Fan drive gear system with improved misalignment capability
An epicyclic gear assembly includes a carrier that includes a first plate axially spaced from a second plate by a connector. A first epicyclic gear set is supported adjacent the first plate and includes a first set of circumferentially offset intermediate gears meshing with a first sun gear and a first ring gear. A second epicyclic gear set is axially spaced from the first epicyclic gear set and supported adjacent the second plate and includes a second set of circumferentially offset intermediate gears meshing with a second sun gear and a second ring gear. The first epicyclic gear is set and the second epicyclic gear set maintain relative intermeshing alignment during flexure-induced deformation of the carrier. The first ring gear includes a first set of teeth that extends from a first flexible flange and the second ring gear includes a second set of teeth that extends from a second flexible flange.
1. An epicyclic gear assembly comprising:
a carrier including a first plate axially spaced from a second plate by a connector;
a first epicyclic gear set supported adjacent the first plate, including a first set of circumferentially offset intermediate gears meshing with a first sun gear and a first ring gear; and
a second epicyclic gear set axially spaced from the first epicyclic gear set and supported adjacent the second plate, and including a second set of circumferentially offset intermediate gears meshing with a second sun gear and a second ring gear with the first set of intermediate gears moveable independent of the second set of intermediate gears, whereby the first epicyclic gear set and the second epicyclic gear set maintain relative intermeshing alignment during flexure-induced deformation of the carrier, and the first ring gear includes a first set of teeth, a first flexible flange extending from a body of the first ring gear, and a first spline on an end of the first flexible flange for engaging a first static structure connection, and the second ring gear includes a second set of teeth, a second flexible flange extending from a body of the second ring gear, and a second spline on an end of the second flexible flange for engaging a second static structure connection, wherein the first sun gear includes a first Set of teeth and the second sun gear includes a second set of teeth and the first set of teeth are clocked to align with a set of tooth roots between the second set of teeth.
2. An epicyclic gear assembly comprising:
a carrier including a first plate axially spaced from a second plate by a connector;
a first epicyclic gear set supported adjacent the first plate, including a first set of circumferentially offset intermediate gears meshing with a first sun gear and a first ring gear; and
a second epicyclic gear set axially spaced from the first epicyclic gear set and supported adjacent the second plate, and including a second set of circumferentially offset intermediate gears meshing with a second sun gear and a second ring gear, whereby the first epicyclic gear set and the second epicyclic gear set maintain relative intermeshing alignment during flexure-induced deformation of the carrier, and the first ring gear includes a first set of teeth, a first flexible flange extending from a body of the first ring gear, and a first ring gear attachment end on the first flexible flange, and the second ring gear includes a second set of teeth, a second flexible flange extending from a body of the second ring gear, and a second ring gear attachment end on the second flexible flange;
wherein the first sun gear includes a first set of teeth and the second sun gear includes a second set of teeth and the first set of teeth are clocked to align with a set of tooth roots between the second set of teeth.
3. The assembly of claim 2 , wherein the first set of intermediate gears move independently of the second set of intermediate gears.
4. The assembly of claim 3 , wherein at least one of the first set of intermediate gears is attached to the carrier by at least one first post and at least one of the second set of intermediate gears are attached to the carrier by at least one second post.
5. The assembly of claim 4 , including at least one first spherical bearing located between the at least one first post and the at least one of the first set of intermediate gears and at least one second spherical bearing located between at least one second post and the at least one second set of intermediate gears.
6. The assembly of claim 4 , wherein the first set of intermediate gears and the second set of intermediate gears are spur gears.
7. The assembly of claim 6 , wherein the gear assembly is a planetary gear assembly with the first ring gear and the second ring gear fixed from rotation.
8. The assembly of claim 6 , wherein the gear assembly is a star gear assembly with the carrier fixed from rotation.
9. The assembly of claim 6 , including at least one intermediate gear opening in the carrier, wherein one of the first set of intermediate gears and one of the second set of intermediate gears are located within the at least one intermediate gear opening.
10. The assembly of claim 6 , wherein the first sun gear is separate from the second sun gear and the first ring gear is separate from the second ring gear.
11. The assembly of claim 10 , wherein a radially inner side of the first sun gear includes a first spline and a radially inner side of the second sun gear includes a second spline.
12. The assembly of claim 2 , wherein the first ring gear attachment end on the first flexible flange includes a first spline for engaging a first static structure connection and the second ring gear attachment end on the second flexible flange includes a second spline for engaging a second static structure connection.
