System for connecting an engine shaft with a retractable nut
View Patent ↗A system for fastening the end of a gas turbine engine shaft engaged inside a sleeve supported by a bearing is disclosed. The system includes a nut that is screwed at one end inside the sleeve, and is connected by a split annular ring with the shaft at the other end.
1. A system for fastening an end of a gas turbine engine shaft engaged inside a cylindrical sleeve of a bevel wheel comprising:
a bearing which supports the cylindrical sleeve of the bevel wheel;
a nut; and
a split annular ring,
wherein the nut is screwed at a first end inside said cylindrical sleeve at a first inner circumference of the cylindrical sleeve, and is connected by the split annular ring with the shaft at a second end of the nut, and
wherein a second inner circumference of the cylindrical sleeve is held in abutting contact with an outer circumference of the shaft.
2. The system as claimed in claim 1 , wherein the nut is of cylindrical shape and comprises an outer groove of sufficient depth to contain the split circular ring in a retracted position.
3. The system as claimed in claim 2 , wherein the nut comprises a first stop-forming surface which the split annular ring in an axial direction, the stop-forming surface being separate from the groove.
4. The system as claimed in claim 3 , wherein the split annular ring is housed over part of its height in a groove disposed in an inner circumference of the shaft when the split annular ring abuts the first stop-forming surface.
5. The system according to claim 3 , wherein the split annular ring abuts the first stop-forming surface in the retracted position and abuts a second stop-forming surface when the nut is screwed inside the cylindrical sleeve.
6. The system as claimed in claim 1 , wherein the system further comprises a nut retainer.
7. The system according to claim 6 , wherein the nut retainer includes a plurality of elastically deformable branches which fit into a recess disposed on an inner circumference of the shaft.
8. The system as claimed in claim 1 , wherein the shaft and the sleeve are guided one within the other by axial splines.
9. The system as claimed in claim 1 , wherein the shaft is an HP compressor shaft of a twin-spool gas turbine engine and the bevel wheel drives a transmission shaft of an accessory gearbox.
10. The system as claimed in claim 9 , wherein the bevel wheel comprises a clamping device which clamps the bearing axially during screwing of the nut.
11. A gas turbine engine compressor comprising a system for fastening its shaft as claimed in claim 1 .
12. A gas turbine engine comprising a system for fastening the compressor shaft as claimed in claim 1 .
13. The system according to claim 1 , wherein a front end of the bevel wheel is fixedly connected to a labyrinth seal.
14. The system according to claim 1 , wherein an outer race of the bearing is supported by an intermediate casing and the cylindrical sleeve of the bevel wheel is shrink-fitted onto an inner race of the bearing.