Lock for retaining minidisks with rotors of a gas turbine engine

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United States of America Patent

PATENT NO 9945237
SERIAL NO

14765491

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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In accordance with one aspect of the disclosure, a rotor is disclosed. The rotor may include a disk having a central axis, an airfoil radially extending from the disk, a bayonet tab extending radially from the disk, and a lock. The lock may further include a short tab and a long tab, both extending radially from the disk and in an axial direction with respect to the central axis. The long tab may have a greater axial length than the short tab.

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Patent Owner(s)

  • UNITED TECHNOLOGIES CORPORATION

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Partyka, Julian West Springfield, US 13 90
Sandoval, Jonathan Perry Hebron, US 10 75

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