13. A gas turbine engine comprising:
a fan section located at an axially upstream end of the gas turbine engine relative to a direction of airflow through the gas turbine engine and rotatable about an axis;
a turbine section located at an axially downstream end of the gas turbine engine relative to the direction of airflow through the gas turbine engine and having a fan drive turbine; and
a speed change mechanism in communication with the fan section, the speed change mechanism including:
a carrier including a first plate axially spaced from a second plate by at least one connector;
a first epicyclic gear set supported adjacent the first plate, including a first set of circumferentially offset intermediate gears meshing with a first sun gear and a first ring gear; and
a second epicyclic gear set axially spaced from the first epicyclic gear set and supported adjacent the second plate, and including a second set of circumferentially offset intermediate gears meshing with a second sun gear and a second ring gear, whereby the first epicyclic gear set and the second epicyclic gear set maintain relative intermeshing alignment during flexure-induced deformation of the carrier, and the first ring gear includes a first set of teeth, a first flexible flange extending from a radially outer side of a body of the first ring gear, and a first ring gear attachment end on the first flexible flange, and the second ring gear includes a second set of teeth, a second flexible flange extending from a radially outer side of a body of the second ring gear, and a second ring gear attachment end on the second flexible flange, wherein a shaft drives the first sun gear and the second sun gear and an upstream most end of the shaft is located axially downstream of the first plate relative to the direction of airflow through the gas turbine engine and the first sun gear includes a first set of teeth and the second sun gear includes a second set of teeth and the first set of teeth are clocked to align with a set of tooth roots between the second set of teeth.
14. The assembly of claim 13 , wherein the upstream most end of the shaft is axially aligned with the first sun gear.
15. The gas turbine engine of claim 13 , wherein the first set of intermediate gears move independently of the second set of intermediate gears and the first ring gear is separate from the second ring gear.
16. A gas turbine engine comprising:
a fan section located at an axially upstream end of the gas turbine engine relative to a direction of airflow through the gas turbine engine and rotatable about an axis;
a turbine section located at an axially downstream end of the gas turbine engine relative to the direction of airflow through the gas turbine engine and having a fan drive turbine; and
a speed change mechanism in communication with the fan section, the speed change mechanism including:
a carrier including a first plate axially spaced from a second plate by at least one connector;
a first epicyclic gear set supported adjacent the first plate, including a first set of circumferentially offset intermediate gears meshing with a first sun gear and a first ring gear; and
a second epicyclic gear set axially spaced from the first epicyclic gear set and supported adjacent the second plate, and including a second set of circumferentially offset intermediate gears meshing with a second sun gear and a second ring gear, whereby the first epicyclic gear set and the second epicyclic gear set maintain relative intermeshing alignment during flexure-induced deformation of the carrier, wherein a shaft drives the first sun gear and the second sun gear and the shaft is located axially downstream of the first plate relative to the direction of airflow through the gas turbine engine;
wherein the first ring gear includes a first set of teeth extending from a first flexible flange and the second ring gear includes a second set of teeth extending from a second flexible flange, the first set of intermediate gears move independently of the second set of intermediate gears, the first sun gear includes a first set of teeth and the second sun gear includes a second set of teeth and the first set of teeth are clocked to align with a set of tooth roots between the second set of teeth.
17. The engine of claim 16 , wherein at least one of the first set of intermediate gears is attached to the carrier by at least one first post and at least one of the second set of intermediate gears are attached to the carrier by at least one second post.
18. The engine of claim 17 , including at least one first spherical bearing located between the at least one first post and the at least one of the first set of intermediate gears and at least one second spherical bearing located between at least one second post and the at least one second set of intermediate gears.
19. The engine of claim 16 , wherein the gear assembly is a planetary gear assembly with the first ring gear and the second ring gear fixed from rotation.
20. The engine of claim 16 , wherein the gear assembly is a star gear assembly with the carrier fixed from rotation.
21. The engine of claim 16 , including at least one intermediate gear opening in the carrier, wherein one of the first set of intermediate gears and one of the second set of intermediate gears are located within the at last one intermediate gear opening.
22. The engine of claim 16 , wherein the first set of intermediate gears and the second set of intermediate gears are spur gears.
23. The engine of claim 16 , wherein the first sun gear is separate from the second sun gear and the first ring gear is separate from the second ring gear.
24. The engine of claim 23 , wherein a radially inner side of the first sun gear includes a first spline and a radially inner side of the second sun gear includes a second spline.