Reduction gear with epicyclic gear train having roller-bearing-mounted planet spindles

• US 8,986,146 B2
• Filed: 05/29/2013
• Issued: 03/24/2015
• Est. Priority Date: 05/30/2012
• Status: Active Grant

• Current Assignee: Safran Aircraft Engine Company
• Original Assignee: Snecma (Safran SA)
• Inventors: Gallet, Francois
• Primary Examiner(s): Mansen, Michael
• Assistant Examiner(s): Dang, Tinh
• Application Number:
  US13/904,483
• Publication Number:
  US 20130324343A1
• Time in Patent Office: 664 Days
• Field of Search: 475/96, 475/233, 475/305, 475/331, 475/348, 192/82.T
• US Class Current: 475/96
• CPC Class Codes: F02C 3/107 with two or more rotors connected by power transmission
• CPC Class Codes: F02C 7/36 Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user F02C3/107 - F02C3/13 and F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H
• CPC Class Codes: F02K 3/06 with front fan
• CPC Class Codes: F05D 2260/4031 as in toothed gearing
• CPC Class Codes: F16H 2057/085 Bearings for orbital gears
• CPC Class Codes: F16H 3/44 using gears having orbital motion the gear-ratio being changed by inversion of torque direction F16H3/005
• CPC Class Codes: F16H 57/082 Planet carriers
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A reduction gear with epicyclic gear train including an annulus gear, and at least one planet gear rolling on the annulus gear and able to rotate about a planet spindle borne by a planet carrier is provided. The planet spindle is mounted such that it can itself rotate about its axis relative to the planet carrier. The reduction gear is suitable for mounting in a high bypass ratio jet engine for driving the fan thereof.

Claims

1. A reduction gear with epicyclic gear train comprising:

an annulus gear; and

at least one planet gear rolling on said annulus gear and able to rotate about a planet spindle borne by a planet carrier, said planet spindle being mounted such that said planet spindle can itself rotate about its axis relative to said planet carrier,

wherein there are two modes of operation;

a first mode in which said planet spindle is rigidly attached to the planet carrier and a second mode in which said planet spindle can rotate freely relative to the planet carrier.

2. The reduction gear as claimed in claim 1, wherein the planet gear rotates about its planet spindle by means of a journal bearing and the planet spindle is mounted on the planet carrier via a rolling bearing.

3. The reduction gear as claimed in claim 1, wherein switching from one mode to the other is performed as a function of temperature of lubrication oil of said reduction gear.

4. The reduction gear as claimed in claim 3, wherein switching from one mode to the other is actuated by an actuation means positioned so as to be in contact with said lubrication oil and comprising a shape memory material.

5. The reduction gear as claimed in claim 4, wherein said actuation means is a flange plate in a shape of a circular annulus, a central bore of which is attached to said spindle and an outer end of which moves in an axial direction as a function of the temperature of the lubrication oil.

6. The reduction gear as claimed in claim 5, wherein said flange plate comprises, at an outer end thereof, a first face which extends in a radial direction facing a first corresponding face positioned on said planet carrier, an axial positioning of said outer end, produced by the oil at a nominal operating temperature of the reduction gear, being designed so as to cause said first and first corresponding faces to press against each other.

7. The reduction gear as claimed in claim 5, wherein said flange plate comprises, at outer end thereof, a second face which extends in a radial direction facing a second corresponding face positioned on said planet gear, an axial positioning of said outer end, produced by the oil at a temperature below a nominal operating temperature of the reduction gear, being designed so as to cause said second and second corresponding faces to press against each other.

8. The reduction gear as claimed in claim 6, wherein said flange plate exerts sufficient pressure against a wall of the planet carrier such that, in the event of an overtorque as the result of the journal bearings seizing, the planet spindle can still rotate in order to prevent the reduction gear from locking up.

9. A fan module comprising a fan shaft driven by a reduction gear as claimed in claim 1.

10. A dual-flow jet engine comprising a fan module as claimed in claim 9.