Robert M Johnson
Physician at E 128 St, Kirkland, WA
License number
Colorado 16468
Issued Date
Apr 14, 1970
Renew Date
May 31, 1987
Expiration Date
May 31, 1987
Type
Physician
Address
Address
11919 N 128Th St, Kirkland, WA 98033
Personal information
See more information about Robert M Johnson at radaris.comName
Address
Phone
505 N F St APT 704, Aberdeen, WA 98520
509 Root St, Port Townsend, WA 98368
Silver Lake, WA
Raymond, WA
Olympia, WA
Professional information
See more information about Robert M Johnson at trustoria.com
Head Positioner And Arm Rest For Eye Surgery
Head Positioner And Arm Rest For Eye Surgery
US Patent:
4058112, Nov 15, 1977
Filed:
Aug 19, 1976
Appl. No.:
5/715651
Inventors:
Robert M. Johnson - Kirkland WA
International Classification:
A61B 1900
US Classification:
128 1R
Abstract:
A right rectangular block of resilient material is provided with a recess or cavity, open top to bottom, shaped to embrace and position an eye patient's head on an operating table. Laterally disposed horizontal surfaces contiguous with the upper end of the cavity or recess serve as arm and hand and instrument supports coplanar with a surgical situs of the eye, established during preparation for surgery.
Composite Resin Window Frame Constructions For Airplanes
Composite Resin Window Frame Constructions For Airplanes
US Patent:
2008007, Apr 3, 2008
Filed:
Aug 15, 2006
Appl. No.:
11/464517
Inventors:
Phillip D. Baggette - Sammamish WA, US
Richard W. Brigman - Everett WA, US
Bernhard Dopker - Bellevue WA, US
Robert W. Johnson - Kirkland WA, US
Jeffery P. Sandys - Shoreline WA, US
Richard W. Brigman - Everett WA, US
Bernhard Dopker - Bellevue WA, US
Robert W. Johnson - Kirkland WA, US
Jeffery P. Sandys - Shoreline WA, US
International Classification:
B64C 1/14
US Classification:
2441293
Abstract:
A composite resin window frame for installation in a composite resin airplane fuselage has an inner flange for receiving and securely affixing an aircraft window transparency and an outer flange adapted for connection to the airplane fuselage structure. The frame has a generally flat configuration which does not require any additional strength enhancing member such as an additional flange perpendicular to the structure. The composite resin window frame has sufficient strength to securely affix a window transparency to a composite resin fuselage.