Scott Michael Collins

US Patent:

D588519, Mar 17, 2009

Filed:

Dec 11, 2007

Appl. No.:

29/293770

Inventors:

Bryan Wayne Westra - LaPalma CA, US
Roxanne Marie Sato - Rancho Palos Verdes CA, US
Douglas Ellwood Shultz - La Habra CA, US
James Franklin Kerswell - Los Angeles CA, US
Perry Bruce Petersen - Pinehurst NC, US
Scott Walter Collins - Upland CA, US

Assignee:

Northrop Gumman Corporation - Los Angeles CA

International Classification:

1212

US Classification:

D12319

US Patent:

D588976, Mar 24, 2009

Filed:

Dec 11, 2007

Appl. No.:

29/293750

Inventors:

Bryan Wayne Westra - LaPalma CA, US
Roxanne Marie Sato - Rancho Palos Verdes CA, US
Douglas Ellwood Shultz - La Habra CA, US
James Franklin Kerswell - Los Angeles CA, US
Perry Bruce Petersen - Pinehurst NC, US
Scott Walter Collins - Upland CA, US

Assignee:

Northrop Gumman Corporation - Los Angeles CA

International Classification:

1212

US Classification:

D12319

US Patent:

8191820, Jun 5, 2012

Filed:

Dec 11, 2007

Appl. No.:

12/001218

Inventors:

Bryan Wayne Westra - LaPalma CA, US
Roxanne Marie Sato - Rancho Palos Verdes CA, US
Douglas Ellwood Shultz - La Habra CA, US
James Franklin Kerswell - Los Angeles CA, US
Perry Bruce Petersen - Pinehurst NC, US
Scott Walter Collins - Upland CA, US

Assignee:

Northrop Gurmman Corporation - Falls Church VA

International Classification:

B64C 39/10
B64C 5/04
B64C 5/12
B64C 21/04

US Classification:

244 36, 244207, 244 45 A, 244 49

Abstract:

The invention is an aircraft that includes a flying wing having a plurality of extendable flaps mounted on the trailing edge of the flying wing. A canard is mounted on the nose of said flying wing. A system is mounted in the flying wing for providing high pressure air over the canard and the flaps. A second system is provided for controlling the flow of air over the canard to provide pitch control of the aircraft.

US Patent:

8292220, Oct 23, 2012

Filed:

Mar 19, 2009

Appl. No.:

12/383193

Inventors:

Bryan Wayne Westra - LaPalma CA, US
Roxanne Marie Sato - Rancho Palos Verdes CA, US
Douglas Ellwood Shultz - La Habra CA, US
James Franklin Kerswell - Los Angeles CA, US
Perry Bruce Petersen - Pinehurst NC, US
Scott Walter Collins - Upland CA, US

Assignee:

Northrop Grumman Corporation - Falls Church VA

International Classification:

B64C 1/22

US Classification:

2441181, 2441371

Abstract:

The invention is a flying wing aircraft having a forward fuselage; an aft fuselage segment; a propulsion segments adapted to mate to the fuselage segments; a pair of wing segments adapted to mate with the propulsion segments. The invention further includes a center section adapted to fit between the forward and aft fuselage sections; the center section adapted to receive multiple compartment systems.

US Patent:

56405669, Jun 17, 1997

Filed:

Aug 1, 1994

Appl. No.:

8/283570

Inventors:

Kenneth E. Victor - Mountain View CA
Peter E. Alley - Saratoga CA
Scott C. Collins - Cupertino CA
Danny L. Dishon - Menlo Park CA
Benjamin W. Sharpe - San Francisco CA

Assignee:

Apple Computer, Inc. - Cupertino CA

International Classification:

G06F 15163

US Classification:

395701

Abstract:

A method of creating an editor that is executed on a first computer system is disclosed in which the editor is arranged to facilitate the editing of data from a first application program executed on a second computer system without requiting that the first application program run on the first computer system. The method includes the steps of creating a display info array that identifies the data fields that may be displayed in a data browser window portion of the editor and creating an edit info array that identifies the data fields may be edited in a detail window portion of the editor. In a preferred embodiment, validation scripts that define the types of data that may be accepted in each of the data fields that is set forth in the edit info array are identified, with the validations scripts forming a portion of the edit info array. This arrangement facilitates editing data using a foreign computer system. Initially, a meta database is created on the first computer system and the meta database is synchronized with a database on the second computer system.