AIRCRAFT PROPELLERS
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United States of America Patent
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app pub date -
Aug 12, 2014
filing date -
Aug 12, 2011
priority date (Note) -
Abandoned
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Abstract
An aircraft propeller taper bore insert apparatus is provided. The apparatus includes a tapered outer surface and an inner surface. The outer surface is dimensioned and configured to fit within and be of substantially a same size and shape as an aircraft propeller taper bore or an aircraft propeller balancing tube. The inner surface defines an inner cavity configured to receive a balancing medium and includes a plurality of retention formations arranged thereon and configured to support the balancing medium.
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