| 发明名称 |
A GAS TURBINE ENGINE, AN AIRCRAFT PROVIDED THEREWITH, AND A METHOD OF CONTROLLING THE OPERATION OF SUCH AN ENGINE |
| 摘要 |
<p>A gas turbine engine with a power transmission device (2) comprising: a first turbine shaft (11) of said gas turbine engine (1); a power output shaft (24); a gear mechanism (14) arranged to provide a variable gear change between said first turbine shaft (11) and said power output shaft (24), said gear mechanism (14) being provided to change between a first gear reduction i <SUB>Lpacc1</</p> |
| 申请公布号 |
WO2008082334(A1) |
申请公布日期 |
2008.07.10 |
| 申请号 |
WO2006SE01516 |
申请日期 |
2006.12.29 |
| 申请人 |
VOLVO AERO CORPORATION;HEDMAN, ANDERS;BRUSVED, LENNART |
发明人 |
HEDMAN, ANDERS;BRUSVED, LENNART |
| 分类号 |
F02C7/32;F02C3/107;F02C7/36 |
主分类号 |
F02C7/32 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
