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Brice A Johnson, 47Indianapolis, IN

Known as:
Brice Andrew Johnson Brice Julie Johnson Andrew Johnson Brice Bob Brice
Related to:
Debra J Johnson Janice B Frye 75 Katie J Goeres 44 Donna E Johnson 78 Julie E Johnson 48 Darren E Frye 43 Delmer D Johnson 85 Laura E Pauli 46 Carroll E Frye 75 Dorothea J Johnson

Brice Johnson Phones & Addresses

Indianapolis, IN   

616 5Th St, Puyallup, WA 98371    253-8452488   

Woodinville, WA   

2400 Wheaton Ct, Ellensburg, WA 98926    509-9629133   

Charleston, SC   

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Brice Johnson resumes & CV records

Resumes

Brice Johnson Photo 41

Director, Human Resources

Location:
48 Wildflower Ct, Nederland, CO 80466
Industry:
Food Production
Work:
Livanova
Director, Human Resources Pinnacle Foods 2017 - Jun 30, 2018
Director, Human Resources University of Colorado Boulder May 2016 - Dec 2016
Senior Human Resources Business Partner, University of Colorado Eli Lilly and Company Jan 2015 - Oct 2015
Director - Global Human Resources Strategic Business Partner Eli Lilly and Company Jan 2013 - Dec 2014
Director - Regional Human Resources Strategic Business Partner Eli Lilly and Company Jan 2010 - Dec 2012
Senior Manager - Human Resources Strategic Business Partner Eli Lilly and Company Jan 2007 - Dec 2009
Manager, Senior Human Resources Consultant Eli Lilly and Company May 2004 - Dec 2006
Human Resources Consultant Eli Lilly and Company Mar 2001 - Apr 2004
Manager - Human Resources Eli Lilly and Company Mar 1999 - Feb 2001
Senior Human Resources Representative Eli Lilly and Company Nov 1996 - Feb 1999
Senior Sales Representative - Internal Medicine Eli Lilly and Company Mar 1995 - Oct 1996
Training Associate - Sales and External Business To Business Customers Eli Lilly and Company Jun 1991 - Feb 1995
Process Engineer
Education:
Georgia Institute of Technology 1986 - 1991
Bachelors, Chemical Engineering Jenks High School
Emmanuel College
Georgia Tech
Skills:
Merger and Acquisition Restructuring, Organizational Design, Organizational Effectiveness, Change Management, Project Management, Compensation, Variable Pay Design, Strategic Workforce Planning, Leadership Development Coaching, Succession Planning, Culture Change, Diversity and Inclusion, Performance Management, Employee Relations, Employee Recognition, Leadership, Management, Customer Service, Microsoft Office, Strategy, Training, Team Building, Recruiting, Employee Engagement, Talent Management, Human Resources, Pharmaceutical Industry, Hr Policies, Sales, Onboarding, Leadership Development, Organizational Development, Organizational Structure, Strategic Planning
Interests:
Kayaking
Home Improvement Projects
Health
Spiritual Formation
Outdoors
Education
Science and Technology
Music
Fitness
Human Rights
Movies
Animal Welfare
Friends
Family
Road Running
Poverty Alleviation
Hiking
Faith
Mountains
Social Services
Trail Running
Learning New Crafts and Tools
Snow Skiing
Mountain Biking
Nature
Books/Reading
Languages:
English
Certifications:
Shrm Essentials of Hr Management
Economics
Shrm
Georgia Institute of Technology
Brice Johnson Photo 42

Director Of Marketing

Location:
505 west Baseline Rd, Tempe, AZ 85283
Industry:
Music
Work:
Arizona State University
Graduate Teaching Assistant Butler University Aug 2012 - May 2014
Graduate Teaching Assistant Musicians Friend Feb 2012 - Sep 2013
Sales Associate Core Feb 2012 - Sep 2013
Director of Marketing
Education:
Arizona State University 2013 - 2016
Doctorates, Doctor of Musical Arts, Composition, Music Butler University 2011 - 2013
Masters, Master of Music, Composition, Music Indiana Wesleyan University 2007 - 2011
Bachelor of Music, Bachelors, Bachelor of Arts, Composition, Music, Percussion South Putnam High School
Skills:
Music, Music Theory, Teaching, Research, Composition, Orchestral Music, Percussion, Piano, Higher Education, Performing Arts, Microsoft Office
Brice Johnson Photo 43

