IP Library › Granted Patent US 10,668,604
Granted Patent B2
US 10,668,604 · App. 15/516,740 · Granted Jun 2, 2020

Non-destructive cold extractions of press fit bushings

Inventors: David W. Caywood (Avon, CT); Timothy James Conti (Shelton, CT)
Assignee: SIKORSKY AIRCRAFT CORPORATION
B25B27/062B64C27/06B64F5/40
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Quick Facts
Patent No.
US 10,668,604
App. No.
15/516,740
Granted
Jun 2, 2020
Kind
B2
Abstract

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.

Claims (18)

1. An assembly for removing a bushing, comprising:

a mandrel having a size and shape similar to the bushing;

a receiver having a hollow interior cavity;

a fastener extending through an opening formed in both the mandrel and the receiver;

a socket attachment having 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; and

a biasing mechanism arranged adjacent a second end of the fastener, the biasing mechanism being configured to generate a biasing force to drive the mandrel against the bushing in response to a coupling of the socket attachment and the fastener.

2. The assembly according to claim 1 , wherein the mandrel includes at least one chamfer configured to ensure proper engagement with a bushing.

3. The assembly according to claim 1 , wherein the first end of the fastener includes a plurality of first threads and the first opening of the socket attachment includes a plurality of second threads, the plurality of second threads being complementary to the plurality of first threads.

4. The assembly according to claim 1 , wherein the biasing mechanism comprises a coil spring.

5. The assembly according to claim 1 , wherein the biasing mechanism is positioned between a portion of the fastener and the mandrel.

6. The assembly according to claim 1 , wherein the biasing mechanism is positioned between a portion of the fastener and the receiver.

7. The socket attachment according to claim 1 , wherein the torque delivery tool is a wrench.

8. The socket attachment according to claim 7 , wherein the torque delivery tool is a socket wrench and the second opening is configured to receive a post extending from a head of the socket wrench.

9. The socket attachment according to claim 1 , further comprising:

a mandrel arranged adjacent a bushing, the mandrel having a size and shape similar to the bushing;

a receiver having a hollow interior cavity;

a fastener extending through an opening formed in both the mandrel and the receiver, the socket attachment being coupled to a first end of the fastener; and

a biasing mechanism arranged adjacent a second end of the fastener, the biasing mechanism being configured to generate a biasing force to drive the mandrel against the bushing in response to a coupling of the socket attachment and the fastener.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 5, 2017
From: CAYWOOD, DAVID W.; CONTI, TIMOTHY JAMES
To: SIKORSKY AIRCRAFT CORPORATION
Reel/Frame 041853/0336 →
Continuity (2)
Provisional Application 62060671 · Oct 7, 2014
Related Publication 20170297185A1 · Oct 19, 2017
Cited By (9)
US 1,128,397 US 1,128,413 US 1,132,695 US 1,136,851 US 1,138,623 US 12,285,847 US 12,358,108 US 12,372,119 US 12,583,084