Gas turbine engine having outlet guide vanes
US-2024418094-A1 · Dec 19, 2024 · US
US9157366B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9157366-B2 |
| Application number | US-201213483449-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 30, 2012 |
| Priority date | May 30, 2012 |
| Publication date | Oct 13, 2015 |
| Grant date | Oct 13, 2015 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A disclosed gas turbine engine includes a first fan section including a plurality of fan blades rotatable about an axis, a compressor in fluid communication with the first fan section, a combustor in fluid communication with the compressor and a first turbine section in fluid communication with the combustor. The first turbine section includes a low pressure turbine that drives the first fan section. A second fan section is supported between the first fan section and the compressor and is driven by a second turbine section disposed between the second fan section and the compressor for driving the second fan section.
Opening claim text (preview).
The invention claimed is: 1. A gas turbine engine comprising: a first fan section including a plurality of fan blades rotatable about an axis; a compressor in fluid communication with the first fan section; a combustor in fluid communication with the compressor; a first turbine section in fluid communication with the combustor, the first turbine section driving the first fan section and the compressor; a core flow path directing airflow to the compressor; a first bypass…
Related publications grouped by family.
Free tools are coming soon. Tell us what you want to track and we'll notify you.
Answers are generated from the same data shown on this page.