Brice Johnson

Brice Johnson Photo 44

Brice Johnson

Brice Johnson Photo 45

Brice Johnson

Brice Johnson Photo 46

Brice Johnson

Brice Johnson Photo 47

Brice Johnson

Location:
Indianapolis, IN
Industry:
Food Production
Skills:
Animal Health, Consulting, Planning, Hr Metrics, Sales, Neuroscience, Workforce Planning, Adjustments, Finance, Job Satisfaction, G&A, Variable Pay, Purchase, Assessment, Risk Reduction, Procurement, Design, Coaching, Hub, Integration, Metrics, Keys, Sales Manager, Leadership, B2B, Structures, Benchmark, Scorecard, Food Safety, Corporate Communications, Utilization, Strategy, Organizational Effectiveness, Supervision, Services Delivery, Turnover, Talent Management, Microsoft Office, Acquisitions, Oncology, Employee Training, Project Management, Organizational Design, Hr Strategy, Market Access, Cost Reduction, Tactics, Employee Engagement, Accountability, Universities, Business Development, Communication, Cost Savings, Operations, New Account Management, Competitive Advantage, Leadership Development, Organizational Culture, Change Management, Governance, Bar, Compensation, Performance Improvement, Development Planning, Restructuring, Pay, Account Management, History, Resources, Hr, Team Performance, Bonus, Expansions, Shaping, Global Marketing, Recruiting, Performance Management

Publications & IP owners

Us Patents

Method And Apparatus For Automated Location Marking

US Patent:
6736180, May 18, 2004
Filed:
Oct 30, 2001
Appl. No.:
10/012609
Inventors:
Donald A. Anderson - Bellevue WA
Brice A. Johnson - Federal Way WA
James B. Andersen - Eatonville WA
Assignee:
The Boeing Company - Chicago IL
International Classification:
B05B 110
US Classification:
156356, 156357, 156384, 101123
Abstract:
A compliant marking tool for attachment to a fiber placement machine that is capable of marking detail locations on a work piece positioned on the fiber placement machine. The marking tool has a flexible member that is configured and adapted to bow and twist in response to the marking tool contacting the work piece. A holder is pivotably connected to the flexible member. A marking member is positioned in the holder and is capable of moving within the holder. The flexing of the flexible member along with the pivoting of the holder and the movement of the marking member allow the marking tool to follow the contours of the work piece and mark detail locations without damaging or at least minimizing the potential of damaging the work piece.

Method And Apparatus For Automated Location Marking

US Patent:
6824628, Nov 30, 2004
Filed:
Mar 9, 2004
Appl. No.:
10/797693
Inventors:
Donald A. Anderson - Bellevue WA
Brice A. Johnson - Federal Way WA
James B. Andersen - Eatonville WA
Assignee:
The Boeing Company - Chicago IL
International Classification:
B05B 110
US Classification:
156 64, 156277, 101123
Abstract:
A compliant marking tool for attachment to a fiber placement machine that is capable of marking detail locations on a work piece positioned on the fiber placement machine. The marking tool has a flexible member that is configured and adapted to bow and twist in response to the marking tool contacting the work piece. A holder is pivotably connected to the flexible member. A marking member is positioned in the holder and is capable of moving within the holder. The flexing of the flexible member along with the pivoting of the holder and the movement of the marking member allow the marking tool to follow the contours of the work piece and mark detail locations without damaging or at least minimizing the potential of damaging the work piece.

Systems And Methods Enabling Automated Return To And/Or Repair Of Defects With A Material Placement Machine

US Patent:
7039485, May 2, 2006
Filed:
Mar 12, 2004
Appl. No.:
10/799306
Inventors:
Roger W. Engelbart - St. Louis MO, US
Michael R. Chapman - Federal Way WA, US
Brice A. Johnson - Federal Way WA, US
Kathryn A. Soucy - Seattle WA, US
Reed Hannebaum - Mount Vernon IL, US
Steve Schrader - Bridgeton MO, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G06F 19/00
B32B 31/00
US Classification:
700110, 700117, 156379
Abstract:
A method generally includes electronically accessing positional data defining a defect location on a composite structure, and automatically causing a material placement machine to return to the defect location as defined by the positional data. The method can also include automatically causing the material placement machine to place or lay down material sufficient for repairing a defect at the defect location. Alternatively, the material placement machine may automatically return to a defect location, and then an operator may manually repair the defect at the defect location.

Method Of Transferring Large Uncured Composite Laminates

US Patent:
7228611, Jun 12, 2007
Filed:
Nov 18, 2003
Appl. No.:
10/717030
Inventors:
Donald A. Anderson - Bellevue WA, US
Brice A. Johnson - Federal Way WA, US
Stephen S. Spoon - Buckley WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B23P 11/02
B29C 65/00
B64C 1/00
US Classification:
29448, 29464, 29559, 156285, 156286, 156382, 156425, 264102, 264571, 244119, 244120
Abstract:
A method of transferring an uncured composite laminate skin from a lay-up surface of a male mandrel tool to a female cure tool includes defining multiple vacuum zones on the lay-up surface, each zone corresponding to one of a multiple of portions into which the skin is to be separated. For example, to separate the skin into two portions, a low profile seal of a first membrane to the lay-up surface is formed at a first vacuum zone and a second low profile seal for a second membrane is formed at a second vacuum zone. The method further includes laying up a composite laminate skin over all the vacuum zones; separating the composite laminate skin into portions, for example, a first portion over the first vacuum zone and a second portion over the second vacuum zone; and releasing the portions individually into cure tools having an outside mold line surface.

