Tapered bearings

Abstract

A gear support assembly for a turbine engine includes an epicyclic gear arrangement and a first tapered bearing and a second tapered bearing spaced apart from the first tapered bearing. The first tapered bearing and the second tapered bearing are arranged axially forward of the epicyclic gear arrangement and support the epicyclic gear arrangement.

1 . A gear support assembly for a turbine engine, comprising:
 an epicyclic gear arrangement;   a first tapered bearing and a second tapered bearing spaced apart from the first tapered bearing, the first tapered bearing and the second tapered bearing being arranged axially forward of the epicyclic gear arrangement and supporting the epicyclic gear arrangement.   
     
     
         2 . The gear support assembly as recited in  claim 1 , wherein the first tapered bearing and the second tapered bearing are located radially inwards from a radially outer surface of the epicyclic gear arrangement. 
     
     
         3 . The gear support assembly as recited in  claim 1 , wherein the first tapered bearing and the second tapered bearing are located radially outwards of a radially inner surface of the epicyclic gear arrangement. 
     
     
         4 . The gear support assembly as recited in  claim 1 , including a support arm extending forward from the epicyclic gear arrangement, at least one of the first tapered bearing and the second tapered bearing being mounted on the support arm. 
     
     
         5 . The gear support assembly as recited in  claim 4 , wherein the support arm is connected at one end at a radially outer location of the epicyclic gear arrangement. 
     
     
         6 . The gear support assembly as recited in  claim 1 , wherein at least one of the first tapered bearing and the second tapered bearing includes a cylindrical roller element. 
     
     
         7 . The gear support assembly as recited in  claim 6 , wherein the cylindrical roller element is supported on a tapered race. 
     
     
         8 . The gear support assembly as recited in  claim 1 , wherein the first tapered bearing and the second tapered bearing are spaced an equivalent radial distance from a central axis of the epicyclic gear arrangement. 
     
     
         9 . The gear support assembly as recited in  claim 1 , wherein the first tapered bearing includes a first roller element defining a first rotational axis and the second tapered bearing includes a second roller element defining a second rotational axis such that the first rotational axis and the second rotational axis intersect at a position that is radially inwards from the first roller element and the second roller element. 
     
     
         10 . The gear support assembly as recited in  claim 1 , wherein the first tapered bearing includes a first roller element defining a first rotational axis and the second tapered bearing includes a second roller element defining a second rotational axis such that the first rotational axis and the second rotational axis intersect at a position that is radially inwards from a central axis of the epicyclic gear arrangement. 
     
     
         11 . A turbine engine comprising:
 a compressor section;   a combustor arranged in fluid receiving communication with the compressor section;   a turbine section arranged in fluid receiving communication with the combustor;   an epicyclic gear arrangement coupled to be driven by the turbine section; and   
       a first tapered bearing and a second tapered bearing spaced apart from the first tapered bearing, the first tapered bearing and the second tapered bearing being arranged axially forward of the epicyclic gear arrangement and supporting the epicyclic gear arrangement. 
     
     
         12 . The turbine engine as recited in  claim 11 , including a fan located axially forward of the compressor section, wherein a forward one of the first tapered bearing and the second tapered bearing is located at an equivalent axial position of the fan. 
     
     
         13 . The turbine engine as recited in  claim 11 , including a fan located axially forward of the compressor section, wherein a forward one of the first tapered bearing and the second tapered bearing is located at an equivalent axial position of the fan and a rear one of the first tapered bearing and the second tapered bearing is located at a non-equivalent axial position of the fan. 
     
     
         14 . The turbine engine as recited in  claim 11 , wherein the first tapered bearing and the second tapered bearing are located radially inwards from a radially outer surface of the epicyclic gear arrangement. 
     
     
         15 . The turbine engine as recited in  claim 11 , including a support arm extending forward from the epicyclic gear arrangement, at least one of the first tapered bearing and the second tapered bearing being mounted on the support arm. 
     
     
         16 . The turbine engine as recited in  claim 15 , wherein the support arm is connected at one end at a radially outer location of the epicyclic gear arrangement. 
     
     
         17 . The turbine engine as recited in  claim 11 , wherein at least one of the first tapered bearing and the second tapered bearing includes a second cylindrical roller element. 
     
     
         18 . The turbine engine as recited in  claim 17 , wherein the cylindrical roller element is supported on a tapered race. 
     
     
         19 . The turbine engine as recited in  claim 11 , wherein the first tapered bearing and the second tapered bearing are spaced an equivalent radial distance from a central axis of the epicyclic gear arrangement. 
     
     
         20 . The turbine engine as recited in  claim 11 , wherein the first tapered bearing includes a first roller element defining a first rotational axis and the second tapered bearing includes a second roller element defining a second rotational axis such that the first rotational axis and the second rotational axis intersect at a position that is radially inwards from the first roller element and the second roller element. 
     
     
         21 . The turbine engine as recited in  claim 11 , wherein the first tapered bearing includes a first roller element defining a first rotational axis and the second tapered bearing includes a second roller element defining a second rotational axis such that the first rotational axis and the second rotational axis intersect at a position that is radially inwards from a central axis of the epicyclic gear arrangement.