Scramjet engine and flying object
US-2020362795-A1 · Nov 19, 2020 · US
US9109539B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9109539-B2 |
| Application number | US-97887610-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 27, 2010 |
| Priority date | Dec 27, 2010 |
| Publication date | Aug 18, 2015 |
| Grant date | Aug 18, 2015 |
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Official abstract text for this publication.
An aircraft powerplant is disclosed that can be operated in at least three modes including as a gas turbine engine, as an engine having a ramburner, and as an engine having a forward compression combustor engine such as a ramjet and/or scramjet. An airflow valve is provided to direct air to a downstream portion of the aircraft engine and can be positioned as a function of the aircraft operating modes. The valve can be used to cocoon the gas turbine engine.
Opening claim text (preview).
What is claimed is: 1. An apparatus comprising: a propulsion engine having an inlet operable to convey a working fluid for combustion and a bypass valve operable to selectively bypass a quantity of the working fluid, the propulsion engine having three thrust producing modes including: a first thrust producing mode including a gas turbine engine having a rotating compressor, a core combustor, and a rotating turbine, wherein the bypass valve is operated to provide air flow to the g…
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