John E Marks

US Patent:

7083753, Aug 1, 2006

Filed:

Dec 16, 2003

Appl. No.:

10/737687

Inventors:

Pat Bonebright - San Diego CA, US
John Marks - Escondido CA, US

Assignee:

Composite Optics, Inc. - San Diego CA

International Classification:

B29C 70/30
B29D 24/00

US Classification:

264214, 264236, 264238, 264257, 264258, 264278, 264324

Abstract:

A method is provided that uses half-period translations, ply-upon-pin repositions, and shape-maintaining pins with a bolster plate, with insertable nodal heating elements that provide heat at their rectangular ends and when driven under pressure against opposing pins with rectangular faces cure portions of a pre-impregnated fabric to make honeycomb core composite articles.

US Patent:

7095379, Aug 22, 2006

Filed:

Jun 6, 2002

Appl. No.:

10/164990

Inventors:

Mark K. Pryor - San Diego CA, US
John E. Marks - Escondido CA, US
Patrick N. Bonebright - San Diego CA, US
Kenneth Neal Segal - Ellicott City MD, US
Alan Kogut - Bowie MD, US

Assignee:

ATK Alliant Techsystems, Inc. - Salt Lake City UT

International Classification:

H01Q 13/00

US Classification:

343786, 343772, 343774

Abstract:

An electrical component and a method of constructing it are disclosed. The component includes a hollow tubular structure. The structure includes a series of axially spaced apart rings and at least one outer perimeter housing member. The housing member interconnects the rings for defining an internal configuration of the hollow tubular structure for electrical purposes. The rings and the housing member each include inter-engageable elements for helping secure mechanically the rings and housing member together to facilitate final assembly of the electrical component.

US Patent:

20050212712, Sep 29, 2005

Filed:

May 10, 2005

Appl. No.:

11/126918

Inventors:

Mark Pryor - San Diego CA, US
John Marks - Escondido CA, US
Patrick Bonebright - San Diego CA, US

International Classification:

H01Q013/00

US Classification:

343786000

Abstract:

An electrical component and a method of constructing it are disclosed. The component includes a hollow tubular structure. The structure includes a series of axially spaced apart rings and at least one outer perimeter housing member. The housing member interconnects the rings for defining an internal configuration of the hollow tubular structure for electrical purposes. The rings and the housing member each include inter-engageable elements for helping secure mechanically the rings and housing member together to facilitate final assembly of the electrical component.

US Patent:

54408016, Aug 15, 1995

Filed:

Mar 3, 1994

Appl. No.:

8/205879

Inventors:

John Marks - Escondido CA
George Pynchon - Poway CA

Assignee:

Composite Optics, Inc. - San Diego CA

International Classification:

H01P 1100
H01Q 1516

US Classification:

29600

Abstract:

A composite antenna and method for constructing same is disclosed. The composite antenna has a grid comprised of electrical conductors woven into the warp of a resin reinforced cloth forming one layer of the multi-layer laminate structure of the antenna.

US Patent:

57710279, Jun 23, 1998

Filed:

Apr 28, 1997

Appl. No.:

8/847864

Inventors:

John Marks - Escondido CA
George Pynchon - Poway CA

Assignee:

Composite Optics, Inc. - San Diego CA

International Classification:

H01Q 138
H01Q 1514

US Classification:

343912

Abstract:

A composite antenna and method for constructing same is disclosed. The composite antenna has a grid comprised of electrical conductors woven into the warp of a resin reinforced cloth forming one layer of the multi-layer laminate structure of the antenna.

US Patent:

58034021, Sep 8, 1998

Filed:

May 13, 1996

Appl. No.:

8/645136

Inventors:

Gary C. Krumweide - Escondido CA
John Marks - Escondido CA
Chris Kingery - San Diego CA
John Richer - Carlsbad CA
William Converse - Fountain Valley CA

Assignee:

Composite Optics, Inc. - San Diego CA

International Classification:

B64C 106

US Classification:

244117R

Abstract:

A composite structure and method for constructing same for use in fabricating the framework of a spacecraft is disclosed. The structure is cut from flat sheets of composite laminate materials, and then assembled. The use of tenons and mortises provides for self-fixturing and adhesive bonding of the structural components.