Coupling system comprising self locking joint

Patent metadata

Field	Value
Publication number	US-10280800-B2
Application number	US-201816149419-A
Country	US
Kind code	B2
Filing date	Oct 2, 2018
Priority date	Nov 19, 2015
Publication date	May 7, 2019
Grant date	May 7, 2019

Abstract

Disclosed is a coupling system comprising joints configured to friction lock under compressive pressure via tapered teeth for joining rotating components, which may be rotating components of a gas turbine, or other engine. The coupling system provides the alignment orientation for the joined components, and eliminates the need for extraneous fasteners, bolts, interference fits and/or keying arrangements. The coupling system further enables material optimization by allowing for use of different materials throughout different engine sections, depending on the operating parameters.

First claim

The invention claimed is:

1. A coupling method for joining rotating components of a jet engine comprising:
stacking the rotating components to form a rotating stack aligned along a central axis, wherein the rotating components are supported on joints, wherein the joints comprise a first joint and a second joint, wherein the rotating stack is formed by adjacently aligning the first joint with the second joint, wherein each of the joints comprises tapered teeth, wherein the tapered teeth of the first joint are configured intermesh and interlock with the tapered teeth of the second joint and vice-versa, wherein each tooth of the tapered teeth comprises tapered side walls, and wherein a first circumferential span of top portions of the tapered teeth of the first joint is greater than a second circumferential span of bottom portions of wells defined circumferentially between adjacent teeth of the tapered teeth of the second joint; and
applying a compressive force to the rotating stack to cause the joints to friction interlock with one another due to the frictional forces between the tapered sidewalls.

2. The coupling method of claim 1 , wherein the rotating components are rotors, and the rotating stack is a rotor stack of the jet engine.

3. The coupling method of claim 1 , wherein the tapered teeth are axially tapered at an angle approximately equal to or less than 45 degrees.

Assignees

• United Technologies Corp

Inventors

• Mariano Thomas A
• Arnold Jason

Classifications

• F01D5/026

  Shaft to shaft connections · CPC title

• Y02T50/671

  Cross-Sectional Technologies · mapped topic

• F01D25/246 Primary

  Fastening of diaphragms or stator-rings · CPC title

• F05D2260/36

  by a form fit connection, e.g. by interlocking · CPC title

• F01D5/06

  Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections {(F01D5/022, F01D5/023 take precedence)} · CPC title