
基本信息:
- 专利标题: Gas turbine engine cooling systems having hub-bleed impellers
- 申请号:EP12180423.1 申请日:2012-08-14
- 公开(公告)号:EP2584142B1 公开(公告)日:2018-10-24
- 发明人: Matwey, Mark , Jan, David K. , Chunduru, Srinivas Jaya
- 申请人: Honeywell International Inc.
- 申请人地址: 115 Tabor Road Morris Plains, NJ 07950 US
- 专利权人: Honeywell International Inc.
- 当前专利权人: HONEYWELL INTERNATIONAL INC.
- 当前专利权人地址: HONEYWELL INTERNATIONAL INC.
- 代理机构: Houghton, Mark Phillip
- 优先权: US201113277034 20111019
- 主分类号: F01D5/04
- IPC分类号: F01D5/04 ; F01D5/08 ; F04D29/28
摘要:
Embodiments of a gas turbine engine cooling system (100) for deployment within a gas turbine engine (18) are provided, as are embodiment of a method for producing the same. In one embodiment, the gas turbine engine cooling system (100) includes an impeller (36) having a hub (52), a plurality of hub bleed air passages (102), and a central bleed air conduit (104). Each hub bleed air passage (102) has an inlet (106) and an outlet (108) formed in outer and inner circumferential surfaces of the hub (52), respectively. The central bleed air conduit (104) is fluidly coupled to the outlets (108) of the plurality of hub bleed air passages (102) and is configured to conduct bleed air discharged by the plurality of hub bleed air passages (102) to a section of the gas turbine engine (18) downstream of the impeller (36) to provide cooling air thereto.
公开/授权文献:
IPC结构图谱:
F | 机械工程;照明;加热;武器;爆破 |
--F01 | 一般机器或发动机;一般的发动机装置;蒸汽机 |
----F01D | 非变容式机器或发动机,如汽轮机 |
------F01D5/00 | 叶片;叶片的支承元件;叶片或元件的加热、隔热、冷却或防止振动装置 |
--------F01D5/02 | .叶片的支承元件,如转子 |
----------F01D5/04 | ..径向流动的机器或发动机 |