IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0437442
(2012-04-02)
|
등록번호 |
US-8764604
(2014-07-01)
|
발명자
/ 주소 |
- McCune, Michael E.
- Portlock, Lawrence E.
|
출원인 / 주소 |
- United Technologies Corporation
|
대리인 / 주소 |
Carlson, Gaskey & Olds, P.C.
|
인용정보 |
피인용 횟수 :
0 인용 특허 :
19 |
초록
▼
A turbine engine includes an input shaft and a fan shaft rotatable about an axis. The fan shaft supports fan blades. An epicyclic gear train is connected between the input shaft and the fan shaft. The epicyclic gear train includes a plurality of star gears, a carrier supporting the plurality of star
A turbine engine includes an input shaft and a fan shaft rotatable about an axis. The fan shaft supports fan blades. An epicyclic gear train is connected between the input shaft and the fan shaft. The epicyclic gear train includes a plurality of star gears, a carrier supporting the plurality of star gears, a sun gear that meshes with the plurality of star gears and a ring gear surrounding and meshing with the plurality of star gears such that the sun gear is rotatable in a first direction and the ring gear is rotatable in a second, opposite direction. The ring gear includes first and second portions that each have an inner periphery with teeth. The first and second portions include respective recesses facing one another to provide an internal annular cavity.
대표청구항
▼
1. A turbine engine comprising: an input shaft and a fan shaft rotatable about an axis, the fan shaft supporting fan blades;an epicyclic gear train connected between the input shaft and the fan shaft, the epicyclic gear train including a plurality of star gears, a carrier supporting the plurality of
1. A turbine engine comprising: an input shaft and a fan shaft rotatable about an axis, the fan shaft supporting fan blades;an epicyclic gear train connected between the input shaft and the fan shaft, the epicyclic gear train including a plurality of star gears, a carrier supporting the plurality of star gears, a sun gear that meshes with the plurality of star gears and a ring gear surrounding and meshing with the plurality of star gears such that the sun gear is rotatable in a first direction and the ring gear is rotatable in a second, opposite direction, the ring gear including first and second portions that each have an inner periphery with teeth, the first and second portions including respective recesses facing one another to provide an internal annular cavity, the first and second portions of the ring gear each having an outer circumferential surface opposite the teeth and a respective flange projecting radially outwardly from the respective outer circumferential surface, the flanges including respective grooves therein; anda seal adjacent the flange, the seal including a slot configured to permit oil to pass through the seal to drain into a gutter outwards of the flange. 2. The turbine engine according to claim 1, wherein the teeth on the inner periphery of the ring gear are exclusive teeth on the ring gear. 3. The turbine engine according to claim 1, wherein the internal annular cavity is axially elongated relative to a radial dimension of the internal annular cavity. 4. The turbine engine according to claim 1, each of the respective outer circumferential surfaces including multiple inclined surfaces with regard to a central axis of the ring gear. 5. The turbine engine according to claim 4, wherein the multiple inclined surfaces includes a first inclined surface joined at one axial end thereof with a second inclined surface, the first inclined surface having a different slope than the second inclined surface. 6. The turbine engine according to claim 5, wherein each of the respective outer circumferential surfaces includes a non-sloped surface joined with the second inclined surface. 7. The turbine engine according to claim 1, the first and second portions each being a monolithic structure. 8. The turbine engine according to claim 1, wherein the teeth on the first portion are angled in a first direction, and the teeth on the second portion are angled in a second direction opposite the first direction, a rotational direction of the ring gear forcing the first and second portions toward one another at the radial interface. 9. The turbine engine according to claim 1, wherein the respective grooves define a passage operable to convey oil though the ring gear, the passage intersecting the internal annular cavity and also extending through the flange and opening at the inner periphery and at a radially outer tip of the flange. 10. The turbine engine as recited in claim 1, wherein the seal includes a knife edge sealing against the gutter. 11. The turbine engine as recited in claim 10, wherein the seal is formed of a first material and the gutter is formed of a second material that is softer than the first material. 12. A turbine engine comprising: a core drive shaft;an epicyclical gear train connected to the drive shaft;a fan shaft connected to the epicyclical gear train,the gear train having a rotatable ring gear that includes forward and aft portions, the forward and aft portions respectively including aft and forward facing radially extending grooves configured to form a guide channel for transferring oil between inner and outer peripheries of the ring gear, andan annular recesses configured to form an annular cavity, an outer periphery of the ring gear being dimensioned to provide the ring gear with a spring rate within a predetermined tolerance; anda seal at the outer periphery of the ring gear, the seal including a slot configured to permit oil to pass through the seal to drain into a gutter outwards of the guide channel. 13. The turbine engine as recited in claim 12, wherein the forward and aft portions each have a radial inner periphery with radially inner facing teeth which interface with a plurality of star gears of the epicyclical gear train, thereby biasing the forward and aft portion towards each other. 14. The turbine engine as recited in claim 12, wherein the epicyclical gear train includes a plurality of star gears, a carrier supporting the plurality of star gears, a sun gear that meshes with the plurality of star gears and the ring gear surrounding and meshing with the plurality of star gears such that the sun gear is rotatable in a first direction and the ring gear is rotatable in a second, opposite direction. 15. The turbine engine as recited in claim 12, wherein the seal includes a knife edge sealing against the gutter. 16. The turbine engine as recited in claim 15, wherein the seal is formed of a first material and the gutter is formed of a second material that is softer than the first material.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.