Propfan engine

US8967967B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-8967967-B2
Application numberUS-201213359194-A
CountryUS
Kind codeB2
Filing dateJan 26, 2012
Priority dateFeb 22, 2011
Publication dateMar 3, 2015
Grant dateMar 3, 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

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The present disclosure relates to a propfan engine comprising: one or more rotor stages comprising a plurality of rotors; and an outer wall comprising an outer profile, at least a portion of the outer profile defining a substantially circular cross-section, wherein the diameter of the substantially circular cross-section increases in the direction of flow over the outer wall and downstream of a leading edge of the rotors, and the diameter increases at substantially all points defining the circumference of the substantially circular cross-section.

First claim

Opening claim text (preview).

The invention claimed is: 1. A propfan engine comprising: one or more rotor stages comprising a plurality of rotors; and an outer wall comprising an outer profile, at least a portion of the outer profile comprising a substantially circular cross-section, wherein the diameter of the substantially circular cross-section increases in the direction of flow over the outer wall and downstream of a leading edge of the rotors, and the diameter increases at substantially all points def…

Assignees

Inventors

Classifications

  • Operations & Transport · mapped topic

  • Mechanical Engineering · mapped topic

  • F02K3/072Primary

    Mechanical Engineering · mapped topic

  • Operations & Transport · mapped topic

  • Cross-Sectional Technologies · mapped topic

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Frequently asked questions

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What does patent US8967967B2 cover?
The present disclosure relates to a propfan engine comprising: one or more rotor stages comprising a plurality of rotors; and an outer wall comprising an outer profile, at least a portion of the outer profile defining a substantially circular cross-section, wherein the diameter of the substantially circular cross-section increases in the direction of flow over the outer wall and downstream of a…
Who is the assignee on this patent?
Stretton Richard G, Howarth Nicholas, Rolls Royce Plc
What technology area does this patent fall under?
Primary CPC classification F02K3/072. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Mar 03 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).