High speeds with heavy loads characterize the operating environment of tires used on business aircraft. In order to design tires which can withstand these operational dynamic forces, the engineer must select the proper tire size, incorporating the necessary design features into the tire construction, and thoroughly testing the tire to ensure compliance with performance requirements established by the airframe engineer. Tire construction considerations include tire carcass (beads, body plies, reinforcement plies, and liner), tread, and sidewalls. Tire size description/designation is explained, including ply rating and speed rating. Tire size selection criteria include tire/gear/airframe size relationship, wheel-well space, braking capacity, strut configuration, gear geometry and loading, flotation (contact area and inflation), speed requirement, water deflection, tire weight limitation, and replacement availability. Tire testing requirements are outlined. Proper selection of tire size results in optimum tire and aircraft performance with minimum cost for both airframe manufacturer and end user.

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  • Supplemental Notes:
    • Presented at SAE Business Aircraft Meeting and Exposition, Wichita, Kansas, 3-6 April 1979.
  • Corporate Authors:

    Society of Automotive Engineers (SAE)

    400 Commonwealth Drive
    Warrendale, PA  United States  15096
  • Authors:
    • Gehrett, L J
  • Publication Date: 1979

Media Info

Subject/Index Terms

Filing Info

  • Accession Number: 00387299
  • Record Type: Publication
  • Source Agency: National Highway Traffic Safety Administration
  • Report/Paper Numbers: SAE 790598, HS-029 347U
  • Files: HSL, USDOT
  • Created Date: Jul 30 1984 12:00AM