Kendall E Goodman, Age 591427 Dartmouth Dr, Southlake, TX 76092

Kendall Goodman Phones & Addresses

Southlake, TX

Dallas, TX

Carrollton, TX

Fort Worth, TX

Mesquite, TX

South Lake, TX

1427 Dartmouth Dr, Southlake, TX 76092

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Kendall E Goodman

Linkedin

Work

Company: Bell helicopter Jun 2014 to Dec 2016 Position: V-280 advanced configurations manager and technical fellow for survivability

Education

Degree: Master of Science, Masters School / High School: Virginia Tech 1988 to 1990 Specialities: Engineering

Skills

Helicopters • Fms • Program Management • Research • Engineering Management • Roadmap • Talent Development • Special Projects • Project Engineering • Program Development • Earned Value Management • Aircraft • Military • Aerospace • Testing • Dod • Engineering • Talent Management • Proposal Writing • Leadership • Systems Engineering • Avionics • Projects • Aviation • Government • Composites • Project Management • Mentoring of Staff • Security Clearance • Executive Leadership

Industries

Aviation & Aerospace

Mentions for Kendall E Goodman

Kendall Goodman resumes & CV records

Resumes

Kendall Goodman Photo 26

President And Chief Operating Officer

Location:
Dallas, TX
Industry:
Aviation & Aerospace
Work:
Bell Helicopter Jun 2014 - Dec 2016
V-280 Advanced Configurations Manager and Technical Fellow For Survivability
Bell Helicopter Jan 2014 - May 2014
South Korea Lch and Lah Engineering Campaign Manager
Bell Helicopter Apr 2013 - Dec 2013
Fvl Variant Program Manager
Bell Helicopter Feb 2012 - Mar 2013
Korea Campaign Manager
Bell Helicopter Mar 2010 - Jan 2012
Military R and D Portfolio Manager
Bell Helicopter Feb 2009 - Feb 2010
Program Manager, Strategic Capital Initiative
Bell Helicopter Nov 2004 - Jan 2009
Chief Engineer - Advanced Concepts
Bell Helicopter Mar 1994 - Oct 2004
Project Manager
Triumph Aerostructures - Vought Aircraft Division Feb 1991 - Feb 1994
Project Engineer
General Dynamics Apr 1990 - Jan 1991
Engineer
Avx Aircraft Company Apr 1990 - Jan 1991
President and Chief Operating Officer
Education:
Virginia Tech 1988 - 1990
Master of Science, Masters, Engineering
The University of Texas at Arlington 1983 - 1988
Bachelors, Bachelor of Science, Mechanical Engineering
North Mesquite High School 1983
Skills:
Helicopters, Fms, Program Management, Research, Engineering Management, Roadmap, Talent Development, Special Projects, Project Engineering, Program Development, Earned Value Management, Aircraft, Military, Aerospace, Testing, Dod, Engineering, Talent Management, Proposal Writing, Leadership, Systems Engineering, Avionics, Projects, Aviation, Government, Composites, Project Management, Mentoring of Staff, Security Clearance, Executive Leadership

Publications & IP owners

Us Patents

Method And Apparatus For Acquiring Accurate Background Infrared Signature Data On Moving Targets

US Patent:
8520896, Aug 27, 2013
Filed:
Feb 2, 2009
Appl. No.:
12/989933
Inventors:
Robert A. Shepherd - Fort Worth TX, US
David R. Schlichte - Irving TX, US
Richard A. Shepherd - Avon IN, US
Kendall E. Goodman - Southlake TX, US
Assignee:
Textron Innovations Inc. - Providence RI
International Classification:
G06K 7/015
US Classification:
382103
Abstract:
A method for measuring an infrared signature of a moving target includes: tracking the moving target with a tracking system along a path from a start position to an end position, measuring infrared radiation data of the moving target along the path, repositioning the tracking system to the start position, retracing the path to measure the infrared radiation data of the background, and determining the infrared signature of the moving target by comparing the infrared radiation data of the moving object with the infrared radiation data of the background without the moving object.

Method For Analyzing And Designing Armor In A Vehicle

US Patent:
2012004, Feb 16, 2012
Filed:
May 5, 2010
Appl. No.:
13/266702
Inventors:
David F. Haynes - Arlington TX, US
William D. Girard - Euless TX, US
Kendall E. Goodman - Southlake TX, US
Kelly R. Tingen - Coppell TX, US
Assignee:
Bell Helicopter Textron Inc. - Fort Worth TX
International Classification:
G06F 17/50
US Classification:
703 1
Abstract:
Properly identifying the most vulnerable areas and quantifying the effectiveness of armor at those locations is critical to achieving efficient armor integration. A method for designing protective armor for a vehicle includes the deriving shotlines through an element; computing a probability of kill value for each shotline in each element; calculating a probability of kill intensity for each element; ranking the elements according to highest probability of kill intensity; mapping the elements in a 3D CAD environment to visually depict the elements having the highest probability of kill intensity; and designing armor taking into account the elements having the highest probability of kill intensity.

Composite Panel Insert With Hold Out Recess Feature

US Patent:
6488460, Dec 3, 2002
Filed:
May 2, 2000
Appl. No.:
09/561652
Inventors:
Andrew D. Smith - Arlington TX
Kendall F. Goodman - Carrollton TX
Assignee:
Bell Helicopter Textron Inc. - Fort Worth TX
International Classification:
F16B 2118
US Classification:
411353, 411339, 411999, 52364
Abstract:
A panel insert for use with a structural panel and a fastener having a hold out mechanism. The panel insert comprises a body portion disposed within the structural panel. The body portion includes a first surface, an opposing second surface, and an aperture passing therethrough for receiving the fastener. A recessed portion opening to the second surface is provided to receive the hold out mechanism and secure the fastener to the structural panel.

Lift Propulsion Module For A Tiltrotor Aircraft

US Patent:
2019003, Jan 31, 2019
Filed:
Jul 27, 2017
Appl. No.:
15/662147
Inventors:
- Fort Worth TX, US
Kendall Goodman - Southlake TX, US
Steven R. Ivans - Ponder TX, US
Assignee:
Bell Helicopter Textron Inc. - Fort Worth TX
International Classification:
B64F 5/10
B64C 29/00
B64C 1/00
Abstract:
A method for facilitating the design and manufacturing of a tiltrotor aircraft, including the steps of: determining a compatible mission data set; identifying lift propulsion module components for the compatible mission data set; determining compatible specifications; and generating a design for a lift propulsion module; wherein the lift propulsion module is configured to be connected to at least two different fuselages. There is also a method of designing a tiltrotor aircraft, comprising the step of modularizing a lift propulsion system, wherein the lift propulsion system is configured to be connected to at least two different fuselages. In another aspect, there is a tiltrotor aircraft including a fuselage; and a lift propulsion module, the lift propulsion module including a mounting surface; wherein the lift propulsion module is coupled to the fuselage on the mounting surface. Also included are methods of assembling and systems including a lift propulsion module.

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