30, 2012
Appl. No.:
13/436631
Inventors:
Michael R. Chapman - Seattle WA, US
Robert M. Watson - Seattle WA, US
Donald A. Anderson - Seattle WA, US
Marc J. Piehl - Seattle WA, US
Joseph L. Sweetin - Seattle WA, US
Douglas L. Grose - Seattle WA, US
Robert M. Watson - Seattle WA, US
Donald A. Anderson - Seattle WA, US
Marc J. Piehl - Seattle WA, US
Joseph L. Sweetin - Seattle WA, US
Douglas L. Grose - Seattle WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B29C 65/00, B32B 37/00
US Classification:
156287, 156173, 156187, 156188, 156195, 156285
Abstract:
Methods for manufacturing composite sections for aircraft fuselages and other structures are disclosed herein. A method for manufacturing a shell structure in accordance with one embodiment of the invention includes applying composite material to an interior mold surface of a tool to form a skin extending 360 degrees around an axis. The method can further include positioning a plurality of stiffeners on an inner surface of the skin. After the stiffeners have been positioned, a vacuum bag can be installed over the stiffeners and evacuated to press the stiffeners and the skin outwardly against the interior mold surface of the tool. Next, the skin/stiffener combination can be cocured to bond the stiffeners to the skin and harden the shell structure.
Composite Sections For Aircraft Fuselages And Other Structures, And Methods And Systems For Manufacturing Such Sections
US Patent:
7503368, Mar 17, 2009
Filed:
Nov 24, 2004
Appl. No.:
10/996922
Inventors:
Michael R. Chapman - Seattle WA, US
Robert M. Watson - Seattle WA, US
Donald A. Anderson - Seattle WA, US
Marc J. Piehl - Seattle WA, US
Joseph L. Sweetin - Seattle WA, US
Douglas L. Grose - Seattle WA, US
Robert M. Watson - Seattle WA, US
Donald A. Anderson - Seattle WA, US
Marc J. Piehl - Seattle WA, US
Joseph L. Sweetin - Seattle WA, US
Douglas L. Grose - Seattle WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B29C 53/58, B29C 53/72
US Classification:
156425, 156443
Abstract:
Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections, are disclosed herein. A method for manufacturing a shell structure in accordance with one embodiment of the invention includes applying composite material to an interior mold surface of a tool to form a skin extending 360 degrees around an axis. The method can further include positioning a plurality of stiffeners on an inner surface of the skin. After the stiffeners have been positioned, a vacuum bag can be installed over the stiffeners and evacuated to press the stiffeners and the skin outwardly against the interior mold surface of the tool. Next, the skin/stiffener combination can be cocured to bond the stiffeners to the skin and harden the shell structure.
Composite Sections For Aircraft Fuselages And Other Structures, And Methods And Systems For Manufacturing Such Sections
US Patent:
2013004, Feb 14, 2013
Filed:
Sep 21, 2012
Appl. No.:
13/624711
Inventors:
THE BOEING COMPANY - Chicago IL, US
Robert M. Watson - Seattle WA, US
Donald A. Anderson - Seattle WA, US
Marc J. Piehl - Seattle WA, US
Joseph L. Sweetin - Seattle WA, US
Douglas L. Grose - Seattle WA, US
Robert M. Watson - Seattle WA, US
Donald A. Anderson - Seattle WA, US
Marc J. Piehl - Seattle WA, US
Joseph L. Sweetin - Seattle WA, US
Douglas L. Grose - Seattle WA, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
B29C 33/14
US Classification:
425110
Abstract:
Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections, are disclosed herein. A method for manufacturing a shell structure in accordance with one embodiment of the invention includes applying composite material to an interior mold surface of a tool to form a skin extending 360 degrees around an axis. The method can further include positioning a plurality of stiffeners on an inner surface of the skin. After the stiffeners have been positioned, a vacuum bag can be installed over the stiffeners and evacuated to press the stiffeners and the skin outwardly against the interior mold surface of the tool. Next, the skin/stiffener combination can be cocured to bond the stiffeners to the skin and harden the shell structure.