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Bruce L Bunin

from Boca Raton, FL
Age ~68
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Also known as:
Bruce Lee Bunin, Bruce L Bonin, Bruce L Bunim
Related to:
Carrianne DoebberShawn P MartinWilliam A Winters, 69Luke Martin, 49Cleo Adams, 76Bradford Chace, 67
Connected to:
Carl B Bunin, 75John C Bunin, 52Alfred G Buning, 62James Bunio, 46Wendy L Bunis, 60Brian L Buniva, 74John R Buniva, 68Sabrina E Buniva, 59Edi Bunjaku, 46Lorraine A Bunjaporte, 70

Bruce Bunin Phones & Addresses

  • Boca Raton, FL
  • 2770 NE 57Th St, Ft Lauderdale, FL 33308 (714) 962-5515
  • Fort Lauderdale, FL
  • Henderson, NV
  • 5651 Mangrum Dr, Huntington Beach, CA 92649
  • 8539 Owens River Cir, Fountain Valley, CA 92708 (714) 962-5515
  • Los Angeles, CA
  • Fontana, CA
  • Orange, CA

Work

Company: Embraer Jan 2019 Position: Vice president, business development - north america, embraer defense and security

Education

Degree: Master of Business Administration, Masters School / High School: University of Southern California - Marshall School of Business 2002 to 2004 Specialities: Business Administration

Skills

Program Management • Strategic Planning • New Business Development • Engineering • Aerospace • Proposal Writing • Systems Engineering • Earned Value Management • Aircraft • Business Development • Project Management • Strategy • Integration • Engineering Management • Product Development • Leadership • Analysis • Government • Cross Functional Team Leadership • Requirements Management • Strategic Partnerships • Process Improvement • Team Leadership • Dod • Military • Operations Management • Risk Management • Manufacturing • Contract Negotiation • Management • Project Planning

Interests

Arts and Culture

Industries

Aviation & Aerospace

Resumes

Resumes

Bruce Bunin Photo 1

Vice President, Business Development - North America, Embraer Defense And Security

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Location:
8539 Owens River Cir, Fountain Valley, CA 92708
Industry:
Aviation & Aerospace
Work:
Embraer
Vice President, Business Development - North America, Embraer Defense and Security
Embraer
Director - Business Development, Embraer Defense and Security
Boeing Mar 2010 - Jun 2013
Director - Next Generation Mobility
Boeing Jan 2009 - Mar 2010
Director and Program Manager - Italy Kc-767 Tanker Program
Boeing Mar 2006 - Jan 2009
Director and Program Manager - Joint Cargo Aircraft Program
Education:
University of Southern California - Marshall School of Business 2002 - 2004
Master of Business Administration, Masters, Business Administration Rensselaer Polytechnic Institute 1974 - 1979
Master of Science, Masters, Bachelors, Bachelor of Science, Civil Engineering University of Southern California
Skills:
Program Management
Strategic Planning
New Business Development
Engineering
Aerospace
Proposal Writing
Systems Engineering
Earned Value Management
Aircraft
Business Development
Project Management
Strategy
Integration
Engineering Management
Product Development
Leadership
Analysis
Government
Cross Functional Team Leadership
Requirements Management
Strategic Partnerships
Process Improvement
Team Leadership
Dod
Military
Operations Management
Risk Management
Manufacturing
Contract Negotiation
Management
Project Planning
Interests:
Arts and Culture

Business Records

Name / Title
Company / Classification
Phones & Addresses
Bruce L. Bunin
President
Cavemanity, Inc
4645 Perham Rd, Corona del Mar, CA 92625
8539 Owens Riv Cir, Santa Ana, CA 92708

Publications

Us Patents

Optimized Bolted Joint

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US Patent:
45794758, Apr 1, 1986
Filed:
Jan 23, 1984
Appl. No.:
6/573162
Inventors:
Leonard J. Hart-Smith - Long Beach CA
Bruce L. Bunin - Huntington Beach CA
Donald J. Watts - Fountain Valley CA
Assignee:
The United States of America as represented by the Administrator of the
National Aeronautics and Space Administration - Washington DC
International Classification:
F16B 202
F16D 102
US Classification:
403312
Abstract:
A joint for joining composite material such as segments of the skin 12 and 13 of an aircraft. Tapered splice plates 30 and 31 overlap the ends 14 and 15 of the skin. The thickest portion 34 of the splice plates overlap the ends 14 and 15. The splice plates are clamped together on the skin segments 12 and 13 by fasteners 50, 52, 54 and 56. The tapered splice plates are designed to minimize load transfer at the outermost bolt row 56 coincident with maximum bypass stress in the skin segments while simultaneously maximizing load transfer in both the skin segments and splice plates at the innermost bolt row 50.
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Bruce L Bunin from Boca Raton, FL, age ~68 Get Report