Catcher ring assembly

US9316231B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9316231-B2
Application numberUS-201213584260-A
CountryUS
Kind codeB2
Filing dateAug 13, 2012
Priority dateSep 2, 2011
Publication dateApr 19, 2016
Grant dateApr 19, 2016

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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 catcher ring assembly ( 170 ) configured to limit axial movement of a turbomachine shaft assembly ( 132, 132′ ) during a failure mode, the catcher ring assembly comprising a catcher ring ( 172 ) disposable about and connectable to the shaft assembly, wherein one of the shaft assembly and the catcher ring comprises a protrusion ( 194, 182 ) and the other of the shaft assembly and the catcher ring comprises a recess ( 192, 184 ), the recess corresponding in shape to the protrusion, wherein the protrusion and recess are circumferentially disposed about a longitudinal axis of the shaft assembly and the protrusion extends in an axial direction.

First claim

Opening claim text (preview).

The invention claimed is: 1. A catcher ring assembly configured to limit axial movement of a turbomachine shaft assembly during a failure mode, the catcher ring assembly comprising: a catcher ring disposable about and connectable to the shaft assembly, both the catcher ring and the shaft assembly include a protrusion and a recess, the recess of the catcher ring corresponding in shape to the protrusion of the shaft assembly, and the recess of the shaft assembly corresponding in shape to the protrusion of the catcher ring, the protrusions and the recesses being circumferentially disposed about a longitudinal axis of the shaft assembly, and the protrusion of the catcher ring extending away from the catcher ring in an axial direction and the protrusion of the shaft assembly extending away from the shaft assembly in an opposing axial direction, and a nut assembly including an intermediate element and a nut, the intermediate element being provided between the nut and the catcher ring, wherein: the catcher ring assembly includes a spline or recess for engagement with a corresponding recess or spline provided on the shaft assembly respectively, the recess and spline being configured to limit rotation of the catcher ring assembly relative to the shaft assembly, and the intermediate element includes the spline or recess for engagement with the corresponding recess or spline provided on the shaft assembly respectively. 2. The catcher ring assembly of claim 1 , wherein the catcher ring includes the spline or recess for engagement with the corresponding recess or spline provided on the shaft assembly respectively. 3. The catcher ring assembly of claim 1 , further comprising a locking member, the locking member being disposable between the intermediate element and the catcher ring to limit rotation of the catcher ring with respect to the intermediate element. 4. The catcher ring assembly of claim 1 , wherein the catcher ring is disposed adjacent to a speed measuring device configured to measure the rotational speed of the shaft assembly. 5. The catcher ring assembly of claim 4 , wherein at least a portion of the speed measuring device is connected to the catcher ring assembly. 6. The catcher ring assembly of claim 4 , wherein at least a portion of the speed measuring device is connected to the catcher ring assembly via said nut assembly. 7. The catcher ring assembly of claim 1 , wherein the catcher ring is configured to abut a shoulder to limit axial movement of the shaft assembly during the failure mode. 8. A turbomachine comprising the catcher ring assembly of claim 1 . 9. A fan assembly comprising the catcher ring assembly of claim 1 . 10. A gas turbine engine comprising the catcher ring assembly of claim 1 .

Assignees

Inventors

Classifications

  • Stop safety or alarm devices, e.g. stop-and-go control; Disposition of check-valves · CPC title

  • special arrangements in stators or in rotors dealing with breaking-off of part of rotor · CPC title

  • F04D29/043Primary

    Shafts · CPC title

  • Axial thrust balancing · CPC title

  • Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps · CPC title

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Frequently asked questions

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What does patent US9316231B2 cover?
A catcher ring assembly ( 170 ) configured to limit axial movement of a turbomachine shaft assembly ( 132, 132′ ) during a failure mode, the catcher ring assembly comprising a catcher ring ( 172 ) disposable about and connectable to the shaft assembly, wherein one of the shaft assembly and the catcher ring comprises a protrusion ( 194, 182 ) and the other of the shaft assembly and the catcher r…
Who is the assignee on this patent?
Simms Paul, Rolls Royce Plc
What technology area does this patent fall under?
Primary CPC classification F04D29/043. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Apr 19 2016 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).