Belt drive arrangement for a drive train of a helicopter
The invention relates to a belt drive assembly for a drive train of a helicopter, comprising a drive shaft that can be functionally connected to a crankshaft of a drive machine of the helicopter, wherein the drive shaft is functionally connected to a belt disk via a torsional vibration damper, wherein the belt disk can rotate via a bearing mechanism on a bearing shaft connected to the drive shaft for conjoint rotation therewith, wherein the belt disk can receive a belt that is functionally connected to a rotor system of the helicopter.
1. A belt drive assembly for a drive train of a helicopter, comprising:
a drive shaft that can be functionally connected to a crankshaft of a drive machine of the helicopter, wherein the drive shaft is functionally connected to a belt disk via a torsional vibration damper, wherein the belt disk can rotate via a bearing mechanism on a bearing shaft connected to the drive shaft for conjoint rotation therewith, wherein the belt disk can receive a belt that is functionally connected to a rotor system of the helicopter, and
further comprising an ancillary drive shaft that-is connected to the belt disk for conjoint rotation, wherein the ancillary drive shaft can be functionally connected to an ancillary unit of the helicopter.
2. The belt drive assembly according to claim 1 , wherein the torsional vibration damper comprises a spring mechanism, wherein the spring mechanism couples at least one input element to at least one output element such that vibrations are dampened.
3. The belt drive assembly according to claim 2 , wherein the at least one input element is located axially between the drive shaft and the bearing shaft, and connected to the drive shaft and the bearing shaft for conjoint rotation.
4. The belt drive assembly according to claim 2 , wherein the at least one input element is an annular disk, and has numerous holes for axially inserting connecting means between the drive shaft and the bearing shaft.
5. The belt drive assembly according to claim 2 , wherein the at least one output element is located on the front surface of the belt disk and is connected to the belt disk for conjoint rotation.
6. The belt drive assembly according to claim 2 , further comprising a first and second output element form a housing of the torsional vibration damper, wherein the first output element forms a housing well, and the second output element forms a housing cover.
7. The belt drive assembly according to claim 1 , wherein the bearing mechanism comprises a first and second tapered roller bearing.
8. The belt drive assembly according to claim 7 , wherein the two tapered roller bearings form an O-assembly.
9. A use of a belt drive assembly according to claim 1 in a drive train of a helicopter.
10. A helicopter that has a belt drive assembly according to claim 1 .
11. A belt drive assembly for a drive train of a helicopter, comprising:
a drive shaft that can be functionally connected to a crankshaft of a drive machine of the helicopter, wherein the drive shaft is functionally connected to a belt disk via a torsional vibration damper, wherein the belt disk can rotate via a bearing mechanism on a bearing shaft connected to the drive shaft for conjoint rotation therewith, wherein the belt disk can receive a belt that is functionally connected to a rotor system of the helicopter,
wherein the torsional vibration damper comprises a spring mechanism, wherein the spring mechanism couples at least one input element to at least one output element such that vibrations are dampened, and
wherein the at least one input element is an annular disk, and has numerous holes for axially inserting connecting means between the drive shaft and the bearing shaft.