Turbine based combined cycle engine

US9109539B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9109539-B2
Application numberUS-97887610-A
CountryUS
Kind codeB2
Filing dateDec 27, 2010
Priority dateDec 27, 2010
Publication dateAug 18, 2015
Grant dateAug 18, 2015

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

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.

First claim

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…

Assignees

Inventors

Classifications

  • Mechanical Engineering · mapped topic

  • F02K7/14Primary

    Mechanical Engineering · mapped topic

  • F02K7/16Primary

    Mechanical Engineering · mapped topic

  • Mechanical Engineering · mapped topic

  • Mechanical Engineering · mapped topic

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Frequently asked questions

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What does patent US9109539B2 cover?
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…
Who is the assignee on this patent?
Duge Robert T, Heathco Craig, King Brian Paul, and 1 more
What technology area does this patent fall under?
Primary CPC classification F02K7/14. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Aug 18 2015 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).