Gas dynamic valve

US10151271B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10151271-B2
Application numberUS-201514754342-A
CountryUS
Kind codeB2
Filing dateJun 29, 2015
Priority dateJul 28, 2014
Publication dateDec 11, 2018
Grant dateDec 11, 2018

How to read this patent

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  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  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 flow-management system may comprise a center body impermeable to air. A conical surface of the center body may face forward. A blocking surface of the center body may be coaxial with the conical surface and may comprise an annular recess. An annular ring may be aft of the center body and fluidly coupled with the blocking surface. A tube may encase the center body and annular ring. The annular ring may comprise an air-foil shape to direct a pulse to the blocking surface. The blocking surface may comprise a central peak and a circular ridge separated by the annular recess.

First claim

Opening claim text (preview).

What is claimed is: 1. A flow-management system, comprising: a center body impermeable to gas; a conical surface of the center body facing forward; a blocking surface of the center body coaxial with the conical surface and comprising an annular recess disposed between a central peak and a circular ridge, wherein the circular ridge extends rearward of the central peak; and an annular ring aft of the center body and fluidly coupled with the blocking surface, wherein the annular ring is symmetrical about a centerline axis, wherein a distance between the centerline axis and a forward edge of the annular ring is smaller than a distance between the centerline axis and an aft edge of the annular ring. 2. The flow-management system of claim 1 , further comprising a tube encasing the center body and annular ring. 3. The flow-management system of claim 1 , wherein the annular ring comprises an air-foil shape to direct a pulse to the blocking surface. 4. The flow-management system of claim 1 , wherein the center body is axially symmetric. 5. The flow-management system of claim 1 , further comprising a strut mounted to the conical surface of the center body. 6. A pulse detonation engine comprising: a tube; a center body fixed to the tube; a conical surface of the center body facing forward; a blocking surface of the center body coaxial with the conical surface and comprising an annular recess disposed between a central peak and a circular ridge, wherein the circular ridge extends rearward of the central peak, wherein the blocking surface is impermeable to gas; a duct defined by the conical surface and tube; and an annular ring aft of the center body comprising an air-foil shape configured to divert a pulse towards the blocking surface, wherein the annular ring is symmetrical about a centerline axis, wherein a distance between the centerline axis and a forward edge of the annular ring is smaller than a distance between the centerline axis and an aft edge of the annular ring. 7. The pulse detonation engine of claim 6 , wherein the air-foil shape of the annular ring is further configured to divert the pulse away from the duct. 8. The pulse detonation engine of claim 6 , wherein the conical surface is impermeable to air. 9. The pulse detonation engine of claim 6 , wherein the center body is axially symmetric. 10. The pulse detonation engine of claim 6 , further comprising: a first strut connecting the tube and center body; and a second strut connecting the tube and annular ring. 11. The pulse detonation engine of claim 6 , further comprising a detonation zone in the tube and aft of the annular ring, wherein the pulse originates from the detonation zone.

Assignees

Inventors

Classifications

  • F02K7/067Primary

    having aerodynamic valves · CPC title

  • the working fluid forming a resonating or oscillating gas column, i.e. the combustion chambers having no positively actuated valves, e.g. using Helmholtz effect · CPC title

  • F02K7/02Primary

    the jet being intermittent, i.e. pulse-jet · CPC title

  • using valveless combustion chambers · CPC title

  • for controlling, signalling, or supervising the conveyance of a product · CPC title

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Frequently asked questions

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What does patent US10151271B2 cover?
A flow-management system may comprise a center body impermeable to air. A conical surface of the center body may face forward. A blocking surface of the center body may be coaxial with the conical surface and may comprise an annular recess. An annular ring may be aft of the center body and fluidly coupled with the blocking surface. A tube may encase the center body and annular ring. The annular…
Who is the assignee on this patent?
United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F02K7/067. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Dec 11 2018 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).