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Francis Schwind Phones & Addresses

  • Kennedale, TX
  • Creede, CO
  • 5385 Brown St, Fort Worth, TX 76140 (817) 478-7509 (817) 563-1886

Work

Company: C-cat Position: Chief executive officer

Industries

Aviation & Aerospace

Resumes

Resumes

Francis Schwind Photo 1

Chief Executive Officer

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Location:
Kennedale, TX
Industry:
Aviation & Aerospace
Work:
C-Cat
Chief Executive Officer

Business Records

Name / Title
Company / Classification
Phones & Addresses
Francis A Schwind
Chief Exec, Director, Chief Executive Offi
CARBON CARBON ADVANCED TECHNOLOGIES, INC
Mfg Carbon/Graphite Products
4704 Eden Rd, Kennedale, TX 76060
53885 Brown Ln, Fort Worth, TX 76140
(817) 985-2500

Publications

Us Patents

Pistons And Cylinders Made Of Carbon-Carbon Composite Materials

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US Patent:
60448199, Apr 4, 2000
Filed:
Feb 28, 1997
Appl. No.:
8/808290
Inventors:
H. Kevin Rivers - Hampton VA
Philip O. Ransone - Gloucester VA
G. Burton Northam - Carrollton VA
Francis A. Schwind - Fort Worth TX
Assignee:
The United States of America as represented by the Administrator of the
National Aeronautics and Space Administration - Washington DC
International Classification:
F02F 7506
US Classification:
1231931
Abstract:
An improved reciprocating internal combustion engine has a plurality of engine pistons, which are fabricated from carbon-carbon composite materials, in operative association with an engine cylinder block, or an engine cylinder tube, or an engine cylinder jug, all of which are also fabricated from carbon-carbon composite materials.

Pistons And Cylinders Made Of Carbon-Carbon Composite Materials

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US Patent:
61487856, Nov 21, 2000
Filed:
Jan 11, 2000
Appl. No.:
9/480421
Inventors:
H. Kevin Rivers - Hampton VA
Philip O. Ransone - Gloucester VA
G. Burton Northam - Carrollton VA
Francis A. Schwind - Fort Worth TX
Assignee:
The United States of America as represented by the Administrator of the
National Aeronautics and Space Administration - Washington DC
International Classification:
F02F 7506
US Classification:
1231931
Abstract:
An improved reciprocating internal combustion engine has a plurality of engine pistons, which are fabricated from carbon--carbon composite materials, in operative association with an engine cylinder block, or an engine cylinder tube, or an engine cylinder jug, all of which are also fabricated from carbon--carbon composite materials.

Carbon-Carbon Piston Architectures

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US Patent:
59001933, May 4, 1999
Filed:
Feb 27, 1997
Appl. No.:
8/805195
Inventors:
H. Kevin Rivers - Hampton VA
Philip O. Ransone - Gloucester VA
G. Burton Northam - Carrollton VA
Francis A. Schwind - Fort Worth TX
Assignee:
The United States of America as represented by the Administrator of the
National Aeronautics and Space Administration - Washington DC
International Classification:
C01B 3100
US Classification:
264 295
Abstract:
An improved structure for carbon-carbon composite piston architectures consists of replacing the knitted fiber, three-dimensional piston preform architecture described in U. S. Pat. No. 4,909,133 (Taylor et al. ) with a two-dimensional lay-up or molding of carbon fiber fabric or tape. Initially, the carbon fabric or tape layers are prepregged with carbonaceous organic resins and/or pitches and are laid up or molded about a mandrel, to form a carbon-fiber reinforced organic-matrix composite part shaped like a "U" channel, a "T"-bar, or a combination of the two. The molded carbon-fiber reinforced organic-matrix composite part is then pyrolized in an inert atmosphere, to convert the organic matrix materials to carbon. At this point, cylindrical piston blanks are cored from the "U"-channel, "T"-bar, or combination part. These blanks are then densified by reimpregnation with resins or pitches which are subsequently carbonized.

Carbon-Carbon Piston Architectures

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US Patent:
61162027, Sep 12, 2000
Filed:
Apr 14, 1999
Appl. No.:
9/291717
Inventors:
H. Kevin Rivers - Hampton VA
Philip O. Ransone - Gloucester VA
G. Burton Northam - Carrollton VA
Francis A. Schwind - Fort Worth TX
Assignee:
The United States of America as represented by the Administrator of the
National Aeronautics and Space Administration - Washington DC
International Classification:
F02F 7506
US Classification:
1231936
Abstract:
An improved structure for carbon--carbon composite piston architectures is disclosed. The improvement consists of replacing the knitted fiber, three-dimensional piston preform architecture described in U. S. Pat. No. 4,909,133 (Taylor et al. ) with a two-dimensional lay-up or molding of carbon fiber fabric or tape. Initially, the carbon fabric or tape layers are prepregged with carbonaceous organic resins and/or pitches and are laid up or molded about a mandrel, to form a carbon-fiber reinforced organic-matrix composite part shaped like a "U" channel, a "T"-bar, or a combination of the two. The molded carbon-fiber reinforced organic-matrix composite part is then pyrolized in an inert atmosphere, to convert the organic matrix materials to carbon. At this point, cylindrical piston blanks are cored from the "U"-channel, "T"-bar, or combination part. These blanks are then densified by reimpregnation with resins or pitches which are subsequently carbonized.

Rotary Vane Pump With Carbon/Carbon Vanes

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US Patent:
51818442, Jan 26, 1993
Filed:
Aug 15, 1991
Appl. No.:
7/745498
Inventors:
Jerry B. Bishop - Wichita KS
Francis A. Schwind - Fort Worth TX
David B. Sawyer - Fort Worth TX
Assignee:
Sigma Tek, Inc. - Augusta KS
International Classification:
F01C 2102
US Classification:
418152
Abstract:
A rotary sliding vane pump having vanes fabricated from a carbon/carbon based material that provides improved performance by inhibiting vane wear, chipping or fracture. The advantages provided by carbon/carbon based materials may be further enhanced by impregnating each carbon/carbon sliding vane with a teflon based coating.
Francis Aloysius Schwind from Kennedale, TX, age ~85 Get Report