Engine systems and methods for removing particles from turbine air
US-2015354461-A1 · Dec 10, 2015 · US
US9410482B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9410482-B2 |
| Application number | US-201113336378-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 23, 2011 |
| Priority date | Dec 24, 2010 |
| Publication date | Aug 9, 2016 |
| Grant date | Aug 9, 2016 |
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Official abstract text for this publication.
A gas turbine engine having a heat exchanger is disclosed. In one form the gas turbine engine includes a particle separator that can be used to separate particles or foreign objects and create a dirty flow and a clean flow. A blower can be used to discharge the particles or foreign objects from the separator. The heat exchanger includes a relatively warm flow path from a downstream region of a compressor and a relatively cool flow path from an upstream region of the compressor. The relatively cool flow path is merged with the dirty flow. In another embodiment, the gas turbine engine is a turbofan and the relatively cool flow path is merged with a bypass flow. In one embodiment of the engine the relatively warm flow path, after having exchanged heat with the relatively cool flow path is delivered to a working component without passing through a turbomachinery component.
Opening claim text (preview).
What is claimed is: 1. An apparatus comprising: a gas turbine engine having a particle separator for cleaning an airflow and a compressor capable of increasing a pressure of a working fluid in the gas turbine engine, the particle separator having a clean flow path and a dirty flow path; a first passageway for the conveyance of a first air flow extracted from a first source of the compressor; a second passageway for the conveyance of a second air flow extracted from a second so…
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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