BRIAN JAMES KRAMER
Pilots at 33 Ave, Seattle, WA
License number
Washington A2931401
Issued Date
May 2016
Expiration Date
May 2018
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
7316 33Rd Ave NW, Seattle, WA 98117
Professional information
Partner &Amp; Principal Architect At Spry Hive Industries Llc.
Position:
Partner & Principal Architect at Spry Hive Industries LLC.
Location:
Greater Seattle Area
Industry:
Computer Software
Work:
Spry Hive Industries LLC.
- Redmond, WA since Mar 2009
-
Partner & Principal Architect
Tableau Software
- Seattle, WA Oct 2010 - Feb 2013
-
Senior Software Engineer
Microsoft Corporation
Aug 2009 - Oct 2010
-
Contract Software Engineer
Microsoft Corporation
Jul 2008 - Aug 2009
-
Senior Software Engineer
Zumobi, Inc.
Jun 2007 - Apr 2008
-
Developer Lead
University of Idaho
Sep 2004 - May 2007
-
Graduate Student
Microsoft
Jun 2002 - Aug 2004
-
Developer Lead
Action Engine
Aug 2000 - Oct 2001
-
Developer
BSQUARE
May 1997 - Sep 2000
-
Developer Lead
Pacific Simulation
Jun 1992 - May 1997
-
Developer
Education:
University of Idaho 1989 - 1994
Centennial High School 1987 - 1989
Centennial High School
Centennial High School 1987 - 1989
Centennial High School
Skills:
Software Development, C#, Software Engineering
Method And Apparatus For Installing And Actuating Movable Airfoils, Including Canards
US Patent:
6929216, Aug 16, 2005
Filed:
Oct 20, 2003
Appl. No.:
10/689972
Inventors:
David L. Bath - Seattle WA, US
Salvatore Carta - Melbourne, AU
Kelly T. Jones - Snohomish WA, US
Brian J. Kramer - Seattle WA, US
Chester P. Nelson - Kirkland WA, US
Pieter S. Penhall - Melbourne, AU
Joseph R. Pineda - Mukilteo WA, US
Andrew Sheppard - Melbourne, AU
Salvatore Carta - Melbourne, AU
Kelly T. Jones - Snohomish WA, US
Brian J. Kramer - Seattle WA, US
Chester P. Nelson - Kirkland WA, US
Pieter S. Penhall - Melbourne, AU
Joseph R. Pineda - Mukilteo WA, US
Andrew Sheppard - Melbourne, AU
Assignee:
The Boeing Company - Seattle WA
International Classification:
B64C005/04
US Classification:
244 45A, 244 75 R, 244 48
Abstract:
Methods and apparatuses for installing and actuating movable airfoils, such as canards. A canard in one embodiment of the invention includes an airfoil positioned external to an aircraft fuselage. The airfoil can include a first portion and a second portion (such as a flight control surface) movable relative to the first portion. A connecting portion depends from the airfoil portion and has an attachment portion configured to attach to an aircraft internal to the aircraft fuselage. A connecting portion can include first and second load paths to carry corresponding first and second load portions between the airfoil portion and the attachment portion. The connecting portion can be rotatable about a rotation axis positioned between the first and second loads paths. Accordingly, the connecting portion can be relatively compact so as to reduce the impact of the connecting portion and the volume of the fuselage.
Brian Kramer
Location:
Greater Seattle Area
Industry:
Telecommunications