Experience
         Ron Nelson, ClosedMold Composites’ founder, has extensive experience in the successful design and development of composite products.
           Successful product lines include Trek Bicycle Company's OCLV line of road and mountain bicycles, which Lance Armstrong has rode to victory in the last 4 Tour de Frances; and Swix Sports' molded downhill ski poles which Picabo Street won a Gold Medal in the 98' Olympics, and Bode Miller won two Silver Medals in the 2002 Olympics. (ClosedMold presentation on bicycle molding.)
          This provides an unparalleled level of practical experience and a knowledge base that can be applied to your product development.              
 

Experience - Ron H. Nelson - President, ClosedMold Composites        

President, Founder, Chief Engineer - Radius Engineering, Inc. - Salt Lake City, Utah - 1988 to 2001

Summary

  • Founded company and built to $3.5MM in annual sales using only limited personal investment. Order backlog exceeded $4.5MM at the time of Mr. Nelson's departure.
  • Developed Radius' closed-mold manufacturing technologies for advanced composite materials that are the foundation of Radius' business and are unequaled in sophistication and productivity in the world today. This allows Radius to count nearly every major aerospace company in the world, and the majority of composites research organizations, as customers.
  • Oversaw all aspects of building and running corporation from choosing company name at inception and completing incorporation process, through negotiation and drafting of all large contracts to date. Includes all financial and facilities management, personnel issues, marketing and direct participation in all technology development.
Commercial Products
Aerospace Structure
Closed–Mold Processes & Equipment Development

  • Tool design and construction including materials, machining methods, surface treatments, design methodology; injection port and resin gating design, cavity venting and vacuum port design, integral heating and cooling systems, bladder fitting design. 
  • Internal pressure bladder design and fabrication for elastomeric and thermoplastic bladder materials formed by methods such as dipping and dispersion coating with lost cores, injection molding, thermoform shaping of films, heat sealing, and rotational molding. 
  • Resin handling and injection/cure processing, including RTM injection system design and construction for Radius' unique dual/single cylinder designs, and its pail unloaders and meter mix designs. Includes vacuum systems and equipment for resin premold degassing, and mold and fiber form evacuation. Fiber preform construction and assembly.
  • Press design and fabrication, including structural and pneumatic systems, press platen heating and cooling system design and construction. Process control system design and construction including distributed control systems and host PC software interface.
Contract Drafting & Negotiation

  • Extensive experience in drafting and negotiating numerous large development contracts, including understanding of legal implications of every contractual term, and potential means of enforcement. These include: non-licensing contracts of $1MM to $3MM negotiated with Bombardier, British Aerospace, and Toyota Motor Sales/USA..
  • Drafted and negotiated 11 major licensing agreements including those with Trek Bicycle Co., Callaway Golf Company, True Temper Sports, Johnson Controls Inc./Automotive Systems Division, Pure Fishing dba Fenwick, Swix Sports, and Raytheon Aircraft. These agreements produced a total royalty income to Radius of approximately $2.25MM, and also typically included contractual work ranging from $500K to $2MM each.
Intellectual Property Management

  • Extensive patent application formulation, preparation, and drafting including detailed construction of claim language, and negotiation of final claim language through office actions and examiner meetings. 
  • Defined strategy for management and protection of intellectual property including drafting nondisclosure/non-compete employment agreements including unique agreements for senior personnel and special situations.

Senior Engineer Composite Structures - Hercules Aerospace, Inc. - Magna, Utah - 1981 to 1988

Structural Design & Analysis
  • Galileo Space Probe Antenna Ribs Critical Design Review Stress Analysis
  • Structural analysis for redesign on Hercules-built McClaren MP4 Formula One race car chassis.
  • Lead engineer over four engineers and group responsible for structural analysis and design on a wide variety of composite structures including all military and commercial airframe, and naval structures. 
Process Analysis & Development
  • Managed four-year $100 K/year IR&D project including extensive work on analytical fabrication process modeling for advanced composite structures, and software development of composite structural analysis methods. 
  • Developed new single cure to replace two-step cure process for a 2 inch thick, 20 foot long cylindrical laminate (largest thick prepreg laminate cured in a single step at that time) used in a bomber rotary launcher shaft, resulting in significant cost savings. 
  • Designed a variety of metal and composite tooling including tool design for fiber placed B1-B rear wing spar. 
Design & Development 767 Torsion Springs
  • Design/Development of Boeing 767 Graphite Torsion Spring 
  • Design, structural analysis, and process development for the production of a graphite torsion spring used in counterbalance mechanism on Boeing 767 doors.
  • Lead engineer on pre-proposal efforts, and proposal preparation through the final qualification stress analysis, including tool design, and analysis of development and qualification programs.
  • One of the largest sales volume and longest running composite structures production programs at Hercules Aerospace (now Alliant TechSystems). Pre-proposal work began in 1983, production in about 1986, and still in production. 

