Rotor assembly apparatus are disclosed. An example rotor assembly includes a twist actuator to drive a first rotation of a first shaft about a first axis, the twist actuator positioned at a center of rotation of the rotor assembly; and a first gear assembly to convert the first rotation into a plura
Rotor assembly apparatus are disclosed. An example rotor assembly includes a twist actuator to drive a first rotation of a first shaft about a first axis, the twist actuator positioned at a center of rotation of the rotor assembly; and a first gear assembly to convert the first rotation into a plurality of second rotations of a plurality of second shafts, each of the second shafts to provide torque to a respective blade coupled to the rotor assembly.
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1. An apparatus comprising: a first gear assembly to convert torque about a first axis provided by a central actuator of a rotor assembly into second torques about second axes, the second axes being different than the first axis, the first gear assembly comprising: a first angled gear concentric wit
1. An apparatus comprising: a first gear assembly to convert torque about a first axis provided by a central actuator of a rotor assembly into second torques about second axes, the second axes being different than the first axis, the first gear assembly comprising: a first angled gear concentric with a first drive shaft of the central actuator; andsecond angled gears, each of the second angled gears to mesh with the first angled gear;a second gear assembly to receive one of the second torques about one of the second axes via a second drive shaft, the second gear assembly comprising: a first planetary gear system driven by the second drive shaft; anda second planetary gear system driven by the first planetary gear system, the second planetary gear system comprising a sun gear coupled to an output shaft, wherein the second gear assembly comprises a planet carrier to house the first planetary gear system and the second planetary gear system. 2. An apparatus as defined in claim 1, wherein the first planetary gear system being driven by the second drive shaft comprises the second drive shaft driving the planet carrier. 3. An apparatus as defined in claim 1, wherein the output shaft is to twist a rotor blade. 4. An apparatus as defined in claim 1, wherein first planetary gear system comprises a sun gear fixed to a pitch shaft. 5. The apparatus as defined in claim 1, further comprising: the central actuator to drive a first rotation of the first drive shaft about the first axis, the central actuator positioned at a center of rotation of the rotor assembly; andthe first gear assembly to convert the first rotation into a plurality of second rotations of a plurality of second shafts including the second drive shaft, each of the second shafts to provide torque to blades coupled to the rotor assembly. 6. The apparatus as defined in claim 5, further comprising carriers, each carrier coupled to a respective one of the second shafts. 7. The apparatus as defined in claim 5, wherein the first gear assembly comprises a bull gear and pinion gears, each of the second shafts extending from respective ones of the pinion gears. 8. The apparatus as defined in claim 7, wherein the bull gear is coupled to the first drive shaft via a diaphragm coupling. 9. The apparatus as defined in claim 7, wherein the bull gear comprises first teeth angled relative to the first axis, and each of the pinion gears comprises second teeth angled relative to the first axis. 10. The apparatus as defined in claim 5, wherein the first axis is different than each of the second axes corresponding to respective ones of the second shafts. 11. The apparatus as defined in claim 5, wherein the torque is applied to a torsion shaft of the respective blades to cause the respective blades to twist. 12. An apparatus comprising: a first gear assembly to convert torque about a first axis provided by a central actuator of a rotor assembly into second torques about second axes, the second axes being different than the first axis, the first gear assembly comprising: a first angled gear concentric with a first drive shaft of the central actuator; andsecond angled gears, each of the second angled gears to mesh with the first angled gear; anda second gear assembly to receive one of the second torques about one of the second axes via a second drive shaft, the second gear assembly comprising: a first planetary gear system driven by the second drive shaft; anda second planetary gear system driven by the first planetary gear system, the second planetary gear system comprising a sun gear coupled to an output shaft;a carrier coupled to the second drive shaft, the second drive shaft extending through a pitch shaft of a rotor assembly, the second drive shaft providing a first amount of torque to the carrier;the first planetary gear system disposed in the carrier, the carrier to drive rotation of the first planetary gear system;the second planetary gear system disposed in the carrier; andan output of the second planetary gear system to provide a second amount of torque to a blade. 13. The apparatus as defined in claim 12, wherein the first planetary gear system comprises a first stage sun gear, the first stage sun gear being fixed to the pitch shaft. 14. The apparatus as defined in claim 13, wherein first stage planet gears mesh with the first stage sun gear, and each of the first stage planet gears is mounted to a planet shaft. 15. The apparatus as defined in claim 14, wherein the second planetary gear system comprises a second stage sun gear, the output of the second planetary gear system comprising the second stage sun gear. 16. The apparatus as defined in claim 15, wherein second stage planet gears mesh with the second stage sun gear, and each of the second stage planet gears is mounted to a respective one of the planet shafts. 17. The apparatus as defined in claim 16, wherein each of the planet shafts comprises an end received by a bore in a cap assembly, the cap assembly being coupled to the carrier. 18. An apparatus comprising: a first gear assembly to convert torque about a first axis provided by a central actuator of a rotor assembly into second torques about second axes, the second axes being different than the first axis, the first gear assembly comprising: a first angled gear concentric with a first drive shaft of the central actuator; andsecond angled gears, each of the second angled gears to mesh with the first angled gear; anda second gear assembly to receive one of the second torques about one of the second axes via a second drive shaft, the second gear assembly comprising: a first planetary gear system driven by the second drive shaft; anda second planetary gear system driven by the first planetary gear system, the second planetary gear system comprising a sun gear coupled to an output shaft;the central actuator to drive a first rotation of the first drive shaft about the first axis, the central actuator positioned at a center of rotation of the rotor assembly;the first gear assembly to convert the first rotation into a plurality of second rotations of a plurality of second shafts including the second drive shaft, each of the second shafts to provide torque to blades coupled to the rotor assembly;carriers, each carrier coupled to a respective one of the second shafts;the first planetary gear system is disposed in at least one of the carriers;the second planetary gear system is disposed in at least one of the carriers; andthe output shaft is coupled to the second planetary gear system to provide the torque to at least one of the blades. 19. The apparatus as defined in claim 18, further comprising pitch shafts, a sun gear of the first planetary gear system being coupled to at least one of the pitch shafts.
Hora Petr (West Chester OH) Hermans Thomas C. (Cincinnati OH) Bulman David E. (Cincinnati OH) Miller Edwin K. (West Chester OH) Wakeman Thomas G. (Lawrenceburg IN) Joyce David L. (West Chester OH), Aircraft pitch change mechanism.
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