Geared architecture for gas turbine engine
A turbofan engine includes a fan section. A turbine section is in driving engagement with the fan section through a geared architecture. A flexible support supports the geared architecture relative to an engine static structure. A deflection limiter includes at least one of an axially extending branch or a radially extending branch. A flexible output shaft is in driving engagement with the fan section and driven by the geared architecture. A speed change mechanism for a gas turbine engine is also disclosed.
1. A turbofan engine comprising:
a fan section;
a turbine section in driving engagement with the fan section through a geared architecture, wherein the geared architecture includes:
a plurality of intermediate gears surrounding a sun gear in driving engagement with a flexible input shaft and the sun gear includes an aft sun gear bearing flange;
a carrier supporting the plurality of intermediate gears and includes a first carrier bearing flange extending axially aft from an aft plate of the carrier and at least one sun gear carrier bearing engages the first carrier bearing flange and the aft sun gear bearing flange; and
a ring gear surrounding the plurality of intermediate gears;
a flexible support supporting the geared architecture relative to an engine static structure;
a deflection limiter including at least one of an axially extending branch or a radially extending branch; and
a flexible output shaft in driving engagement with the fan section and driven by the geared architecture.
2. The turbofan engine of claim 1 , wherein the deflection limiter includes the axially extending branch and a radial damper housing at least partially surrounds the axially extending branch.
3. The turbofan engine of claim 2 , wherein at least one seal at least partially defines a fluid damper passage with the axially extending branch and the radial damper housing and a damper fluid is located in the fluid damper passage.
4. The turbofan engine of claim 1 , wherein the deflection limiter includes the radially extending branch and an axial damper housing at least partially surrounds the radially extending branch.
5. The turbofan engine of claim 4 , wherein at least one seal at least partially defines a fluid damper passage with the radially extending branch and the axial damper housing and a damper fluid is located in the fluid damper passage.
6. The turbofan engine of claim 1 , wherein the ring gear includes a ring gear bearing flange and at least one ring gear carrier bearing engaging the first carrier bearing flange and the ring gear bearing flange.
7. The turbofan engine of claim 6 , wherein the at least one ring gear carrier bearing includes at least one inner race that engages a radially outer side of the ring gear bearing flange and an outer race that engages a radially inner side of the first carrier bearing flange.
8. The turbofan engine of claim 7 , wherein the ring gear includes an axially forward extending portion extending forward of a forward plate of the carrier and a radially inward extending portion having the ring gear bearing flange.
9. The turbofan engine of claim 8 , wherein the ring gear bearing flange extends axially downstream from the radially inward extending portion of the ring gear.
10. A speed change mechanism for a gas turbine engine comprising:
a geared architecture including:
a plurality of intermediate gears surrounding a sun gear in driving engagement with a flexible input shaft;
a carrier supporting the plurality of intermediate gears includes a first carrier bearing flange;
a ring gear surrounding the plurality of intermediate gears and including a ring gear bearing flange; and
at least one ring gear carrier bearing engaging the first carrier bearing flange and the ring gear bearing flange;
a flexible support for supporting the geared architecture;
a deflection limiter including at least one of an axially extending branch or a radially extending branch; and
the geared architecture is in driving engagement with a flexible output shaft.
11. The speed change mechanism of claim 10 , wherein the deflection limiter includes the axially extending branch and a radial damper housing at least partially surrounds the axially extending branch and the radially extending branch and an axial damper housing at least partially surrounds the radially extending branch.
12. The speed change mechanism of claim 11 , wherein at least one seal at least partially defines a fluid damper passage with the axially extending branch and the radial damper housing and a damper fluid is located in the fluid damper passage.
13. The speed change mechanism of claim 11 , wherein at least one seal at least partially defines a fluid damper passage with the radially extending branch and the axial damper housing and a damper fluid is located in the fluid damper passage.
14. The speed change mechanism of claim 10 , wherein the at least one ring gear carrier bearing includes at least one inner race that engages a radially outer side of the ring gear bearing flange and an outer race that engages a radially inner side of the first carrier bearing flange.
15. The speed change mechanism of claim 14 , wherein the ring gear includes an axially forward extending portion extending forward of a forward plate of the carrier and a radially inward extending portion having the ring gear bearing flange.
16. The speed change mechanism of claim 10 , wherein the first carrier bearing flange extends axially aft from an aft plate of the carrier.
17. The speed change mechanism of claim 15 , wherein sun gear includes an aft sun gear bearing flange and at least one sun gear carrier bearing engaging the first carrier bearing flange and the aft sun gear bearing flange.