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A rotor retaining system for a rotor assembly of a gas turbine engine includes a washer interlocking multiple retaining nuts to prevent relative rotation. The retaining nuts retain a rotor disc and a cover plate in position, respectively. A wire is provided to retain the washer in position and which

A rotor retaining system for a rotor assembly of a gas turbine engine includes a washer interlocking multiple retaining nuts to prevent relative rotation. The retaining nuts retain a rotor disc and a cover plate in position, respectively. A wire is provided to retain the washer in position and which may dampen vibration during engine operation.

대표청구항 ▼

1. A rotor retaining system for a rotor assembly of a gas turbine engine, the rotor assembly including a shaft, a rotor disc mounted on the shaft, a plurality of blades extending radially from the rotor disc and a cover plate attached to a side of the rotor disc, the rotor retaining system comprisin

1. A rotor retaining system for a rotor assembly of a gas turbine engine, the rotor assembly including a shaft, a rotor disc mounted on the shaft, a plurality of blades extending radially from the rotor disc and a cover plate attached to a side of the rotor disc, the rotor retaining system comprising: a first retaining nut threadingly engaging the shaft and retaining the rotor disc in position on the shaft;a second retaining nut disposed around the first retaining nut, threadingly engaging the rotor disc and retaining the cover plate in position relative to the rotor disc;a washer engaging both the first and second retaining nuts to interlock one retaining nut relative to another to impede relative rotation between first and second retaining nuts; anda wire removably engaging one of the first and second retaining nuts and disposed axially adjacent to the washer to retain the washer in position. 2. The rotor retaining system as defined in claim 1 wherein the wire comprises a single wire in a split ring configuration. 3. The rotor retaining system as defined in claim 1 wherein the wire is received in a circumferentially extending groove defined in the second retaining nut. 4. The rotor retaining system as defined in claim 1 wherein the washer comprises a ring disposed radially between the first and second retaining nuts, a first lock member extending radially inwardly from the ring into a recess in the first retaining nut and a second lock member extending radially outwardly from the ring into a recess in the second retaining nut. 5. The rotor retaining system as defined in claim 4 wherein each of the recesses defines an opening on an axial end of the respective first and second retaining nuts for axial access to the recesses. 6. The rotor retaining system as defined in claim 5 wherein the second lock member of the washer is restrained axially between a radial surface of the radial recess of the second retaining nut and the wire. 7. The rotor retaining system as defined in claim 1 wherein one of the first and second retaining nuts comprises a plurality of circumferentially spaced radial recesses for selectively receiving a corresponding one of the first and second lock members of the washer. 8. The rotor retaining system as defined in claim 1 wherein the second retaining nut comprises a plurality of circumferentially spaced radial recesses for selectively receiving the second lock member of the washer. 9. The rotor retaining system as defined in claim 1 wherein a thread direction of the threaded engagement between the second retaining nut and the cover plate is opposite to a thread direction of the threaded engagement between the first retaining nut and the shaft. 10. A rotor assembly of a gas turbine engine comprising: a shaft;a rotor disc mounted on the shaft and retained in position by a first retaining nut which threadingly engages the shaft in a first rotational direction;a plurality of blades received in circumferentially spaced slots in the rotor disc and axially extending across the rotor disc;a cover plate attached to the rotor disc and retaining the blades in the respective slots of the rotor disc, the cover plate being retained in position relative to the rotor disc, by a second retaining nut which threadingly engages the rotor disc in a second rotational direction opposite to the first rotational direction;a washer positioned adjacent the first and second retaining nuts to impede relative rotation between the first and second retaining nuts; anda wire removably engaging one of the first and second retaining nuts and disposed axially adjacent to the washer to retain the washer in position. 11. The rotor assembly as defined in claim 10 wherein each of the first and second retaining nuts comprises a threaded section and an end section, the end sections defining at least one recess, the washer having first and second lock members received in the respective recesses to thereby prevent the respective retaining nuts from rotation relative to each other. 12. The rotor assembly as defined in claim 11 wherein the second retaining nut comprises a plurality of recesses including said at least one recess, for selectively receiving the second lock member of the washer. 13. The rotor assembly as defined in claim 11 wherein the wire comprises a split ring configuration received in a circumferential groove in the end section of the second retaining nut, the split ring configuration abutting the second lock member of the washer against a radial surface of the recess receiving the second lock member. 14. The rotor assembly as defined in claim 11 wherein the rotor disc comprises a cylindrical wall forming a rearward end portion of the rotor disc, the cylindrical wall extending around and radially spaced apart from the first retaining nut, the second retaining nut engaging a threaded outer surface of the cylindrical wall. 15. The rotor assembly as defined in claim 11 wherein the washer comprises a flat ring, the first lock member extending radially inwardly from the flat ring and the second lock member extending radially and outwardly from the flat ring. 16. A method for retaining components of a rotor assembly of a gas turbine engine, the method comprising: a) providing a first retaining nut threadingly engaging the rotor assembly in a first rotational direction for retaining a first one of the components in position;b) providing a second retaining nut threadingly engaging the rotor assembly in a second rotational direction opposite the first rotational direction, for retaining a second one of the components in position;c) using a washer to interlock the first and second retaining nuts one relative to another to impede relative rotation between the first and second retaining nuts; andd) engaging a wire to one of the first and second retaining nuts for retaining the washer in position. 17. The method as defined in claim 16 further comprising a step of selecting a type of wire to be used in step (d) for damping vibration of the rotor assembly during engine operation.