Aircraft powerplant with steam system and bypass
US-2024369014-A1 · Nov 7, 2024 · US
US9399951B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9399951-B2 |
| Application number | US-201213448517-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 17, 2012 |
| Priority date | Apr 17, 2012 |
| Publication date | Jul 26, 2016 |
| Grant date | Jul 26, 2016 |
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Official abstract text for this publication.
Louver systems for gas turbine bleed air systems are disclosed. An example louver system may include a bleed system discharge opening arranged to vent bleed air from a bleed flow conduit and a plurality of pivotable louvers disposed proximate the discharge opening, the pivotable louvers being pivotable between a shut position and an open position. In the shut position, individual louvers may at least partially obstruct the discharge opening. In the open position, individual louvers may at least partially control a direction of flow of the bleed air exiting the discharge opening.
Opening claim text (preview).
What is claimed is: 1. A louver system for a gas turbine engine bleed system, the louver system comprising: a bleed system discharge opening arranged to vent bleed air from a bleed flow conduit; and a plurality of pivotable louvers disposed in a core engine casing and proximate the discharge opening, the pivotable louvers being pivotable between a shut position and an open position; wherein, in the shut position, individual louvers at least partially obstruct the discharge ope…
Mechanical Engineering · mapped topic
Cross-Sectional Technologies · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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