Bearing chamber with mapped thermal heat exchange fins
US-2024151155-A1 · May 9, 2024 · US
US8998569B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8998569-B2 |
| Application number | US-201113211404-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 17, 2011 |
| Priority date | Aug 17, 2011 |
| Publication date | Apr 7, 2015 |
| Grant date | Apr 7, 2015 |
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A gas turbine engine includes a gas turbine engine internal compartment structure having an integral passageway. Wiring is routed through the integral passageway of the gas turbine engine internal compartment structure.
Opening claim text (preview).
What is claimed is: 1. A gas turbine engine, comprising: a gas turbine engine internal compartment structure having an integral passageway; wiring routed through said integral passageway and along a downstream wall of said gas turbine engine internal compartment structure; and wherein said gas turbine engine internal compartment structure includes a radially inner portion, a radially outer portion and a flange that extends between said radially inner portion and said radially…
Mechanical Engineering · mapped topic
Cross-Sectional Technologies · mapped topic
Mechanical Engineering · mapped topic
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