Stub shaft

Abstract

A controlled collapse stub shaft allows controlled axial-movement of a mainline shaft joining a fan or compressor to a turbine. A first end of the stub shaft is joined to the mainline shaft. A second end of the stub shaft is joined to an engine part axially stationary relative to the mainline shaft controlled axial-movement. The stub shaft has an annular-body between first and second ends. The body contains plurality of axially-spaced circumferential rows of circumferentially-extending slots, inter-slot ligaments formed between each row slots. Successive rows are offset. The ligaments of the axially forwardmost and rearwardmost rows excepted, each ligament sandwiched between forward and rearward slots of neighbouring rows. Each ligament joined to adjacent ligaments of neighbouring rows by circumferentially-extending bars having thickness in axial direction corresponding to axial spacing between rows. The bars are axially-deflectable allowing the axial-distance between first and second ends of the stub shaft to decrease.

1 . A controlled collapse stub shaft for allowing controlled axial movement of a mainline shaft which joins a fan or compressor to a turbine of a gas turbine engine, a first end of the stub shaft being adapted to be joined to the mainline shaft, a second end of the stub shaft being adapted to be joined to a part of the engine which is axially stationary relative to the controlled axial movement of the mainline shaft, and the stub shaft further having an annular body between the first and second ends, the annular body containing a plurality of axially-spaced circumferential rows of circumferentially-extending slots, inter-slot ligaments being formed between the slots of each row, and successive axially-spaced rows being offset, whereby, the ligaments of the axially forwardmost and rearwardmost rows excepted, each ligament is sandwiched between a forward slot and a rearward slot of its neighbouring rows, and each ligament is joined to adjacent ligaments of its neighbouring rows by circumferentially-extending bars having a thickness in the axial direction corresponding to the axial spacing between the rows, wherein the bars are axially deflectable to allow the axial distance between the first and second ends of the stub shaft to decrease. 
     
     
         2 . The stub shaft according to  claim 1 , wherein the ratio of the length to the width of the slots is at least 3:1. 
     
     
         3 . The stub shaft according to  claim 1 , wherein the ratio of the length of the slots to the thickness in the circumferential direction of the ligaments is at least 3:1. 
     
     
         4 . The stub shaft according to  claim 1 , wherein the thickness in the axial direction of the bars is less than the width of the slots. 
     
     
         5 . The stub shaft according to  claim 1 , wherein the thickness in the axial direction of the bars is less than the thickness in the circumferential direction of the ligaments. 
     
     
         6 . The stub shaft according to  claim 1 , wherein every other row is aligned such that the ligaments of these rows are at the same angular positions. 
     
     
         7 . The stub shaft according to  claim 1 , wherein each ligament is sandwiched between the mid-points of the forward and rearward slots of its neighbouring rows. 
     
     
         8 . The stub shaft according to  claim 1  which has a first annular flange at the first end for joining to the mainline shaft. 
     
     
         9 . The stub shaft according to  claim 8  which has a second annular flange at the second end for joining to the axially stationary part of the engine. 
     
     
         10 . The stub shaft according to  claim 1  which further has one or more shear formations at the second end of the stub shaft, the shear formations forming a load path for transmitting axial loads between the axially stationary part of the engine and the mainline shaft. 
     
     
         11 . A gas turbine engine having a mainline shaft which joins a fan or compressor of the engine to a turbine of the engine, and a stub shaft for allowing controlled axial movement of the mainline shaft, the stub shaft having a first end and a second end, the first end of the stub shaft joining to the mainline shaft, and the second end of the stub shaft joining to a part of the engine which is axially stationary relative to the controlled axial movement of the mainline shaft; the first end of the stub shaft being adapted to be joined to the mainline shaft, the second end of the stub shaft being adapted to be joined to a part of the engine which is axially stationary relative to the controlled axial movement of the mainline shaft, and the stub shaft further having an annular body between the first and second ends, the annular body containing a plurality of axially-spaced circumferential rows of circumferentially-extending slots, inter-slot ligaments being formed between the slots of each row, and successive axially-spaced rows being offset, whereby, the ligaments of the axially forwardmost and rearwardmost rows excepted, each ligament is sandwiched between a forward slot and a rearward slot of its neighbouring rows, and each ligament is joined to adjacent ligaments of its neighbouring rows by circumferentially-extending bars having a thickness in the axial direction corresponding to the axial spacing between the rows, wherein the bars are axially deflectable to allow the axial distance between the first and second ends of the stub shaft to decrease.