Variable area bypass nozzle

US10260427B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10260427-B2
Application numberUS-201414203637-A
CountryUS
Kind codeB2
Filing dateMar 11, 2014
Priority dateMar 15, 2013
Publication dateApr 16, 2019
Grant dateApr 16, 2019

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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 gas turbine engine includes a first duct, a second duct, and a bladder. The bladder is disposed in the first duct and communicates with the second duct. A first gas flow is capable of passing through the first duct and a second gas flow is capable of passing through the second duct. The bladder is adapted to receive a bleed gas flow from the second duct and inflate within the first duct, thereby decreasing an area in the first duct through which the first gas flow is capable of traveling.

First claim

Opening claim text (preview).

The invention claimed is: 1. A kit for a gas turbine engine comprising: a movable component; a bias element connected to the movable component; and a bladder configured to be connected to the movable component and adapted to receive a bleed air therein, wherein the bias element is adapted to exert a bias force on the movable component and the bladder, and wherein the bladder is permeable to allow a gas flow to pass through the bladder. 2. The kit of claim 1 , wherein the bladder comprises a wire mesh. 3. The kit of claim 1 , wherein the bias force of the bias element biases the bladder toward a deflated and flattened position. 4. The kit of claim 1 , wherein the kit further includes: a stationary component, wherein the bias element is connected between the stationary component and the movable component.

Assignees

Inventors

Classifications

  • controlling flow ratio between flows · CPC title

  • by transversely deforming an internal member · CPC title

  • F02C9/18Primary

    by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages {(F02C3/113 takes precedence)} · CPC title

  • Self-proportioning flow systems · CPC title

  • For producing proportionate flow · CPC title

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Frequently asked questions

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What does patent US10260427B2 cover?
A gas turbine engine includes a first duct, a second duct, and a bladder. The bladder is disposed in the first duct and communicates with the second duct. A first gas flow is capable of passing through the first duct and a second gas flow is capable of passing through the second duct. The bladder is adapted to receive a bleed gas flow from the second duct and inflate within the first duct, ther…
Who is the assignee on this patent?
United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F02C9/18. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Apr 16 2019 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).