![Dual Flow APU Inlet and Associated Systems and Methods](/abs-image/US/2008/07/31/US20080179466A1/abs.jpg.150x150.jpg)
基本信息:
- 专利标题: Dual Flow APU Inlet and Associated Systems and Methods
- 专利标题(中):双流APU入口及相关系统和方法
- 申请号:US11829497 申请日:2007-07-27
- 公开(公告)号:US20080179466A1 公开(公告)日:2008-07-31
- 发明人: Thomas A. Campbell , David S. Chambers , Robert H. Willie , Charles W. Rust
- 申请人: Thomas A. Campbell , David S. Chambers , Robert H. Willie , Charles W. Rust
- 申请人地址: US IL Chicago
- 专利权人: The Boeing Company
- 当前专利权人: The Boeing Company
- 当前专利权人地址: US IL Chicago
- 主分类号: B64D33/02
- IPC分类号: B64D33/02 ; F02C7/04
摘要:
Dual flow auxiliary power unit (APU) inlets and associated systems and methods are disclosed. An inlet in accordance with one embodiment of the invention includes an entrance aperture and a divider positioned in the inlet and located to separate a first portion of the inlet from a second portion of the inlet. The first portion can be configured to couple to an engine air intake of an APU, and the second portion can be configured to direct air away from the air intake. The divider can be positioned to direct air having a first total pressure level and a first distortion level to the first portion of the inlet, and direct air having a second total pressure level and second distortion level to the second portion of the inlet. The first total pressure level can be approximately the same as or higher than the second total pressure level, or the second distortion level can be approximately the same as or higher than the first distortion level, or both.
摘要(中):
公开了双流辅助动力单元(APU)入口及相关系统和方法。 根据本发明的一个实施例的入口包括入口孔和分隔件,其定位在入口中并且定位成将入口的第一部分与入口的第二部分分开。 第一部分可以被配置成联接到APU的发动机进气口,并且第二部分可被配置成将空气引导离开进气口。 分隔器可以定位成将具有第一总压力水平和第一失真水平的空气引导到入口的第一部分,并且具有第二总压力水平和第二失真水平的直接空气到入口的第二部分。 第一总压力水平可以大致等于或高于第二总压力水平,或者第二失真水平可以大致等于或高于第一失真水平,或两者。
公开/授权文献:
- US07611093B2 Dual flow APU inlet and associated systems and methods 公开/授权日:2009-11-03
IPC结构图谱:
B | 作业;运输 |
--B64 | 飞行器;航空;宇宙航行 |
----B64D | 用于与飞机配合或装到飞机上的设备;飞行衣;降落伞;动力装置或推进传动装置的配置或安装 |
------B64D33/00 | 其他类目不包含的动力装置部件或辅助设备在飞机内的布置 |
--------B64D33/02 | .进气口燃烧的 |