Direct drive electrically-geared turbofan
US-2024218837-A1 · Jul 4, 2024 · US
US9850820B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9850820-B2 |
| Application number | US-201414506226-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 3, 2014 |
| Priority date | Apr 6, 2012 |
| Publication date | Dec 26, 2017 |
| Grant date | Dec 26, 2017 |
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A power transmission system for a turbine engine is provided. The power transmission system includes a transmission shaft that is connected to a drive shaft by bevel gears, and that drives equipment or accessories. The transmission shaft is designed to operate under supercritical conditions and includes a damper system for damping vibration at its resonant speed.
Opening claim text (preview).
The invention claimed is: 1. A power transmission system for a turbine engine, the power transmission system comprising: a transmission shaft connected to a drive shaft; a connection system that connects the transmission shaft to equipment or accessories driven by the transmission shaft; and a removable housing engaged around a radially outer end of the transmission shaft, wherein the transmission shaft is designed to operate under supercritical conditions and includes a damper system which damps vibration at a resonant speed of the transmission shaft, wherein a guide bearing is mounted on a cylindrical bearing surface of the radially outer end of the transmission shaft, and wherein the damper system includes an oil film compression damper formed in an annular space between an inner annular surface of the removable housing and an annular part surrounding an outer ring of the guide bearing. 2. The power transmission system according to claim 1 , wherein the removable housing is carried by a stationary structural element. 3. The power transmission according to claim 2 , wherein the removable housing is mounted in a housing of the connection system for connecting the transmission shaft to the equipment or the accessories driven by the transmission shaft. 4. The power transmission system according to claim 1 , wherein the oil film is confined laterally by at least two annular sealing gaskets engaged in at least one of annular housings in the annular part and the removable housing. 5. The power transmission system according to claim 4 , wherein the annular gaskets are made of carbon. 6. A turbine engine, comprising at least one power transmission system according to claim 1 , wherein the transmission shaft extends in a radial arm of an intermediate casing. 7. The turbine engine according to claim 6 , wherein the removable housing is mounted inside an opening in a stationary structure carried by the intermediate casing. 8. The power transmission system according to claim 1 , wherein the guide bearing is axially held at a first end by a nut which is screwed onto a threaded portion of the cylindrical bearing surface or of the annular part, and is axially held at a second end by a radial rim of the transmission shaft. 9. A method of transmitting power to equipment or accessories of a turbine engine by a transmission shaft connected to a drive shaft via a connection system that connects the transmission shaft to the equipment or accessories of the turbine engine, the method comprising: causing the transmission shaft to rotate at a supercritical speed; and damping vibration via a damping system while the transmission shaft is operating at a resonant speed of the transmission shaft, wherein a removable housing engaged around a radially outer end of the transmission shaft, wherein a guide bearing is mounted on a cylindrical bearing surface of the radially outer end of the transmission shaft, and wherein the damper system includes an oil film compression damper formed in an annular space between an inner annular surface of the removable housing and an annular part surrounding an outer ring of the guide bearing. 10. The method according to claim 9 , wherein the guide bearing is axially held at a first end by a nut which is screwed onto a threaded portion of the cylindrical bearing surface or of the annular part, and is axially held at a second end by a radial rim of the transmission shaft.
comprising conical gears only · CPC title
Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title
Flexible supports; Vibration damping means associated with the bearing · CPC title
Arrangement, mounting, or driving, of auxiliaries · CPC title
Bevel · CPC title
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