Method and assembly for extracting press fit bushings
AssigneeSikorsky Aircraft Corporation
InventorsDavid W. Caywood, Timothy James Conti
Life of this patent
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AssigneeSikorsky Aircraft Corporation
InventorsDavid W. Caywood, Timothy James Conti
Estimating the term…
An assembly for removing a bushing is provided including a mandrel having a size and shape similar to the bushing and a receiver having a hollow interior cavity. A fastener extends through an opening formed in both the mandrel and the receiver. A socket attachment has a first opening configured to removably couple to a first end of the fastener and a second opening configured to removably couple to a torque delivery tool. A biasing mechanism arranged adjacent a second end of the fastener is configured to generate a biasing force to drive the mandrel against a bushing in response to a coupling of the socket attachment and the fastener.
A socket attachment, comprising:
A method of removing a bushing, comprising:
Dependencies are inferred from the claim text.