Multiple Head Automated Composite Laminating Machine For The Fabrication Of Large Barrel Section Components

US Patent:
7282107, Oct 16, 2007
Filed:
Aug 22, 2003
Appl. No.:
10/646509
Inventors:
Brice A. Johnson - Federal Way WA, US
Stephen S. Spoon - Buckley WA, US
Randal S. Darras - Auburn WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B65H 81/00
US Classification:
156169, 156173, 156175, 156425, 156433, 156441
Abstract:
An aircraft part manufacturing device for automated composite lamination on a mandrel surface of a tool having a rotational axis includes a mechanical supporting structure that supports multiple material delivery heads. The tool is moveable and rotatable relative to the mechanical supporting structure. The mechanical supporting structure provides for axial translation of the material delivery heads relative to the mandrel surface while the mandrel surface is rotated for laying down courses of composite material over the entire mandrel surface of the tool. The position and movement of each of the plurality of material delivery heads is individually adjustable. Arm mechanisms provide motion of each material delivery head in a direction normal to the mandrel surface; rotation about an axis normal to the mandrel surface; circumferential position adjustment in a hoop direction relative to the mandrel surface; and axial position adjustment relative to the other material delivery heads.

Optimizing Non-Productive Part Motion In An Automated Tape Laydown Machine

US Patent:
7720561, May 18, 2010
Filed:
Sep 21, 2007
Appl. No.:
11/859125
Inventors:
Wei-Pai Tang - Redmond WA, US
Brice Johnson - Federal Way WA, US
Daniel Edward Gonsor - Issaquah WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
G06F 19/00
G05B 13/02
US Classification:
700122, 700 28, 700111, 700173
Abstract:
The non-productive motion of an automatic composite tape laydown machine is optimized to increase the overall rate of the laydown. Ordering of tape courses is analyzed to determine the time required to move between courses using a time function that reflects operating characteristics and limitations of the tape laydown machine. The ordering is optimized by re-ordering, grouping and/or partitioning the tape courses so as to reduce the non-productive motion of the machine. The optimized ordering is used by a NC program that controls the operation of the machine.

Composite Material Placement Method And System

US Patent:
7867352, Jan 11, 2011
Filed:
Feb 13, 2006
Appl. No.:
11/352274
Inventors:
Brice A. Johnson - Federal Way WA, US
David J. Carbery - Vashon WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B32B 38/04
US Classification:
156250, 156256, 156193
Abstract:
To apply a course on a layup mold, a ply boundary that defines a ply area on the layup mold is determined and a tape of composite material is applied on the ply area at an oblique angle relative to the ply boundary. In addition, a leading edge of the tape is butt cut and the leading edge, and the ply boundary essentially converge. Furthermore, a trailing edge is generated. The trailing edge is a butt cut and the trailing edge and the ply boundary essentially converge.

Method Of Making Composite Panels For A Fuselage

US Patent:
7935289, May 3, 2011
Filed:
Apr 2, 2007
Appl. No.:
11/695561
Inventors:
Donald A. Anderson - Bellevue WA, US
Brice A. Johnson - Federal Way WA, US
Stephen S. Spoon - Buckley WA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B32B 37/00
US Classification:
264257, 264500, 264510, 264511, 264258
Abstract:
A method is provided for making a composite laminate aircraft skin for a fuselage in multiple composite panels. A resin-impregnated composite tape is placed on a lay-up surface of a mandrel tool to form the composite laminate aircraft skin as a barrel that is substantially the shape of a fuselage section. The barrel is cut into a plurality of panels on the mandrel tool, and at least one panel of the plurality of panels is transferred, individually and independently of all other of the plurality of panels, from the lay-up surface of the mandrel tool to a first cure tool of a plurality of cure tools having an aero surface tooled to an outer mold line. The at least one of the panels is cured on the first cure tool to form a cured composite panel. The first cure tool defines and controls the outer mold line of the at least one panel. The cured composite panel is removed from the first cure tool.

Possible Relatives

Cynthia L Johnson  David W Johnson  A Johnson  Cyril H Johnson  Cyrus Johnson  Cythina Johnson  D Johnson  Brice S Johnston  Brice R Meadows  Brice E Lamb 

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