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Gary Gilbert Cassatt, 8313111 39Th St, Derby, KS 67037

Known as:
Gary G Cassatt Gary G Cassett Brian Cassatt Mary Cassatt
Related to:
Dennis Cassatt

Gary Cassatt Phones & Addresses

13111 39Th St, Derby, KS 67037    316-7330966   

Grove, OK   

Frontenac, KS   

1038 Saint Peter St, New Orleans, LA 70116   

Andover, KS   

Louisville, KY   

13111 E 39Th St S, Derby, KS 67037    316-3901539   

Work

Position: Machine Operators, Assemblers, and Inspectors Occupations

Education

Degree: High school graduate or higher

Emails

b***[email protected]
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Mentions for Gary Gilbert Cassatt

Gary Cassatt resumes & CV records

Resumes

Gary Cassatt Photo 9

Manager, Structures

Location:
Derby, KS
Industry:
Biotechnology
Work:
Spirit Aerosystems 1961 - 2010
Magager Boeing May 1991 - Jun 2005
Manager, Structures Spirit Aerpsystems May 1991 - Jun 2005
Structures Manager Spirit Aerosystems May 1991 - Jun 2005
Manager, Structures
Education:
Wichita State University 1962 - 1965
Masters, Master of Arts, Aerospace Engineering Missouri University of Science and Technology 1959 - 1961
Bachelor of Science In Mechanical Engineering, Bachelors, Mechanical Engineering
Skills:
Stress Analysis, Composites, Damage Tolerance, Aerospace, Aircraft, Msc.patran, Aircraft Design, Aerospace Engineering, Fatigue Analysis, Nastran, Structural Analysis, Engineering Management, As9100, Manufacturing Engineering, Engineering, Composite Structures, Propulsion, Airworthiness, Femap, Finite Element Analysis, Mechanical Engineering, Fracture Mechanics, Design Engineering, Enovia Lca, Avionics, Catia, Systems Engineering, Aerodynamics, Gd&T, Aircraft Maintenance, Mrb, Design For Manufacturing, Root Cause Analysis, Abaqus, Matrixone, Flight Test, Ansys, Vpm, Fortran, Aeronautics, Cfd, Aircraft Interiors, Mathcad, Aerospace Structures, Earned Value Management, Aerostructures, Fibersim, Nei Nastran, Hypermesh
Gary Cassatt Photo 10

Gary Cassatt

Position:
Manager,Stress and certification, Br725 Program at Spirit AeroSystems Inc.
Location:
Wichita, Kansas Area
Industry:
Aviation & Aerospace
Work:
Spirit AeroSystems Inc. - Wichita, Kansas Area since Jun 1961
Manager,Stress and certification, Br725 Program
Education:
University of Missouri-Rolla 1959 - 1961
B.S. Mechanical, Mechanical Engineering

Publications & IP owners

Us Patents

Damage-Tolerant Monolithic Structures

US Patent:
7673433, Mar 9, 2010
Filed:
Apr 29, 2005
Appl. No.:
11/117527
Inventors:
Alexander Rutman - Wilmington DE, US
Gary G. Cassatt - Derby KS, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
E04C 3/00
US Classification:
52843, 52831, 52850
Abstract:
A variety of a damage-tolerant monolithic structures are disclosed, such structures having a substantially-planar element integral with or welded to one or more stiffening elements. Each stiffening element can includes a first stiffening flange having a generally rail-like structure running along the length of the planar element and one or more webbings connected to the planar element and extending away from the planar element to the stiffening flange, wherein each webbing includes a row of integral holes running along the length of the webbing, the holes being in a shape designed to hinder the propagation of a crack in the monolithic structure.

Low Cost/High Performance Blind Fastener

US Patent:
2007024, Oct 25, 2007
Filed:
Apr 21, 2006
Appl. No.:
11/379710
Inventors:
Gary Cassatt - Derby KS, US
Dinh Vu - Wichita KS, US
Robert Mock - Wichita KS, US
International Classification:
F16B 13/04
US Classification:
411034000
Abstract:
A blind fastener is provided comprising a core bolt comprised of a bolt shaft and a bolt head. A metal sleeve is included comprising a rigid cylindrical base and a malleable cylindrical tail, the metal sleeve is positioned around the bolt shaft with the malleable cylindrical tail in communication with the bolt head. A travel stop feature is formed on the rigid cylindrical base opposite the malleable cylindrical tail. A drive feature includes a threaded bolt section extending from a foot end of the bolt shaft and a drive nut rotatably thereto. The drive nut allows the core bolt to be pulled within the metal sleeve such that the bolt head compresses the malleable cylindrical tail to form a retention button.

Lost Cost/High Performance Blind Fastener

US Patent:
2010029, Nov 25, 2010
Filed:
Aug 2, 2010
Appl. No.:
12/848446
Inventors:
GARY G. CASSATT - Derby KS, US
DINH Q. VU - Wichita KS, US
ROBERT J. MOCK - Wichita KS, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
F16B 35/00
F16B 21/00
US Classification:
411337, 411500
Abstract:
A blind fastener is provided comprising a core bolt comprised of a bolt shaft and a bolt head. A metal sleeve is included comprising a rigid cylindrical base and a malleable cylindrical tail, the metal sleeve is positioned around the bolt shaft with the malleable cylindrical tail in communication with the bolt head. A travel stop feature is formed on the rigid cylindrical base opposite the malleable cylindrical tail. A drive feature includes a threaded bolt section extending from a foot end of the bolt shaft and a drive nut rotatably thereto. The drive nut allows the core bolt to be pulled within the metal sleeve such that the bolt head compresses the malleable cylindrical tail to form a retention button.

Flaw Growth Correlator

US Patent:
4164874, Aug 21, 1979
Filed:
Jan 19, 1978
Appl. No.:
5/870616
Inventors:
Gary G. Cassatt - Wichita KS
Richard J. Miller - Wichita KS
Assignee:
Boeing Wichita Company - Wichita KS
International Classification:
G01N 332
US Classification:
73799
Abstract:
A flaw growth correlator for monitoring flaw growth potential in a structural body. The correlator providing a major increase in the sensitivity of flaw growth when compared to current designs of constant thickness crack gauges.

Structural Blind Fastener

US Patent:
5947667, Sep 7, 1999
Filed:
Jan 11, 1996
Appl. No.:
8/587159
Inventors:
Gary G. Cassatt - Derby KS
R. Todd Briscoe - Benton KS
Assignee:
The Boeing Company - Seattle WA
International Classification:
F16B 1304
F16B 1306
US Classification:
411 34
Abstract:
Extended fatigue endurance and high pre-load are achieved in a structural blind fastener by combining the best features of screw type and pull type blind fasteners. We replace fatigue critical details from the shear plane with close tolerance, slip fit, core bolt and outer bolt shanks to obtain the desired structural load paths while retaining anchoring features of screw type fasteners to introduce adequate pre-load. These fasteners are compatible with currently available blind bolt insertion tooling.

Possible Relatives

David D Cassatt  Debra Cassatt  Danielle I Cassatt  Donna L Cassatt  Joe F Cassatt  John M Cassatt  Mary A Cassatt  Gary R Johnson  Gary Stamps  Gary H Stancil 

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