Duramold

Duramold

Duramold

Composite wood material process


Duramold is a composite material process developed by Virginius E. Clark. Birch or poplar plies are impregnated with phenolic resin and laminated together in a mold under heat (280 °F, 138 °C) and pressure for use as a lightweight structural material.[1] Similar to plywood, Duramold and other lightweight composite materials like the similar Haskelite were considered critical during periods of material shortage in World War II, replacing scarce materials such as aluminum alloys and steel.[2][3]

The Hughes H-4 Hercules, made of birch ply Duramold
Samples of Duramold at the Evergreen Aviation & Space Museum

The material has some advantages over metal in strength, construction technique, and weight. A cylinder made of Duramold is 80% stronger than a cylinder made of aluminum.[4] Over 17 varieties of Duramold were developed, using various combinations of types of wood in thin plies.[5] The Duramold process has also been used to make radomes for aircraft, as well as missile bodies.[citation needed]

Virginius Clark developed Duramold for Fairchild Aircraft, working with George Meyercord of the Haskelite Corporation.[6] Fairchild patented the process, designing and constructing the F-46 as the first aircraft made using the Duramold process, and forming the Duramold Corporation.[7] Several aircraft used Duramold in parts of their structure, the largest manufactured with the process being the Hughes H-4 Hercules designed by Howard Hughes and Glenn Odekirk, which was built almost completely with Duramold including very large sections.[3] For this use, Hughes Aircraft bought the rights to use of Duramold on aircraft exceeding 20,000 lb; Fairchild and Meyercord otherwise retained the rights,[8] but the material was found to be poorly adapted to heavy aircraft.[5]

The Duramold and Haskelite process was first developed in 1937, followed by Gene Vidal's Weldwood and later the Timm Aircraft Company's Aeromold process, which differs in that it is baked at a low 100 °F (38°C) at cutting and forming, and 180 °F (82°C) for fusing together sections after the resins are added.[9] In the United Kingdom, the De Havilland Aircraft Company (founded by Geoffrey de Havilland, a cousin of Olivia de Havilland, the actress who dated Howard Hughes in 1938) used similar composite construction for aircraft, including the DH.88 Comet, DH.91 Albatross, the Mosquito, and Vampire.

See also


References

  1. Flight International, Volume 42.
  2. Popular Science, September 1943.
  3. Dana T. Parker, Building Victory: Aircraft Manufacturing in the Los Angeles Area in World War II, Cypress, CA, 2013, ISBN 978-0-9897906-0-4, pp. 51-52, 56. ISBN 978-0-9897906-0-4.
  4. Journal of the American Society of Naval Engineers, Volume 52.
  5. Charles Barton (1982). Howard Hughes and His Flying Boat. Fallbrook, California: Aero Publishers. p. 85. OCLC 561599885.
  6. Barton, p. 83.
  7. Frank Woodring; Suanne K. Woodring (1982). Fairchild Aircraft. Charleston, South Carolina: Arcadia. p. 22. ISBN 9780738544397.
  8. Barton, p. 84.
  9. Richard Ballard, "Plastic Airplanes", The Ohio State Engineer, April 1942, pp. 24, 26.

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