Gas turbine engine with variable area fan nozzle

US8997497B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-8997497-B2
Application numberUS-91520810-A
CountryUS
Kind codeB2
Filing dateOct 29, 2010
Priority dateOct 29, 2010
Publication dateApr 7, 2015
Grant dateApr 7, 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.

A bypass gas turbine engine includes a variable area fan nozzle with a second fan nacelle section axially movable relative to a first fan nacelle section to define an auxiliary port to vary a fan nozzle exit area and adjust fan bypass airflow. The second fan nacelle section includes a leading edge region that defines a concave external contour and the first fan nacelle section includes a trailing edge region that defines a convex internal contour.

First claim

Opening claim text (preview).

What is claimed is: 1. A nacelle assembly for a gas turbine engine comprising: a core nacelle defined about an engine centerline axis of rotation; a fan nacelle mounted at least partially around said core nacelle to define a fan bypass flow path; a variable area nozzle in communication with said fan bypass flow path, said variable area nozzle having a first fan nacelle section and a second fan nacelle section, said second fan nacelle section axially movable relative said first…

Assignees

Inventors

Classifications

  • Mechanical Engineering · mapped topic

  • Operations & Transport · mapped topic

  • Mechanical Engineering · mapped topic

  • F02K1/30Primary

    Mechanical Engineering · mapped topic

  • Mechanical Engineering · mapped topic

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What does patent US8997497B2 cover?
A bypass gas turbine engine includes a variable area fan nozzle with a second fan nacelle section axially movable relative to a first fan nacelle section to define an auxiliary port to vary a fan nozzle exit area and adjust fan bypass airflow. The second fan nacelle section includes a leading edge region that defines a concave external contour and the first fan nacelle section includes a traili…
Who is the assignee on this patent?
Hall Andre M, Kohlenberg Gregory A, Gilson Jonathan, and 1 more
What technology area does this patent fall under?
Primary CPC classification F02K1/30. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Apr 07 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).