Structural Considerations of Steel Landing Gear Springs

710400

02/01/1971

Event
National Business Aircraft Meeting and Engineering Display
Authors Abstract
Content
Aircraft produced by Cessna have, for a number of years, used steel landing gear springs as the major portion of the aircraft main or tail landing gears. These steel springs are relatively simple in design and manufacture, and have proved to be durable.
This paper discusses some of the factors involved in the design of a spring steel landing gear, analysis methods, and design goals used at Cessna. Certification requirements and methods of compliance for landing gears are also discussed. The analysis methods employed have been proved acceptable by the ability of the gears to pass certification tests without modification, and by service experience.
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DOI
https://doi.org/10.4271/710400
Pages
12
Citation
McCosh, D., "Structural Considerations of Steel Landing Gear Springs," SAE Technical Paper 710400, 1971, https://doi.org/10.4271/710400.
Additional Details
Publisher
Published
Feb 1, 1971
Product Code
710400
Content Type
Technical Paper
Language
English