Gear arrangement

• US 8,568,089 B2
• Filed: 06/03/2010
• Issued: 10/29/2013
• Est. Priority Date: 06/03/2010
• Status: Active Grant

• Current Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Lemmers, Glenn C. Jr., Behling, David S., Rateike, Leroy R.
• Primary Examiner(s): Wiehe, Nathaniel
• Assistant Examiner(s): SEABE, JUSTIN D
• Application Number:
  US12/793,122
• Publication Number:
  US 20110299971A1
• Time in Patent Office: 1,244 Days
• Field of Search: 415/122.1, 415/124.1, 415/124.2, 416/170.R, 310/75.R, 310/83
• US Class Current: 415/122.1
• CPC Class Codes: F01D 11/10 using sealing fluid, e.g. steam
• CPC Class Codes: F02C 7/32 Arrangement, mounting, or driving, of auxiliaries
• CPC Class Codes: F16D 1/10 Quick-acting couplings in which the parts are connected by simply bringing them together axially
• CPC Class Codes: F16D 11/14 with clutching members movable only axially F16D11/02, F16D11/08 take precedence
• CPC Class Codes: F16D 2001/103 the torque is transmitted via splined connections
• CPC Class Codes: F16D 3/06 specially adapted to allow axial displacement

Abstract

An example gear arrangement includes a gearbox shaft and a journal shaft. The journal shaft establishes an opening that receives an end portion of the gearbox shaft. The gearbox shaft is configured to rotate the journal shaft. The journal shaft is configured to selectively rotatably couple with another shaft. The journal shaft is allowed to align to the bearing surface while the gearbox shaft allows for misalignment between the accessory and gearbox drive.

Claims

1. A gas turbine engine gearbox arrangement, comprising:

a disconnect shaft;

a gearbox shaft having a first end rotatably coupled to an accessory gearbox; and

a cup shaped journal shaft received over an opposing second end of the gearbox shaft, the cup shaped journal shaft configured to rotate together with the gearbox shaft, the cup shaped journal shaft further configured to selectively rotatably engage with the disconnect shaft to drive a rotor shaft of the gas turbine engine, wherein the cup shaped journal shaft includes walls extending along a rotational axis and a floor extending radially toward the axis past splines on the second end of the gearbox shaft.

2. The gas turbine engine gearbox arrangement of claim 1, wherein the first end of the gearbox shaft comprises splines that rotatably couple the gearbox shaft to the accessory gearbox, and the second end of the gearbox shaft comprises splines that rotatably couple the gearbox shaft to the journal shaft.

3. The gas turbine engine gearbox arrangement of claim 1, wherein the first end of the gearbox shaft has a first diameter and the second end of the gearbox shaft has a second diameter, the first end greater than the second end.

4. The gas turbine engine gearbox arrangement of claim 1, wherein the disconnect shaft is rotatably coupled to a variable frequency generator.

5. The gas turbine engine gearbox arrangement of claim 1, wherein the gearbox shaft is configured to rotate the journal shaft about a first axis when the gearbox shaft is rotating about a second axis transverse to the first axis.

6. The gas turbine engine gearbox arrangement of claim 1, including bearings configured to limit axial and radial movements of the journal shaft.

7. The gas turbine engine gearbox arrangement of claim 6, wherein the bearings comprise carbon.

8. The gas turbine engine gearbox arrangement of claim 7, wherein the bearings further comprise steel.