7 U.S. Patents Issued (12 as of 8/02')and 10 Pending With Most Licensed For Commercial Use

Issued Patents

  • Method of Making a Composite Bicycle Frame Using Composite Lugs, No. 5,624,519. Licensed to Trek Bicycle Corporation for OCLV line of bicycles.
  • Method for Manufacturing Composite Shafts with Injection Molded, Rigidized Bladder with Varying Wall Thickness, No. 6,143,236. Licensed to Swix Sports and then to True Temper Sports, both for golf shafts.
  • Composite Golf Club Shaft, No. 5,692,970. Licensed to Swix Sport and then to True Temper Sports both for golf shafts.
  • Method of Manufacturing a Composite Golf Club Head, No. 5,985,197. Applied for during development pursuant to licensing agreement with Callaway Golf Co.
  • Composite Backing Structure for Spray metal Tooling, No. 5,073,589. "Soft" tooling for closed-mold processing, developed with two Utah Technology Finance Corp. grants.
  • Composite Pole Manufacturing Process for Varying Non-Circular Cross-Sections 
    and Curved Center lines
    , No. 5,534,203.
    Licensed to Swix Sport for downhill ski poles. Licensed to Pure Fishing dba Fenwick for fishing rods.
  • Composite Pole and Manufacturing Process for Composite Poles of Varying Non-Circular Cross-Sections and Curved Center lines, No. 5,505,492. Licensed to Swix Sports for downhill ski poles.
Pending Patents

  • Composite Bicycle Frame And Method , No. 08/865,491, is a article patent on bike lugs with high interleave ratio plies; Method for Manufacture of Composite Bicycle Frame , No. 09/333,792 is a method patent on the fabrication process. Both applications cover a successor technology to Trek OCLV process.  Applications published as: Composite Bicycle Frame And Method Of Construction Thereof, No. WO09854046A2.
  • Injection Molded, Rigidized Bladder With Varying Wall Thickness For Manufacturing Composite Shafts , No. 09/333,724. Licensed to Swix Sport and True Temper Sports both for golf shafts. Application published as: Method For Manufacturing Composite Shafts With Injection Molded, Rigidized Bladder With Varying Wall Thickness, No. WO09737725A2, and separately as: No. WO09737725A3.
  • Method for Manufacture of Composite Aircraft Control Surfaces No. 09/471,620. Licensed to Raytheon Aircraft Co. for Premier 1 control surfaces. 
  • Composite Golf Club Head No. 09/441,357. Applied for during development pursuant to licensing agreement with Callaway Golf Co. 

Bachelor of Science Mechanical Engineering - University of Wyoming - 1980

 

  • Overall/Major G.P.A. = 3.83/3.97 (4.00 scale), President's Honor Roll six semesters, Dean's List two semesters Laramie, Wyoming
  • Lab Assistant, Composite Materials Research Group, Mechanical Engineering Department.

Notable Publications

 
  • R. H. Nelson, D. S. Cairns, Prediction of Dimensional Changes in Composite Laminates During Cure , 34th International SAMPE Symposium and Exhibition,  May 8-11, 1989. Note: First paper analyzing dimensional changes occurring in curved composites laminates during cure due to tool induced residual stresses, and thermal and resin chemical shrinkage strain.
  • Milovich, D., Nelson, R., "Aerospace Resin Transfer Molding, A Multidisciplinary Approach", SME Technical Paper, Resin Transfer Molding for the Aerospace Industry Conference: March 1990. Note: One of first studies of aerospace RTM including testing and analytical process modeling. First analytical modeling of greatly increased resin flow on tool surfaces relative to inside fiber bed.

Professional memberships and Accreditations

 
  • Licensed Professional Engineer, State of Utah
  • Member, Industrial Advisor Board, Dept. of Mechanical Engineering, University of Utah
  • LES (Licensing Executive Society)
  • SAMPE (Society for Advancement of Materials and Process Engineering) 

Computer Skills

 

 

 

ClosedMold Composites
4210 South Monarch Way
Salt Lake City, Utah 84124

Phone (801) 277-0309
Fax (801) 277-0298
Cellular (801) 231-4912

Email:mailto:ronnelson@closedmold.com
(alt: ronnelson@xmission.com)

 

 

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