Casing for use in a turbofan engine and method of scavenging fluid therefrom

US10316856B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10316856-B2
Application numberUS-201514955327-A
CountryUS
Kind codeB2
Filing dateDec 1, 2015
Priority dateDec 1, 2015
Publication dateJun 11, 2019
Grant dateJun 11, 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 casing for use in a turbofan engine is provided. The casing includes an inner hub including a first fluid opening defined at bottom dead center of the casing. The casing also includes an intermediate casing positioned radially outward from the inner hub, an outer casing positioned radially outward from the intermediate casing, and struts spaced circumferentially about the inner hub and extending between the inner hub and the outer casing. The struts include a first strut and a second strut positioned on opposing sides of bottom dead center of the casing such that a first fluid sump is defined between the inner hub, the intermediate casing, and the first and second struts. At least one of said first and second struts includes a flow channel extending therethrough such that a fluid flow path is defined from the first fluid opening, through the first fluid sump, and through the flow channel.

First claim

Opening claim text (preview).

What is claimed is: 1. A casing for use in a turbofan engine, said casing comprising: an inner hub comprising a first fluid opening defined at about bottom dead center of the casing, a second fluid opening, and a third fluid opening defined therein; an intermediate casing positioned radially outward from said inner hub; an outer casing positioned radially outward from said intermediate casing; and a plurality of struts spaced circumferentially about said inner hub and extending between said inner hub and said outer casing, said plurality of struts comprising a first strut, a second strut, a third strut, and a fourth strut, wherein the first strut and the second strut are positioned on opposing sides of bottom dead center of the casing such that a first fluid sump is defined between said inner hub, said intermediate casing, and said first and second struts, wherein at least one of said first and second struts comprise a flow channel extending therethrough such that a fluid flow path is defined from said first fluid opening, through said first fluid sump, and through said flow channel, wherein said third strut is spaced circumferentially from said first strut and on an opposite side of the first strut from said second strut such that a second fluid sump is defined between said first and third struts, said intermediate casing, and said inner hub, wherein said second fluid opening is positioned between said first and third struts, and wherein said fourth strut is spaced circumferentially from said second strut and on an opposite side of the second strut from said first strut such that a third fluid sump is defined between said second and fourth struts, said intermediate casing, and said inner hub, wherein said third fluid opening is positioned between said second and fourth struts. 2. The casing in accordance with claim 1 , wherein each of said first strut and said second strut comprises a flow channel extending therethrough. 3. The casing in accordance with claim 2 , wherein a first fluid flow path is defined from said first fluid opening, through said first fluid sump, and through said flow channel defined within the first strut, and wherein a second fluid flow path is defined from said first fluid opening, through said first fluid sump, and through said flow channel defined within the second strut. 4. The casing in accordance with claim 1 further comprising a fluid scoop defined within said inner hub at a circumferential position offset from bottom dead center of the casing. 5. The casing in accordance with claim 4 , wherein said fluid scoop comprises a scoop opening defined by a guide member that is radially offset from a radially inner surface of said inner hub. 6. The casing in accordance with claim 5 further comprising a collector that couples said fluid scoop in flow communication with said flow channel such that a third fluid flow path is defined from said scoop opening, through said collector, and through said flow channel defined in at least one of said first and second struts. 7. A turbofan engine for use with an aircraft, said turbofan engine comprising: a gearbox; and a casing that at least partially circumscribes said gearbox, wherein said casing comprises: an inner hub comprising a first fluid opening defined at about bottom dead center of the casing; an intermediate casing positioned radially outward from said inner hub; an outer casing positioned radially outward from said intermediate casing; a plurality of struts spaced circumferentially about said inner hub and extending between said inner hub and said outer casing, said plurality of struts comprising a first strut and a second strut positioned on opposing sides of bottom dead center of the casing such that a first fluid sump is defined between said inner hub, said intermediate casing, and said first and second struts, wherein each of said first and second struts comprise a flow channel extending therethrough such that a first fluid flow path is defined from said first fluid opening, through said first fluid sump, and through said flow channel; further comprising at least one suction device comprising a first suction device coupled in flow communication with the flow channel defined within said first strut and the flow channel defined within said second strut, wherein said at least one suction device is configured to maintain a negative pressure within said first fluid sump; and further comprising: at least one valve coupled in flow communication with said flow channel defined within the first strut and said flow channel defined within the first strut; and an actuating device coupled in communication with said first suction device and with said at least one valve, wherein said actuating device is configured to selectively actuate said first suction device and said at least one valve based on an orientation of the turbofan engine relative to a roll axis thereof. 8. The turbofan engine in accordance with claim 7 , wherein said plurality of struts further comprises a third strut spaced circumferentially from said first strut and on an opposite side of the first strut from said second strut such that a second fluid sump is defined between said first and third struts, said intermediate casing, and said inner hub, and wherein said plurality of struts further comprises a fourth strut spaced circumferentially from said second strut and on an opposite side of the second strut from said first strut such that a third fluid sump is defined between said second and fourth struts, said intermediate casing, and said inner hub. 9. The turbofan engine in accordance with claim 7 , wherein said inner hub comprises a fluid scoop defined therein at a circumferential position offset from bottom dead center of said casing. 10. A method of assembling a casing for use with a turbofan engine, said method comprising: positioning an intermediate casing radially outward from an inner hub, wherein the inner hub includes a first fluid opening defined at about bottom dead center of the casing; defining a second fluid opening in the inner hub; defining a third fluid opening in the inner hub; positioning an outer casing radially outward from the intermediate casing; spacing a plurality of struts circumferentially about the inner hub, wherein the plurality of struts extend between the inner hub and the outer casing, the plurality of struts including a first strut, a second strut, a third strut, and a fourth strut, wherein the first strut and the second strut are positioned on opposing sides of bottom dead center of the casing such that a first fluid sump is defined between the inner hub, said intermediate casing, and said first and second struts, wherein at least one of the first and second struts include a flow channel extending therethrough such that a fluid flow path is defined from the first fluid opening, through the first fluid sump, and through the flow channel; spacing a third strut circumferentially from the first strut and on an opposite side of the first strut from the second strut such that a second fluid sump is defined between the first and third struts, said intermediate casing, and said inner hub, wherein said second fluid opening is positioned between said first and third struts; and spacing a fourth strut circumferentially from the second strut and on an opposite side of the second strut from the first strut such that a third fluid sump is defined between the second and fourth struts, the intermediate casing, and the inner hub, wherein said third fluid opening is positioned between said second and fourth struts. 11. The method in accordance with claim 10 , wherein each of the first strut and the second strut include a flow chann

Assignees

Inventors

Classifications

  • Casings or housings protecting or supporting assemblies within · CPC title

  • Dry-sumps · CPC title

  • Means for collecting, retaining, or draining-off lubricant in or on machines or apparatus (oil separators for separating oil from exhaust steam F22G) · CPC title

  • Lubricating arrangements (of machines or engines in general F01M) · CPC title

  • of the epicyclical, planetary or differential type · CPC title

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What does patent US10316856B2 cover?
A casing for use in a turbofan engine is provided. The casing includes an inner hub including a first fluid opening defined at bottom dead center of the casing. The casing also includes an intermediate casing positioned radially outward from the inner hub, an outer casing positioned radially outward from the intermediate casing, and struts spaced circumferentially about the inner hub and extend…
Who is the assignee on this patent?
Gen Electric
What technology area does this patent fall under?
Primary CPC classification F01D25/26. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jun 11 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 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).