基本信息:
- 专利标题： Propeller gas turbine engine
- 申请号：EP13171359.6 申请日：2013-06-11
- 公开(公告)号：EP2685065B1 公开(公告)日：2018-11-28
- 发明人： Stretton, Richard , Howarth, Nicholas
- 申请人： Rolls-Royce plc
- 申请人地址： 62 Buckingham Gate London SW1E 6AT GB
- 专利权人： Rolls-Royce plc
- 当前专利权人： ROLLS-ROYCE PLC
- 当前专利权人地址： ROLLS-ROYCE PLC
- 代理机构： Rolls-Royce plc
- 优先权： GB201212384 20120712
- 主分类号： F02C3/067
- IPC分类号： F02C3/067 ; F02K3/02 ; F02K3/06 ; F02C7/04 ; F02K3/04 ; B64D27/00 ; F02C7/05
摘要：
A gas turbine engine (10) having an axial flow direction (X) therethrough in use. The gas turbine engine (10) comprises one or more rotor stages each comprising at least one rotor blade (120) having a root portion (122). The gas turbine engine (10) comprises a shroud (126) located upstream of one or more of the rotor stages relative to the axial flow direction (X). The shroud (126) defines a through passageway (128) extending between an inlet (130) and an outlet (132) which comprises a diffuser region (138). The diffuser region (138) is configured to reduce the axial velocity of air exiting the outlet (132) relative to air entering the diffuser portion (138) in use, wherein the outlet (132) is located such that air exiting the outlet (132) is directed substantially to the root portion (122) only of the rotor blades (120).
公开/授权文献:
- EP2685065A3 A gas turbine engine 公开/授权日：2018-03-07
IPC结构图谱:
| F | 机械工程；照明；加热；武器；爆破 |
| --F02 | 燃烧发动机；热气或燃烧生成物的发动机装置 |
| ----F02C | 燃气轮机装置；喷气推进装置的空气进气道；空气助燃的喷气推进装置燃料供给的控制 |
| ------F02C3/00 | 以利用燃烧产物作为工作流体为特点的燃气轮机装置 |
| --------F02C3/04 | .涡轮机驱动压气机的 |
| ----------F02C3/06 | ..只带轴流级的压气机 |
| ------------F02C3/067 | ...具有反转式转子的 |